Infrared emission from radio-loud active nuclei

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施勇 教育经历:!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!

施勇 教育经历:!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!

施勇1980年11月出生。

南京大学 天文与空间科学学院email: yong@教育经历: 1999.9-­‐2003.7 北京大学,地球物理系,天文专业,学士学位。

2003.8-­‐2008.8 亚利桑那大学(美国),天文学,博士学位。

工作经历: 2008.8-­‐2009.8: 亚利桑那大学(美国),博士后。

2009.9-­‐2013.2: 加州理工学院(美国),博士后。

2013.3至今: 南京大学,教授,博导,国家青年千人。

科研基金项目:国家自然科学基金面上项目,11373021,极端贫金属星系:尘埃特性和恒星形成,2014/01-2017/12,80 万元,在研,主持。

中国科学院战略性先导B专项,XDB09000000, 宇宙结构起源B类先导,2014/01-至今,66万,在研,参与(骨干成员)。

中央组织部青年千人项目(第四批),2013.1-2015.12, 200万,在研、主持。

江苏省基金杰出青年项目,BK20150014, 2015.7-2018.7, 100万,在研、主持。

空间望远镜项目: • P I o n H erschel O T2 y shi 3 (16.1 h rs, p riority 1):“Extremely-­‐metal p oor g alaxies: m apping d ust e mission”• T echnical C ontact a nd C o-­‐I o n S pitzer-­‐50507, 50508 (14.2 h rs, P I: G. R ieke)“Quasar a nd U LIRG E volution”• T echnical C ontact∗ a nd C o-­‐I o n S pitzer-­‐50196 (25.1 h rs, P I: G. R ieke.):“Cosmic Evolution of Star Formation in Quasar Hosts from z=1 to the Present”• T echnical C ontact∗ a nd C o-­‐I o n S pitzer-­‐40385 (2.1 h rs, P I: G. R ieke.):“A C hallenge t o t he U nification M odel”地面望远镜项目:• K eck 10 m: D EIMOS• I RAM 30 m: 24 h rs (2014A), 59.5 h rs (2016A).• P alomar 200 i nch: D BSP; L FC; W IRC• C FHT: M egaCAM• B ok 2.3 m• A rizona R adio O bservatory N RAO-­‐12m• A rizona R adio O bservatory S MT-­‐10m学术服务:ApJ, A pJL, A&A, A J, S ciChina, R AA的审稿人Telescope A ccess P rogram 望远镜分配委员会委员论文发表情况汇总(共36篇)通讯作者 非通讯作者 总计Nature 1 0 1Nature子刊 0 1 117 18 35ApJ, ApJS, ApJL,MNRAS, A&A(全部为NatureIndex高影响力科学期刊)AJ 0 1 1总计 18 20 38第一或通讯作者论文: 18. Zhang, Z.; Shi, Y* et al. 2016, ApJL, 819, 27“Distributions of quasar hosts on the galaxy main-sequence plane”17. Zhou, L.; Shi, Y* et al. 2016, MNRAS, 458, 772“Spatially resolved dust emission of extremely metal poor galaxies”16. S hi, Y.*, W ang, J., Z hang, Z.-­‐Y. e t a l. 2015, A pJL, 804, 11“The Weak Carbon Monoxide Emission in an Extremely Metal-­‐poor Galaxy, Sextans A”15. S hi, Y.*, A rmus, L., H elou, G. e t a l. 2014, N ature, 514, 335–338“Inefficient s tar f ormation i n e xtremely m etal p oor g alaxies”14. Shi, Y.*, Rieke, G., Ogle, P. et al., 2014, ApJS, 214, 23 “Infrared spectra and photometry o f c omplete s amples o f P G a nd 2MASS q uasars”13. Shi, Y.*, Helou, G., Armus, L. 2013, ApJ, 777, 6 “A Joint Model Of X-­‐ray And Infrared B ackgrounds. I I. C ompton-­‐Thick A GN A bundance”12. Shi, Y.*, Helou, G., et al. 2013, ApJ, 764, 28 “A Joint Model of the X-­‐Ray and Infrared E xtragalactic B ackgrounds. I. M odel C onstruc-­‐ t ion a nd F irst R esults”11. Shi, Y.*, Helou, G., et al. 2011, ApJ, 733, 87 “Extended Schmidt Law: Roles Of Existing S tars I n C urrent S tar F ormation”10. Shi, Y.*, Rieke, G. H., et al. 2010, ApJ, 714, 115 “Unobscured Type 2 Active Galactic N uclei”9. Shi, Y.*, Rieke, G. H., et al. 2009, ApJ, 703, 1107 “Cosmic Evolution of Star Formation i n T ype-­‐1 Q uasar H osts S ince z = 1”8. Shi, Y.*, Rieke, G. H., et al. 2009, ApJ, 697, 1764 “Role of Major Mergers In Cosmic S tar F ormation E volution”7. Shi, Y.*, Rieke, G. H. et al. 2008, ApJ, 688, 794 “BH Accretion in Low-­‐Mass Galaxies S ince z∼1”6. Shi, Y.*, Ogle, P., Rieke, G. H. et al. 2007, ApJ, 669, 841 “Aromatic Features in AGN: S tar-­‐Forming I nfrared L uminosity F unction o f A GN H ost G alaxies”5. Shi, Y.*, Rieke, G. H., Hines, D. C. et al. 2007, ApJ, 655, 781 “Thermal and Nonthermal I nfrared E mission f rom M87”4. Shi, Y.*, Rieke, G. H., Hines, D. C. et al. 2006, ApJ, 653, 127 “9.7 um Silicate Features i n A ctive G alactic N uclei: N ew I nsights i nto U nification M odels”3. Shi, Y.*, Rieke, G. H., Papovich, C. et al. 2006, ApJ, 645, 199 “Morphology of Spitzer 24 u m D etected G alaxies i n t he U DF: T he L inks b etween S tar F or-­‐ m ation and G alaxy M orphology”2. Shi, Y.*, Rieke, G. H., Hines, D. C. et al. 2005, ApJ, 629, 88 “Far-­‐Infrared Observations o f R adio Q uasars a nd F R I I R adio G alaxies”1.Shi, Y., & Xu, R. X.* 2003, ApJ, 596, 75 “Can the Age Discrepancies of NeutronStars B e C ircumvented b y a n A ccretion-­‐assisted T orque?”其他作者论文:20. G uo R. e t a l. (Shi Y. 5th a uthor), 2016, A pJ a ccepted, a rXiv:1604.0712219. Chen, Y. et al. (Shi Y. 4th author), 2016, MNRAS accepted, “Boxy Hα EmissionProfiles i n S tar-­‐Forming G alaxies”18. Bian, W. H. et al. (Shi Y. 4th author), 2016, MNRAS, 456, 4081, “Spectral principal component analysis of mid-infrared spectra of a sample of PG QSOs”17. Wang, J. et al. (Shi Y. 4th author), 2016, MNRAS, 455, 3986, “Dense-gas properties in Arp 220 revealed by isotopologue lines”16. Wang, J. et al. (Shi Y. 7th author), 2014, Nature Communication, 5, 5449 “SiO and C H3OH m ega-­‐masers i n N GC 1068”15. Kirkpatrick, A. et al. (Shi Y. 10th author) , 2014, ApJ, 796, 135 “Early Science with the Large Millimeter Telescope: Exploring the Effect of AGN Activity on the Relationships b etween M olecular G as, D ust, a nd S tar F ormation”14. Wang, J. et al. et al. (Shi Y. 4th author) , 2014, ApJ, 796, 57 “Isotopologues o f Dense G as T racers i n N GC 1068”13. Jin, S. et al. (Shi Y. 4th author), 2014, ApJ, 787, 63 “Color-­‐Magnitude Distribution o f F ace-­‐on n earby G alaxies i n S loan D igital S ky S urvey D R7”12. D ale, D. e t a l. (Shi Y. 6th a uthor), 2014, A pJ, 784, 83 “A T wo-­‐parameter M odel for the Infrared/Submillimeter/Radio Spectral Energy Distributions of Galaxies and A ctive G alactic N uclei”11. Wang, J. et al. (Shi Y. 3rd author), 2013, ApJL, 778, 39 “A SiO 2-­‐1 Survey toward G as-­‐rich A ctive G alaxies”10. Magdis, G. E. et al. (Shi Y. 22th author), 2013, A&A, 558, 136 “Mid-­‐ to far infrared p roperties o f s tar-­‐forming g alaxies a nd a ctive g alactic n uclei”9. Kim, Ji Hoon, et al. (Shi Y. 16th author), 2012, ApJ, 760, 120 “The 3.3 m Polycyclic A romatic H ydrocarbon E mission a s a S tar F ormation R ate I ndicator”8. Wang, J., et al. (Shi Y. 3rd author) 2011, MNRAS, 416, 21 “CS (5-­‐4) survey towards n earby i nfrared b right g alaxies”7. T yler, K. D., R ieke, G. H. e t a l. (Shi Y. 9th a uthor) 2011, A pJ, 738, 56 “The N ature of S tar F ormation a t 24 m i n t he G roup E nvironment a t 0.3 < z < 0.55”6. Wu, Y., et al. (Shi Y. 2nd author) 2011, ApJ, 734, 40 “The Mid-­‐infrared Luminosity Function at z < 0.3 from 5MUSES: Understanding the Star Formation/Active G alactic N ucleus B alance f rom a S pectroscopic V iew”5. W u, Y., e t a l. (Shi Y. 5th a uthor) 2010, A pJ, 723, 895 “Infrared L uminosities a nd Aromatic F eatures i n t he 24um F lux L imited S ample o f 5MUSES”4. Mason, R. E., et al. (Shi Y. 3nd author) 2009, ApJ, 693, 136 “The Origin of the Silicate E mission F eatures i n t he S eyfert 2 G alaxy N GC 2110”3. B allantyne, D. R., e t a l. (Shi Y. 2nd a uthor) 2006, A pJ, 653, 1070 “Does t he A GN Unified M odel E volve w ith R edshift? U sing t he X-­‐Ray B ackground t o P re-­‐ d ict t he Mid-­‐Infrared E mission o f A GNs”2. J iang, L. e t a l. (Shi Y. 4th a uthor) 2006, A J, 132, 2127 “Probing t he E volution o f Infrared P roperties o f z ∼6 Q uasars: S pitzer O bservations”1. Wu, Y. et al. (Shi Y. 4th author) 2004, A&A, 426, 503 “A study of high velocity molecular o utflows w ith a n u p-­‐to-­‐date s ample”。

电气工程及其自动化专业毕业论文外文翻译

电气工程及其自动化专业毕业论文外文翻译

本科毕业设计(论文)中英文对照翻译院(系部)工程学院专业名称电气工程及其自动化年级班级 11级2班学生姓名蔡李良指导老师赵波Infrared Remote Control SystemAbstractRed outside data correspondence the technique be currently within the scope of world drive extensive usage of a kind of wireless conjunction technique, drive numerous hardware and software platform support。

Red outside the transceiver product have cost low,small scaled turn, the baud rate be quick,point to point SSL, be free from electromagnetism thousand Raos etc. characteristics,can realization information at dissimilarity of the product fast,convenience,safely exchange and transmission, at short distance wireless deliver aspect to own very obvious of advantage。

Along with red outside the data deliver a technique more and more mature, the cost descend, red outside the transceiver necessarily will get at the short distance communication realm more extensive of application.The purpose that design this s ystem is transmit customer’s operation information with infrared rays for transmit media, then demodulate original signal with receive circuit。

Hard X-ray and Infrared Emission from Apparently Single White Dwarfs

Hard X-ray and Infrared Emission from Apparently Single White Dwarfs
The hard X-ray emission from these three apparently single WDs is illustrated in Figure 1. The ROSAT Position Sensitive Proportional Counter (PSPC) images in the 0.6–2.4 keV energy band show clearly point sources coincident with the WDs, and the PSPC spectra show distinct emission near 1 keV.
1
2
Chu et al.
Figure 1. ROSAT PSPC observations of KPD 0005+5106, PG 1159, and WD 2226−210. The top two rows show soft (0.1–0.4band images. The poor point-spread-function in the soft band is caused by an electronic ghost image at energies below 0.2 keV. The bottom row shows the PSPC spectra. To show the hard counts of PG 1159, its spectrum above 0.6 keV is scaled up by a factor of 50 as marked and plotted in open symbols.
arXiv:astro-ph/0701025v1 1 Jan 2007
**FULL TITLE** ASP Conference Series, Vol. **VOLUME**, **YEAR OF PUBLICATION** **NAMES OF EDITORS**

and

and
Mon. Not. R. Astron. Soc. 000, 000{000 (1996)
Printed 11 November 1996
A (MN L TEX style le v1.4)
Is the rapid radio variability seen in PKS 0537-441 due to microlensing ?
Within our own galaxy, microlensing by individual halo stars can amplify the light from stars in the Galactic bulge and the LMC (Paczynski 1986b; Alcock et al. 1995). Due to the low optical depth of microlensing stars in the Galactic halo, such events are rare and tend to be very simple in form. At cosmological distances, however, the action of stars in an intervening galaxy can induce violent uctuations in the observed light curve of a high redshift quasar, resulting in complex variability (Wambsganss 1990). Such variability was rst observed in Q2237+0305, the Einstein Cross Lens (Irwin et al. 1989). Microlensing has also been cited as a source of the residuals seen between the light curves of the Double Quasar, Q0957+561 (Schild and Thomson 1994), and as a mechanism to explain all of quasar variability (Hawkins 1993; Hawkins 1996). Recently, Romero et al. (1995) have analyzed the radio variability seen in the BL Lac object PKS 0537-441. They concluded, from time-scale arguments, that the variability seen in this system is consistent with microlensing by stars in a foreground galaxy. This subject is the focus of this paper. The paper begins with a review of the theory of microlensing, followed by its applicability to BL Lac systems.

电器电子辞汇英语翻译

电器电子辞汇英语翻译

模拟数字转换器模数转换器 a d converter 缓冲存储器 abbreviated code快速呼唤 abbreviated dialing象差 aberration?异样辉光放电 abnormal glow discharge 异样反射 abnormal reflections磨耗 abrasion?磨粉 abrasive dust磨料喷射加工 abrasive jet machining? 磨料喷射蝶 abrasive jet trimming磨蚀剂 abrasive paste?研磨蝶 abrasive trimming磨料 abrasive?急剧退化 abrupt degradation突变异质结 abrupt heterojunction 突变结 abrupt junction绝对亮度阈absolute threshold of luminance吸收功率 absorbed power吸收剂 absorber?吸收能力 absorbing capacity?吸收电路 absorbing circuit吸收层 absorbing layer吸收媒质 absorbing medium?吸收跃迁 absorbing transition吸收带 absorption band吸收长度 absorption length吸收线 absorption line吸收损失 absorption loss?吸收测定 absorption measurement吸收灯 absorption modulation吸收点 absorption point吸收电阻 absorption resistance 吸收 absorption?对接 abutment joint?截割水晶片 ac cut quartz ac加速老化 accelerated aging?加速粒子 accelerated particle 加速实验 accelerated test?加速阳极 accelerating anode加速周期 accelerating cycle?加速电极 accelerating electrode 加速栅极 accelerating grid加速缝 accelerating slit加速管 accelerating tube?加速波 accelerating wave? 带电粒子加速acceleration of charged particles加速空间 acceleration space加速电压 acceleration voltage?加重 accentuation较佳对照度 acceptable contrast ratio受主 acceptor受汁子 acceptor atom受中心 acceptor center受周度 acceptor density受钟质 acceptor impurity受周级 acceptor level受滞半导体 acceptor type semiconductor存取码 access code访问方式 access method适应性第 accommodation第系数 accommodation coefficient? 积存层 accumulation layer再生精准度 accuracy in reproduction 精准定位 accurate positioning改良型专用射极耦合逻辑 ace消色差区 achromatc region消色差透镜 achromatic lens?消色差阈值 achromatic threshold针状结晶 acicular crystal酸侵蚀 acid etch橡实管 acorn tube吸声系数 acoustic absorptivity?滤声器 acoustic filter?声频 acoustic frequency? 声像 acoustic image声阻抗 acoustic impedance?声迷路 acoustic labyrinth声动录音机acoustic manipulated recorder声面波 acoustic surface waves声能转换器 acoustic transducer声学处置 acoustic treatment音波 acoustic wave表面声波振荡器 acoustic wave oscillator声延时线 acoustical delay line受钟质 acceptor impurity受周级 acceptor level受滞半导体 acceptor type semiconductor存取码 access code访问方式 access method适应性第 accommodation第系数 accommodation coefficient? 积存层 accumulation layer再生精准度 accuracy in reproduction 精准定位 accurate positioning改良型专用射极耦合逻辑 ace消色差区 achromatc region消色差透镜 achromatic lens?消色差阈值 achromatic threshold针状结晶 acicular crystal酸侵蚀 acid etch橡实管 acorn tube吸声系数 acoustic absorptivity?滤声器 acoustic filter?声频 acoustic frequency? 声像 acoustic image声阻抗 acoustic impedance?声迷路 acoustic labyrinth声动录音机acoustic manipulated recorder声面波 acoustic surface waves声能转换器 acoustic transducer声学处置 acoustic treatment音波 acoustic wave表面声波振荡器 acoustic wave oscillator声延时线 acoustical delay line酌半径 action radius?活化阴板 activated cathode活化分子 activated molecule?激活能 activation energy?激活 activation?有源区 active area有效分量 active component踊跃干扰 active counter measures 活性粉尘 active dust有源元件 active element有源元件组 active element group 活性纤维 active fiber有源滤波器 active filter织制导 active guidance织寻的制导 active homing guidance 有源激光元件 active laser element 激光皮捉质 active laser substance 活性液体 active liquid有源波模同步 active mode locking 有源寄生元件 active parasitics有源 q 开关 active q switching有源备份 active redundancy有源中继器 active repeater有源四端网络的反射损耗 active return loss有源卫星转发器active satellite repeater有源衬底 active substrate有源衬底蝶 active substrate trimming传动机构 actuator?锐度 acuity适应性均衡器 adaptability equalizer适应 adaptation?套筒式联轴器 adapter coupling转接器 adapter?自适应相关器 adaptive correlator自适应增量灯 adaptive delta modulation自适应接收机 adaptive receiver吸附原子 adatom爱德考克天线 adcock antenna爱德考克测向仪 adcock direction finder附加元件 add ons加色法混合 additive color mixture加色法合成 additive color synthesis加色法系统 additive color system基色的相加混合additive mixing of primaries加色法原色 additive primaires印刷电路的添加技术additive printed circuit technique加色法 additive process? 寻址系统 addressing system附着 adherence?粘着强度 adhesion strength?粘合剂 adhesive粘合剂涂敷 adhesive coating芯片粘附 adhesive die attachment胶粘密封 adhesive sealing粘合带 adhesive tape邻道伴音载波 adjacent audio carrier相邻信道 adjacent channel邻信道衰减 adjacent channel attenuation邻信道干扰adjacent channel interference邻频道抑制器 adjacent channel rejector相邻信道选择性adjacent channel selectivity相邻线路 adjacent lines邻信道图象载波 adjacent picture carrier相邻图象载波距离adjacent picture carrier spacing邻频道图象载波陷波器 adjacent picture carrier trap可单减器 adjustable attenuator可堤路 adjustable short可敌值金属氧化物半导体adjustable threshold mos蝶 adjustment?导纳矩阵 admittance matrix导纳 admittance?混合物 admixture?吸附质 adsorbate吸附剂 adsorbent?吸附层 adsorption layer? 吸附 adsorption?低劣半导体材料adulterated semiconductor material超前角 advance angle?改良型低功耗肖特基晶体管晶体管逻辑电路 advanced low power schottky ttl改良型自对准多晶硅栅工艺advanced polysilicon self aligned process改良型肖特基晶体管逻辑电路advanced schottky transistor logic改良型肖特基晶体管晶体管逻辑电路 advanced schottky ttl天线阵 aerial array天线衰减器 aerial attenuator天线电缆 aerial cable天线电容 aerial capacity天线扼力 aerial choke天线电路 aerial circuit天线藕合 aerial coupling天线藕合线圈 aerial coupling coil 天线电流 aerial current天线效率 aerial efficiency天线鼓励 aerial excitation天线馈电 aerial feed天线馈线 aerial feeder天线阻抗 aerial impedance天线电感 aerial inductance天线引入线 aerial lead in透镜天线 aerial lens天线损耗 aerial loss天线噪声 aerial noise天线功率 aerial power 天线辐射电阻aerial radiation resistance天线电抗 aerial reactance天线电阻 aerial resistance天线系统 aerial system天线接头 aerial terminal天线杆 aerial tower?天线党电容器 aerial tuning capacitor天线党线圈 aerial tuning coil天线 aerial?航空电子学的 aeroelectronic航空电子学 aeroelectronics?无线电报 aerogram导航电台 aeronautical station飞机天线 aeroplane antenna飞机反射的干扰信号 aeroplane flutter俄歇电子能谱学 aes音频 af?亲合力 affinity?后加速 after acceleration余晖 afterglow余像 afterimage后处置 aftertreatment?老化条件 ageing condition老化 ageing?集聚 aggregate?雪崩注入 ai雪崩注入二极管 aid半自动跟踪 aided tracking雪崩感生徙动 aim空气隔离型单片集成电路 aimic 空气轴承台 air bearing stage间隙 air clearance?空气冷却式激光器 air cooled laser空对地通信 air ground communication空气隔离 air isolation空气隔离型集成电路air isolation integrated circuit空气隔离型集成工艺air isolation process漏气 air leak?空气氧化物隔离 air oxide isolation空中位置指示器 air position indicator吹气清洗 air purge侦查海面舰艇的飞机监视雷达air to surface vessel radar风动传送设备 air track飞机无线电信标 airborne beacon空传污染 airborne contamination机载雷达 airborne radar机载电视接收机airborne television receiver拦截飞机雷达aircraft interception radar飞机电台 aircraft station机场信标 airport beacon机场危险信标 airport danger beacon机场交通操纵 airport traffic control气密接合 airtight joint报警信号 alarm signal?反射率测量 albedo measurement反照率 albedo?自动逻辑设计 ald 阿尔福德环形天线 alford loop antenna 铝栅 alg算法 algorithm?对准器 aligner对准精度 alignment accuracy对准误差 alignment error蝶用激光器 alignment laser对准标记 alignment mark定位锁 alignment pin?周密对准 alignment registration校准要求 alignment requirements定位 alignment?碱金属锑化物 alkali antimonide无碱环境 alkali free environment由碱可除光刻胶alkaline strippable resist全波段电视党器 all band tv tuner全扩散型集成电路all diffused integrated circuit交直两用接收机 all mains receiver全天候雷达 all weather radar分派器 allotter?允许能带 allowed band?允许能级 allowed level允许线 allowed line允许跃迁 allowed transition合金薄膜 alloy film合金结 alloy junction合金结晶体管 alloy junction transistor合金晶体管 alloy transistor合金 alloy? 合金接触 alloyed contact合金型二极管 alloyed diode合金区域 alloyed region接字母顺序的 alpha抗射线性 alpha immunity粒子轰击 alpha particle bombardment粒子爱惜 alpha particle protection粒子辐射灵敏度alpha radiation sensitivity粒子闪烁计数器alpha scintillation counter字符印字管 alphanumeric printing tube管 alphatron?更替路由 alternate route隔行扫描 alternate scanning交流 alternating current交菱量 alternating current measurement交羚阻 alternating current resistance超导交流 alternating supercurrent高度计 altimeter?高度指示器 altitude indicator?算术与逻辑部件 alu氧化铝陶瓷板划线alumina ceramic scribing氧化铝管壳 alumina package氧化铝 alumina?铝金属化 aluminizing铝硅酸盐玻璃 aluminosilicate glass铝线热压焊 aluminum bonding氧化铝陶瓷 aluminum oxide ceramics铝尖峰形成 aluminum spiking氧化物阶梯的铝覆盖aluminum step coverage铝线热压焊接 aluminum wire bond爹收音机 am receiver爹接收 am reception爹 am?爱好者 amateur业余波段 amateur band业余无线电台 amateur radio station 环境空气监测器 ambient air monitor 周围环境 ambient enviroment环境湿度 ambient humidity环境压力 ambient pressure?周围介质温度 ambient temperature 非单值性 ambiguity?双极性扩散 ambipolar diffusion?氨微波激射器氨脉泽 ammonia maser铵分子束频率标准ammonium molecular beam frequency standard无定形化 amorphization非晶态晶态转变amorphous crystalline transition对非晶半导体离子注入amorphous implantation非晶半导体 amorphous semiconductor非晶半导体掐amorphous semiconductor device非晶形状态 amorphous state?无定形结构 amorphous structure?信息量 amount of information?放大系数 amplification constant?放大谱线宽 amplification linewidth放大 amplification? 放大屁频带 amplifier band放大齐声 amplifier noise放大级 amplifier stage放大器 amplifier?放大速弟 amplifying klystron放大跃迁 amplifying transition放大管 amplifying tube特高频功率放大管 amplitron幅度校正 amplitude correction?鉴幅器 amplitude discriminator?振幅失真 amplitude distortion?振幅误差校正 amplitude error correction振幅偏移 amplitude excursion振幅频率失真amplitude frequency distortion振幅频率响应amplitude frequencyresponse?限幅歧路 amplitude limiter circuit限幅器 amplitude limiter?爹发射机amplitude modulated transmitter爹甚高频发射机 amplitude modulated vhf transmitter爹监视器 amplitude modulation monitor爹噪声 amplitude modulation noise爹抑制 amplitude modulation suppression爹器 amplitude modulator视频信号振幅 amplitude of videosignal视频信号振幅范围amplitude range of videosignal振幅特性曲线 amplitude response?振幅稳固激光器amplitude stabilized laser 酌距离 amplitude?模拟阵列 analog array模拟集成电路 analog chip模拟运算机 analog computer?模拟数字网络 analog digital network 模拟电子学 analog electronics模拟信息 analog information模拟微电子学 analog microelectronics 模拟灯 analog modulation模拟网络 analog network模拟移相器 analog phase shifter模拟记录 analog recording模拟信号 analog signal?模拟开关 analog switch模拟的 analogue模拟放大器 analogue amplifier模拟计算 analogue computation模拟式乘法运算器 analogue multiplier 分析器 analyzer?与电路 and circuit?与元件 and element或非门 and nor gate 与与操作 and operation与或电路 and or circuit无回声室 anechoic room磨角 angle lap角灯 angle modulation?射束偏转角 angle of beam deflection 发散角 angle of divergence仰角 angle of elevation? 槽倾斜角 angle of groove inclination入射角 angle of incidence?倾斜角 angle of inclination?光入射角 angle of light incidence辐射角 angle of radiation角度数字变换器 angle to digit converter角跟踪 angle tracking倾斜离子注入 angled ion implantation角散布 angular distribution?角分辨率 angular resolution?阴离子互换尸 anion resin阴离子 anion?蛤异性侵蚀 anisotropic etch蛤异性侵蚀断面图anisotropic etch profile蛤异性侵蚀性质anisotropic etchproperty蛤异性侵蚀剂 anisotropic etchant 蛤异性材料 anisotropic material? 蛤异性 anisotropy?退火炉 annealer?退火杂质活化 annealing activation 退火覆盖层 annealing cap热处置 annealing?广播员 announcer环形锯片 annular blade环形接触 annular contact环形锯片切割 annular cutting环状电阻器 annular resistor 环状旋转接头 annular rotary joint 环形锯 annular saw环状裂缝 annular slot阳极特性 anode characteristic阳极暗区 anode dark space阳极检波 anode detection屏极耗散 anode dissipation阳极效率 anode efficiency阳极电解侵蚀 anode etching屏极输出器 anode follower阳辉光 anode glow阳极栅极电容 anode grid capacity 屏极负载 anode load阳极中和 anode neutralization阳极氧化 anode oxidation阳极射线 anode rays屏极检波 anode rectification阳极电阻 anode resistance阳极溅射 anode sputtering?阳极寄生振荡抑制器 anode stopper 阳极电源 anode supply阳极端子 anode terminal阳极电压 anode voltage阳极 anode?阳极的 anodic阳极处置 anodization 异样晶体生长 anomalous crystal growth应答塞绳 answering cord应答装置 answering device应答塞 answering plug天线放大器 antenna amplifier天线电容器 antenna capacitor天线转换开关 antenna change over switch天线接线 antenna connection天线耦合电容器 antenna coupling condenser天线效应 antenna effect天线元件 antenna element天线电动势 antenna emf天线输入阻抗 antenna feed impedance天线场强增益 antenna field gain天线接地开关 antenna grounding switch平均地表面上天线高度 antenna height above average terrain天线引线 antenna lead天线插座 antenna socket天线仰角 antenna tilt防撞雷达 anti collision device消感网络 anti induction network抗氧化层 anti oxidation layer天线收发转换开关 anti transmit receive switch 对阴极 anticathode?预报信号 anticipating signal反符合电路 anticoincidence circuit 抗衰落犬线 antifading antenna抗衰落装置 antifading device反铁电体 antiferroelectric阻厄电路 antihunt circuit抗干扰接收机 antijam receiver抗干扰装置 antijamming unit锑 antimony?抗噪声 antinoise反雷达 antiradar反雷达导弹 antiradar missile反雷达学 antiradiolocation反卫星导弹 antisatellite missile防静电剂 antistatic agent防静电设备 antistatic aids防静电组装 antistatic assembly防静电袋 antistatic bag防静电手套 antistatic gloves防静电掩模底版 antistatic mask blank防静电台 antistatic station防静电表面处置 antistatic surface treatment防静电工具 antistatic tool反斯托克斯线 antistockes line收发开关盒 antitrans mit receive box常压化学汽相淀积 apcvd非党天线 aperiodic antenna非周期电路 aperiodic circuit 张角 aperture angle孔径失真补偿 aperture compensation 孔径耦合 aperture coupling孔径失真 aperture distortion孔径均衡 aperture equalization针孔透镜 aperture lens孔径损失 aperture loss多孔障板 aperture mask孔镜 aperture mirror孔径光阑 aperture stop口径 aperture?外观检查 appearance inspection?苹果彩色显象管 apple tube敷料器 applicator应用全息照相术 applied holography 进场信标 approach beacon进场治理 approach control进场指挥雷达 approach control radar 水清洗器 aqueous cleaner水处置 aqueous processing电弧阴极 arc cathode弧光灯鼓励 arc lamp pumping电弧等离子体 arc plasma弧 arc? 逆弧 arcback构造 architecture?电弧放电 arcing显光管 arcotron区域码 area code面积型成像机 area imager氩激光器 argon laser?氩 argon?运算装置 arithmetical unit?盗丹振荡器 armstrong oscillator 排列 arrangement?阵列 array阵列式芯片 array chip阵列集成电路 array device阵列布图 array layout阵列逻辑 array logic存贮企列 array memory阵列图象形成 array patterning阵列间距 array pitch阵列处置 array processing阵列结构 array structure输入电流 arrival current掺砷发射极 arsenic doped emitter掺砷外延层 arsenic doped epi砷搀杂 arsenic doping涂布的砷溶液 arsenic spin on solution 砷 arsenic? 砷化物 arsenide可听清楚度 articulation?假天线 artificial aerial人工老化 artificial ageing?仿真天线 artificial antenna黑电平测试信号 artificial black signal 仿真延迟线 artificial delay line假回波 artificial echo人造电子眼 artificial electronic eye 仿真全息图 artificial hologram仿置线 artificial line版图检查工具 artwork checking tool原图设计 artwork design图形发生 artwork generation 图形发生器 artwork generator 原图制备刀 artwork knife照相底图 artwork master原图 artwork?超声波水下探测器 asdic长宽比 aspect ratio?微观粗糙度 asperity汇编程序;装配器 assembler组装错误 assembly defect装配图 assembly drawing?装配设备 assembly equipment 装配夹具 assembly fixture? 装配室 assembly room 组装台 assembly station?组装成品率 assembly yield组装 assembly?分派频率 assigned frequency交莲磁 assistating current magnetic biasing相联存储器 associative memory非稳固电路 astable circuit非稳态多谐振荡器 astable multivibrator 像散现象 astigmatism天文电子学 astrionics天体电子学 astronics天体脉泽 astronomical maser天文航海 astronomical navigation非对称振幅灯 asymmetric amplitude modulation不对称边带传送 asymmetric sideband transmission不对称偏转 asymmetrical deflection异先操作 asynchronous operation异步应答方式 asynchronous response mode异步传输 asynchronous transmission切割晶体 at cut crystal at自动测试设备 ate大气模型 atmosphere model 大气 atmosphere?大气吸收带 atmospheric absorption band 大气吸收 atmospheric absorption?大气衰减 atmospheric attenuation大气波导 atmospheric duct大气电场 atmospheric electric field大气波导管 atmospheric guide大气压激光器 atmospheric pressure laser大气透射带 atmospheric transmission band大气透射系数 atmospheric transmittance 大气窗 atmospheric window?大气干扰 atmospherics原子吸收分光光度法 atomic absorption spectrophotometry原子束频率标准 atomic beam frequency standard原子束激光器 atomic beam laser原子钟 atomic clock?原子发射光谱仪 Atomic Emission Spectrometer AES原子频率标准 atomic frequency standard原子氢 atomic hydrogen原子型杂质 atomic impurity原子电离 atomic ionization原子激光器 atomic laser原子谱线宽度 atomic linewidth原子核 atomic nucleus?原子时标准 atomic time standard自动测试系统 ats可达清楚度 attainable resolution衰减常数 attenuation constant? 衰减器 attenuation pad?衰减 attenuation?听觉的 audio声频放大器 audio amplifier伴音载波 audio carrier伴音中心频率 audio center frequency伴音通道 audio channel声频放大 audio frequency amplification 音几回带 audio frequency band音频扼力 audio frequency choke音频发生器 audio frequency generator音几回率计 audio frequency meter音频峰值限幅器 audio frequency peak limiter音频变压器 audio frequency transformer音频电平指示器 audio level indicator音频混频器 audio mixer音频回音装置 audio output unit音频范围 audio range音频信号 audio signal音几回谱 audio spectrum音几回谱分析器 audio spectrum analyzer声道 audio track音频发射机 audio transmitter听力图 audiogram 听力计 audiometer测听技术 audiometry三极检波管 audion检查 audit?听能听能 audition俄歇电子发射 auger electron emission 俄歇电子 auger electron?俄歇微探针 auger microprobe俄歇复合 auger recombination俄歇能谱仪 auger spectrometer俄歇跃迁 auger transition无线电导航有声信标 aural radio range 收听 aural reception伴音发射机 aural transmitter南极光 aurora australis北极光 aurora borealis极光 aurora?故障 autage确认 authentication自动加速 autoacceleration自动补偿器 autocompensator自动操纵 autocontrol?自相关数 autocorrelation?自差接收法 autocyne reception 自搀杂 autodoping自差 autodyne 自拍接收机 autodyne receiver自动标引 autoindexing自动掩模对准器 automask aligner自动设计 automated design?自动应答装置 automatic answering device对照度与亮度自动平稳 automatic balance of contrast and brightness自动黑电平电路 automatic black level circuit自动黑电平操纵 automatic black level control自动查验 automatic check?自动色度蝶 automatic chrominancecontrol自动元件装卸装置 automatic componenthandler自动运算机 automatic computer对照度自动蝶 automatic contrast control自动操纵系统 automatic control system?自动消磁 automatic degaussing自动电话互换机 automatic exchange自动聚焦 automatic focusing自动频率操纵特性 automatic frequency control characteristic自动频率操纵 automatic frequency control?自动增益操纵 automatic gain control自偏压 automatic grid bias自动色地制 automatic hue control自动插入 automatic insertion自动布图技术 automatic layout technique 自动行同步 automatic line phasing直接远程拨号 automatic long distance service自动监视器 automatic monitor自动图象稳固操纵 automatic picture stabilization自动定线器 automatic router自动停机 automatic stop?自动副载波平稳操纵 automatic subcarrier balance control自动电报 automatic telegraphy自动电话互换局 automatic telephone exchange自动电话互换系统 automatic telephone switching system自动发射机 automatic transmitter自动党 automatic tuning自动真空淀积系统 automatic vacuum deposition system自动视频杂波限制器 automatic video noise limiter自动白电平操纵 automatic white control汽车收音机 automobile radio汽车电话 automobile telephone自对准 autoregistration辅助阳极 auxiliary anode辅助栅极 auxiliary grid辅助塞孔 auxiliary jack 辅助存储器 auxiliary memory辅助信号 auxiliary signal备份发射机 auxiliary transmitter可用功率 available power雪崩酌 avalanche action雪崩哗 avalanche breakdown雪崩哗电压 avalanche breakdown voltage雪崩二极管 avalanche diode雪崩注入多层栅金属氧化物半导体 avalanche injection stacked gate mos雪崩电离 avalanche ionization雪崩倍增 avalanche multiplication雪崩倍增系数 avalanche multiplication factor雪崩噪声 avalanche noise雪崩光电探测器 avalanche photodetector雪崩光电二极管 avalanche photodiode雪崩晶体管 avalanche transistor雪崩渡越时刻二极管 avalanche transit time diode雪崩渡越时刻二极管振荡器 avalanche transit time oscillator电子雪崩 avalanche?平均亮度 average brightness平均图象电平 average picture level求平均数 averaging?轴向电子感应加速岂荡 axial betatron oscilations轴向侵蚀不均匀性 axial etch nonuniformity轴向通量分米波超高功率四极管 axial flow resnatron轴向注入 axial injection 轴向引线成形设备 axial lead former 轴心线 axial lead?轴向稳固性 axial stability轴向鼓励激光器 axially excited laser 波导管轴 axis of a waveguide方位角精度 azimuth accuracy方位蝶 azimuth adjustment方位角驱动 azimuth drive方位角仰角指示器 azimuth elevation indicator方位角损失 azimuth loss方位角分辨率 azimuth resolution方位角;方位角 azimuth?方位角群聚 azimuthal bunchingDN A及蛋白质的测序和合成仪-- Sequencers and Synthesizers for DNA and Protein。

《万能遥控器英》课件

《万能遥控器英》课件
1 Macro Functionality
Create custom sequences of commands with one button press, allowing you to automate complex tasks.
2 Backlit Buttons
Control your devices in dim or dark environments with ease using remote control buttons that illuminate.
devices.
making them ideal
offer additional
for home theaters.
features and
customization
Benefits of Using a Universal Remote Control
1 Simplicity & Convenience
Challenges and Limitations of Using a Universal Remote Control
Understand the potential challenges and limitations of universal remote controls, including compatibility issues, complex setup processes, and limitations in controlling certain devices.
The History of Remote Control
Explore the fascinating origins of remote control technology, from early wired devices to the wireless infrared and radio-frequency remotes that we use today.

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。

声导抗基础知识

声导抗基础知识
• Stapedius muscle controlled by facial nerve (CN VII) 镫骨肌由第七对颅神经-面神经支配
• Network in brainstem consists of ipsilateral and contralateral paths 脑干层面由同侧和对侧神经通路组成
声导抗基础知识
Sound travel 声音传导
2020/11/30
2
Getting sound into a different medium 声音在不同媒介中的传导
Most of the sound energy is reflected when confronting a another medium... 大部分声能在临界面处被反射回来
…and less low frequency sound can get through the middle ear
因而进入中耳的低频声波减少
2020/11/30
19
The Middle ear - Immittance tests 中耳声导纳测试
Acoustic reflex threshold 声反射阈
• Three small bones forming a chain between the tympanic membrane and the inner ear 听骨链位于鼓膜和内耳之间,由3块听小骨组成
• Airborne sound wave energy becomes mechanical vibration
B型:平坦型。鼓室积液或鼓膜穿孔,根据ECV值区分
-200 Type C: Abn0ormal pressure 200
2020/11/30

【精品】:154英语

【精品】:154英语

154新题[1] Which signal of the follwings is not provided with onboard lifeboat? 哪种信号救生艇不配备?A. Rocket parachute signalsB. Buoyant smoke signalsC. Hand flare signalsD. Self-igniting signals答案:D Self-igniting signals自动点火信号(记忆题)[2]According to IMO regulations,______shall be posed outside lifeboat? 救生艇外面应安放 A. the retro-reflective tapes B. the reflective tapesC. the flashing bandsD. the anti-flashing bands答案:A)反光带 (the retro-reflective tapes) (记忆题)[3]Which one of the following is not required on survival crafts? 救生筏上哪一个不做要求?A.Anti-seasickness medicineB.Immersion suitsC.axesD.lifebuoys答案:D. lifebuoys救生圈(记忆题)[4]Have the safety belts for _______been examined?全封闭式救生艇的安全带已经检查过了吗?A.total enclosed lifeboatsB.totally enclosing lifeboatsC.totally enclosed lifeboatsD.total encloseing lifeboats答案:C. totally enclosed 全封闭式lifeboats[5]The fire-protected lifeboats are found________. (经检查)发现防火救生艇状况A.in satisfactorily conditionB.satisfactorilyC.satisfactoryD.satisfactored答案:C. satisfactory令人满意[6]We test the water spray fire protection system of fire-protected lifeboats every3 months, ______ the abandon ship drill. 我们每三个月测试防火救生艇的喷水防火系统,bining withbined withbining tobined to答案:B. combined with (the abandon ship drill) 连同弃船训练。

光纤通信复习题(含答案)

光纤通信复习题(含答案)

1.Make a choice (共十题 每题1分)10p(1).Which of the following dispersion (色散)dose not exist in single-mode optical fiber? ( D )A .material (材料)dispersion B.waveguide (波导) dispersionC.polarization-mode (偏振)dispersionD.intermodal (联合) dispersion(2).The unit (单位)of the fiber attenuation coefficient (衰减系数)is (C)A. dBB. dBmC. dB/kmD. dBm/km(3).the bands of Optical fiber communication is (B)A.0.01um-0.39umB. 0.8um-2.0umC.0.39um-0.79umD.100um-1000um(4).If the optical input power of a Optical amplifier is 10mW ,and the optical output power is 100mW as well ,then its output gain level is (A)A.10dBB.20dBC.30dBD.40dB(5)In order to make sure of the system BER (比特误差率) conditions , if the minimum optical input power of the receiver is 1 uW, the sensitivity of the receiver must be (A)A.-30dBmB.-40dBmC.-20dBmD.-43dBm(6)The principal (主要)light sources used for fiber optical communications applications are :(D )A.OA 、LDB.PIN 、APDC.PD 、LEDD.LD 、LED(7)laser (激光) action is the result of three key process ,which one of the following is not be included ?(D )A.photon absorption (光子吸收)B.spontaneous emission (自发发射)C.stimulated emission (受激发射)pound radiation (复合发射)(8) A single mode fiber usually has a core diameter (芯径)of A.A. 10mB. 62.5nmC. 125nmD. 50mm (9)To make sure that the APD photo-detector works properly, a sufficiently D is applied across the p-n junction.A. high forward-bias voltage (高的前置偏压)B. low forward-bias voltageC. low reverse-bias voltage (低的反相偏压)D. high reverse-bias voltage(10) When DFA fiber amplifier uses as light Repeaters (中继器), its main effect is B.A. amplifying and regenerating the signalB. regenerating the signalC. amplifying the signalD. reducing the signal noise(11) In graded-index optical fiber, the numerical aperture (数值孔径) NA can be expressed as C. A. 21n n - B. ∆2a C. ∆2n 1 D. 21n n a -(12) In practical SMFs, the core diameter is just below the cutoff (截止) of the first higher-order (高阶)mode; that is, for V slightly A.A. <2.4B. > 2.4C. =3D. =3.5(13) It is well known that the total dispersion in the single-mode regime is composed of two components: C.A. mode-partition noise (电流分配噪声), inter- symbol InterferenceB. frequency chirp, modal dispersionC. material dispersion, waveguide dispersionD. modal dispersion, waveguide dispersion(14)At present, erbium doped (涂饵的)fiber amplifier’s maximum small signal gain (小信号增益)is around A.A. 40 dBB. 30 dBC. 20 dBD. 10 dB(15)Which of the following doesn’t belong to passive optical components (无源光学组件)BA. Directional coupler(定向耦合器)B. Semiconductor laser(半导体激光)C. Optical fiber connector(光纤连接器)D. Optical attenuator(光学衰减器)(16) The A mode has no cut off(截止)and ceases(停止)to exist only when the core diameter (芯径)is zero.A. HE11B. TE01C. TM01D. EH11(17)When the phase difference(相位差)is an integral multiple(整数倍)of A, the two modeswill beat and the input polarization(偏振)state will be reproduced.A. 2πB. πC. 1800D. π/2(18)which one of the following model can transmit in the single-mode optical fiber ?(A)A.HE11B. TE01C. TM01D. EH112. Write the full name of the following acronym(共十题每题1分)10p(1)DCF: dispersion compensating fiber(色散补偿光纤)(2)CNR: carrier to noise ratio(载噪比)(3)SRS: Stimulated Raman Scattering(受激的拉曼色散)(4)SOA: Semiconductor optical amplifier(半导体激光放大器)(5)NA: numerical aperture(数值孔径)(6)PON: passive optical network(无源光网络)(7)SLM: single longitudinal mode(单纵向模式)(8)NEP: noise-equivalent power(噪声等效功率)(9)DSF: dispersion shift fiber(色散转移光纤)(10)SONET: synchronous optical network(同步光网络)(11)A TM: asynchronous transfer mode(异步传输模式)(12)ISDN: integrated services digital network(综合业务数字网)(13)WDM: wavelength-division multiplexing(波分多路复用)(14)SDH: Synchronous digital hierarchy(同步数据系列)(15)TLLM: transmission-line laser model(传输线激光模式)(16)ONSL: optical network simulation layer(光网络模拟层)(17)OVPO: outside vapor-phase oxidation(外气相沉积法)(18)V AD: vapor-phase axial deposition(汽相轴向沉积)(19)CDMA: code-division multiple access(码分多址)(20)FDM: frequency-division multiplexing(频分复用)(21)DSP: digital signal processing(数字信号处理)(22)MCVD: modified chemical vapor deposition(修正的化学汽相沉积)(23)EDFA: erbium-doped fiber amplifier(惨饵光纤放大器)(24)FDDI: fiber distributed data interface(光纤分布式数据接口)(25)SIOF: step index optical fiber(阶跃指数光纤)(26)GIOF: graded index optical fiber(渐变性光纤)(27)SQW: single quantum-well(单量子井)(28)ARQ: automatic reapt request(自动重发请求)(29)FEC: forward error correction(前向纠错)3. Filling blanks(共20空每空1分) 20p(1) According the mode which propagate(传播)in the fiber, the fiber can be divided into (single mode) fiber) and (multimode) fiber.(2) The most common misalignment(非线性)occurring in practice, which also causes the greatest power loss, is (axial displacement轴向移位).(3) The electromagnetic energy(电磁能)of a guided mode is carried partly in the (core) and partly in the (cladding包层).(4)The basic attenuation mechanisms(衰减机制)in a fiber are (absorption吸收), (scattering散射) and (radiative losses辐射损耗) of the optical waveguide.(5) The two main optical amplifier types can be classified as (SOAs半导体激光放大器) and (DFAs).(6) Networks are traditionally divided into: (LANs局域网), (MANs城域网),(W ANs广域网).(7)The principal light sources used for fiber optic communications applications are (ILDs注入型激光二极管) and (LEDs发光二级管) .(8) The dominant noise generated in an optical amplifier is (ASE).(9) The two most common samples of these spontaneous fluctuations(波动)are (shot noise) and (thermal noise热噪声).(10)According to the refractive index(折射率)of the core, the fiber can be divided into (step-index) fiber and (graded-index) fiber .(11)The total dispersion in single-mode fibers consists mainly of (material) and (waveguide) dispersion.(12) The most meaningful criterion(标准)for measuring the performance of a digital communication system is the (average error probability平均概率误差). In an analog system the fidelity criterion is usually specified in terms of a (peak signal-to-noise ratio).(13) The simplest transmission link is a (point-to-point line) that has a transmitter on one end an a receiver on the other.(14)The commonly used materials for fiber lasers are (erbium) and (neodymium).(15)Absorption is related to the fiber material, whereas scattering is associated both with the (fiber material) and with (structural imperfections) in the optical waveguide.(16)The two basic LED configurations being used for fiber optics are (surface emitters) and (edge emitters).(17) The basic schemes for improving the reliability are (ARQ自动重发请求) and (FEC前向纠错).4. Give a brief description of following terms and questions(共5题每题3分)15p (1) Briefly describe the key system features of WDM.波分复用1) capacity upgrade(容量升级)2) transparency (透明度)3) wavelength routing(波长选路)4) wavelength switching(波长转换)5) the connectors used to join individual fiber cables to each other and to the source anddetector(2) Briefly describe there major goals of SDH.同步数据系列1) Avoid the problems of PDH2) Achieve higher bit rates3) Better means for operation, administration and Maintenance(3) List at least three advantages of SOA半导体激光放大器.1) Small size, and easy to be integrated with semiconductor circuits.2) Fabrication(制造)is simple and with low power consumption(功耗), long life-span and low cost.3) Gain response is very quick and well suited for switching and signal processing in optical networks application.4) Can amplify optical signal and process signal in the same time such as switch, so can be used in wavelength converting and optical switch.(4) List more than three disadvantages of SOA.1) The coupling loss with optical fiber is too large2) Sensitive to polarization3) Noise figure is high(~8 dB)4) crosstalk串音干扰5) Easy to be affected by temperature, low stability(5) Stimulated Emissions受激发射If a photon(光子)of energy hv12 impinges on(撞击)the system while the electron is still in its excited state, the electron is immediately stimulated to drop to the ground state and give off a photon of energy hv12.(6)Dynamic rangeSystem dynamic range is the maximum optical power range to which any detector must be able to respond.(7) What conditions should be met to achieve a high signal-to-noise ratio?1) The photodetector(光电探测器)must have a high quantum efficiency(量子效率)to generate a large signal power.2) The photodetector and amplifier noises should be kept as low as possible.(8) Please write the three basic categories(类别)of degradation of light sources1) internal damage2) ohmic contact degradation3) damage to the facets of laser diodes(激光二极管)(9)List the three factors largely determining the frequency response of an LED1) the doping level(掺杂度)in the active region2) the injected carrier lifetime Ti in the recombination region3) the parasitic capacitance(寄生电容) of the LED.(10)Write the three basic types of two-level binary line codes that can be used for optical fiber transmission links.1) non-return-to-zero (NRZ) format2) return-to-zero (RZ) format3) phase-encoded (PE) format(11) Please write the three different mechanisms causing absorption briefly1) Absorption by atomic defects (原子缺陷) in the glass composition.2) Extrinsic (非固有的) absorption by impurity atoms in the glass material.3) Intrinsic absorption by the basic constituent atoms of the fiber material.(12) The disadvantage of Raman amplifierNeed large output power pump laser. As Raman Scattering, the energy is transferred from high frequency to low frequency. Cross talk will affect signal.5. Figure (共1题 每题5分)5p(1)Please draw the basic step for an automatic-repeat-request (ARQ) error-correction scheme. Solution:(ARQ纠错机制)(2)Please draw out the basic elements of the optical receiver.(5p)(光接收器)Solution:(3)Please draw out the basic elements of an analog link and the major noise contributions. Solution:(模拟链路及噪声源)光发送机电模拟输入信号谐波失真互调失真RIN激光削波光纤信道模式失真损耗GVD 光放大器ASE 噪声光检测器散弹噪声热噪声放大器噪声APD 倍增噪声电模拟输出到RF 接收机(3) consider the encoder shown in Fig.1that changes NRZ data into a PSK ing this encoder,draw the NRZ and PSK waveforms for the data sequence 0001011101001101.clock/2PSK dataNRZ datafrequency Afrequency BFig.1Solution:6. Calculation Problems(共3-4题,统计40分) 40p(1) A wave is specified by 8cos 2(20.8)y t z π=-,where y is expressed in micrometers and the propagation constant (传播常数) is given in 1m μ-.Find (a) the amplitude,(b) the wavelength,(c) the angular frequency (角频率), and (d) the displacement at time 0t = and 4z m μ=. Solution:The general form is:y = (amplitude) cos()cos[2(/)]t kz A vt z ωπλ-=-.Therefore(a) amplitude 8m μ=(b) wavelength: 11/0.8m λμ-= so that 1.25m λμ=(c) 22(2)4v ωπππ===(d) At 0t = and 4z m μ= we have 18cos[2(0.8)(4)]8cos[2( 3.2)] 2.472y m m πμμπ-=-=-=(2) A certain optical fiber has an attenuation of 0.6dB/km at 1300nm and 0.3dB/km at 1550nm.Suppose the following two optical signals are launched simultaneously into the fiber: an optical power of 150W μ at 1300nm and an optical power of 100W μ at 1550nm. What are the Solution:power levels in W μof these two signals at (a) 8km and (b) 20km?Since the attenuations are given in dB/km, first find the power levels in dBm for100W μ and 150W μ. These are, respectively,P(100W μ) = 10 log (100 W μ/1.0 mW) = 10 log (0.10) = - 10.0 dBmP(150W μ) = 10 log (150 W μ/1.0 mW) = 10 log (0.15) = - 8.24 dBm(a) At 8 km we have the following power levels:P 1300(8 km) = - 8.2 dBm – (0.6 dB/km)(8 km) = - 13.0 dBm = 50W μP 1550(8 km) = - 10.0 dBm – (0.3 dB/km)(8 km) = - 12.4 dBm = 57.5W μ(b) At 20 km we have the following power levels:P 1300(20 km) = - 8.2 dBm – (0.6 dB/km)(20 km) = - 20.2 dBm = 9.55W μP 1550(20 km) = - 10.0 dBm – (0.3 dB/km)(20 km) = - 16.0 dBm = 25.1W μ(3) A double-heterojunction (异质结) InGaAsP LED emitting at a peak wavelength of 1310nm has radiative and nonradiative recombination times of 25 and 90ns, respectively. The drive current is 35mA.(a) Find the internal quantum efficiency and the internal power level.(b) If the refractive index (折射率) of the light source material is n=3.5, find the power emitted from the device.Solution: (a) From Eq. int 11/r nr rτητττ==+, the internal quantum efficiency is int 10.783125/90η==+, and from Eq.int intint I hcI p hv q q ηηλ== the internal power level is int (35)(0.783)26(1310)hc mA p mW q nm ==(b) From Eq.int e int 2p (1)n t p P n n η==+, 21260.373.5(3.51)P mW mW ==+ (4) An LED with a circular emitting area of radius 20m μ has a lambertian emission pattern with a 1002()W cm sr ∙axial radiance at a 100mA drive current. How much optical power can be coupled into a step-index fiber having a 100m μ core diameter and NA=0.22? How much optical power can be coupled from this source into a 50m μ core-diameter graded-index fiber having 12.0, 1.48n α== and 0.01∆=?Solution:The source radius (半径) is less than the fiber radius,so Eq. 222222,1()2LED step s o s o P r B NA r B n ππ==∆ holds: 22223222,()(210)(100/)(0.22)191LED step s o P r B NA cm W cm W ππμ-==⨯= From Eq. 222,122[1()]2s LED graded s o r P r B n απαα=∆-+ 232222,122(210)(100/)(1.48)(0.01)[1()]15925LED graded P cm W cm W πμ-=⨯-=(5)Suppose an avalanche photodiode hasthe following parameters :1/231,1,0.85,,10L D L I nA I nA F M R η=====Ω, and 1B kHz=.Consider a sinusoidally(正弦) varying 850nm signal, which has a modulation index m=0.85 and an average power level 050P dBm =-, to fall on the detector at room temperature. At what value of M does the maximum signal-to-noise ratio occur?Solution: Using Eq.2222()()24/p P D L B Li M S N q I I M F M B qI B k TB R <>=+++ we have 22005/2001()22()24/D L B LR P m M S N qB R P I M qI B k TB R =+++ 162235/2191.215102.17610 1.65610M M ---⨯=⨯+⨯ The value of M for maximum S/N is found from Eq.224/()x L B L opt P D qI k T R M xq I I ++=+, with x = 0.5:Moptimum = 62.1.(6)An LED operating at 1300 nm injects 25W μ of optical power into a fiber. If the attenuation (衰减) between the LED and the photodetector (光电探测器) is 40 dB and the photodetector quantum efficiency (量子效率) is 0.65, what is the probability that fewer than 5 electronhole pairs (电子空穴对) will be generated at the detector in a 1-ns interval ?Solution: From ⎰==τηη0)(hvN hv E dt t P ,the average number of electron-hole pairs generated in a time t is 6.10)/103)(106256.6()103.1)(101)(1025(65.0/8346910=⨯⨯⨯⨯⨯===----s m Js m s W hc Pt h E N ληνη Then,from Eq.(7-2)%505.0120133822!5)6.10(!)(6.106.105=====---e e n e N n P N n(7) An engineer has the following components available:(a) GaAlAs laser diode operating at 850 nm and capable of coupling 1 mW (0 dBm) into a fiber. (b) Ten sections of cable each of which is 500 m long, as a 4-dB/km attenuation, and hasconnectors on both ends.(c) Connector loss of 2dB/connector.(d) A pin photodiode receiver.(e) An avalanche photodiode receiver.Using these components, the engineer wishes to construct a 5-km link operating at 20 Mb/s. If the sensitivities of the pin and APD receivers are -45 and -56 dBm, respectively, which receiver should be used if a 6-dB system operating margin is required?Solution:(a)Use margin 2system L l P P P f C R S T ++=-=α,to analyze the link power budget.(a) For the pin photodiode,with 11 jointsdB L km dB dB dBm dBm insystemm L l P P P f C R S T 6)/4()2(11)45(0arg )(11++=--=++=-=αWhich gives L=4.25km. the teansmission distance cannot be met with these components. (b)For the APDdB L km dB dB dBm dBm 6)/4()2(11)56(0++=--Which gives L=7.0km. the transmission distance can be met with these components.(8) Suppose we want to frequency-division multiplex 60 FM signals. If 30 of these signals have a per-channel modulation index i m =3 percent and the other 30 signals have i m =4 percent, find the optical modulation index (调制指数) of the laser.Solution:The total optical modulation index is%4.27])04(.30)03(.30[][2/1222/12=+==∑ii m m(9) An optical transmission system is constrained to have 500-GHz channel spacings. How many wavelength channels can be utilized in the 1536-to-1556-nm spectral band (频谱带)? Solution: In terms of wavelength,at acentral wavelength of 1546nm a 500-GHz channel spacing isnm s sm nm f c 410500/103)1546(19822=⨯⨯=∆=∆-λλ The number of wavelength channels fitting into the 1536-to-1556 spectral band then is 54/)15361556(=-=nm nm N(10) The output saturation (饱和) power sat out P , is defined as the amplifier output power for which the amplifier gain G is reduced by 3 dB (a factor of 2) from its unsaturated value 0G . Assuming 0G >>1, show that in terms of the amplifier saturation power sat amp P ,, the output saturation power issat amp sat out P G G P ,00,)1(2ln -=Solution: Let 2/0G G = and 0,/22/G P P P sat out out in ==.then Eq.(11-15) yields2ln 212,,00satout sat amp P P G G += Solving for s a t out P , and with 10>>G ,we havesat amp sat amp sat amp sat out P P P G G P ,..00,693.0)2(ln 22ln =≈-=。

光伏逆变器EMC测试报告及认证报告书

光伏逆变器EMC测试报告及认证报告书
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GENERAL PRODUCT INFORMATION ...................................................................................................... 5
TEST SET-UP AND OPERATION MODES ................................................................................................. 6
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15061668 001
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TEST SUMMARY
4.1.1 HARMONICS ON AC MAINS Result: N/A 4.1.2 VOLTAGE CHANGES, VOLTAGE FLUCTUATIONS AND FLICKER ON AC MAINS Result: N/A 4.1.3 MAINS TERMINAL CONTINUOUS DISTURBANCE VOLTAGE Result: Passed 4.2.1 RADIATED EMISSION Result: Passed 5.1.1 ELECTROSTATIC DISCHARGE Result: Passed 5.1.2 RADIO FREQUENCY ELECTROMAGNETIC FIELD Result: Passed 5.1.3 POWER FREQUENCY MAGNETIC FIELDS Result: Passed 5.2.1 ELECTRICAL FAST TRANSIENTS AND BURSTS Result: Passed 5.2.2 CONDUCTED DISTURBANCES, INDUCED BY RF FIELDS Result: Passed 5.2.2 SURGES TO AC POWER PORT Result: Passed 5.2.3 VOLTAGE DIPS AND INTERRUPTIONS TO AC POWER PORT Result: N/A

信息技术发展对radio的影响英语作文

信息技术发展对radio的影响英语作文

信息技术发展对radio的影响英语作文With the rapid advancement of information technology, the radio industry has undergone significant changes. The emergence of online streaming services, podcasts, and digital radio platforms has revolutionized the way people consume radio content. These technological developments have both positive and negative impacts on traditional radio broadcasting.One of the positive impacts of information technology on radio is the increased accessibility and convenience for listeners. Online streaming services and digital radio platforms allow people to listen to their favorite radio programs anytime, anywhere, using their smartphones or other electronic devices. This has expanded the reach of radio broadcasting, enabling it to reach a global audience and engage with listeners in new ways.Furthermore, information technology has also provided radio stations with new opportunities for content creation and distribution. Podcasts, for example, have become a popular medium for radio stations to deliver on-demand audio content to their audience. Radio stations can now produce and distribute a wide variety of programs, reachingniche audiences and catering to specific interests.However, the development of information technology has also posed challenges for traditional radio broadcasters. The competition from online streaming services and digital platforms has led to a fragmented audience and increased pressure to adapt to changing consumer preferences. Radio stations must now find innovative ways to attract and retain listeners in a highly competitive media landscape.In conclusion, the development of information technology has had a profound impact on the radio industry, transforming the way radio content is created, distributed, and consumed. While these technological advancements have brought new opportunities for radio broadcasters, they have also presented challenges that require adaptation and innovation to thrive in the digital age.中文翻译:随着信息技术的快速发展,广播行业发生了重大变化。

关于汽车音响的英语作文

关于汽车音响的英语作文

关于汽车音响的英语作文Car Audio。

Car audio has become an essential part of modern cars. It is not only a tool for entertainment, but also a way to enhance the driving experience. With the development of technology, car audio has evolved from simple radio and cassette players to advanced multimedia systems that can play music, videos, and connect to the internet.The most common car audio system is the head unit, which controls all the audio functions. It includes a display screen, CD/DVD player, and radio tuner. Some head units also have Bluetooth connectivity, allowing drivers to stream music from their smartphones or make hands-free calls. The speakers are another important component of car audio, producing the sound that the driver and passengers hear. They come in different sizes and shapes, and can be mounted in various locations throughout the car.In addition to the head unit and speakers, car audio systems can also include amplifiers, subwoofers, and equalizers. Amplifiers increase the power of the audio signal, making the music louder and clearer. Subwoofers are specialized speakers that produce low-frequency sounds, such as bass and drums. Equalizers allow drivers to adjust the sound to their preferences, such as boosting the bass or treble.When choosing a car audio system, there are several factors to consider. The first is the budget, as car audio systems can range from a few hundred dollars to several thousand dollars. The second is the type of music thedriver listens to, as different genres may requiredifferent types of speakers and amplifiers. The third is the size and layout of the car, as larger cars may require more powerful speakers and amplifiers.In conclusion, car audio has come a long way since its early days, and has become an important part of the driving experience. With the right system, drivers can enjoy theirfavorite music while on the road, and enhance their overall driving experience.。

emission英文作文

emission英文作文

emission英文作文Emission from cars and factories pollutes the air and contributes to global warming. It's a serious problem that needs to be addressed.The government should implement stricter regulations on emissions to protect the environment and public health.It's important for everyone to do their part in reducing emissions and finding alternative, sustainable solutions.Investing in renewable energy sources such as solar and wind power can help reduce emissions and combat climate change. It's time to prioritize the planet over profit.We need to educate the public about the impact of emissions and encourage people to make environmentally-friendly choices in their daily lives. It's not just about saving the planet, but also creating a healthier future for generations to come.It's crucial for businesses to take responsibility for their emissions and work towards sustainable practices. We can't continue to prioritize economic growth over the well-being of the planet.Emissions from agriculture also contribute to environmental pollution. We need to find ways to reduce these emissions while still meeting the demand for food production.Individuals can make a difference by reducing their carbon footprint through simple actions like using public transportation, conserving energy, and supporting eco-friendly products.It's time for a collective effort to reduce emissions and protect the planet for future generations. We can't afford to ignore this problem any longer.。

雷达的发明英语作文

雷达的发明英语作文

雷达的发明英语作文英文回答:The invention of radar is one of the most significant technological advancements of the 20th century. It has revolutionized the way we navigate the world, from air travel to marine navigation to weather forecasting.The basic principle of radar is to emit radio waves and then listen for the reflected signals. By measuring the time delay and frequency shift of the reflected signals, it is possible to determine the distance and velocity of the object that reflected the waves.The first practical radar system was developed in the early 1930s by a team of British scientists led by Robert Watson-Watt. This system was used to detect incoming aircraft during the Battle of Britain in 1940, and it played a crucial role in the Allied victory.Since then, radar has been continuously developed and refined. Today, there are many different types of radar systems, each with its own unique applications. Some of the most common types of radar include:Air traffic control radar: This type of radar is used to track the movement of aircraft in the air. It helps to ensure the safety of air travel by preventing collisions between aircraft.Marine radar: This type of radar is used to detect and track ships at sea. It helps to prevent collisions between ships and other objects, and it can also be used to navigate in fog or bad weather.Weather radar: This type of radar is used to track the movement of weather systems. It can be used to forecast the weather, and it can also be used to issue warnings about severe weather events.Radar has had a profound impact on our world. It has made air travel safer, marine navigation more efficient,and weather forecasting more accurate. It is a technology that continues to be developed and refined, and it is likely to play an even greater role in our lives in the years to come.中文回答:雷达的发明是20世纪最重要的技术进步之一。

专八阅读理解练习题《声音处理》

专八阅读理解练习题《声音处理》

专八阅读理解练习题《声音处理》2018专八阅读理解练习题《声音处理》2018年的专八看似很遥远,但是对于难度大的专八考试来说,考生如不及早备考,可是难以取得理想的成绩的。

下面,店铺就为大家送上一篇2018专八阅读理解练习题,供大家练习。

Every year television stations receive hundreds of complaints about the loudness of advertisements. However. federal rules forbid the practice of making ads louder than the programming. In addition, television stations always operate at the highest sound level allowed for reasons of efficiency. According to one NBC executive. no difference exists in the peak sound level of ads and programming. Given this information. whydo commercials sound so loud?The sensation of sound involves a variety of factors in addition to its peak level. Advertisers are skilful at creating the impression of loudness through their expert use of such factors. One major contributor to the perceived loudness of commercials is that much less variation in sound level occurs during a commercial. In regular programming the intensity of sound varies over a large range. However, sound levels in commercials tend to stay at or near peak levels.Other "tricks of the trade" are also used. Because low-frequency sounds can mask higher frequency sounds. advertisers filter out any noises that may drown out the primary message. In addition, the human voice hasmore auditory (听觉的) impact in che middle frequency ranges. Advertisers electronically vary voice sounds so that they stay within such a frequency band. Another approach is to write the script so that lots of consonants(辅音) are used, because people are more aware ofconsonants than vowel (元音) sounds. Finally, advertisers try to begin commercials with sounds that are highly different from those of the programming within which the commercial is buried. Because people become adapted to the type of sounds coming from programming. a dramatic change in sound quality draws viewer attention. For example. notice how many commercials begin with a cheerful song of some type.The attention-getting property of commercials can be seen by observing one-to-two-year-old children who happen to be playing around a television set. They may totally ignore the programming. However. when a commercial comes on.their attention is immediately drawn to it because of its dramatic sound quality.1. According to the passage, the maximum intensity of sound coming from commercials________.A) does not exceed that of programsB) is greater than that of programsC) varies over a large range than that of programsD) is less than that of programs2. Commercials create che sensation of loudness because____________________.A) TV stations always operate at the highest sound levelsB) their sound levels are kept around peak levelsC) their sound levels are kept in the middle frequency rangesD) unlike regular programs their intensity of sound varies over a wide range3. Many commercials begin with a cheerful song of some kind because_________________.A) pop songs attract viewer attentionB) it can increase their loudnessC) advertisers want to make them sound different fromregular programsD) advertisers want to merge music with commercials4. One of the reasons why commercials are able to attract viewer attention is that_____________.A) the human voices in commercials have more auditory impactB) people like cheerful songs that change dramatically in sound qualityC) high-frequency sounds are used to mask sounds that drown out the primary messageD) they possess sound qualities that make the viewer feel that something unusual is happening5. In the passage, the author is trying to tell us________________.A) how TV ads vary vocal sounds to attract attentionB) how the loudness of TV ads is overcomeC) how advertisers control the sound properties of TV adsD) how the attention-getting properties of sounds are made use of in TV ads答案:1.根据文章的内容,电视广告中最高强度的声音_____________。

外文翻译原文--基于红外报警技术的防盗系统

外文翻译原文--基于红外报警技术的防盗系统

Based on infrared alarm technology security systems1the introduction1.1the research significance of this topic research situation at home and abroad.With the development of society and science and technology unceasing development,people's living standards been improved greatly,and to the private property protection means in the unceasing enhancement,the intelligent facilities for anti-theft puts forward new requirements.This design is to meet the need of modern residential anti-theft designed family electronic alarm system.It in previous devices based on improved greatly, because use the single-chip processor signal,not only can used for single residential area,also can be used in a large-scale residential security systems.It's the job of the performance is good,do not appear to report and misstatement phenomenon,safe and reliable.In our country,the present market condition alarm basically has triggered alarm system pressure switch electron and alarm system and pressure shading triggered alarm system,etc.Various kinds of alarm,but this several common alarm there are some shortcomings.This system USES a human pyroelectric infrared sensor in the human body detector in the field, passive pyroelectric infrared detectors because of its low cost,easy fabrication,low cost,installation is more convenient,anti-theft performance is stable and high sensitivity,safe and reliable,has attracted broad family characteristics such as popular with the customers. And alarms installation concealment,not easily by rogue found.1.2infrared alarm technology introductionInfrared sensing technology can be divided into active sensing technology and passive sensing technology.Therefore infrared alarm is divided again active infrared alarm and passive infrared alarm.1.2.1active alarm technologyActive infrared alarm is by sending and receiving device two parts. Infrared transmitter drive infrared light emitting diode modulation issued a bunch of the infrared beam.In a certain distance from the transmitter, and placed in a infrared receiver alignment.It through the photo transistor receiving launch end issued ir radiation energy,and pass byphotoelectric convert to electrical signals.This signal after proper treatment again sent alarm controller circuit.Respectively in charge and inchoative place a infrared optical lenses,will be gathered into fine parallel beams,in order to make the infrared energy can concentrate ing the infrared light modulation has the following advantages:(1)reduce power consumption.(2)make infrared detector has strong resistance to?1.2.2passive quote with technologyPassive infrared detector does not need additional infrared radiation lamp-house,itself not to external launch any energy,but by directly from a moving target detection probe the infrared radiation,so just have passive said.Passive infrared detector is with pyroelectricity effect on detecting.1.2.2.1nature objects of the infrared radiationThe nature of any object,as long as the temperature above absolute zero (273℃),constantly outward issued infrared radiation,and travel at the speed of light energy.Object radiate outward infrared radiation of energy and the object of temperature and infrared radiant wavelength.Assuming objects launching infrared radiation of peak wavelength for a few,,its temperature for T,the radiation energy equals infrared radiation of peak wavelength gerben and object product temperature T.This product is a constant,namely:The higher the temperature of the objects,emit infrared radiation of the smaller peak wavelength,send out infrared radiation energy is bigger also.1.2.2.2pyroelectric effectPassive infrared detector also called pyroelectric infrared detector,its main working principle is pyroelectric effect.Pyroelectric effect means if make some strong dielectric material(such as qin batio3,qin wrong acid lead P(zT),etc.)of the surface temperature changes,then with the temperature rise or fall,material surface occurs polarization,namely onthe surface of the charge will be produced change,and material surface charge lost balance and eventually charge will change with voltage or current form output.In pyroelectric infrared detectors are two key components,one is pyroelectric infrared sensor P(TR),infrared signal changes can be theptr shift into electrical signal to the white light signal has a natural inhibition.Another is the Fresnel lens,?Fresnel thoroughly1.2.2.3pyroelectric infrared sensor basic structurePyroelectric infrared sensors from sensor detection yuan,interference filters and mosfet verifier three parts.According to the number of detecting yuan to points,pyroelectric infrared sensors have unit,double yuanhe four yuan to wait for a few kinds,for human detection of infrared sensor adopts double yuan or four yuan type structure.According to pyroelectric infrared sensor utility cent,have the following kinds:used for measuring temperature sensor,it's the job of the wavelength of(1-20) nano,Used for flame detection sensor,it's the job of the wavelength for 0.435+/-0.15nano,For human detection sensor,it's the job of the wavelength of7to15feet.Figure 1.2is a double detection yuan pyroelectric infrared sensor structure schematic drawing.The sensor will two opposite polarity,specialWhen using general in the tube and shell capped with filter of films and window,to choose receive different wavelengths.In the window jacket filter is designed to make don't need infrared sensors cannot enter. General pyroelectric infrared sensor in spectral range sensitivity is quite flat(and not being visible effect).Usually used siliceouspolyethylene material filter,it can not contact form detect objects to radiate the infrared energy changes,and converts it into electrical signal output.Sensor probe the Fresnel lens with front.The Fresnel lens is with transparent made of plastic with a special optical coefficient of lenses, it consists of a set of parallel prism type lens is composed of its each unit is only a little of the lens,?view AngleWhen someone from the lens body before walked out of the infrared ray unceasingly in the"blind"and"high sensitive areas]switch,it makes received signals to suddenly strong suddenly weak pulse form input, strengthened the energy changes amplitude,thereby improving the detection sensitivity.1.2.2.4pyroelectric infrared detector basic principlePyroelectric infrared sensor by receiving mobile human radiation that certain wavelengths of infrared radiation,can be transformed into and human body movement speed and distance,the direction of low-frequency signals about.When pyroelectric infrared sensor by ir radiation sources of radiation,its internal sensitive materials temperatures will rise, polarization intensity is abate,surface charge reduce,usually will release this part of the charge called pyroelectric charge.Because of pyroelectric charge how many can reflect material changes of temperature, so by pyroelectric charge by circuit transformed into the output voltage can also reflect material changes in temperature,thus detect ir radiation energy changes.The optical system of the infrared detector can be more than?from2hardware system design2.1infrared anti-theft alarm system hardware designBecause this design focuses on family guard against theft,real-time monitoring of a narrower range,so this design by simply using a passive infrared detector is enough.Therefore,infrared intelligent anti-theft alarm system,and the specific design requirements for:1completes to high sensitive infrared sensor design,make its can warning of what happened real-time and accurate detection.2automatic alarm(automatic dial-up alarm audible and visual alarm). We design the system must have the following function module:3passive infrared detector,4sound-light alarm,5telephone automatic dial-up function;6continued uninterrupted power supply,According to the system to complete functions,we adopt single chip microcomputer as the core of the system unit,electronic detection, intelligent control and telephone tong2.2telephone automatic dial-up alarm circuit designIn order to simplify the whole system design process,we do not adopt MT880 chip dialing.Realization process is as follows:First in telephone storage inside put on domestic host cell phone number or alarm call110.From MCU pins p2.0and p2.1drawn two wiring connect relays,a pick telephone keyboard MianDiJian,another connect telephone keyboard keys,automatic weighing dial because the phone keypad scanning is similar microcontroller keypad scanning,so can make SCM give first p2.0 a signal,lets telephone h-f,then give the p2.1a signal,let relay connected,automatic weighing dial the key a potential,let telephone automatic dial-up,so they could finish the system alarm function.2.3system working principleThe whole system hardware part mainly includes six parts:MCU module; Infrared detector,Acousto-optic alarm circuit;Telephone automatic dial-up alarm circuit;Power supply circuit,Working state instructions circuit.Its system working principle for:the sensors will be detected signals to lead signal processor processing,microcontroller judgment to P1.0mouth have pulse falling edge jumping signal immediately transferred to the acousto-optic alarm program,at this moment,the red light buzzer alarm rapid flashes,lasted30s.In the30s inside if someone press the switch,then eliminate alarm remove alarm.If this time no one remove alarm, the proof nobody at home in30s system will automatically triggers telephone finish the whole system of police work ter, microcontroller will continue to cycle back?sentenced3.4system total diagramIn proteus simulation system,the system circuit by crystals circuit, sound-light alarm circuit composed.Among them,we use connect the dedication of the P1.0simulated infrared sensors,requirement when switch when pressed by the high jump,level is low,the equivalent of,sensor detects the state of man,the telephone line with P2.0and P2.1derivation, here without simulation telephone circuit diagram.Figure 3.53software system design3.1control module design programMicrocomputer in the initial plus electric,voltage is not steady state, causing instability,at this time the SCM in commonly after power up to system with a piece of delay.Time-lapse after detecting P1mouth microcontroller state,detection level signal whether mutations,if is then calls the police processing procedure,including automatic dial-up audible and visual alarm procedures,if no changes,ChuXiang leveldetection continues to P1mouth state.Figure 4.1main program flowchart3.2system development adopted by the programming and commissioning of the platformThis system language using assembly language preparation,so choose wave6000,he has the microcontroller program edit,compile and debugging, etc.,and generate hexadecimal.Files,through:machine TOPWIN burning software writeable microcontroller program memory.The simulation software use Proteus,he is from Britain Labcenter electronics company EDA software.The circuit of the simulation is interactive,aiming at the microprocessor application,still can directly based on schematic diagram of the virtual prototype programming,and implementing software source code level of real-time debugging,if have display and output,still can see after the operation of input and output effect.4system debugging and test4.1software debuggingAdopt modularization program design thought,first debugging subroutines, then gradually superposition debugging,through Proteus simulation software debugging,proof program can realize its function.4.2system debuggingThrough the circuit of welding,each module function commissioning.I put the hardware that occur errors adjusted,in addition,infrared that piece, because is employing redirected of pyroelectric switch modified,so in must be taping photoconductive resistance to rise,has arrived in the days and nights can alarm function.The total system commissioning,through,error meets the requirement.5closingThis system USES a pyroelectric infrared sensor,its make simple low cost and installation are more convenient and anti-theft performance is stable and strong anti-jamming capability,high sensitivity,safe and reliable. In addition,the system also has the very big function expansion,for example,in the warehouse,community or monitoring range is wider place, can add a few road infrared detector,using interface communication technology and computer connection,be helpful for the unified administration.Doing single family anti-theft system,we can also add LCD module,display alarming time,add more keyboard locks,let family or friends know the password of cases remove alarm,in case the misstatement occur).。

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a r X i v :a s t r o -p h /9902143v 1 9 F eb 1999INFRARED EMISSION FROM RADIO-LOUD ACTIVE NUCLEIIlse M.van Bemmel 1,Peter D.Barthel 2,Thijs de Graauw 31European Southern Observatory,Garching bei M¨u nchen,Germany 2Kapteyn Astronomical Institute,Groningen,The Netherlands 3Dutch Space Research Organisation,Groningen,The NetherlandsABSTRACTIn order to test the unification scheme for double-lobed radio sources,the far-infrared properties of matched samples of radio-galaxies and radio-loud quasars were studied using ISOPHOT.The quasar data were complemented with nearly simultaneous submillimeter and centimeter radio data.The re-sults show that quasars are generally brighter than radio-galaxies in their far-infrared output and that beamed non-thermal radiation must be excluded as source for this infrared excess.However,non-thermal flares or optically thick tori can still reconcile these results with the unification scheme.Key words:active galactic nuclei;unification;spec-tral energy distributions1.INTRODUCTIONThe unified theory for radio-loud active galaxies (Barthel,1989;Urry &Padovani,1995)predicts the existence of a dusty torus surrounding the central engine.Models for the reprocessing of the hard non-thermal nuclear radiation by this torus show that at wavelengths longward of 60µm the torus will be op-tically thin (Pier &Krolik,1992;Granato &Danese,1994).However,in the IRAS observations quasars are two to four times brighter at 60µm than radio galaxies (Heckman et al.,1994).In some special ge-ometries of the torus,models can account for this infrared excess.Also the torus could still be op-tically thick at 60µm,or there could be a signifi-cant amount of angle dependent non-thermal con-tamination in quasars.Non-thermal beamed radia-tion has been proposed as a possible solution (Hes et al.,1995).In order to discover the true cause of the infrared excess in quasars,observations are needed at longer wavelengths.All current torus models predict that beyond 80µm the thermal emission will be isotropic.According to unified schemes,the output of quasars should then equal that of matched radio-galaxies at these long far-infrared wavelengths.ISOPHOT ob-servations of quasars and radio-galaxies have been obtained to test this hypothesis.To quantify any possible non-thermal contamination in quasars,thelatter were in addition observed with SCUBA at the JCMT,and the NRAO Very Large Array (VLA).2.SAMPLE SELECTION AND OBSERVATIONS The target sample is selected using several crite-ria.First of all the objects must have the edge-brightened,double-lobed radio structure typical for Fanaroff&Riley class II sources (Fanaroff&Riley,1974).Six matched pairs were constructed,contain-ing one quasar and radio-galaxy each,having com-parable redshift,radio-lobe power and angular size.Lobe radio power is a reasonably good measure of the active nucleus power,and is furthermore independent of the orientation of the objects.Observations were carried out with ISOPHOT at three wavelengths,during the period October 1996to April 1998.We made raster-mode mini-maps with C100and C200(AOTs P3and P22).The rasters have a size of 3×3(C100)and 4×2(C200)in Y ×Z direction.The filters used were the 60µm,90µm (C100)and 160µm (C200).Observations of only four pairs were completed during the lifetime of ISO;for the other two pairs only the radio-galaxy was observed.For the quasars these data were comple-mented with nearly simultaneous VLA A-array data at 6,2,1.2and 0.7cm (April 17,1998)and JCMT SCUBA data at 2mm and 850µm (May 28,1997),addressing their non-thermal radio core strengths.These observations were made in order to detect pos-sible non-thermal contamination of the far-infrared emission.Since the effect of non-thermal emission in radio-galaxies is negligible (Hoekstra et al.,1997),these objects were not observed with the VLA and SCUBA.3.DATA REDUCTION 3.1.ISO Data ReductionAll ISO data have been processed with OLP version 6.11and raw data have been reduced using the Phot Interactive Analysis tool (PIA)version 7.2(e).The steps from ERD to AAP level were all done using the default procedures.Deglitching at ERD level wasTable1.Flux densities in mJy as plotted in Figure1(table added after submission to proceedings).For3C351 theflux density at6cm is from our VLA observation,while in Figure1we plotted the datapoint from Bridle et al.(1994).3C19––––––≤25≤50≤45 3C42––––––21±6≤55≤50 3C67––––––≤40≤8072±35 3C277.1≤1522.7±0.721.5±1.09.6±1.8≤17–31±336±1455±28 3C323.138±235±1.3≤8.5≤10≤14≤1214±641±20109±36 3C334167.7±0.8112.3±0.491.4±0.7≤1020±1015±856±889±16132±33 3C3519.2±1.2–≤5.0≤10––133±14262±18323±71 3C460––––––73±22≤50≤22miniminiFigure 1.The complete spectra for the four pairs observed with ISO.For the quasars:plusses are VLA data,triangles are SCUBA data,red diamonds are ISO data.The solid line is an empirical fit to the radio-core spectra,the dash-dotted line is a black body fit to the ISO data.For the radio-galaxies:asterisks are ISO data and the dotted line is a black-body fit.5.DISCUSSION5.1.Non-thermal ContaminationRadio-quiet and radio-loud quasars show remarkable similarities in their broad band spectra.The simi-lar infrared to submillimeter slope and far-infrared turnover frequency point to an identical source of infrared emission.Since radio-quiet quasars have no significant non-thermal component,the infrared emission must be thermal (Sanders et al.,1989).As-suming the models for thermal torus emission show the correct trends,an aspect angle dependent non-thermal contamination must be present in radio-loud quasars to reconcile the observed infrared excess in these objects with the unification theory.There are two possibilities:continuous beaming,or flaring,which requires a rapidly varying beamed component.Continuous beaming is in most cases not more than a 30per cent effect (Hoekstra et al.,1997)and has been solidly ruled out for causing the excess in at least two quasars (van Bemmel et al.,1998).Here,only onequasar is detected at 7mm and the detections with SCUBA are marginal at best.In our results continu-ous non-thermal contamination of the far-infrared is negligible,as can also be seen from the fits to the ra-dio data in Figure 1.It is important to use only core flux densities,as this is the only source of beamed non-thermal radiation in active galaxies.When us-ing the total radio flux densities as done by Haas et al.(1998),the centimeter flux densities will be dom-inated by emission from the radio lobes.These have generally steep spectra and are not beamed,thus they do not contribute significantly to the infrared emission in these sources.A varying component can easily be missed.Strongly beamed radiation from non-thermal flares has been observed in blazars (Brown et al.,1989);such flares are both very strong and short-lived,with typical timescales of several days.They could be observed in quasars due to the small aspect angle of these ob-jects.In previous work two out of three quasars showed high 3mm fluxes,which could not be fit-ted with a radio core model and were suggestive of flaring (van Bemmel et al.,1998).In radio-galaxies beamed flare radiation is much less likely to be ob-served,because of the larger aspect angles in these sources.Strongflares can cause large differences in far-infrared output,whilst being missed in the non-thermal core spectra.5.2.Optically Thick TorusThe persistence of the infrared-excess at longer wave-lengths can also be explained if the torus is optically thick up to140µm at least.Arguing in favour of this concept is the fact that a lower temperature is needed for the black-bodyfit in at least two of the radio-galaxies.Here maybe only the cooler edge of the torus is seen,while in quasars the hot inner parts dominate the infra-red output.This is in contradic-tion with the present models for dusty tori,but in broad agreement with predictions from the unified models.Since changing the models for the torus also has implications for the X-ray spectra observed in these sources,new modelling has to be done to study this possibility in more detail.5.3.Evolution Between TypesEvolution has been proposed as a solution to the infrared-excess(van Bemmel et al.,1998).This would then imply that quasars are younger and still contain more dust in their host galaxy,whereas radio-galaxies are older and have processed their dust and gas into stars.A link with the ultra-luminous galax-ies has been made in this respect as these being very young quasars who are in the phase of birth(Sanders et al.,1988).However,during a recent conference on this topic,most evidence showed that these so-called ULIRGs are in many cases driven by strong starbursts and not by a central active nucleus(Mon-sters or Babies:What powers ultra-luminous infrared galaxies?,Ringberg Castle,1998).The fact that we find one pair in which the far-infrared spectra are identical,also argues against evolution between the types.Any evolutionary model is obviously in con-flict with orientation based unification concepts.6.CONCLUSIONSObservations of matched pairs of quasars and radio-galaxies show that the previously reported infrared-excess is still present in quasars,up to140µm rest-frame wavelength.This cannot be accounted for by current torus models,without causing a contradic-tion with unified schemes.Continuous beaming has to be excluded in our objects,but non-thermalflares can explain the excess,without necessary adjust-ments to either theory.Also the models for the torus have to be examined in more detail to explain ob-served temperature differences between quasars and radio-galaxies.This is currently under investigation and will be described in future publications.Future work will also include the search forflares in 3C334with SCUBA and the investigation of orienta-tion dependence of optical emission lines in a sample of double-lobed active galactic nuclei.ACKNOWLEDGEMENTSOur thanks to all people who helped us during the hard reduction process,especially Martin Haas who provided a lot of useful tips and advice.Also thanks to Ronald Hes for initial involvement.And thanks to Eric Hooper,Mari Poletta,Belinda Wilkes,Thierry Courvoisier and Rolf Chini for advice and discus-sions.Thanks to Xander Tielens for useful comments and advice while making this manuscript.ISO is an ESA project with instruments funded by ESA Member States(especially the PI countries: France,Germany,the Netherlands and the United Kingdom)and with the participation of ISAS and NASA.PIA is a joint development by the ESA As-trophysics division and the ISOPHOT consortium. The National Radio Astronomy Observatory is a fa-cility of the National Science Foundation operated under cooperative agreement by Associated Univer-sities,Inc.The James Clerk Maxwell Telescope is op-erated by The Joint Astronomy Centre on behalf of the Particle Physics and Astronomy Research Coun-cil of the United Kingdom,the Netherlands Organi-sation for Scientific Research,and the National Re-search Council of Canada.7.BIBLIOGRAPHIC REFERENCESREFERENCESBarthel,P.D.,1989,ApJ,336,606Bridle,A.H.,Hough,D.H.,Lonsdale,C.J.,Burns, J.O.,Laing,R.A.,1994,AJ,108,766Brown,L.M.J.,Robson, E.I.,Gear,W.K.,et al., 1989,ApJ,340,129Fanaroff,B.L.,Riley,J.M.,1974,MNRAS,167,31P Granato,G.L.,Danese,L.,1994,MNRAS,268,235 Haas,M.,Chini,R.,Meisenheimer,K.,et al.,1998, ApJ,503,L109Heckman,T.M.,O’Dea, C.P.,Baum,S.A.,Lau-rikainen,E.,1994,ApJ,428,65Hes,R.,Barthel,P.D.,Hoekstra,H.,1995,A&A, 303,8Hoekstra,H.,Barthel,P.D.,Hes,R.,1997,A&A, 319,757Lemke,D.,Klaas,U.,Abolins,J.,et al.,1996,A&A, 315,L64Pier,E.A.,Krolik,J.H.,1992,ApJ,401,99 Sanders,D.B.,Phinney,E.S.,Neugebauer,G.,Soifer,B.T.,Matthews,K.,1989,ApJ,347,29 Sanders,D.B.,Soifer,B.T.,Elias,J.H.,et al.,1988, ApJ,325,74Urry,C.M.,Padovani,P.,1995,PASP,107,803 van Bemmel,I.M.,Barthel,P.D.,Yun,M.S.,1998, A&A,334,799。

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