Synchronization and spindle oscillation in noisy integrate-and-fire-or-burst neurons with i

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原虫概论阿米巴

原虫概论阿米巴
×1000
3、生活史
经口
四核包囊 小肠下段脱囊 4个核滋养体
核分裂
8个单核小滋养体
肠粘膜
邹褶或隐窝,二分裂繁(以细菌粘膜 肠内容

已消化食物为食) 胞质分泌囊液
虫体团缩形成囊前期 包囊
包囊→滋养体→包囊为疾病阿米巴生活史型
在一定条件下
抵抗力下降
滋养体侵入肠粘膜组织
肠腔内
组织内(肠壁、肝脑) 、
染色后胞核形态特征是医学原虫病 原诊断的重要依据
致病特点
1、增殖作用:大量增殖到一定数量后引起 损害,血液、体液及分泌物中原虫的检查 可为临床诊断提供可靠信息。
2、播散作用:由于快速增殖而具有的全身 播散的倾向。病原学诊断不仅要考虑原发 病灶,而且还要考虑到继发病灶乃至全身 各器官。
3、机会致病:有些原虫对健康宿主不表现 出明显致病性,但当宿主免疫功能低下时, 可导致严重甚至致死性的感染。
常见医学原虫分类
1、生物学分类:隶属于4个纲: 动鞭纲 叶足纲 孢子纲 动基裂纲 (鞭毛虫)(阿米巴)(孢子虫) (纤毛虫) 2、按寄生部位分类:腔道内寄生原虫(肠
道、阴道)和血液及组织内寄生原虫(红 细胞内、有核细胞内、肝、肺、脑及其他 组织内寄生)。
阿米巴概述
以伪足为运动细胞器,多数生 活史有滋养体和包囊两个时期, 滋养体期为运动、摄食、繁殖和 致病期,包囊为静止期,是阿米 巴传播期。
对成形粪便,用碘液染色法查包囊。包囊形成有 间歇,故检查时应隔日1次并连续3次以上送检 为宜。 (2)十二指肠液或胆汁检查滋养体 (3)肠检胶囊法。 (4)小肠活组织检查,利用纤维胃镜取小肠粘 膜组织检查。
五、流行
、分布: 1本病在发达与发展中国家均有流行,我国平均 感染率为2.65%

翻译--西医神经科术语英文翻译

翻译--西医神经科术语英文翻译

西医神经科术语英文翻译以下是常见的西医神经科术语英文翻译:1. 神经学:Neurology2. 神经系统:Nervous System3. 大脑:Brain4. 脊髓:Spinal Cord5. 神经元:Neuron6. 神经胶质细胞:Glial Cells7. 突触:Synapse8. 轴突:Axon9. 树突:Dendrites10. 髓鞘:Myelin Sheath11. 神经递质:Neurotransmitters12. 神经传导通路:Nerve Conduction Pathways13. 反射:Reflex14. 痛觉:Pain Sensation15. 感觉运动传导通路:Sensorimotor Pathways16. 自主神经系统:Autonomic Nervous System17. 中枢神经系统:Central Nervous System (CNS)18. 外周神经系统:Peripheral Nervous System (PNS)19. 神经肌肉接头:Neuromuscular Junction20. 癫痫:Epilepsy21. 帕金森病:Parkinson's Disease22. 多发性硬化症:Multiple Sclerosis (MS)23. 脑卒中:Stroke24. 脑外伤:Traumatic Brain Injury (TBI)25. 脑瘤:Brain Tumors26. 脑炎:Brain Infections / Encephalitis27. 神经痛:Neuralgia28. 头痛:Headache29. 失眠:Insomnia30. 肌肉萎缩:Muscle Atrophy31. 肌无力:Muscle Weakness32. 神经根病:Radiculopathy33. 神经丛病变:Plexopathy34. 脊髓病变:Myelopathy35. 脑积水:Hydrocephalus36. 脊髓空洞症:Syringomyelia37. 脑电图(EEG):Electroencephalogram (EEG)38. 肌电图(EMG):Electromyogram (EMG)39. 经颅磁刺激(TMS):Transcranial Magnetic Stimulation (TMS)40. 正电子发射断层扫描(PET):Positron Emission Tomography (PET)41. 功能磁共振成像(fMRI):Functional Magnetic Resonance Imaging (fMRI)42. 单光子发射计算机断层扫描(SPECT):Single Photon Emission Computed Tomography (SPECT)43. 经颅多普勒超声(TCD):Transcranial Doppler Ultrasound (TCD)44. 认知障碍:Cognitive Dysfunction45. 情绪障碍:Mood Disorders46. 神经退行性疾病:Neurodegenerative Diseases47. 中毒性脑病:Toxic Encephalopathy48. 脑死亡:Brain Death49. 昏迷:Coma50. 意识障碍:Disorders of Consciousness。

摆动假说名词解释

摆动假说名词解释

变偶假说(wobble hypothesis)又名摆动假说Crick为解释反密码子中某些稀有成分的配对以及许多氨基酸有两个以上密码子的问题而提出的假说。

根据这个假说,以往的由结构决定tRNA对密码子识别多样性的问题就得到了很好的说明。

(1)mRNA上的密码子的第一、第二个碱基与tRNA上的反密码子相应的碱基形成强的配对;密码的专一性,主要是由于这两个碱基对的作用。

(2)反密码子的第一个碱基(以5'→3'方向,与密码子的第三个碱基配对)决定一个tRNA所能解读的密码子数目。

当反密码子的第一个碱基是C或A时,则只能和一个密码子结合。

但当反密码子上的第一个碱基是U或G时,则可以和两个密码子结合,即U可以和A或G配对,G可以和C或U配对。

即U可以和A或G配对,G可以和C或U配对。

而当反密码子的第一个碱基是I时,便可以和3个密码子结合,即I可以和A,U 或C配对。

(3)当一种氨基酸是由几个不同的密码子编码时,如果密码子的头2个碱基的任一个是不同的,便必须有不同的tRNA。

(4)这样,便要求至少要有32种tRNA,来与61个密码子相结合(31个tRNA用于氨基酸转运,1个tRNA用于起始)。

钙离子振荡英语

钙离子振荡英语

钙离子振荡英语Calcium ions play a pivotal role in various cellular processes, including signal transduction, gene expression, and cell division. One of the most intriguing phenomena involving calcium ions is the occurrence of calcium oscillations.Calcium oscillations refer to the rhythmic changes in intracellular calcium ion concentration. These oscillations are not random but are tightly regulated and can be initiated by a variety of stimuli, such as hormones, neurotransmitters, and growth factors. The frequency, amplitude, and duration of these oscillations can convey different signals to the cell, influencing its behavior.The process of calcium ion oscillation typically begins with the binding of a signaling molecule to its receptor on the cell surface. This binding event triggers a cascade of intracellular reactions that ultimately lead to the release of calcium ions from internal stores, such as the endoplasmic reticulum. The released calcium ions can then bind to various intracellular targets, initiating a series of downstream responses.One of the key mechanisms that regulate calcium oscillations is the calcium/calmodulin-dependent protein kinase II (CaMKII). This enzyme is activated by the binding of calcium ions to calmodulin, a calcium-binding protein.Once activated, CaMKII can phosphorylate a variety of substrates, modulating their activity and contributing to the overall response to the calcium signal.Another important aspect of calcium oscillations is their spatial characteristics. Calcium signals can be localized to specific regions of the cell, allowing for the precise regulation of localized cellular processes. This spatial regulation is achieved through the selective release of calcium ions from specific internal stores and the targeted activation of calcium-sensitive proteins.In conclusion, calcium ion oscillations are a complex and highly regulated phenomenon that is crucial for the proper functioning of cells. Understanding the mechanisms that govern these oscillations is essential for unraveling the intricate web of cellular signaling pathways and could provide valuable insights into the treatment of various diseases associated with calcium dysregulation.。

斯仑贝谢所有测井曲线英文名称解释

斯仑贝谢所有测井曲线英文名称解释

斯仑贝谢所有测井曲线英文名称解释OCEAN DRILLING PROGRAMACRONYMS USED FOR WIRELINE SCHLUMBERGER TOOLS ACT Aluminum Clay ToolAMS Auxiliary Measurement SondeAPS Accelerator Porosity SondeARI Azimuthal Resistivity ImagerASI Array Sonic ImagerBGKT Vertical Seismic Profile ToolBHC Borehole Compensated Sonic ToolBHTV Borehole TeleviewerCBL Casing Bond LogCNT Compensated Neutron ToolDIT Dual Induction ToolDLL Dual LaterologDSI Dipole Sonic ImagerFMS Formation MicroScannerGHMT Geologic High Resolution Magnetic ToolGPIT General Purpose Inclinometer ToolGR Natural Gamma RayGST Induced Gamma Ray Spectrometry ToolHLDS Hostile Environment Lithodensity SondeHLDT Hostile Environment Lithodensity ToolHNGS Hostile Environment Gamma Ray SondeLDT Lithodensity ToolLSS Long Spacing Sonic ToolMCD Mechanical Caliper DeviceNGT Natural Gamma Ray Spectrometry ToolNMRT Nuclear Resonance Magnetic ToolQSST Inline Checkshot ToolSDT Digital Sonic ToolSGT Scintillation Gamma Ray ToolSUMT Susceptibility Magnetic ToolUBI Ultrasonic Borehole ImagerVSI Vertical Seismic ImagerWST Well Seismic ToolWST-3 3-Components Well Seismic ToolOCEAN DRILLING PROGRAMACRONYMS USED FOR LWD SCHLUMBERGER TOOLSADN Azimuthal Density-NeutronCDN Compensated Density-NeutronCDR Compensated Dual ResistivityISONIC Ideal Sonic-While-DrillingNMR Nuclear Magnetic ResonanceRAB Resistivity-at-the-BitOCEAN DRILLING PROGRAMACRONYMS USED FOR NON-SCHLUMBERGER SPECIALTY TOOLSMCS Multichannel Sonic ToolMGT Multisensor Gamma ToolSST Shear Sonic ToolTAP Temperature-Acceleration-Pressure ToolTLT Temperature Logging ToolOCEAN DRILLING PROGRAMACRONYMS AND UNITS USED FOR WIRELINE SCHLUMBERGER LOGSAFEC APS Far Detector Counts (cps)ANEC APS Near Detector Counts (cps)AX Acceleration X Axis (ft/s2)AY Acceleration Y Axis (ft/s2)AZ Acceleration Z Axis (ft/s2)AZIM Constant Azimuth for Deviation Correction (deg)APLC APS Near/Array Limestone Porosity Corrected (%)C1 FMS Caliper 1 (in)C2 FMS Caliper 2 (in)CALI Caliper (in)CFEC Corrected Far Epithermal Counts (cps)CFTC Corrected Far Thermal Counts (cps)CGR Computed (Th+K) Gamma Ray (API units)CHR2 Peak Coherence, Receiver Array, Upper DipoleCHRP Compressional Peak Coherence, Receiver Array, P&SCHRS Shear Peak Coherence, Receiver Array, P&SCHTP Compressional Peak Coherence, Transmitter Array, P&SCHTS Shear Peak Coherence, Transmitter Array, P&SCNEC Corrected Near Epithermal Counts (cps)CNTC Corrected Near Thermal Counts (cps)CS Cable Speed (m/hr)CVEL Compressional Velocity (km/s)DATN Discriminated Attenuation (db/m)DBI Discriminated Bond IndexDEVI Hole Deviation (degrees)DF Drilling Force (lbf)DIFF Difference Between MEAN and MEDIAN in Delta-Time Proc. (microsec/ft) DRH HLDS Bulk Density Correction (g/cm3)DRHO Bulk Density Correction (g/cm3)DT Short Spacing Delta-Time (10'-8' spacing; microsec/ft)DT1 Delta-Time Shear, Lower Dipole (microsec/ft)DT2 Delta-Time Shear, Upper Dipole (microsec/ft)DT4P Delta- Time Compressional, P&S (microsec/ft)DT4S Delta- Time Shear, P&S (microsec/ft))DT1R Delta- Time Shear, Receiver Array, Lower Dipole (microsec/ft)DT2R Delta- Time Shear, Receiver Array, Upper Dipole (microsec/ft)DT1T Delta-Time Shear, Transmitter Array, Lower Dipole (microsec/ft)DT2T Delta-Time Shear, Transmitter Array, Upper Dipole (microsec/ft)DTCO Delta- Time Compressional (microsec/ft)DTL Long Spacing Delta-Time (12'-10' spacing; microsec/ft)DTLF Long Spacing Delta-Time (12'-10' spacing; microsec/ft)DTLN Short Spacing Delta-Time (10'-8' spacing; microsec/ftDTRP Delta-Time Compressional, Receiver Array, P&S (microsec/ft)DTRS Delta-Time Shear, Receiver Array, P&S (microsec/ft)DTSM Delta-Time Shear (microsec/ft)DTST Delta-Time Stoneley (microsec/ft)DTTP Delta-Time Compressional, Transmitter Array, P&S (microsec/ft)DTTS Delta-Time Shear, Transmitter Array, P&S (microsec/ft)ECGR Environmentally Corrected Gamma Ray (API units)EHGR Environmentally Corrected High Resolution Gamma Ray (API units) ENPH Epithermal Neutron Porosity (%)ENRA Epithermal Neutron RatioETIM Elapsed Time (sec)FINC Magnetic Field Inclination (degrees)FNOR Magnetic Field Total Moment (oersted)FX Magnetic Field on X Axis (oersted)FY Magnetic Field on Y Axis (oersted)FZ Magnetic Field on Z Axis (oersted)GR Natural Gamma Ray (API units)HALC High Res. Near/Array Limestone Porosity Corrected (%)HAZI Hole Azimuth (degrees)HBDC High Res. Bulk Density Correction (g/cm3)HBHK HNGS Borehole Potassium (%)HCFT High Resolution Corrected Far Thermal Counts (cps)HCGR HNGS Computed Gamma Ray (API units)HCNT High Resolution Corrected Near Thermal Counts (cps)HDEB High Res. Enhanced Bulk Density (g/cm3)HDRH High Resolution Density Correction (g/cm3)HFEC High Res. Far Detector Counts (cps)HFK HNGS Formation Potassium (%)HFLC High Res. Near/Far Limestone Porosity Corrected (%)HEGR Environmentally Corrected High Resolution Natural Gamma Ray (API units) HGR High Resolution Natural Gamma Ray (API units)HLCA High Res. Caliper (inHLEF High Res. Long-spaced Photoelectric Effect (barns/e-)HNEC High Res. Near Detector Counts (cps)HNPO High Resolution Enhanced Thermal Nutron Porosity (%)HNRH High Resolution Bulk Density (g/cm3)HPEF High Resolution Photoelectric Effect (barns/e-)HRHO High Resolution Bulk Density (g/cm3)HROM High Res. Corrected Bulk Density (g/cm3)HSGR HNGS Standard (total) Gamma Ray (API units)HSIG High Res. Formation Capture Cross Section (capture units) HSTO High Res. Computed Standoff (in)HTHO HNGS Thorium (ppm)HTNP High Resolution Thermal Neutron Porosity (%)HURA HNGS Uranium (ppm)IDPH Phasor Deep Induction (ohmm)IIR Iron Indicator Ratio [CFE/(CCA+CSI)]ILD Deep Resistivity (ohmm)ILM Medium Resistivity (ohmm)IMPH Phasor Medium Induction (ohmm)ITT Integrated Transit Time (s)LCAL HLDS Caliper (in)LIR Lithology Indicator Ratio [CSI/(CCA+CSI)]LLD Laterolog Deep (ohmm)LLS Laterolog Shallow (ohmm)LTT1 Transit Time (10'; microsec)LTT2 Transit Time (8'; microsec)LTT3 Transit Time (12'; microsec)LTT4 Transit Time (10'; microsec)MAGB Earth's Magnetic Field (nTes)MAGC Earth Conductivity (ppm)MAGS Magnetic Susceptibility (ppm)MEDIAN Median Delta-T Recomputed (microsec/ft)MEAN Mean Delta-T Recomputed (microsec/ft)NATN Near Pseudo-Attenuation (db/m)NMST Magnetometer Temperature (degC)NMSV Magnetometer Signal Level (V)NPHI Neutron Porosity (%)NRHB LDS Bulk Density (g/cm3)P1AZ Pad 1 Azimuth (degrees)PEF Photoelectric Effect (barns/e-)PEFL LDS Long-spaced Photoelectric Effect (barns/e-)PIR Porosity Indicator Ratio [CHY/(CCA+CSI)]POTA Potassium (%)RB Pad 1 Relative Bearing (degrees)RHL LDS Long-spaced Bulk Density (g/cm3)RHOB Bulk Density (g/cm3)RHOM HLDS Corrected Bulk Density (g/cm3)RMGS Low Resolution Susceptibility (ppm)SFLU Spherically Focused Log (ohmm)SGR Total Gamma Ray (API units)SIGF APS Formation Capture Cross Section (capture units)SP Spontaneous Potential (mV)STOF APS Computed Standoff (in)SURT Receiver Coil Temperature (degC)SVEL Shear Velocity (km/s)SXRT NMRS differential Temperature (degC)TENS Tension (lb)THOR Thorium (ppm)TNRA Thermal Neutron RatioTT1 Transit Time (10' spacing; microsec)TT2 Transit Time (8' spacing; microsec)TT3 Transit Time (12' spacing; microsec)TT4 Transit Time (10' spacing; microsec)URAN Uranium (ppm)V4P Compressional Velocity, from DT4P (P&S; km/s)V4S Shear Velocity, from DT4S (P&S; km/s)VELP Compressional Velocity (processed from waveforms; km/s)VELS Shear Velocity (processed from waveforms; km/s)VP1 Compressional Velocity, from DT, DTLN, or MEAN (km/s)VP2 Compressional Velocity, from DTL, DTLF, or MEDIAN (km/s)VCO Compressional Velocity, from DTCO (km/s)VS Shear Velocity, from DTSM (km/s)VST Stonely Velocity, from DTST km/s)VS1 Shear Velocity, from DT1 (Lower Dipole; km/s)VS2 Shear Velocity, from DT2 (Upper Dipole; km/s)VRP Compressional Velocity, from DTRP (Receiver Array, P&S; km/s) VRS Shear Velocity, from DTRS (Receiver Array, P&S; km/s)VS1R Shear Velocity, from DT1R (Receiver Array, Lower Dipole; km/s) VS2R Shear Velocity, from DT2R (Receiver Array, Upper Dipole; km/s) VS1T Shear Velocity, from DT1T (Transmitter Array, Lower Dipole; km/s) VS2T Shear Velocity, from DT2T (Transmitter Array, Upper Dipole; km/s) VTP Compressional Velocity, from DTTP (Transmitter Array, P&S; km/s) VTS Shear Velocity, from DTTS (Transmitter Array, P&S; km/s)#POINTS Number of Transmitter-Receiver Pairs Used in Sonic Processing W1NG NGT Window 1 counts (cps)W2NG NGT Window 2 counts (cps)W3NG NGT Window 3 counts (cps)W4NG NGT Window 4 counts (cps)W5NG NGT Window 5 counts (cps)OCEAN DRILLING PROGRAMACRONYMS AND UNITS USED FOR LWD SCHLUMBERGER LOGSAT1F Attenuation Resistivity (1 ft resolution; ohmm)AT3F Attenuation Resistivity (3 ft resolution; ohmm)AT4F Attenuation Resistivity (4 ft resolution; ohmm)AT5F Attenuation Resistivity (5 ft resolution; ohmm)ATR Attenuation Resistivity (deep; ohmm)BFV Bound Fluid Volume (%)B1TM RAB Shallow Resistivity Time after Bit (s)B2TM RAB Medium Resistivity Time after Bit (s)B3TM RAB Deep Resistivity Time after Bit (s)BDAV Deep Resistivity Average (ohmm)BMAV Medium Resistivity Average (ohmm)BSAV Shallow Resistivity Average (ohmm)CGR Computed (Th+K) Gamma Ray (API units)DCAL Differential Caliper (in)DROR Correction for CDN rotational density (g/cm3).DRRT Correction for ADN rotational density (g/cm3).DTAB AND or CDN Density Time after Bit (hr)FFV Free Fluid Volume (%)GR Gamma Ray (API Units)GR7 Sum Gamma Ray Windows GRW7+GRW8+GRW9-Equivalent to Wireline NGT window 5 (cps) GRW3 Gamma Ray Window 3 counts (cps)-Equivalent to Wireline NGT window 1GRW4 Gamma Ray Window 4 counts (cps)-Equivalent to Wireline NGT window 2GRW5 Gamma Ray Window 5 counts (cps)-Equivalent to Wireline NGT window 3GRW6 Gamma Ray Window 6 counts (cps)-Equivalent to Wireline NGT window 4GRW7 Gamma Ray Window 7 counts (cps)GRW8 Gamma Ray Window 8 counts (cps)GRW9 Gamma Ray Window 9 counts (cps)GTIM CDR Gamma Ray Time after Bit (s)GRTK RAB Gamma Ray Time after Bit (s)HEF1 Far He Bank 1 counts (cps)HEF2 Far He Bank 2 counts (cps)HEF3 Far He Bank 3 counts (cps)HEF4 Far He Bank 4 counts (cps)HEN1 Near He Bank 1 counts (cps)HEN2 Near He Bank 2 counts (cps)HEN3 Near He Bank 3 counts (cps)HEN4 Near He Bank 4 counts (cps)MRP Magnetic Resonance PorosityNTAB ADN or CDN Neutron Time after Bit (hr)PEF Photoelectric Effect (barns/e-)POTA Potassium (%) ROPE Rate of Penetration (ft/hr)PS1F Phase Shift Resistivity (1 ft resolution; ohmm)PS2F Phase Shift Resistivity (2 ft resolution; ohmm)PS3F Phase Shift Resistivity (3 ft resolution; ohmm)PS5F Phase Shift Resistivity (5 ft resolution; ohmm)PSR Phase Shift Resistivity (shallow; ohmm)RBIT Bit Resistivity (ohmm)RBTM RAB Resistivity Time After Bit (s)RING Ring Resistivity (ohmm)ROMT Max. Density Total (g/cm3) from rotational processing ROP Rate of Penetration (m/hr)ROP1 Rate of Penetration, average over last 1 ft (m/hr).ROP5 Rate of Penetration, average over last 5 ft (m/hr)ROPE Rate of Penetration, averaged over last 5 ft (ft/hr)RPM RAB Tool Rotation Speed (rpm)RTIM CDR or RAB Resistivity Time after Bit (hr)SGR Total Gamma Ray (API units)T2 T2 Distribution (%)T2LM T2 Logarithmic Mean (ms)THOR Thorium (ppm)TNPH Thermal Neutron Porosity (%)TNRA Thermal RatioURAN Uranium (ppm)OCEAN DRILLING PROGRAMADDITIONAL ACRONYMS AND UNITS(PROCESSED LOGS FROM GEOCHEMICAL TOOL STRING)AL2O3 Computed Al2O3 (dry weight %)AL2O3MIN Computed Al2O3 Standard Deviation (dry weight %) AL2O3MAX Computed Al2O3 Standard Deviation (dry weight %) CAO Computed CaO (dry weight %)CAOMIN Computed CaO Standard Deviation (dry weight %) CAOMAX Computed CaO Standard Deviation (dry weight %) CACO3 Computed CaCO3 (dry weight %)CACO3MIN Computed CaCO3 Standard Deviation (dry weight %) CACO3MAX Computed CaCO3 Standard Deviation (dry weight %) CCA Calcium Yield (decimal fraction)CCHL Chlorine Yield (decimal fraction)CFE Iron Yield (decimal fraction)CGD Gadolinium Yield (decimal fraction)CHY Hydrogen Yield (decimal fraction)CK Potassium Yield (decimal fraction)CSI Silicon Yield (decimal fraction)CSIG Capture Cross Section (capture units)CSUL Sulfur Yield (decimal fraction)CTB Background Yield (decimal fraction)CTI Titanium Yield (decimal fraction)FACT Quality Control CurveFEO Computed FeO (dry weight %)FEOMIN Computed FeO Standard Deviation (dry weight %) FEOMAX Computed FeO Standard Deviation (dry weight %) FEO* Computed FeO* (dry weight %)FEO*MIN Computed FeO* Standard Deviation (dry weight %) FEO*MAX Computed FeO* Standard Deviation (dry weight %) FE2O3 Computed Fe2O3 (dry weight %)FE2O3MIN Computed Fe2O3 Standard Deviation (dry weight %) FE2O3MAX Computed Fe2O3 Standard Deviation (dry weight %) GD Computed Gadolinium (dry weight %)GDMIN Computed Gadolinium Standard Deviation (dry weight %) GDMAX Computed Gadolinium Standard Deviation (dry weight %) K2O Computed K2O (dry weight %)K2OMIN Computed K2O Standard Deviation (dry weight %)K2OMAX Computed K2O Standard Deviation (dry weight %) MGO Computed MgO (dry weight %)MGOMIN Computed MgO Standard Deviation (dry weight %) MGOMAX Computed MgO Standard Deviation (dry weight %)S Computed Sulfur (dry weight %)SMIN Computed Sulfur Standard Deviation (dry weight %) SMAX Computed Sulfur Standard Deviation (dry weight %)SIO2 Computed SiO2 (dry weight %)SIO2MIN Computed SiO2 Standard Deviation (dry weight %) SIO2MAX Computed SiO2 Standard Deviation (dry weight %) THORMIN Computed Thorium Standard Deviation (ppm) THORMAX Computed Thorium Standard Deviation (ppm)TIO2 Computed TiO2 (dry weight %)TIO2MIN Computed TiO2 Standard Deviation (dry weight %) TIO2MAX Computed TiO2 Standard Deviation (dry weight %) URANMIN Computed Uranium Standard Deviation (ppm) URANMAX Computed Uranium Standard Deviation (ppm) VARCA Variable CaCO3/CaO calcium carbonate/oxide factor。

forcing oscillation物理含义

forcing oscillation物理含义

forcing oscillation物理含义
在物理中,forcing oscillation(强迫振动)通常指的是一个系统在受到周期性外力的作用下的振动行为。

这个周期性外力(也被称为强迫函数或激励函数)可以由其他系统的振动、声音、电磁场变化、化学反应过程等等产生。

当这个周期性外力的频率与系统的自然频率(即在没有外部激励的情况下,系统自己振动的频率)相近或者成整数倍关系时,系统将产生共振,此时系统的振动幅度会显著增加,这可能会带来积极(例如,共振可以用于驱动机械系统,如扬声器)或消极(例如,共振可以导致桥梁等结构的破坏)的影响。

此外,强迫振动也可以用来描述在混沌理论和非线性动力学中,当一个系统受到微小扰动时,其行为可能会产生的复杂、不可预测的变化。

例如,一个简单的线性弹簧振荡器在受到持续的微小扰动时,其运动轨迹可能会变为一个复杂的驼峰形状或者其它非线性形状。

Glider Flying Handbook说明书

Glider Flying Handbook说明书

Glider Flying Handbook2013U.S. Department of TransportationFEDERAL AVIATION ADMINISTRATIONFlight Standards Servicei iPrefaceThe Glider Flying Handbook is designed as a technical manual for applicants who are preparing for glider category rating and for currently certificated glider pilots who wish to improve their knowledge. Certificated flight instructors will find this handbook a valuable training aid, since detailed coverage of aeronautical decision-making, components and systems, aerodynamics, flight instruments, performance limitations, ground operations, flight maneuvers, traffic patterns, emergencies, soaring weather, soaring techniques, and cross-country flight is included. Topics such as radio navigation and communication, use of flight information publications, and regulations are available in other Federal Aviation Administration (FAA) publications.The discussion and explanations reflect the most commonly used practices and principles. Occasionally, the word “must” or similar language is used where the desired action is deemed critical. The use of such language is not intended to add to, interpret, or relieve a duty imposed by Title 14 of the Code of Federal Regulations (14 CFR). Persons working towards a glider rating are advised to review the references from the applicable practical test standards (FAA-G-8082-4, Sport Pilot and Flight Instructor with a Sport Pilot Rating Knowledge Test Guide, FAA-G-8082-5, Commercial Pilot Knowledge Test Guide, and FAA-G-8082-17, Recreational Pilot and Private Pilot Knowledge Test Guide). Resources for study include FAA-H-8083-25, Pilot’s Handbook of Aeronautical Knowledge, FAA-H-8083-2, Risk Management Handbook, and Advisory Circular (AC) 00-6, Aviation Weather For Pilots and Flight Operations Personnel, AC 00-45, Aviation Weather Services, as these documents contain basic material not duplicated herein. All beginning applicants should refer to FAA-H-8083-25, Pilot’s Handbook of Aeronautical Knowledge, for study and basic library reference.It is essential for persons using this handbook to become familiar with and apply the pertinent parts of 14 CFR and the Aeronautical Information Manual (AIM). The AIM is available online at . The current Flight Standards Service airman training and testing material and learning statements for all airman certificates and ratings can be obtained from .This handbook supersedes FAA-H-8083-13, Glider Flying Handbook, dated 2003. Always select the latest edition of any publication and check the website for errata pages and listing of changes to FAA educational publications developed by the FAA’s Airman Testing Standards Branch, AFS-630.This handbook is available for download, in PDF format, from .This handbook is published by the United States Department of Transportation, Federal Aviation Administration, Airman Testing Standards Branch, AFS-630, P.O. Box 25082, Oklahoma City, OK 73125.Comments regarding this publication should be sent, in email form, to the following address:********************************************John M. AllenDirector, Flight Standards Serviceiiii vAcknowledgmentsThe Glider Flying Handbook was produced by the Federal Aviation Administration (FAA) with the assistance of Safety Research Corporation of America (SRCA). The FAA wishes to acknowledge the following contributors: Sue Telford of Telford Fishing & Hunting Services for images used in Chapter 1JerryZieba () for images used in Chapter 2Tim Mara () for images used in Chapters 2 and 12Uli Kremer of Alexander Schleicher GmbH & Co for images used in Chapter 2Richard Lancaster () for images and content used in Chapter 3Dave Nadler of Nadler & Associates for images used in Chapter 6Dave McConeghey for images used in Chapter 6John Brandon (www.raa.asn.au) for images and content used in Chapter 7Patrick Panzera () for images used in Chapter 8Jeff Haby (www.theweatherprediction) for images used in Chapter 8National Soaring Museum () for content used in Chapter 9Bill Elliot () for images used in Chapter 12.Tiffany Fidler for images used in Chapter 12.Additional appreciation is extended to the Soaring Society of America, Inc. (), the Soaring Safety Foundation, and Mr. Brad Temeyer and Mr. Bill Martin from the National Oceanic and Atmospheric Administration (NOAA) for their technical support and input.vv iPreface (iii)Acknowledgments (v)Table of Contents (vii)Chapter 1Gliders and Sailplanes ........................................1-1 Introduction....................................................................1-1 Gliders—The Early Years ..............................................1-2 Glider or Sailplane? .......................................................1-3 Glider Pilot Schools ......................................................1-4 14 CFR Part 141 Pilot Schools ...................................1-5 14 CFR Part 61 Instruction ........................................1-5 Glider Certificate Eligibility Requirements ...................1-5 Common Glider Concepts ..............................................1-6 Terminology...............................................................1-6 Converting Metric Distance to Feet ...........................1-6 Chapter 2Components and Systems .................................2-1 Introduction....................................................................2-1 Glider Design .................................................................2-2 The Fuselage ..................................................................2-4 Wings and Components .............................................2-4 Lift/Drag Devices ...........................................................2-5 Empennage .....................................................................2-6 Towhook Devices .......................................................2-7 Powerplant .....................................................................2-7 Self-Launching Gliders .............................................2-7 Sustainer Engines .......................................................2-8 Landing Gear .................................................................2-8 Wheel Brakes .............................................................2-8 Chapter 3Aerodynamics of Flight .......................................3-1 Introduction....................................................................3-1 Forces of Flight..............................................................3-2 Newton’s Third Law of Motion .................................3-2 Lift ..............................................................................3-2The Effects of Drag on a Glider .....................................3-3 Parasite Drag ..............................................................3-3 Form Drag ...............................................................3-3 Skin Friction Drag ..................................................3-3 Interference Drag ....................................................3-5 Total Drag...................................................................3-6 Wing Planform ...........................................................3-6 Elliptical Wing ........................................................3-6 Rectangular Wing ...................................................3-7 Tapered Wing .........................................................3-7 Swept-Forward Wing ..............................................3-7 Washout ..................................................................3-7 Glide Ratio .................................................................3-8 Aspect Ratio ............................................................3-9 Weight ........................................................................3-9 Thrust .........................................................................3-9 Three Axes of Rotation ..................................................3-9 Stability ........................................................................3-10 Flutter .......................................................................3-11 Lateral Stability ........................................................3-12 Turning Flight ..............................................................3-13 Load Factors .................................................................3-13 Radius of Turn ..........................................................3-14 Turn Coordination ....................................................3-15 Slips ..........................................................................3-15 Forward Slip .........................................................3-16 Sideslip .................................................................3-17 Spins .........................................................................3-17 Ground Effect ...............................................................3-19 Chapter 4Flight Instruments ...............................................4-1 Introduction....................................................................4-1 Pitot-Static Instruments ..................................................4-2 Impact and Static Pressure Lines................................4-2 Airspeed Indicator ......................................................4-2 The Effects of Altitude on the AirspeedIndicator..................................................................4-3 Types of Airspeed ...................................................4-3Table of ContentsviiAirspeed Indicator Markings ......................................4-5 Other Airspeed Limitations ........................................4-6 Altimeter .....................................................................4-6 Principles of Operation ...........................................4-6 Effect of Nonstandard Pressure andTemperature............................................................4-7 Setting the Altimeter (Kollsman Window) .............4-9 Types of Altitude ......................................................4-10 Variometer................................................................4-11 Total Energy System .............................................4-14 Netto .....................................................................4-14 Electronic Flight Computers ....................................4-15 Magnetic Compass .......................................................4-16 Yaw String ................................................................4-16 Inclinometer..............................................................4-16 Gyroscopic Instruments ...............................................4-17 G-Meter ........................................................................4-17 FLARM Collision Avoidance System .........................4-18 Chapter 5Glider Performance .............................................5-1 Introduction....................................................................5-1 Factors Affecting Performance ......................................5-2 High and Low Density Altitude Conditions ...........5-2 Atmospheric Pressure .............................................5-2 Altitude ...................................................................5-3 Temperature............................................................5-3 Wind ...........................................................................5-3 Weight ........................................................................5-5 Rate of Climb .................................................................5-7 Flight Manuals and Placards ..........................................5-8 Placards ......................................................................5-8 Performance Information ...........................................5-8 Glider Polars ...............................................................5-8 Weight and Balance Information .............................5-10 Limitations ...............................................................5-10 Weight and Balance .....................................................5-12 Center of Gravity ......................................................5-12 Problems Associated With CG Forward ofForward Limit .......................................................5-12 Problems Associated With CG Aft of Aft Limit ..5-13 Sample Weight and Balance Problems ....................5-13 Ballast ..........................................................................5-14 Chapter 6Preflight and Ground Operations .......................6-1 Introduction....................................................................6-1 Assembly and Storage Techniques ................................6-2 Trailering....................................................................6-3 Tiedown and Securing ................................................6-4Water Ballast ..............................................................6-4 Ground Handling........................................................6-4 Launch Equipment Inspection ....................................6-5 Glider Preflight Inspection .........................................6-6 Prelaunch Checklist ....................................................6-7 Glider Care .....................................................................6-7 Preventive Maintenance .............................................6-8 Chapter 7Launch and Recovery Procedures and Flight Maneuvers ............................................................7-1 Introduction....................................................................7-1 Aerotow Takeoff Procedures .........................................7-2 Signals ........................................................................7-2 Prelaunch Signals ....................................................7-2 Inflight Signals ........................................................7-3 Takeoff Procedures and Techniques ..........................7-3 Normal Assisted Takeoff............................................7-4 Unassisted Takeoff.....................................................7-5 Crosswind Takeoff .....................................................7-5 Assisted ...................................................................7-5 Unassisted...............................................................7-6 Aerotow Climb-Out ....................................................7-6 Aerotow Release.........................................................7-8 Slack Line ...................................................................7-9 Boxing the Wake ......................................................7-10 Ground Launch Takeoff Procedures ............................7-11 CG Hooks .................................................................7-11 Signals ......................................................................7-11 Prelaunch Signals (Winch/Automobile) ...............7-11 Inflight Signals ......................................................7-12 Tow Speeds ..............................................................7-12 Automobile Launch ..................................................7-14 Crosswind Takeoff and Climb .................................7-14 Normal Into-the-Wind Launch .................................7-15 Climb-Out and Release Procedures ..........................7-16 Self-Launch Takeoff Procedures ..............................7-17 Preparation and Engine Start ....................................7-17 Taxiing .....................................................................7-18 Pretakeoff Check ......................................................7-18 Normal Takeoff ........................................................7-19 Crosswind Takeoff ...................................................7-19 Climb-Out and Shutdown Procedures ......................7-19 Landing .....................................................................7-21 Gliderport/Airport Traffic Patterns and Operations .....7-22 Normal Approach and Landing ................................7-22 Crosswind Landing ..................................................7-25 Slips ..........................................................................7-25 Downwind Landing ..................................................7-27 After Landing and Securing .....................................7-27viiiPerformance Maneuvers ..............................................7-27 Straight Glides ..........................................................7-27 Turns.........................................................................7-28 Roll-In ...................................................................7-29 Roll-Out ................................................................7-30 Steep Turns ...........................................................7-31 Maneuvering at Minimum Controllable Airspeed ...7-31 Stall Recognition and Recovery ...............................7-32 Secondary Stalls ....................................................7-34 Accelerated Stalls .................................................7-34 Crossed-Control Stalls ..........................................7-35 Operating Airspeeds .....................................................7-36 Minimum Sink Airspeed ..........................................7-36 Best Glide Airspeed..................................................7-37 Speed to Fly ..............................................................7-37 Chapter 8Abnormal and Emergency Procedures .............8-1 Introduction....................................................................8-1 Porpoising ......................................................................8-2 Pilot-Induced Oscillations (PIOs) ..............................8-2 PIOs During Launch ...................................................8-2 Factors Influencing PIOs ........................................8-2 Improper Elevator Trim Setting ..............................8-3 Improper Wing Flaps Setting ..................................8-3 Pilot-Induced Roll Oscillations During Launch .........8-3 Pilot-Induced Yaw Oscillations During Launch ........8-4 Gust-Induced Oscillations ..............................................8-5 Vertical Gusts During High-Speed Cruise .................8-5 Pilot-Induced Pitch Oscillations During Landing ......8-6 Glider-Induced Oscillations ...........................................8-6 Pitch Influence of the Glider Towhook Position ........8-6 Self-Launching Glider Oscillations During Powered Flight ...........................................................8-7 Nosewheel Glider Oscillations During Launchesand Landings ..............................................................8-7 Tailwheel/Tailskid Equipped Glider Oscillations During Launches and Landings ..................................8-8 Aerotow Abnormal and Emergency Procedures ............8-8 Abnormal Procedures .................................................8-8 Towing Failures........................................................8-10 Tow Failure With Runway To Land and Stop ......8-11 Tow Failure Without Runway To Land BelowReturning Altitude ................................................8-11 Tow Failure Above Return to Runway Altitude ...8-11 Tow Failure Above 800' AGL ..............................8-12 Tow Failure Above Traffic Pattern Altitude .........8-13 Slack Line .................................................................8-13 Ground Launch Abnormal and Emergency Procedures ....................................................................8-14 Abnormal Procedures ...............................................8-14 Emergency Procedures .............................................8-14 Self-Launch Takeoff Emergency Procedures ..............8-15 Emergency Procedures .............................................8-15 Spiral Dives ..................................................................8-15 Spins .............................................................................8-15 Entry Phase ...............................................................8-17 Incipient Phase .........................................................8-17 Developed Phase ......................................................8-17 Recovery Phase ........................................................8-17 Off-Field Landing Procedures .....................................8-18 Afterlanding Off Field .............................................8-20 Off-Field Landing Without Injury ........................8-20 Off-Field Landing With Injury .............................8-20 System and Equipment Malfunctions ..........................8-20 Flight Instrument Malfunctions ................................8-20 Airspeed Indicator Malfunctions ..........................8-21 Altimeter Malfunctions .........................................8-21 Variometer Malfunctions ......................................8-21 Compass Malfunctions .........................................8-21 Glider Canopy Malfunctions ....................................8-21 Broken Glider Canopy ..........................................8-22 Frosted Glider Canopy ..........................................8-22 Water Ballast Malfunctions ......................................8-22 Retractable Landing Gear Malfunctions ..................8-22 Primary Flight Control Systems ...............................8-22 Elevator Malfunctions ..........................................8-22 Aileron Malfunctions ............................................8-23 Rudder Malfunctions ............................................8-24 Secondary Flight Controls Systems .........................8-24 Elevator Trim Malfunctions .................................8-24 Spoiler/Dive Brake Malfunctions .........................8-24 Miscellaneous Flight System Malfunctions .................8-25 Towhook Malfunctions ............................................8-25 Oxygen System Malfunctions ..................................8-25 Drogue Chute Malfunctions .....................................8-25 Self-Launching Gliders ................................................8-26 Self-Launching/Sustainer Glider Engine Failure During Takeoff or Climb ..........................................8-26 Inability to Restart a Self-Launching/SustainerGlider Engine While Airborne .................................8-27 Self-Launching Glider Propeller Malfunctions ........8-27 Self-Launching Glider Electrical System Malfunctions .............................................................8-27 In-flight Fire .............................................................8-28 Emergency Equipment and Survival Gear ...................8-28 Survival Gear Checklists ..........................................8-28 Food and Water ........................................................8-28ixClothing ....................................................................8-28 Communication ........................................................8-29 Navigation Equipment ..............................................8-29 Medical Equipment ..................................................8-29 Stowage ....................................................................8-30 Parachute ..................................................................8-30 Oxygen System Malfunctions ..................................8-30 Accident Prevention .....................................................8-30 Chapter 9Soaring Weather ..................................................9-1 Introduction....................................................................9-1 The Atmosphere .............................................................9-2 Composition ...............................................................9-2 Properties ....................................................................9-2 Temperature............................................................9-2 Density ....................................................................9-2 Pressure ...................................................................9-2 Standard Atmosphere .................................................9-3 Layers of the Atmosphere ..........................................9-4 Scale of Weather Events ................................................9-4 Thermal Soaring Weather ..............................................9-6 Thermal Shape and Structure .....................................9-6 Atmospheric Stability .................................................9-7 Air Masses Conducive to Thermal Soaring ...................9-9 Cloud Streets ..............................................................9-9 Thermal Waves...........................................................9-9 Thunderstorms..........................................................9-10 Lifted Index ..........................................................9-12 K-Index .................................................................9-12 Weather for Slope Soaring .......................................9-14 Mechanism for Wave Formation ..............................9-16 Lift Due to Convergence ..........................................9-19 Obtaining Weather Information ...................................9-21 Preflight Weather Briefing........................................9-21 Weather-ReIated Information ..................................9-21 Interpreting Weather Charts, Reports, andForecasts ......................................................................9-23 Graphic Weather Charts ...........................................9-23 Winds and Temperatures Aloft Forecast ..............9-23 Composite Moisture Stability Chart .....................9-24 Chapter 10Soaring Techniques ..........................................10-1 Introduction..................................................................10-1 Thermal Soaring ...........................................................10-2 Locating Thermals ....................................................10-2 Cumulus Clouds ...................................................10-2 Other Indicators of Thermals ................................10-3 Wind .....................................................................10-4 The Big Picture .....................................................10-5Entering a Thermal ..............................................10-5 Inside a Thermal.......................................................10-6 Bank Angle ...........................................................10-6 Speed .....................................................................10-6 Centering ...............................................................10-7 Collision Avoidance ................................................10-9 Exiting a Thermal .....................................................10-9 Atypical Thermals ..................................................10-10 Ridge/Slope Soaring ..................................................10-10 Traps ......................................................................10-10 Procedures for Safe Flying .....................................10-12 Bowls and Spurs .....................................................10-13 Slope Lift ................................................................10-13 Obstructions ...........................................................10-14 Tips and Techniques ...............................................10-15 Wave Soaring .............................................................10-16 Preflight Preparation ...............................................10-17 Getting Into the Wave ............................................10-18 Flying in the Wave .................................................10-20 Soaring Convergence Zones ...................................10-23 Combined Sources of Updrafts ..............................10-24 Chapter 11Cross-Country Soaring .....................................11-1 Introduction..................................................................11-1 Flight Preparation and Planning ...................................11-2 Personal and Special Equipment ..................................11-3 Navigation ....................................................................11-5 Using the Plotter .......................................................11-5 A Sample Cross-Country Flight ...............................11-5 Navigation Using GPS .............................................11-8 Cross-Country Techniques ...........................................11-9 Soaring Faster and Farther .........................................11-11 Height Bands ..........................................................11-11 Tips and Techniques ...............................................11-12 Special Situations .......................................................11-14 Course Deviations ..................................................11-14 Lost Procedures ......................................................11-14 Cross-Country Flight in a Self-Launching Glider .....11-15 High-Performance Glider Operations and Considerations ............................................................11-16 Glider Complexity ..................................................11-16 Water Ballast ..........................................................11-17 Cross-Country Flight Using Other Lift Sources ........11-17 Chapter 12Towing ................................................................12-1 Introduction..................................................................12-1 Equipment Inspections and Operational Checks .........12-2 Tow Hook ................................................................12-2 Schweizer Tow Hook ...........................................12-2x。

自旋偶合

自旋偶合

K1H41+K2H42+K3H43+K4H44=K4E
计算矩阵元
<i|Ĥ|j> 建久期方程
为简化,记 c1= UB0(1-U)
c2= VB0(1-V)
U -(c /ħ)Î V +(h/ħ2)JÎ UÎ V Ĥ=-(c1/ħ)Î z 2 z
利用
Î x=(1/2)ħ Î x =(1/2)ħ
AX系统
J
J
U
V
一级裂分
化学位移以频率(Hz)为单位 /J>6 /J<6 弱耦合 强耦合 一级类型谱 高级类型谱
2 当U-V0时, U=V
1 2
1={v0(2-U- V)-J-[J2+v202]1/2}/2=v0(1- V)-J
3 4
2={v0(2-U- V)+J-[J2+v202]1/2}/2=v0(1- V)
允许跃迁 1 2 1={v0(2-U- V)-J-[J2+v202]1/2}/2
3 4 2={v0(2-U- V)+J-[J2+v202]1/2}/2
1 3 3={v0(2-U- V)-J+[J2+v202]1/2}/2 2 4 4={v0(2-U- V)+J+[J2+v202]1/2}/2 v0=B0 4- 3=J = U- V 2- 1=(E4-E3)-(E2-E1)=(E1+E4)-(E2+E3)=J
Î y=(1/2)iħ
Î y =(-1/2)iħ Î z =(1/2)ħ
Î z =(-1/2)ħ
U +(c /ħ) Î V +(h/ħ2)JÎ U Ĥ1=(c1/ħ) Î z 2 z V UÎ V = (c1/2ħ)ħ UV+(c2/2ħ)ħUV +

分子生物名词解释

分子生物名词解释

【先看了这么多,之后看了再补充】Gene(基因):【经典版:基因是孤立的排列在染色提上的实体,有特定的功能,能独立的而发生突变和遗传的“三位一体的”,最小的遗传单位】重复基因(duplicate factor):即在基因组中有多个拷贝的基因顺反子(cistron):断裂基因/不连续基因(Split genes / interrupted or discontinus genes):即在基因编码蛋白质的序列中插入与蛋白质编码无关的DNA间隔区,使一个基因分隔成不连续的若干区段。

跳跃基因/转座子(Jumping gene / Transposable element):即可移动的或可转移的遗传因子。

假基因(Pseudogenes):是基因组中与编码基因序列非常相似的非功能性基因组DNA 拷贝,一般情况都不被转录,且没有明确生理意义。

拟等位基因(Pseudo allele):紧密连锁,控制同一形状的非等位基因重叠基因(overlapping gene):指在同一段DNA顺序上,由于阅读框架不同或终止早晚不同,同时编码两个以上基因的现象。

极性突变(Polarity mutation):在一个操纵子中,与操纵基因近邻的结构基因发生终止突变后,它除了影响该基因自身产物的翻译外,还影响其后结构基因多肽的翻译,并且具有极性梯度的特征。

C值矛盾(C value paradox):在原核生物中, c > C 在真核生物钟C>>c【c :编码结构基因的核苷酸数C: 生物单倍体基因组DNA的核苷酸数】复制子(replicon): 基因的一个单位,为DNA分子中能从起始点进行复制的部分。

复制体(replisome):是参与DNA复制的蛋白质复合物,包含DNA聚合酶,引发酶,解旋酶,单链结合蛋白和其它辅助因子。

半保留复制(semiconservative replication):DNA复制的一种方式。

每条链都可用作合成互补链的模板,合成出两分子的双链DNA,每个分子都是由一条亲代链和一条新合成的链组成。

库什曼螺旋体英文介绍

库什曼螺旋体英文介绍

库什曼螺旋体英文介绍《库什曼螺旋体:一种奇特的微生物》The "Kushman Spirillum: An Extraordinary Microorganism"Introduction:Microorganisms constitute a diverse range of life forms on Earth, including bacteria, viruses, fungi, and protozoa. One intriguing microbe is the Kushman spirillum, also known as the spirochete bacterium. This microorganism exhibits distinctive physical characteristics and a fascinating mode of life that has captivated the attention of scientists worldwide.Physical Description:The Kushman spirillum is a helical-shaped bacterium, resembling a tightly coiled spring or a corkscrew. Its spiral shape is the result of their unique cell structure and motility machinery, which includes periplasmic flagella. These flagella allow it to twist and rotate its body, propelling itself through the surrounding environment. With an average length of 10 to 20 micrometers, the Kushman spirillum appears as a long, thin filament under a microscope.Habitat and Distribution:These microorganisms inhabit a variety of environments, including freshwater bodies, marine ecosystems, and even gastrointestinal tracts of animals. They are often found in environments with high organic content, such as sewage and decaying matter. Kushman spirilla are known to form biofilms – communities of microorganisms attached to surfaces – in order to protect themselves and efficiently access nutrients.Metabolism:Kushman spirilla are chemoorganotrophic bacteria, meaning they obtain energy by breaking down organic compounds through respiration. They are capable of using a wide range of organic substances, including sugars, amino acids, and fatty acids, as energy sources. These microorganisms also play critical roles in various biochemical cycles, such as nitrogen and sulfur cycles, contributing to the recycling of essential elements in the ecosystem.Role in Disease:While the majority of Kushman spirilla are harmless, certain strains have been associated with diseases in humans and other animals. For example, some species of spirochetes are responsible for causing Lyme disease and syphilis. Understanding the pathogenic characteristics and mechanisms of these bacteria is essential for the development of effective treatments and preventive measures. Scientific Research:Research on Kushman spirilla is multidisciplinary, involving microbiology, genetics, molecular biology, and ecology. Scientists are keen to decipher the mechanisms of its unique helical structure, motility, and its ability to adapt to various environments. Furthermore, investigations into the genetics and metabolism of this microorganism have contributed to advancements in biotechnology, such as the production of useful enzymes and biofuels.Conclusion:The Kushman spirillum is an extraordinary microorganism that continues to fascinate scientists due to its distinct helical shape and unique biological characteristics. Its ability to adapt to diverse environments and perform various essential functions highlights its ecological importance. Furthermore, research on this microorganism has paved the way for numerous applications in biotechnology and medical science. As we delve deeper into the world of microorganisms, the Kushman spirillum remains a remarkable subject of study, unveiling the mysteries of the microbial world.。

胆固醇的以酵素为基础决心使用这石英水晶的听觉波感应器

胆固醇的以酵素为基础决心使用这石英水晶的听觉波感应器

Analytica Chimica Acta487(2003)91–100Enzyme-based determination of cholesterol using thequartz crystal acoustic wave sensorS.P.Martin,mb,J.M.Lynch,S.M.Reddy∗Centre for Clinical Science&Measurement,School of Biomedical&Life Sciences,University of Surrey,Guildford,Surrey GU27XH,UK Received11December2002;received in revised form1April2003;accepted23April2003AbstractWe have used the AT-cut quartz crystal sensor to measure in real-time the total cholesterol concentration in buffer and serum,using the trienzyme system of cholesterol esterase(ChE),cholesterol oxidase(ChOx)and horseradish peroxidase (HRP).The hydrogen peroxide produced from the ChE–ChOx reaction oxidises diaminobenzidine(DAB),in the presence of HRP.The response of the sensor to cholesterol is optimal in the presence of0.1%(v/v)Triton X-100at0.2U/ml ChOx, and1U/ml ChE.A response is obtained in less ing the optimal concentrations of the reagents,the linear range for free cholesterol and low density lipoprotein(LDL)cholesterol determination was between50and300␮M,and25 and400␮M,respectively.It was found that the concentration of high density lipoprotein(HDL)cholesterol could not be determined because it solubilised the oxidised DAB,leading to poor adsorption at the crystal surface.We obtained a response to the use of cholesterol in serum at300␮M,demonstrating that this biosensor could be used for cholesterol determination in clinical samples.©2003Elsevier Science B.V.All rights reserved.Keywords:Cholesterol;Quartz crystal acoustic wave sensor;Cholesterol oxidase;Diaminobenzidine1.IntroductionCholesterol is routinely measured for the risk assessment of cardiovascular conditions,such as atherosclerosis and hypertension,which can develop into coronary heart disease,myocardial and cerebral infarction(stroke).In conditions such as hypothy-roidism,nephrosis,diabetes mellitus,myxedema,and obstructive jaundice,the patient will have increased levels of cholesterol and its esters above the physio-logical norm.Decreased levels are found in patients ∗Corresponding author.Tel.:+44-1483-876396;fax:+44-1483-576978.E-mail address:s.reddy@(S.M.Reddy).suffering from hyperthyroidism,anaemia,malabsorp-tion and wasting syndromes.The desired total plasma cholesterol for an in-dividual is less than 5.2mM(200mg/dl),and a high level being considered as greater than6.2mM (240mg/dl)[1].Plasma cholesterol levels increase with age,and are generally less in women than men, until menopause,when the values in women exceed those in men[2].Cholesterol is carried in plasma by a series of protein-containing micelles known as lipoproteins.The lipoproteins are classified into dis-tinct subtypes according to their density,very low density lipoprotein(VLDL),low density lipoprotein (LDL),intermediate density lipoprotein(IDL)and high density lipoprotein(HDL).About70%of total plasma cholesterol contained within lipoproteins is0003-2670/03/$–see front matter©2003Elsevier Science B.V.All rights reserved. doi:10.1016/S0003-2670(03)00504-X92S.P .Martin et al./Analytica Chimica Acta 487(2003)91–100esterified by fatty acids.Hence,the concentration of free cholesterol within lipoproteins is approximately 1.0–2.2mM (40–85mg/dl)[3].Historically,cholesterol was measured using non-enzymatic spectrometry,via the production of a coloured substance,chiefly via cholestapolyenes and cholestapolyene carbonium ions (Liebermann–Bur-chard reaction).This method suffered from poor specificity,instability of the colour reagent,standardi-sation difficulties,the variable reactivity of esters and the unstable and corrosive nature of the reagents used [4,5].The selectivity of the chemical reaction was im-proved with the introduction of the enzymes,choles-terol esterase (ChE)and cholesterol oxidase (ChOx):cholesterol esters +H 2O ChE→cholesterol +fatty acids(1)cholesterol +O 2ChOx→cholest-4-en-3-one +H 2O 2(2)The cholest-4-en-3-one can be reacted with 2,4-dini-trophenylhydrazine to produce a coloured hydrazone [6],although the consumption of O 2[7],or the pro-duction of H 2O 2[3,8–10]are the easier methods of quantifying cholesterol spectrophotometrically,with the latter being the preferred method.The presenceTable 1A comparison of previous methods for determining cholesterol ReferenceDetection methodResponse time (min)Linear range (mM)Detection limit (␮M)Lifetime (days)Known interferents[14]Fibre-optic fluorescence 7–12Not linear for FC 200–Not tested [12]Fibre-optic luminescence <0.50.15–3for FC 500>60Ascorbic acid[20]Potentiometric 160.05–3for TC10–Ascorbic acid,bilirubin and proteins had negligible effects [19]Amperometric <20.58–3.68for FC 605Ascorbic acid,paracetamol,glutathione,uric acid were major interferents [18]Amperometric 5No data for FC ––Oxygen,urea [17]Amperometric 1Not linear for TC 5001Not tested[15]Fluorometric <300.005–0.05for TC 5pM –Minimal inteference from bilirubin[3]Spectrophotometric52.6–15.6for TC2.6–Negligible interference from ascorbic acid,uric acid and haemoglobinFC refers to the fact that the biosensor was used to measure free cholesterol only,while TC means total cholesterol was determined.of molecular oxygen in clinical samples will result in false positives in any method measuring consumption of oxygen unless steps are taken to remove it [11].The oxygen will be consumed by other substances,which are present in clinical samples,such as ascorbic acid,as found by Marazuela et al.[12].A number of cholesterol biosensors have been de-veloped over the past 30years.Examples of optical biosensors,which determine cholesterol enzymati-cally have been developed [12–15].Some of these methods suffer from interference from other sub-stances found in the serum,as has been previously commented upon [12](see Table 1).Amperometric and potentiometric methods have been researched to determine cholesterol [16–20].The major disadvan-tages of these types of transducers include the need for calibration of the sensor both before and after the measurement,the lifetime of the sensor is short,and the oxidation of other electrochemically active species (known as interferents)present in the test sample may lead to false positive signals.The major interferents are ascorbic and uric acid (see Table 1).This problem can be overcome through the use of polymer layers,which are more selective for the analyte of interest and eliminate or reduce the interferences,but this requires more time for preparation,and increases the complexity of the biosensor.If the interferents areS.P.Martin et al./Analytica Chimica Acta487(2003)91–10093not reduced,this can lead to an overestimation of the analyte concentration.It has been clearly demonstrated by Chang and Shih[21]that neither ascorbic acid nor uric acid in-terfere with the operation of the quartz crystal sensor. Bilirubin proved to act as an interferent in absorption measurements,because it absorbed light at the same wavelength as the analyte being measured,and there-fore will not be an interferent for the quartz crystal. There is the possibility that ascorbic acid and uric acid act as hydrogen donors in the peroxidase reac-tion,which was raised by Nguyen et al.[22].However in other peroxidase reactions such as Allain et al.[3],using4-aminoantipyrine and phenol or the Sigma Infinity TM kit which uses4-aminoantipyrine and hy-droxybenzoic acid,there was no reported interference at normal physiological concentrations.Therefore, the same would be true for the cholesterol quartz crystal sensor,since all three assays are peroxidase reactions.The operation of the quartz crystal acoustic wave sensor as described by the Sauerbrey equation[23] provides a relationship between a shift in the reso-nant frequency and a corresponding change in mass on the crystal surface.The relationship is only ap-plicable if crystal measurements are made under dry conditions.Developments in quartz crystal the-ory[24,25]have now allowed the application of the quartz crystal for measuring analytes in liquid me-dia.This is due to the oscillating crystal’s ability to respond to mass and viscoelastic changes in the liq-uid phase.The acoustic wave sensor operates in the thickness shear mode resulting in the propagation of a shear wave into the interfacing liquid.By monitoring changes in the resonant frequency and impedance, it is possible to attribute changes in the solution conductivity,viscosity and density[24],as well as mass and viscoelasticity[25]at the liquid–crystal interface.The quartz crystal has been recently used as an immunosensor[26–28],a DNA sensor[29–31],and an enzyme-based sensor[31–33].We have also pre-viously used the quartz crystal for the enzymatic de-termination of glucose[31].This was accomplished by means of the two enzyme(glucose oxidase(GOx) and HRP)catalysed oxidation and dimerisation of the benzidine,DMOB.The ensuing precipitation led to a concentration-dependent frequency(f s)and impedance(Z s)shift at series resonance(the param-eter,f s refers to the frequency when the phase angle of the oscillation wave is zero,and Z s refers to the corresponding impedance at this point).We moni-tored changes in Z s for the same reason as previously mentioned by Reddy et al.[31],where they found it was difficult to establish f s,when the crystal load is dissipative.The changes in both parameters are directly proportional to the other,so in effect we are still measuring changes in the viscosity and density of the solution,as well as any additional mass loading due to adsorption[34].The biosensor was used to determine glucose in the range60–160␮M.The use of the quartz crystal to measure oxidase-catalysed production of hydrogen peroxide offers an alternative approach to the determination of low molecular weight solutes,such as glucose,lactate and cholesterol.Indeed,we have optimised the hy-drogen peroxide response with different benzidines (diaminobenzidine(DAB),DMOB,and tetramethyl-benzidine(TMB))through the use of the non-ionic surfactants,Triton X-100,and Tween80[35].In this paper,we describe our method for using the quartz crystal microbalance for the determination of free cholesterol(using the enzymes ChOx and HRP)and total cholesterol(using the enzymes ChOx,ChE and HRP).In doing so,we have determined the optimal concentration of ChOx,ChE and Triton X-100for this assay.We also determined total cholesterol in human LDL and HDL sub-fractions and in human serum using this assay.2.Experimental2.1.MaterialsPhosphate buffer tablets were purchased from Ox-oid(Basingstoke,UK),propan-2-ol from BDH(Poole, UK),and potassium bromide(KBr)from Fisher (Loughborough).Horseradish peroxidase(HRP type I,EC1.11.1.7,180PU/mg),Cholesterol oxidase(EC 1.1.3.6.from Streptomyces sp.,19U/mg),Choles-terol esterase(EC3.1.1.13from Pseudomonas sp.), 3,3 -diaminobenzidine tetrahydrochloride(D5637), Cholesterol(C8667),Triton X-100,Infinity TM choles-terol reagent(401-25P)and cholesterol calibrators (C0534)were obtained from Sigma(Poole,UK).94S.P.Martin et al./Analytica Chimica Acta487(2003)91–1003.Methods3.1.Solution preparationDiaminobenzidine was prepared in phosphate buffer(0.01M,pH7.4)to give afinal concentration of0.3mM.Cholesterol(10mM)was prepared in iso-propanol;the latter solvent has been shown to have no effect upon the activity of the enzymes at thefinal concentration used[36].All enzymes were prepared in phosphate buffer,giving afinal activity of360,50 and70U/ml for HRP,ChE and ChOx,respectively. Triton X-100was prepared in phosphate buffer,to give afinal concentration of1%(v/v).When not in use,all solutions were stored at4◦C.The diaminobenzidine and HRP solutions were prepared daily;and the Tri-ton X-100and Cholesterol solutions were prepared weekly.The ChOx and ChE were prepared in PBS and stored at−80◦C until1h before use(the remaining enzyme was discarded after that day’s experiments).3.2.Crystal preparationGold-on-chromium electrodes(100and5nm,re-spectively)were vapour-deposited onto either side of a blank AT-cut quartz crystal(IQD,Crewkerne,UK). The crystals had a fundamental resonance frequency of10MHz,and diameter of8.2mm.Crystals were cleaned with acetone and isopropanol,and dried with vacuum suction,prior to electrode deposition.One crystal piece was then sealed in the sample chamber as previously described[37].A HP4194A impedance analyser coupled to a PC was used to record resonant frequency and impedance changes at series resonance.3.3.Measurement procedureFor all experiments, 3.5ml DAB containing 0.2U/ml HRP was added to the test cell.Various con-centrations of Triton X-100(0.01–0.2%,v/v),choles-terol(0–400␮M),LDL(0–400␮M),HDL(300␮M) or serum(300␮M),ChOx(0–0.5U/ml)and if appli-cable,ChE(0.5–2U/ml)were then added.The test solution was stirred,during all experiments.After each experiment,the crystal was cleaned thoroughly with N,N-dimethylformamide(DMF)and deionised water.The use of DMF removed the oxidised DAB adsorbed to the crystal during the experiment,and was confirmed by the crystal frequency returning to its original value.All experiments were performed at room temperature.3.4.Spectrophotometric measurementsAll measurements were taken at492nm using a 96-well plate reader(Labsystems iEMS Reader MF and Labsystems Genesis Version3.05software).For the spectrophotometric measurements,all solutions were prepared as previously described.For the HRP experiments,300␮l of DAB,1␮l of HRP,3␮l of Tri-ton X-100,and a range of H2O2concentrations from 0to60␮M were added to each well.The absorbance was measured every15s,over10min at492nm.For the HRP–ChOx experiments,300␮l of DAB,1␮l of HRP,1␮l of ChOx,and a range of Triton X-100con-centrations were added,after which was added9␮l of cholesterol.Again,the absorbance was measured every15s,over10min at492nm.3.5.Isolation of HDL/LDLThe method of isolation used has been previously described by Rankin et al.[38].One hundred millil-itres of venous blood from healthy volunteers was collected into2ml of Na2EDTA(150mM,pH7.4, prepared in water,andfilter sterilised)using a20 gauge butterfly catheter(Abbott,Sligo,Rep.,Ire-land).The blood was centrifuged at800×g for 30min at4◦C in a Beckman GPR centrifuge(High Wycombe,Buckinghamshire)to obtain plasma.The density of the plasma was adjusted to1.019g/ml, by the addition of a“high density”(η=1.32g/ml) potassium bromide solution.The plasma was then transferred into11ml ultracentrifugation tubes(ultra clear,16mm×76mm)from Beckman Instruments (High Wycombe,Buckinghamshire)and centrifuged at108,000×g for18h at4◦C in a Beckman70Ti rotor,and Beckman Optima XL-100K ultracentrifuge (Beckman Instruments,High Wycombe,Bucking-hamshire).Following centrifugation,the fraction containing LDL and HDL was recovered,its density adjusted to1.063g/ml by the addition of KBr and then dialysed against a PBS solution containing KBr for 4h,to give afinal density of1.063g/ml.Following this,it was centrifuged as previously described under the same conditions.The LDL and HDL fractionsS.P .Martin et al./Analytica Chimica Acta 487(2003)91–10095were recovered and dialysed against four changes of PBS to remove any KBr.The separate LDL and HDL sub-fractions were filter sterilised (pore size,0.2␮M from Sartorius Group,Epsom,Surrey),to remove lipoprotein aggregates and stored at 4◦C.3.6.Spectrophotometric determination of cholesterol concentrationThis method is a modification of the Sigma Diag-nostics procedure No.401.Three microlitres of stan-dard (cholesterol calibrator 100,200and 400g/l,and 6␮l of 400g/l to obtain 800g/l),LDL,HDL,or serum was pipetted per well in replicate on a 96-well plate.Three hundred microlitres of Sigma Infinity TM choles-terol reagent was added per well and incubated at room temperature for 30min.The absorbance at 525nm was measured using a 96-well plate reader (Labsystems iEMS Reader MF,and Labsystems Genesis Version 3.05software).The cholesterol concentration was then calculated from the standard curve.4.Results and discussion4.1.Optimisation of Triton X-100with cholesterol oxidaseThe Triton X-100concentration required for the op-timal response for the measurement of freecholes-Fig.1.Triton X-100concentration profile for the optimum response to 300␮M cholesterol in the crystal impedance (Z s )at 10MHz.Each value is the mean ±S .E .M.(n =3).terol was determined.A range of Triton X-100con-centrations were used (0.001–0.2%,v/v),while the ChOx concentration was maintained at 0.1U/ml,and the cholesterol concentration at 300␮M (Fig.1).In-creasing concentrations of Triton X-100increased the change in crystal impedance (Z s )reaching a maximum at around 0.1%(v/v)(Fig.1).We have previously found that the optimal con-centration of Triton X-100for the determination of hydrogen peroxide using DAB was 0.1%(v/v)[35].Indeed,the data shows (Fig.1)that this is also the optimal concentration of Triton X-100for the deter-mination of cholesterol.We believe this is due to the surfactant improving the enzyme activity,and also improving the dimerisation of oxidised DAB,which is supported by spectrophotometric analysis.When measuring the absorbance at 492nm,we found that for the hydrogen peroxide determination,the V max increased from 1.06 A min −1(no surfactant present)to 2.46 A min −1in the presence of Triton X-100(data not shown).The K m remained reasonably con-stant (0.68and 0.66mM in the absence and presence of surfactant,respectively).Another possibility is the Triton is increasing the solubility of the substrate [14,20,39].We found previously that Triton X-100at 0.1%(v/v)led to increased adsorption of the oxi-dised DAB product at the crystal surface.It has also been demonstrated previously that Triton X-100at a concentration range of 0.05–0.1%(v/v),increases the activity of ChOx [36,40–42].At concentrations96S.P .Martin et al./Analytica Chimica Acta 487(2003)91–100above this,Triton X-100was found to inhibit the activity of the enzyme [40].Therefore,Triton X-100is not only increasing adsorption of the oxidised DAB,but also ChOx activity,and the activity profile may result from a combination of these two effects.Upon measuring the change in absorbance at 492nm,for various concentrations of Triton X-100with the ChOx-HRP reaction,we found that the change in absorbance peaked at about 0.1–0.05%(v/v)Triton X-100(0.11 A and 0.12 A min −1,respectively),compared to 0.2and 0%(v/v)Triton X-100(0.08 A and 0.09 A min −1,respectively)(data not shown).4.2.Optimisation of cholesterol oxidaseTo determine the optimal ChOx concentra-tion,a range of ChOx concentrations were used (0.01–0.5U/ml),using Triton X-100at 0.1%(v/v)and cholesterol at 300␮M.Increasing concentrations of ChOx (0.1–0.01U/ml)resulted in a decrease in the observed Z s (Fig.2).However,increasing concentrations of ChOx de-creased the response time from 34.5±1.5min for 0.01U/ml,to 22.3±0.3min using 0.2U/ml (data not shown).It was decided that the optimal concentra-tion of ChOx for the determination of cholesterol was 0.2U/ml,when both response size and time were con-sidered.This concentration of ChOx is similar to op-timal concentration used by others [43].4.3.Calibration with cholesterolUsing the previously optimised Triton X-100and ChOx concentrations,the response tocholesterolFig.2.The optimisation of ChOx,using 0.1%(v/v)Triton X-100,and 300␮M cholesterol.Each value is the mean ±S .E .M .(n =3).was determined over the range,0–400␮M.A linear relationship between the cholesterol concentration (0–300␮M)and change in Z s was observed (Fig.3).For clinical measurement of free cholesterol in serum,a 1:10sample dilution would be required,so that the cholesterol concentration would fall inside the linear range of our biosensor.4.4.Optimisation of cholesterol esteraseWe isolated LDL from human blood as a substrate for the optimisation of ChE,since cholesterol es-ters occur naturally in aqueous solution within LDL,whilst cholesterol esters,e.g.cholesteryl oleate,re-quire preparation in various solvents,the presence of which may have unforeseen effects on enzyme activ-ity and stability.The cholesterol concentration within LDL was established by means of the cholesterol determination spectrophotometrically.The optimal concentration of the enzyme,ChE was determined,using the previously optimised concentra-tions of Triton X-100and ChOx.The ChE was used at 0.2,1,and 2U/ml,and it was found that 1U/ml gave the best response in terms of response size and re-producibility (see Fig.4).For all further experiments,1U/ml ChE was used.4.5.Calibration curve with LDLUsing the isolated LDL,a series of experiments were performed to produce a calibration curve over the concentration range of 25–400␮M LDL cholesterol (Fig.5).This produced a linear rela-tionship between the concentration of LDL,and theS.P.Martin et al./Analytica Chimica Acta487(2003)91–10097Fig.3.The calibration curve for cholesterol determination,using0.2U/ml ChOx,and0.1%(v/v)Triton X-100.Each value is the mean±S.E.M.(n=3).Fig.4.The optimisation of ChE,using0.1%Triton X-100,0.2U/ml ChOx,and300␮M LDL.Each value is the mean±S.E.M.(n=3).Fig.5.The calibration curve for LDL determination,between the concentrations of0and400␮M,when using0.1%Triton X-100,0.2U/ml ChOx,and1U/ml ChE.Each value is the mean±S.E.M.(n=3).98S.P .Martin et al./Analytica Chimica Acta 487(2003)91–100Fig.6.The Z s responses for the use of serum,HDL,and LDL as the substrates at 300␮M.Each value is the mean ±S .E .M .(n =3).corresponding change in Z s .For clinical measurement of total cholesterol in serum,a 1:20sample dilution would be required,so that the total cholesterol con-centration would fall within the linear range of our biosensor.4.6.Determination of cholesterol in serumFig.6shows the Z s responses to the use of LDL,HDL and serum at 300␮M cholesterol,as the sub-strates for determination.Experiments with all three substrates were performed,with the enzymes,Triton X-100,and DAB being used at the optimal concen-trations.It was found that isolated LDL gave an en-hanced response and HDL gave a poor response,in comparison to serum,which was found to be statisti-cally significant (P <0.001).To identify possible causes of this reduced re-sponse to HDL,the LDL and HDL subfractions were re-isolated by centrifugation at the end of the exper-iment.It can be seen from the photographs of the two tubes (Fig.7),the oxidised DAB was distributed differently.In the LDL tube,the LDL fraction is at the top of the tube,and the oxidised DAB pelleted at the bottom.However,the HDL and the oxidised DAB co-localised at the top of the HDL tube.This would suggest that the oxidised DAB is dissolving within HDL,leading to a lack of adsorption to the crystal surface,and the correspondingly small change in Z s .It will be noted that in Fig.6,there is a difference between the Z s response for LDL and serum.This measured difference is perhaps due to the negative in-terference caused by the HDL in the serumsampleFig.7.The results from the ultracentrifugation of LDL and HDL,after a normal assay for the determination of cholesterol content.The photos show the regions of oxidised DAB accumulation in the two tubes,in relation to the areas of LDL and HDL (M:meniscus;H:HDL;L:LDL;D:oxidised DAB).S.P.Martin et al./Analytica Chimica Acta487(2003)91–10099as previously discussed,but also may in part be due to the activity of catalase,which will be present in serum.Catalase will compete with HRP for the hydro-gen peroxide produced,but will not oxidise the DAB, thereby reducing the response.This problem may be overcome by the addition of sodium azide,though at high concentrations this may inhibit the activity of HRP[44,45].The influence of other possible interfer-ents may be overcome by constructing a calibration curve using serum with known cholesterol concentra-tions.5.ConclusionsWe have successfully applied our optimised hydro-gen peroxide detection system using the quartz crystal acoustic wave sensor to the determination of both free and total cholesterol in biological samples.We found that the optimal concentration of Triton X-100was 0.1%(v/v),for ChOx was0.2and1U/ml for ChE. Using the reagents at these concentrations,we found that there was a linear range for LDL cholesterol determination up to400␮M.For clinical measure-ment of total cholesterol using this method,a dilution (1/20)of the serum would be required.The quartz crystal technique offers advantages over the more conventional electrochemical and optical biosensing strategies;by virtue of its mass/viscoelasticity sensing mode,it is not affected by electrochemical and optical interferents.AcknowledgementsThe authors wish to thank the EPSRC(GR/M63744) forfinancial support during this project.We would like to thank Mr.Ian Davies for his help with the ultracentrifugation.References[1]National Cholesterol Education Program,Arch.Intern.Med.148(1988)36.[2]A.Kaplan,R.Jack,K.E.Opheim,B.Toivola,A.W.Lyon,in:Clinical Chemistry:Interpretations and Techniques,fourth ed.,Williams&Wilkins,London,1995,p.240.[3]C.C.Allain,L.S.Poon,C.S.G.Chan,W.Richmond,P.C.Fu,Clin.Chem.20(1974)470.[4]W.Richmond,Clin.Chem.19(1973)1350.[5]D.L.Witte,D.A.Barrett Jr.,D.A.Wycoff,Clin.Chem.20(1974)1282.[6]H.M.Flegg,Ann.Clin.Biochem.10(1973)79.[7]M.Mascini,M.Iannello,G.Palleschi,Anal.Chim.Acta146(1983)135.[8]H.Huang,J.W.Kuan,G.G.Guilbault,Clin.Chem.21(1975)1605.[9]F.O.Sale,S.Marchesini,P.H.Fishman, B.Berra,Anal.Biochem.142(1984)347.[10]A.Carpenter,W.C.Purdy,Anal.Lett.23(1990)425.[11]T.Tatsuma,T.Watanabe,Anal.Chim.Acta242(1991)85.[12]M.D.Marazuela,B.Cuesta,M.C.Moreno-Bondi,A.Quejido,Biosens.Bioelectron.12(1997)233.[13]G.Pasin,G.M.Smith,M.O’Mahony,Food Chem.61(1998)255.[14]W.Trettnak,O.S.Wolfbeis,Anal.Biochem.184(1990)124.[15]D.M.Amundson,M.Zhou,J.Biochem.Biophys.Methods38(1999)43.[16]L.Charpentier,N.El Murr,Anal.Chim.Acta318(1995)89.[17]T.Nakaminami,S.Ito,S.Kuwabata,H.Yoneyama,Anal.Chem.71(1999)1068.[18]T.Nakaminami,S.Kuwabata,H.Yoneyama,Anal.Chem.69(1997)2367.[19]M.A.T.Gilmartin,J.P.Hart,Analyst119(1994)2331.[20]M.Situmorang,P.W.Alexander,D.B.Hibbert,Talanta49(1999)639.[21]M.Chang,J.Shih,Sens.Actuators B67(2000)275.[22]V.K.Nguyen,C.M.Wolff,J.L.Seris,J.P.Schwing,Analysis18(1990)582.[23]G.Z.Sauerbrey,Physik155(1959)206.[24]M.Rodahl,F.Hook,B.Kasemo,Anal.Chem.68(1996)2219.[25]F.Ferrante,A.L.Kipling,M.Thompson,J.Appl.Phys.76(1994)3448.[26]X.D.Su,S.F.Y.Li,Anal.Chim.Acta429(2001)27.[27]B.S.Attili,A.A.Suleiman,Anal.Lett.28(1995)2149.[28]I.S.Park,W.Y.Kim,N.Kim,Biosens.Bioelectron.15(2000)167.[29]H.Su,P.Williams,M.Thompson,Anal.Chem.67(1995)1010.[30]S.Tombelli,M.Mascini,C.Sacco,A.P.F.Turner,Anal.Chim.Acta418(2000)1.[31]S.M.Reddy,J.P.Jones,T.J.Lewis,P.M.Vadgama,Anal.Chim.Acta363(1998)203.[32]F.Patolsky,M.Zayats,E.Katz,I.Willner,Anal.Chem.71(1999)3171.[33]L.Alfonta,E.Katz,I.Willner,Anal.Chem.72(2000)927.[34]S.J.Martin,G.C.Frye,A.J.Ricco,S.D.Senturia,Anal.Chem.65(1993)2910.[35]S.P.Martin,J.M.Lynch,S.M.Reddy,Biosens.Bioelectron.17(2002)735.[36]L.Pollegioni,G.Gadda, D.Ambrosius,S.Ghisla,M.S.Pilone,Biotech.Appl.Biochem.30(1999)27.[37]S.M.Reddy,Mater.Sci.Eng.C12(2000)23.[38]S.M.Rankin,M.E.Knowles,D.S.Leake,Atherosclerosis79(1989)71.100S.P.Martin et al./Analytica Chimica Acta487(2003)91–100[39]J.L.Besombes,S.Cosnier,bbe,G.Reverdy,Anal.Chim.Acta317(1995)275.[40]A.Noma,K.Nakayama,Clin.Chem.22(1976)336.[41]H.Huang,S.Kuan,G.G.Guilbault,Clin.Chem.23(1977)671.[42]W.Miner-Williams,Clin.Chim.Acta101(1980)77.[43]P.H.Lolekha,Y.Teerajetkul,b.Anal.10(1996)167.[44]Y.Hahn,C.L.Olson,Anal.Chem.51(1979)444.[45]A.Noma,K.Nakayama,Clin.Chem.22(1976)336.。

磁共振成像技术中英文名词对照之欧阳化创编

磁共振成像技术中英文名词对照之欧阳化创编
中央处理单元
Touch screen
触摸屏
System software
系统软件
Operating system ,OS
操作系统
Application software
应用软件
Worklist
工作表
File transfer protocal , FTP
文件传输
Send / receive
传输/接收
信号采集
signal sampling
信号采样
data acquisition
数据采集
raw data
原始数据
Analogue to digital converter , ADC
模数转换器
frequency resolution
频率分辨力
Analog to digital conversion data
射频
RF coil ,or RF resonator
射频线圈
transmit coil
发射线圈
receive coil
接受线圈
array
阵列
Solenoidal RF antenna
螺线管线圈
saddle-shaped RF antenna
鞍形线圈
Bird cage coil
鸟笼式线圈
detuning
磁共振成像技术中英文名词对照
时间:2021.02.12
创作人:欧阳化
abdomen
腹部
Apparent diffusion coefficient, ADC
表现扩散系数
Analog-digital conversion ,ADC
模数转换
Arterial spin labeling ,ASL

机体的工作机制 英文

机体的工作机制 英文

机体的工作机制英文《The Mechanism of the Organism》The human body is an incredibly complex and wondrous machine, with countless intricate systems working together to keep us alive and functioning. Understanding the mechanism of the organism involves delving into the physiology of various body systems, including the cardiovascular, respiratory, digestive, and nervous systems, among others.At the most basic level, the human body works by converting food and oxygen into energy through the process of metabolism. The digestive system breaks down food into nutrients, which are then absorbed into the bloodstream and transported to cells throughout the body. Oxygen is delivered to cells via the respiratory system, where it is used in conjunction with nutrients to produce energy.The cardiovascular system, composed of the heart and blood vessels, is responsible for delivering oxygen and nutrients to tissues and organs, as well as removing waste products and carbon dioxide. The heart pumps blood throughout the body, ensuring that every cell receives the necessary components for energy production.The nervous system plays a crucial role in coordinating and controlling the functions of the body. It consists of the brain, spinal cord, and a network of nerves that transmit signals to and from different parts of the body. This system regulates essential bodily functions such as breathing, heart rate, and digestion, as well as voluntary movements and higher cognitive functions.The endocrine system, composed of various glands that produce hormones, also plays a vital role in regulating bodily processes. Hormones act as chemical messengers, influencing metabolism, growth and development, mood, and stress response.The immune system serves as the body's defense against pathogens and foreign invaders, protecting us from infection and disease. It consists of a complex network of cells, tissues, and organs that work together to identify and eradicate harmful substances.Lastly, the musculoskeletal system enables movement and provides structural support for the body. Muscles, bones, and joints work in harmony to allow us to walk, run, lift objects, and perform a multitude of other activities.The mechanism of the organism is truly a marvel of nature, with each system intricately designed and finely tuned to ensure the body's survival and optimal functioning. Understanding and appreciating the inner workings of the human body can lead to greater insight into the importance of maintaining a healthy lifestyle and taking care of our physical and mental well-being.。

花粉和柱头之间的相互识别的机制

花粉和柱头之间的相互识别的机制

花粉和柱头之间的相互识别的机制英文回答:The mechanism of mutual recognition between pollen and pistil is a fascinating process in plant reproduction. It involves a series of intricate interactions and molecular signals that enable the pollen to identify and successfully fertilize the appropriate pistil. This recognition mechanism is crucial for ensuring successful pollination and subsequent seed development.One of the key components in the recognition process is the presence of specific proteins on the surface of both pollen and pistil. These proteins, known as recognition factors or receptors, play a vital role in mediating the recognition and interaction between the two. They act as molecular keys and locks, ensuring that only compatible pollen and pistil can recognize and bind to each other.In the case of pollen, the recognition factors aretypically located on the surface of the pollen grain. These factors can vary between different plant species and even within the same species. They are often glycoproteins or glycolipids that possess unique carbohydrate structures. These structures are recognized by corresponding receptors on the pistil, initiating the recognition process.On the other hand, the pistil also possesses recognition factors that are responsible for identifying compatible pollen. These factors are usually present on the surface of the stigma, the receptive part of the pistil. They can be receptor proteins or other molecules that have the ability to recognize and bind to specific pollen proteins or carbohydrates.Once the recognition factors on the pollen and pistil come into contact, a series of biochemical reactions and signal transduction pathways are initiated. These pathways lead to the activation of various cellular processes, such as pollen tube growth and guidance towards the ovary. The successful growth of the pollen tube ensures the delivery of sperm cells to the ovule, where fertilization takesplace.It is worth noting that the recognition mechanism between pollen and pistil is highly specific and selective. This specificity ensures that only compatible pollen is able to fertilize the pistil, while incompatible pollen is rejected. This mechanism is crucial for maintaining genetic diversity and promoting successful reproduction in plants.中文回答:花粉和柱头之间的相互识别机制是植物繁殖过程中的一个迷人的过程。

启动子和增强子区域中常见的顺式作用元件的英文

启动子和增强子区域中常见的顺式作用元件的英文

启动子和增强子区域中常见的顺式作用元件的英文【中英文实用版】Title: Common Cis-acting Elements in Promoter and Enhancer RegionsIn the intricate tapestry of gene regulation, cis-acting elements hold a position of paramount importance. These sequences, found within non-coding regions of the DNA, play a pivotal role in orchestrating the transcriptional machinery. Among them, the promoter and enhancer regions are hotspots for regulatory activity, harboring a myriad of cis-elements that are crucial for the precise control of gene expression.在基因调控的复杂网络中,顺式作用元件占据了至关重要的位置。

这些序列存在于DNA的非编码区域中,对调控转录机制起着关键作用。

其中,启动子和增强子区域是调控活动的热点,它们包含了诸多对精确控制基因表达至关重要的顺式元件。

Distinct from their trans-acting counterparts, cis-acting elements exert their influence locally, bound by the physical constraints of the genomic loci they inhabit. In the promoter region, for instance, the TATA box and the Initiator element are iconic cis-elements that facilitate the assembly of the transcriptional pre-initiation complex.与它们的反式作用对应物不同,顺式作用元件在其所处的基因座物理限制内局部发挥作用。

基因振荡原理范文

基因振荡原理范文

基因振荡原理范文基因振荡是一种生物体内的自发性周期性变化现象,也称为生物钟。

在生物体内存在着一定的基因网络调控系统,这个系统会通过调控特定的基因表达来控制生物体的周期性变化。

基因振荡是这一调控系统的核心原理之一基因振荡主要通过负反馈回路来实现。

负反馈回路是一种调控系统中常见的自调节机制,它能够根据系统的当前状态来改变调控信号,使系统趋向平衡状态。

在基因网络调控系统中,负反馈回路作为一个调控环节,能够控制细胞内特定的基因表达。

基因振荡的核心机制就是利用这种负反馈回路来实现周期性的基因表达。

基因振荡最早在果蝇中被发现。

果蝇的生物钟调控系统中存在一个叫做"黄素射线细胞"的特殊细胞群。

这些细胞内部存在一种叫做周期蛋白(周期蛋白Drosophila per)的蛋白质。

周期蛋白会在细胞内周期性地合成和降解,导致细胞内的周期性变化。

合成和降解的过程中包含一个负反馈回路:周期蛋白在细胞核中转录和翻译形成新的周期蛋白,在细胞质中降解,形成周期性波动。

基因振荡在生物体的许多生理和行为过程中都起着重要的调控作用。

例如,人类的生物钟调控系统是由一组相互调控的基因网络构成的,其中包括多个基因振荡的负反馈回路。

这个调控系统使我们的身体具有了一定的生物节律,如昼夜节律。

这些生物节律能够调控我们的睡眠-清醒周期、体温、激素分泌等生理过程。

基因振荡也在其他生物体内起到重要的作用。

比如,酵母菌的细胞周期就是由基因振荡来调控的。

酵母菌的细胞周期分为四个阶段:G1、S、G2和M期。

每个阶段都有特定的基因表达模式,其中一些基因通过周期性地表达来驱动细胞周期的进行。

除了以上提到的调控作用,基因振荡还在很多其他生理和行为过程中扮演着重要角色。

例如,植物的生长节律、动物的繁殖周期、昆虫的飞行活动等都受到基因振荡的调控。

此外,一些疾病如癌症、心血管疾病等也与基因振荡失调相关。

总结来说,基因振荡是生物体内自发发生的周期性变化现象,通过负反馈回路实现调控。

金属硫化物 自旋-轨道耦合效应

金属硫化物 自旋-轨道耦合效应

金属硫化物自旋-轨道耦合效应金属硫化物是一类具有广泛应用价值的材料,在化学、物理、材料科学等领域均有重要的应用。

金属硫化物的独特性质主要来源于其内部原子之间的相互作用,其中最重要的一种是自旋-轨道耦合效应(SOC)。

本文将详细介绍金属硫化物中自旋-轨道耦合效应的相关知识。

自旋-轨道耦合效应是指原子的自旋(spin)和轨道(orbital)运动之间的相互作用。

在金属硫化物中,由于硫原子与金属原子之间的化学键比较共价,因此硫原子的轨道往往与金属原子的轨道之间的耦合比较强,从而导致自旋-轨道耦合效应的出现。

另外,金属原子本身具有不同的自旋磁矩,这也会进一步增强自旋-轨道耦合效应。

自旋-轨道耦合效应对金属硫化物的物理性质产生重要影响。

首先,它会改变体系的基态。

例如,在一些金属硫化物中,自旋-轨道耦合效应可以导致材料的基态为反铁磁性或者亚铁磁性,而非费米子的Pauli磁性。

其次,自旋-轨道耦合效应还会影响材料的输运性质、光学性质等。

例如,在某些情况下,自旋-轨道耦合效应可以导致电子微观结构的改变,从而影响材料的导电性。

同样地,在某些金属硫化物中,自旋-轨道耦合效应也可以导致光学性质的改变,从而影响材料的吸收谱和发射谱。

自旋-轨道耦合效应在材料科学中有着广泛的应用。

首先,由于自旋-轨道耦合效应对材料性质的影响非常明显,因此它已经成为材料设计和材料优化的一个重要指标之一。

其次,自旋-轨道耦合效应也可以用于制备一些新型的材料,例如拓扑绝缘体和拓扑半金属等。

这些材料一般具有特殊的电子能带结构和拓扑特性,因此被广泛应用于材料、器件等领域。

总之,自旋-轨道耦合效应是金属硫化物中一个非常重要的物理效应。

它对于金属硫化物的基态、输运性质、光学性质等方面产生着重要的影响。

未来,我们可以通过进一步的研究,探索其他类型的材料中自旋-轨道耦合效应对材料性质的影响,从而为材料科学的发展做出更大的贡献。

北京大学基础分子生物学考题-考研及期中、期末复习资料

北京大学基础分子生物学考题-考研及期中、期末复习资料

北京大学基础分子生物学考题-考研及期中、期末复习资料1.名词解释:中心法则厘摩基因蛋白质免疫沉淀染色质免疫沉淀核酶上游启动元件引物凝胶滞缓技术 RNA编辑2.选择题:摆动假说的决定位点~~(忘了题目具体怎么说了)成熟蛋白N端第一个碱基是什么蛋白最不稳定链霉素为什么能抑制蛋白质的合成哪些抑制剂只与原核细胞核糖体发生作用hnRNA是什么RNA的前体什么的内含子剪接过程中会出现锁套结构转录抑制剂中的模板结合抑制剂有关转录的选择错误选项的题增强子特点RNA聚合酶中负责模板链选择和转录起始的亚基蛋白质磷酸化修饰Φ174病毒编码蛋白需要的DNA序列比实际中多的原因SSB蛋白的作用Ds-Ac自主与非自主3.判断题:人与猿猴不同的基因是编码DNARNA聚合酶 1 有3’-5’外切酶活性和的5’-3’的外切酶活性转运后翻译的的指标之一是可溶性活性蛋白水解酶位于叶绿体基质中颠换是指嘌呤到嘌呤,嘧啶到嘧啶分子伴侣参与最终产物的形成tRNA的尾巴是CCA5’起始tRNA进入A位点,核糖体蛋白又能构建结构,又能调控(大概这个意思Ba)TATA 区控制转录起始频率1类内含子需要鸟苷辅助三元复合物形成时,RNA聚合酶离开起始位点分泌蛋白和膜蛋白几乎都是糖基化蛋白4.简答:五种碱基的结构式酵母双杂交基因定点突变技术完全基因敲除和条件基因敲除基因芯片技术及应用为什么Bard1和WUS基因作用要用超凝胶滞缓TaqMan探针比SYBR Green探针好感受态细胞制备的原理和方法蓝白斑筛选的分子机制cDNA合成的方向是如何实现的5.问答题:3种实验现象说明染色质中DNA和蛋白质有作用为什么dsRNA 与蛋白质作用没有序列特异性原核和真核生物在转录起始的第一步有什么不同设计6种抑制翻译的方法蛋白质前体加工。

转录的多种终止机制

转录的多种终止机制

转录的多种终止机制展开全文转录进行到一定程度,会停止下来,复合物解体,新生RNA释放出来,称为转录的终止(termination)。

终止通常需要一个标志,即终止子(terminator),DNA模板上作为转录终止信号的顺式作用元件(cis-acting element)。

元件(element)指DNA上有特定功能的一段序列。

相对来说,与之作用的蛋白质被称为“因子”(factor)。

顺式(cis)与反式(trans)来自拉丁文前缀,是“在同一侧”和“在另一侧”的意思。

这两个词在顺反异构中比较好理解,在分子生物中的用法与早期研究有关。

在早期的分子遗传学研究中,经常要判断对某基因的调控作用是来自DNA分子本身,还是来自另一个分子。

前者称为顺式作用,比如增强子对启动子的作用;后者称为反式作用,比如某个蛋白因子对启动子的作用。

在顺反子的定义中也是同样的含义。

原核生物有两类终止子:依赖ρ因子的终止子和不依赖ρ因子的终止子。

ρ因子(Rho)是一种高度保守的终止因子,存在于几乎所有的原核生物。

除了终止转录以外,Rho还有抑制反义转录,影响tRNA和小调节RNA的合成,沉默外源DNA等多种功能。

两类终止子都有一段回文结构。

简单终止子有两个对称的富含GC的片段,下游还有一段富含A的序列。

而依赖ρ因子的终止子不需要GC序列和寡聚A序列。

简单终止子转录出RNA后,两段富含GC的片段会形成茎环结构,破坏了RNA和模板DNA的杂合双链结构。

此时下游恰好是结合力较弱的AU对,进一步造成了转录延伸复合物的不稳定,导致聚合酶解离和转录终止。

转录的内部终止模型。

Biomolecules. 2015 Jun; 5(2): 1063–1078.这种终止也称为内部终止(intrinsic termination)。

大肠杆菌中的大多数基因采用内部终止,Rho依赖的终止大约占20-30%。

大肠杆菌的Rho因子是环状六聚体,每个亚基47KD。

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a r X i v:q-bi o/5723v1[q-b io.N C]14J ul25Synchronization and spindle oscillation in noisy integrate-and-fire-or-burst neurons with inhibitory coupling Hidetsugu Sakaguchi and Shoko Tobiishi,Department of Applied Science for Electronics and Materials,Interdisciplinary of Engineering Sciences,Kyushu University,Kasuga Fukuoka 816-8580,Japan February 9,2008We propose another integrate-and-fire model as a single neuron model.We study a globally coupled noisy integrate-and-fire model with inhibitory interac-tion using the Fokker-Planck equation and the Langevin equation,and find a reentrant transition of oscillatory states.Intermittent time evolutions of neuron firing are found in strongly inhibited systems.We propose another integrate-and-fire-or-burst model including the dynamics of the low-threshold Ca 2+current based on the new integrate-and-fire model.We study a globally coupled noisy integrate-and-fire-or-burst model with inhibitory interaction us-ing the Fokker-Planck equation,and find bistability of the tonic mode and burst mode.Doubly periodic oscillation appears in a coupled system of two neuron assemblies,which is similar to the spindle oscillation in thalamic cells.1Introduction The limit cycle oscillation and the synchronization are found in various natural phenomema such as the firing of fireflies and the stick-slip motion of a fault in the earthquake.Coherent oscillation appears as the global synchronization of the coupled oscillators.The synchronization of oscillators is also considered to playimportant roles in neural information processing [1].Winfree and Kuramoto studied the global synchronization in general coupled oscillators including the phase oscillators [2,3].The leaky-integrate-and-fire model (IF model)is one of the simplest models for a single neuron and often used to study dynamical behaviors of neural networks.Each neuron receives an input via synaptic con-nections from other neurons.The neuron fires,when the membrane potential goes over a threshold,and sends out an impulse as an output to other neurons.Mirollo and Strogatz studied a globally coupled system of integrate-and-fire neu-rons,and showed that perfect synchronization occurs in a finite time [4].Mutual1synchronization is often observed among a large number of neurons with exci-tatory interaction.Inhibitory neurons can exhibit synchronization under some appropriate conditions[5,6,7].However,the synchronization among inhibitory neurons is not so robust against some noises or heterogeneities,as was studied in several models in Refs.[8]and[9].On the other hand,the synchronization among thalamic neurons is known to be rather robust experimentally,although the synaptic coupling is inhibitory.The synchronousfiring among the thalamic neurons generates characteristic brain waves called spindle waves in an early stage of sleep[10].The reason of the robust synchronization among inhibitory neurons is not well understood.In this paper,we will study the synchronization among noisy inhibitory neurons,using a new type of IF model.A single neuron may be affected by environmental noises,then,the model equation is generalized to a Langevin type equation such as a noisy integrate-and-fire model.In the noisy system,the coherent oscillation appears as an ana-logue of the phase transition in the statistical mechanics.Nykamp-Tranchina and Brunel-Hakim showed that a population density approach using the Fokker-Planck equation is a useful method to study a large neural network of noisy integrate-and-fire neurons[11,12,13].We studied a nonlocally coupled noisy integrate-and-fire model and found a traveling pulse state using the Fokker-Planck equation corresponding to the Langevin equation[14].The phase tran-sition in a large population of noisy elements can be studied with the Fokker-Planck equation in a clear manner,since the Fokker-Planck equation is a deter-ministic equation.In this paper,we apply the method to a large population of noisy integrate-and-fire neurons to clarify several phase transitions in some mod-els of neural networks,although related subjects have been intensively studied with different methods and models[15,16,17].The sleep spindle oscillations are a kind of brain waves,which appear in an early stage of sleep.The oscillations have a characteristic waveform of waxing-and-waning.It is known that these oscillations are generated by the interaction between thalamic reticular(RE)and thalamocortical(TC)cells[10,18,19]. The interactions from RE cells to TC cells are inhibitory and the interactions from TC cells to RE cells are excitatory,the mutual interaction among RE cells is inhibitory,and there is no mutual interaction among TC cells.The low-threshold Ca2+current plays an important role for the excitation of the thalamic cells.The integrate-and-fire-or-burst model(IFB model)is a generalized model of the IF model,which takes the dynamics of the low-threshold Ca2+current into consideration[18].The dynamics of the IFB model under external stimuli was studied in Ref.[19].We will propose a new type of IFB model including the dynamics for the low-threshold Ca2+current based on the new IF model. We will study a globally coupled noisy IFB model with inhibitory interaction as a neural network model of the RE cells,andfinally study a coupled systems of two types of IFB neuron assemblies as a coupled model of the RE cells and TC cells.We will investigate the coupled noisy integrate-and-fire models stepwise.In §2,we propose a new type of integrate-and-fire(IF)model with inhibitory cou-pling and show the synchronization between two neurons.In§3,we investigate2a globally coupled noisy integrate-and-fire model using the Fokker-Planck equa-tion.In§4,we propose a new type of integrate-and-fire-or-burst(IFB)model by combining the new type of integrate-and-fire model with the dynamics of the low-threshold Ca2+current,and investigate the global oscillation in the globally coupled noisy IFB model.In§5,we investigate a coupled system of two neuron assemblies and show doubly periodic oscillation.2Synchronization of two integrate-and-fire neu-rons with inhibitory couplingIn the usual integrate-and-fire model,the membrane potential v is reset to a cer-tain value V R∼−50mV,just after the membrane potential reaches a threshold value,which is assumed to be about−35∼−45mV.In more realistic models, the neuron is excited after the membrane potential goes over the threshold,the membrane potential takes positive values for a while,and then the membrane potential returns to a negative value around the resting potential.Taking the dynamics in the excited state into consideration,we propose another type of simple integrate-and-fire model.Our new IF model keeps the most favorable point of the IF model that thefiring of a neuron can be described using only one variable,in contrast to the Hodgkin-Huxley model including four variables[20] or the FitzHugh-Nagumo model including two variables[21].We study the synchronization of two neurons with inhibitory coupling,using the new IF model.The model equation is written asdv iC=−α(v i−V′0)+I s,for v i>V T,(1) dtwhere v i denotes the membrane potential for the i th cell,V0=−65denotes the resting potential,V′0is another parameter which controls the dynamics in the excited state v i>V T and isfixed to be V′0=35in this paper,I0is a constant external stimulus current,I s is a synaptic current,and C=2and α=0.035are constants.The units of v and t are mV and ms.When the membrane potential exceeds the threshold V T=−35,the cell is excited.In the usual integrate-and-fire model,v i is reset to a potential V R=−50just after thefiring.However,in our generalized model,the membrane potential jumps to a potential V1>0(V1=60is assumed in this paper.)and then it tends to decay toward V′0if I s=0,obeying the second equation of Eq.(1).When the membrane potential reaches a second threshold V2,v i is reset to V R.The two kinds of time evolutions correspond to the slow dynamics on the two branches of nullclines in the excitable equations such as FitzHugh-Nagumo model[21] and the McKean model[22].There are several model equations which describe the dynamics of the synap-tic current I s(t)[23].In this paper,we use a simple model including a response3Figure1:(a)Two time evolutions by Eq.(1)starting from v1=−50(solid line),v2=50(dashed line)and I s=−0.9973for I0=1.5,K=−0.5,V2=40 andτ=10.(b)Stability exponent r as a function ofτfor K=0.1,−0.1and −0.5at I0=1.5andτ=10.(c)Two time evolutions by Eq.(1)starting from v1=−48(solid line)and v2=59.9(dashed line)and I s=−0.9973for I0=1.5,K=−0.5,V2=58andτ=10.(d)Stability exponent r as a function of V2for K=0.1,−0.1and−0.5at I0=1.5andτ=10.time.The synaptic current for a coupled system of two neurons is assumed to obeydI sτthat the mutual synchronization is attained.The solution of the synchronized oscillation can be explicitly solved,because the model equation is a piecewise linear equation.The stability of the synchronized motion can be studied by the linearized equation of Eqs.(1)and(2).The deviationδv=v1−v2obeys a simple equation:Cdδv/dt=−αδv.The deviationδv changes discontinuously at the moment t1of thefirst threshold satisfying v1(t1)=V T,asδv(t1+)=(dv/dt)v1=V1/(dv/dt)v1=V Tδv(t1−),and at the moment t2of the second thresh-old satisfying v1(t2)=V2,asδv(t2+)=(dv/dt)v1=V R /(dv/dt)v1=V2δv(t2−).Therefore,the deviationδv(t)growsδv(t+T)=rδv(t)after a period T of the synchronized motion,where the stability exponent r is expressed asr=(dv/dt)v1=V1(dv/dt)v1=V2e−α/C·T.(3)Figure1(b)displays the stability exponent r as a function ofτfor I0=1.5,K=−0.5andτ=10.If the stability exponent r is smaller than1,the synchronized motion is stable.As K<0and|K|is larger,the synchronized motion becomes more stable.There is an optimum response timeτwhere r takes a minimum value,although the synchronized motion is stable even for very smallτfor K<0.In the case of excitatory coupling K>0,r is larger than1and the synchronized motion is unstable.That is,the mutual synchronization is attained in the case of inhibitory coupling and the synchronized motion becomes more stable,as the inhibitory coupling is stronger.If the second threshold V2approaches V1,the duration time of the excita-tion becomes smaller,and in the limit of V2=V1,the duration time of the excitation becomes0and our model approaches the original integrate-and-fire model.Figure1(c)displays the mutual synchronization of two neurons start-ing from v1=−48(solid line)and v2=59.9(dashed line)and I s=−0.9973 at I0=1.5,K=−0.5,V2=58andτ=10.The duration time of the ex-cited state is much shorter than the case of Fig.1(a)owing to the smallness of|V1−V2|,however,the mutual synchronization is still attained.Figure1(d) displays the stability exponent r of the synchronized state as a function of V2 for K=−0.5,−0.1and0.1at I0=1.5andτ=10.As V2approaches V1=60, the stability exponent approaches1,because the duration time of the excited state becomes shorter,and then the synaptic interaction becomes weaker ef-fectively.In the following numerical simulations,we use the parameter value of V2=40(except in Fig.4(b)),because mutual synchronization occurs fairly strongly,although the duration time of the excitation might be too long as a typical neuron.3Global synchronization in a large population of noisy integrate-and-fire neuronsNext,we consider a large population of integrate-and-fire neurons with in-hibitory coupling.The total number of the neurons is assumed to be N.The5elemental dynamics for each neuron obeys Eq.(1).The synaptic current is expressed asτdI sdt=−α(v i−V0)+I0+I s+Cξi(t),for v i<V T,Cdv idt =−{I s−K∂t =−∂∂x2+δ(x−V1)J1(t)+δ(x−V R)J2(t),τdI sxFigure3:(a)Oscillation amplitude as a function of|K|for I0=2.5,D=0.2 andτ=20.(b)Parameter region where the global synchronization appears in the parameter space of(τ,|K|)for I0=2.5and D=0.2.The coupling constant K is negative,and the same parameter values I0and D are used for(a)and(b)thefiring of all neurons.Neurons whichfire earlier,inhibit thefiring of the other neurons.Which neuronfires is not determined but change randomly in our noisy system,in contrast to a clustered state found in some deterministic systems[25]. That is,the global oscillation appears,but the globally synchronousfiring does not occur in the region of large K.We have shown numerical results for the Fokker-Planck equation.The Fokker-Planck equation is favorable to investigate the global oscillation clearly, since the equation is deterministic.However,the time evolution of individual neuron cannot be seen.The direct Langevin simulation can show the time evo-lutions of each neuron.The difference of the two types of global oscillation can be clearly seen in the Langevin simulation of Eq.(4).We have performed a direct Langevin simulation for N=2000neurons,and got time evolutions of membrane potentials v i’s for all neurons and the average value of the membrane potentials.We have performed some numerical simulations by changing parame-ter values of D,V2and K.Figures4(a),(b)and(c)display the time evolutions of v i=1(t)of thefirst neuron(solid line)and the average v = N j=1v j/N (dashed line)for I0=2.5,τ=20and N=2000.Figure4(a)displays the time evolutions at K=−2,D=0.2and V2=40,which corresponds to the solid linein Fig.2(a).Thefiring of each neuron is almost synchronized to the average activity v .The timing of thefiring is slightly different for each neuron owing to the external noise,that is,the phase of the oscillator is randomized by the external noise.The average value v exhibits limit cycle oscillation,which is al-most equal to E(t)in Fig.2(a).The global synchronization may be interpreted by the concept of the phase synchronization as studied in Ref.[3].Figure4(b) displays the time evolution at K=−2,D=0.02and V2=58.At V2=58,the duration time of the excited state is much shorter,and the effective interaction becomes weak as shown in Fig.1(c)and(d),but almost synchronizedfiring is seen for the smaller noise strength D=0.02.For the same parameter values8Figure4:Time evolutions of v i(solid line)and the average v (dashed line) in the Langevin simulation of Eq.(4)for a globally coupled noisy IF model at(a)K=−2,D=0.2,V2=40,(b)K=−2,D=0.02,V2=58and(c) K=−10,D=0.2,V2=40for I0=2.5,τ=20and N=2000.(d)Raster plot at I0=2.5,K=−10,D=0.2,V2=40,τ=20and N=2000which corresponds to(c),in which a dot is plotted at time t=n(n is an integer)and the position i satisfying v i(t=n)>0for1≤i≤100.K=−2and D=0.2as Fig.4(a),the global synchronization was not observed at V2=58,because the timing of thefiring is randomly distributed.Inhibitory neurons can exhibit the global synchronization even if the duration time of the excited state is short,but the stability becomes weaker.Figure4(c)displays the time evolutions at K=−10,D=0.2and V2=40,which corresponds to the dashed line in Fig.2(a).The average value v exhibits limit cycle oscillation, which is close to E(t)in Fig.2(a).The activity v i(t)of each neuron shows that thefiring occurs intermittently at some peaks of v .A fraction of neuronsfire near the peak of v ,and the other neurons are inhibited tofire by the strong global inhibition by thefired neurons.Which neurons are selected forfiring is not determined but changes randomly.As a result,the intermittent time evo-lution appears as shown in Fig.4(c).The random but somewhat synchronized firing is seen in the raster plot of Fig.4(d)at the same parameter values as in Fig.4(c),wherefiring sequences of neurons for1≤i≤100are denoted by dot patterns.Intermittentfiring was found also in a numerical simulation by Wang et al.[16],but their model is deterministic and the coupling strengths among neurons are randomly distributed.Similar intermittent behaviors are observed also experimentally[26].94Bistability in a large population of the integrate-and-fire-or-burst neuronsThe integrate-and-fire model is a simpler model than realistic model equations such as the Hodgkin-Huxley equation[20],in that the detailed dynamics of ion channels are neglected.Specific ion channels play an important role in thefir-ing process of specific neurons.The low-threshold Ca2+current is important for thalamic neurons.The integrate-and-fire-or-burst model was proposed asa simple model to describe the dynamics of the membrane potential of thala-mic cells[18].It is a coupled equation of the integrate-and-fire model and the dynamics of the low-threshold Ca2+current I T(t).The current I T(t)is given by I T(t)=g T h(t)(V H−v(t))θ(v(t)−V h),where the parameters are given asg T=0.07,V H=120and V h=−60,and h(t)is a slow variable determined by the membrane potential v.In the integrate-and-fire-or-burst model,the slow variable h(t)(0≤h≤1)is assumed to obeyτh(v)dhdt=−α(v i−V0)+I0+I s+I T i+Cξi(t),for v i<V T,Cdv idt=−h i+θ(V h−v i(t)),I T i(t)=g T h i(t)(V H−v i(t))θ(v i(t)−V h),τdI sNNj=1θ(v j)}.(6)The slow variable h i(t)is another stochastic variable,because v i(t)is a stochastic variable.Therefore,the corresponding Fokker-Planck equation takes a form of a two-dimensional partial differential equation:∂P∂x {f(x,I0,I s+I T)}P(x)−∂∂x2+δ(x−V1)J1(t,y)+δ(x−V R)J2(t,y),τdI swhere P(x,y,t)is the probability density that the membrane potential v takes a value x and the slow variable h takes a value y,f(x,I0,I s+I T)denotes the deterministic part of the elemental dynamics of the membrane potential, I T(x,y)=g T y(V H−x)θ(x−V h),and J1(t,y)=−D(∂P/∂x)x=VTand J2(t,y)=−D(∂P/∂x)x=V2.Since h(t)does not receive a random force,there is no diffu-sion term with respect to y in Eq.(7).The deterministic forces to the membrane potential v(t)and the variable h(t)appear in thefirst two drift terms on the right-hand side of Eq.(7).We have performed numerical simulations of the two-dimensional partial differential equation(7)using the Euler method with ∆x=0.1,∆t=0.005and∆y=0.05.Figure5:(a)Two time evolutions of the average membrane potential E(t)by Eq.(7)for I0=1.6,K=−40,D=0.2andτ=20.The initial conditions for the two time evolutions are different.(b)The range of the temporal variation of the average value: h as a function of I0for K=−40,D=0.2andτ=20. The solid line denotes the burst mode and the dashed line denotes the tonic mode.(c)Oscillation amplitude of E(t)as a function of I0for the burst mode at K=−40and D=0.2.(d)Oscillation amplitude of E(t)as a function of I0 for the tonic mode at K=−40and D=0.2.Figure5(a)displays two time evolutions of E(t)= ∞−∞ 10P(x,y)xdxdy for I0=1.6,K=−40,D=0.2andτ=20.The initial conditions are different for the two time evolutions.That is,the two kinds of stable oscillatory states have appeared for the same parameters.It implies the bistability.The average membrane potential is always larger than V h in the dashed line,so h(t)is almost110.The low-threshold Ca2+current does not play a role,and the frequency of the oscillation is relatively high.This is called the tonic mode.On the other hand,the average membrane potential E(t)oscillates around V h=−60in the solid line.The low-threshold Ca2+current plays an important role in this mode.The low-threshold current I T depolarizes the IFB neuron and thefiring is facilitated.If many neurons arefired,the strong inhibitory coupling hyperpolarizes each neuron and the membrane potential goes down below V h,and then is rebound togo over the threshold V h again.The low-threshold Ca2+current facilitates the oscillation of thefiring,and therefore the amplitude of oscillation is relatively large and the frequency of oscillation is relatively low in this mode.This mode iscalled the burst mode or the rebound mode.The tonic mode and the burst mode are bistable at the parameters in Fig.5(a)in our model.Figure5(b)displays the range of the temporal oscillation of the average h(t) = ∞−∞ 10P(x,y,t)ydxdy as a function of I0for K=−40,D=0.2andτ=20.Thefinite width of the temporal variation of h(t) at a certain I0implies the limit cycle oscillation of h(t) .The upper branch represents the burst mode and the lower branch( h =0)represents the tonic mode.(We have distinguished the two modes in this paper from a viewpoint that the low-threshold Ca2+current plays an important role or not,that is,the average value of h(t)isfinite or almost zero.) The bistability occurs for0.55≤I0≤2.3.Figure5(c)displays the peak-peak amplitude∆E of the burst oscillation as a function of I0.The supercritical Hopf bifurcation is seen at I0∼−0.15.Near the threshold,the oscillation is sinusoidal,but a period doubling bifurcation occurs for the burst mode for I0>0.7.The burst-mode oscillation shown by the solid line in Fig.5(a)displays the time evolution of E(t)after the period doubling bifurcation.In the tonic mode,the Hopf bifurcation occurs near I0=0.95,as shown in Fig.5(d).Figure 5(c)and(d)show that the oscillation amplitude in the burst mode is relatively large compared to the tonic mode.5Spindle oscillation in a coupled system of two neuron assembliesWe investigate a coupled system of two neuron assemblies in this section,as a model of the thalamic neural network.There are two kinds of neurons:thalamic reticular(RE)cells and thalamocortical(TC)cells in the thalamus.The low threshold Ca2+current plays an important role in both types of thalamic cells. The interaction among RE cells is inhibitory.In the previous section,we have investigated the dynamical behaviors of a globally coupled system of one kind of inhibitory IFB neurons,which corresponds to an assembly of RE cells alone.It is known that the interaction between the RE cells and the TC cells is important for generation of spindle waves,which are characteristic brain waves in the second stage of sleep.We will study a coupled system of two neuron assemblies corresponding to RE cells and TC cells.It is known that the interaction from the RE cells to the TC cells is inhibitory and the interaction from the TC cells12to the RE cells is excitatory,and there is no mutual interaction among the TC cells.We investigate a Fokker-Planck equation for the coupled system of two neuron assemblies composed of noisy IFB neurons.The Fokker-Planck equation for the coupled neuron assemblies is expressed as∂P1∂x {f(x,I01,I s1+I s2+I T)P1}−∂∂x2+δ(x−V1)J11(t,y)+δ(x−V R)J12(t,y),∂P2∂x {f(x,I02,I s3+I T)P2}−∂∂x2+δ(x−V1)J21(t,y)+δ(x−V R)J22(t,y),τ1dI s1dt=−(I s2−K2 ∞0 10P2(x)dxdy),τ3dI s3Figure6:Time evolutions of the average membrane potential E1(t)of the RE neurons in Eq.(8)at(a)I01=I02=2.2and(b)I01=−0.25,I02=1,and the corresponding average membrane potential E2(t)of the TC neurons at(c)I01= I02=2.2and(d)I01=−0.25,I02=1.oscillatory motion is caused by the mutual interaction between the RE and TC neurons.The fast oscillation appears owing to the synchronization among the RE neurons,which was shown in the previous section.The two kinds of os-cillations are overlapped and the doubly-periodic motion appears in the time evolution of E1(t).The mechanism of the doubly periodic motion is as follows. The fast oscillation of the RE neurons repeats for a while.The TC neurons are inhibited strongly below the V h2by the repetition of the fast oscillations of the RE neurons.Thefiring of the RE neurons becomes weak,as the input from the TC neurons becomes small.The TC neurons are rebound after the strong inhibition,and the membrane potential of the TC neurons goes over V h2.The low threshold Ca2+currentflows into the TC neurons and the TC neuronsfire. Then,the RE neurons are excited by thefiring of the TC neurons.The long period is determined by the slow rebound time.The waxing-and-waning motion of the fast oscillation is seen clearly in Fig.6(b).The fast oscillations repeat several times and then disappear.In the repetition of the fast oscillations,the period increases gradually,the amplitude of the fast oscillation is decreasing. This type of motion is characteristic of the spindle oscillation in the thalamic networks[27].In our model,the doubly periodic oscillation is caused by the interaction14between the RE neurons and TC neurons,but there are other neuron modelswhere the slow oscillation is caused by slow dynamics of some ion channels[28,29].In their models,the doubly periodic behavior can be generated even in one neuron.Figure7:Time evolutions of v i(solid line)and the average v (dashed line)in the Langevin simulation corresponding to Eq.(8)withτ1=5,τ2=τ3=100,K1=K3=−30,K2=30,D=0.2,I01=−0.25,I02=1,and N=1000.The spindle oscillation is also seen in the corresponding Langevin simulation.Figure7displays the time evolutions of the membrane potential v1of thefirstRE neuron and the average value v for the RE neurons atτ1=5,τ2=τ3=100,K1=K3=−30,K2=30,D=0.2,I01=−0.25,I02=1and N=1000,which corresponds to Fig.6(b).The time evolution of the average value v exhibits the doubly periodic oscillation similar to Fig.6(b).Thefiring of each neuron is well synchronized to the averaged membrane potential,but thefiringis sometimes skipped and the intermittentfiring is seen.The intermittentfiringmight be characteristic of strongly inhibited systems.Similar intermittentfiringof the RE neurons is observed experimentally[27].The bistability is also observed in this coupled system.Figure8(a)displays the maximum value in the time evolution of the average h1(t) = ∞−∞ 10P1(x,y,t)ydxdy as a function of I0=I01=I02.The upper branch represents the burst modeand the lower branch represents the tonic mode for the RE neurons.The bista-bility occurs in0.3≤I0≤1.4.Figure8(b)displays the maximum value in the time evolution of the average h1(t) = ∞−∞ 10P1(x,y,t)ydxdy as a function ofI01for afixed value of I02=1.The bistability is observed in0.5≤I01≤1.8, although the classification to the two burst and tonic modes seems to be difficultin this case.The thalamus is considered to be a relay point between the sensory organs and the cerebrum.The bistability of the activity of the coupled systemof the RE cells and TC cells might be related to some switching function of the information transmission at the relay point.15Figure8:Maximum value of the average h1(t) = ∞−∞ 10P1(x,y,t)ydxdy as a function of(a)I0=I01=I02,and(b)as a function of I01at I02=1.Both figures display the existence of the bistability and the hysteresis.6SummaryWe have proposed another IF model including the dynamics in the excited state. We have studied the stability of the synchronized motion of a coupled system of two neurons and N neurons.In our model,the synchronization is rather robust even in the case of inhibitory coupling.We have investigated global synchronization of noisy IF neurons with in-hibitory coupling using the Fokker-Planck equation,and found the reentrant Hopf bifurcation.In the parameter region of weak coupling,almost all neurons fire synchronously,but in the parameter region of strong coupling,only a frac-tion of neuronsfires synchronously owing to the strong inhibition.Intermittent firing is seen in each neuron as is clearly shown by the Langevin simulation.We have proposed another IFB model including the dynamics of the low-threshold Ca2+current based on the new IF model.We have performed direct numer-ical simulations of the Fokker-Planck equation for the globally coupled IFB model,and found the bistability of the tonic model and the burst mode.In the burst mode,the low-threshold Ca2+current facilitates the global oscillation. We have further performed numerical simulations of the Fokker-Planck equa-tion for the coupled system of the RE neurons and TC neurons,and found a doubly-periodic motion similar to the spindle oscillation observed in the second stage of the sleep.The doubly-periodic motions are also bistable in a certain parameter range of the inputs,which might be related to a switching function of information transmission at the relay point.We have found various bifurcations including the Hopf bifurcation,period doubling bifurcation and jump phenomena between bistable states in globally coupled noisy IF and IFB models.Our model includes many control parameters.Our choice of the parameters may not be physiologically suitable.In future work,we will adjust the parameter values and perform numerical simulations more relevant to realistic neurons.16。

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