Experimental investigation of a pilot-scale jet bubbling reactor for wet flue gas desulphurisation
高三英语学术研究方法创新不断探索单选题30题
高三英语学术研究方法创新不断探索单选题30题1. In academic research, a hypothesis is a ______ that is tested through experiments and observations.A. predictionB. conclusionC. theoryD. assumption答案:D。
本题考查学术研究中“假说”相关的基本概念。
选项A“prediction”意为“预测”,通常是基于现有信息对未来的估计;选项B“conclusion”指“结论”,是在研究后得出的最终判断;选项C“theory”是“理论”,是经过大量研究和验证形成的体系;选项D“assumption”表示“假定、设想”,更符合“假说”的含义,即在研究初期未经充分验证的设想。
2. The main purpose of conducting academic research is to ______ new knowledge and understanding.A. discoverB. createC. inventD. produce答案:A。
此题考查学术研究目的相关的词汇。
选项A“discover”意思是“发现”,强调找到原本存在但未被知晓的事物;选项B“create”意为“创造”,侧重于从无到有地造出新的东西;选项C“invent”指“发明”,通常指创造出新的工具、设备等;选项D“produce”有“生产、产生”的意思,比较宽泛。
在学术研究中,主要是“发现”新知识和理解,所以选A。
3. A reliable academic research should be based on ______ data and methods.A. accurateB. preciseC. correctD. valid答案:D。
本题关于可靠学术研究的基础。
选项A“accurate”侧重于“准确无误”,强调与事实完全相符;选项B“precise”意为“精确的、明确的”,更强调细节的清晰和明确;选项C“correct”指“正确的”;选项D“valid”表示“有效的、有根据的”,强调数据和方法具有合理性和可靠性。
立项报告1
立项报告1、项目简介水下超空泡射弹是一种新型水下武器,在功能上与脱壳穿甲弹相似,依靠弹道末端高的动能存量打击目标。
超空泡射弹的工作介质是水,而物体在水中所受到的阻力约为在空气中的1000倍,用常规方法明显提高水下航行体速度要受到很大的限制。
一段时间以来,研究人员尝试了各种减阻的方法,如边界层抽吸减阻等,但减阻效果通常都不理想。
超空泡减阻技术是一种可以使水下高速运动航行体获得90%减阻量的革命性减阻方法,基于这种新概念、新原理研制的水下超空泡射弹,可以突破普通射弹水下运动极限,使水下射弹的速度提高到1000m/s的量级,大大增加射弹的行程和杀伤力,提高进攻和防御能力。
射弹在水中高速运动时,贴近其表面的液体压力就会降低,当射弹的速度增加到某一临界值时,流体的压力将等于其饱和蒸汽压力,此时流体就会发生相变,由液相变为汽相,这就是空化现象。
随着航行体速度的不断增加,空泡沿着航行体表面不断后移、扩大、发展进而形成超空泡。
它的形成使液体对物体表面的浸湿面积减少,从而大大降低了粘性阻力,达到减阻的效果。
本项目拟通过对已有的射弹结构进行动力特性和流体动力分析,并综合考虑阻力系数、升力系数等各种水动力系数以及应用情况来最终优化结构设计,进一步减小射弹运动时受到的阻力、提高其运动时的稳定性。
2、申请理由本试验小组四人,均来自航天学院飞行器设计与工程专业,在中学时都受过专门的数学竞赛培训,拥有扎实的数学功底和娴熟的研究技能。
通过一年的大学学习,我们熟练掌握了高等数学和线性代数这两项研究中基础性的工具以及必要的工程制图知识,学会了查阅文献的基本方法。
在导师魏英杰教授的指导下,我们查阅了相关的文献,对本课题已经具有了充分的了解和认识。
在与学长们的交流中,我们接触并自学了Matlab、AutoCAD等工具软件。
在接下来的暑假中,我们计划自学相关的专业知识如流体力学和结构动力学等,并自学相关的力学分析软件如Fluent,为接下来的设计优化工作打好基础。
汽车发动机英文参考文献(精选120个最新))
汽车发动机是为汽车提供动力的装置,是汽车的心脏,决定着汽车的动力性、经济性、稳定性和环保性。
下面是搜索整理的汽车发动机英文参考文献,欢迎借鉴参考。
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IOP Conference Series: Earth and Environmental Science,2019,257(1).[116]Guorui Jia,Huanhuan Ren,Dongchang Zhao,Chuan Chen,Rujie Yu,Peng Ge,Shaohui Liu. Numerical Simulation of Multiple Injections on the Combustion of Reactivity Distribution in Automotive Engine[J]. IOP Conference Series: Earth and Environmental Science,2019,252(3).[117]Xitong Zhang,Tao Peng,Fuxin Mao,Ming Cheng. Research on Key Technologies of Integrated Teaching Platform for Automotive Engine ECU Control System[J]. Journal of Physics: Conference Series,2019,1237(4).[118]Huanhuan Ren,Guorui Jia,Dongchang Zhao,Chuan Chen,Rujiex Yu,Peng Ge,Shaohui Liu. Simulation Study of Injection Strategy on the Emission in Automotive Engine[J]. IOP Conference Series: Earth and Environmental Science,2019,252(3).[119]Olufemi Sylvester Bamisaye,Anthony Yinka Oyerinde,Ubong Akpan Essien. Investigation of the Effects of Air-Conditioning System on the Temperature and Speed of Automobile Engine Using Paired T-Test and Regression Analysis[J]. Open AccessLibrary Journal,2019,06(01).[120]Huali Guo,Jia Cui,Guofu Wang,Hongwang Zhao. Analysis and Research on the Teaching Principle of Automotive Engine Based on CDIO Concept[P]. Proceedings of the 2018 International Conference on Sports, Arts, Education and Management Engineering (SAEME 2018),2018.以上就是关于汽车发动机英文参考文献的分享,希望对你有所帮助。
工程流体力学 (6)
Chapter4 Similitude and Dimensional Analysis
3. Viscosity has the dimensions
(a) FL-2T (b) FL-1T-1 (c) FLT-2 (d) FL2T (e) FLT2
4. Select the incorrect completion. Shear forces
(a) zero (b) one-fourth its value when cylinder was full (c) indeterminable; insufficient data (d) greater than a similar case with water as liquid (e) none of these answers
Ⅱ、Single choice questions
Chapter4 Similitude and Dimensional Analysis
1. A fluid is a substance that (a) always expands until it fills any container (b) is practically incompressible (c) cannot be subjected to shear forces (d) cannot remain at rest under action of any shear force (e) has the same shear stress at a point regardless of its motion
(a) can never occur when the fluid is at rest (b) may occur owing to cohesion when the liquid is at rest (c) depend upon molecular interchange of momentum (d) depend upon cohesive forces (e) can never occur in a frictionless fluid, regardless of its
冲击波和气泡作用下舰船结构动态响应的数值模拟
冲击波和气泡作用下舰船结构动态响应的数值模拟王诗平;孙士丽;张阿漫;陈海龙【摘要】针对水下爆炸载荷、瞬态流固耦合效应在舰船水下爆炸数值模拟中的困难,在现有水下爆炸载荷计算模型(Geers and Hunter)的基础上,结合边界元法,修正水下爆炸气泡载荷计算方法.针对用二阶双渐近法(the second-order doubly-asymptotic approximation,DAA2)在处理低频大幅运动流固耦合问题时的局限性,提出非线性双渐近法(nonlinear doubly-asymptotic approximation,NDAA),计入了舰船大幅低频运动、自由面效应等非线性因素,并与结构有限元程序相结合,形成一套适合于工程应用研究的舰船水下爆炸数值模拟程序.数值模拟结果与实验结果的平均误差在16.8%左右,说明NDAA方法可为冲击波和气泡对舰船结构毁伤数值模拟提供参考.%Aimed at the difficulties of underwater explosion load and instantaneous fluid-structure interaction in the numerical simulation of dynamic response of warship structures, based on the Geers-Hupter model, a modified model for calculating the underwater explosion bubble load was proposed by combining with the boundary element method. To overcome the shortcoming of the second-order doubly-asymptotic approximation (DAA2) method in treating the fluid-structure interaction with low frequency and large amplitude motion, a nonlinear double asymptotic approximation (NDAA) method was presented by considering the nonlinear factors such as the violent low-frequency response of the warship and its free surface effect. And a code was developed by combining the presented NDAA method with the finite element code to numerically investigate the dynamic response of warship structuressubjected to underwater explosion Shockwaves and bubbles. The mean error between numerical and experimental vertical vibration velocities at the different positions is about 16. 8% , and it displays that the presented NDAA method is feasible.【期刊名称】《爆炸与冲击》【年(卷),期】2011(031)004【总页数】6页(P367-372)【关键词】爆炸力学;非线性双渐近法;边界元法;舰船;水下爆炸;冲击波;气泡【作者】王诗平;孙士丽;张阿漫;陈海龙【作者单位】哈尔滨工程大学船舶工程学院,黑龙江哈尔滨150001;哈尔滨工程大学船舶工程学院,黑龙江哈尔滨150001;哈尔滨工程大学船舶工程学院,黑龙江哈尔滨150001;哈尔滨工程大学船舶工程学院,黑龙江哈尔滨150001【正文语种】中文【中图分类】O382.1水下爆炸主要包括冲击波和气泡[1-13],通常冲击波对舰船结构造成严重的局部毁伤,气泡对舰船造成总体和局部双重毁伤。
泰勒锥、界面湍动、冲击波等物理现象;
泰勒锥、界面湍动、冲击波等物理现象;泰勒锥、界面湍动和冲击波都是一些常见的物理现象,它们在自然界和工程应用中都具有重要的意义。
本文将分别对这些物理现象进行介绍,并提供相关的参考内容。
一、泰勒锥(Taylor Cone)泰勒锥是在电喷雾等现象中观察到的一种形态。
当液体被高电场作用下从尖端或小孔中喷射时,由于电场的强烈作用,液体表面会变得不稳定并形成一个尖锥形。
泰勒锥有着尖锐的尖端和弯曲的边缘,液体从尖锥的尖端喷出。
该现象最早由英国物理学家泰勒(G. I. Taylor)于1964年发现,并用于解释电喷雾等领域的现象。
泰勒锥的形成和演化过程涉及了电场、表面张力、离子溶液等多个因素的作用,其研究对于理解电喷雾的机理和应用具有重要意义。
参考内容:1. Suong, N. & Wang, Y. Experimental investigation of electrohydrodynamic jetting and the formation of Taylor cones from sharp needles. Journal of Colloid and Interface Science, 99(1), 56-78 (1984).2. Lin, J. et al. Electrohydrodynamic cone-jet breakup: Effects of viscosity and electric conductivity. Physics of Fluids, 23(5), 052101 (2011).3. Bazylewski, P. et al. Electric field enhanced fluid flow near the apex of a Taylor cone. Physical Review Letters, 117(4), 044502 (2016).二、界面湍动(Interfacial Turbulence)界面湍动是指在两个不同的流体(气体和液体、液体和液体等)交界处形成湍流的现象。
case studies in thermal engineering参考文献缩写
case studies in thermal engineering参考文献缩写以下是几个关于热工程的案例研究的参考文献缩写例子:1. DBS: Gharehkhani, Samira, and Matteo Bortolini. "Exergy analysis of a proton exchange membrane fuel cell system." Energy 36.4 (2011): 2119-2129.2. JES: Wang, Tao, and Ruzhu Wang. "Performance characteristics of an adsorption refrigeration system using activated carbon-R134a pair." Applied Thermal Engineering 27.5-6 (2007): 992-998.3. JFE: Tavanaie, Mohammad Ali, Mohammad Haji-Sheikh, and Ali A. Rownaghi. "Experimental investigation of the effects of internal ribs on heat transfer and pressure drop in a rectangular channel." Journal of Fluids Engineering 130.7 (2008): 071702.4. AEE: Yu, Zhibin, et al. "Effect of saline water on the performance of a solar thermoelectric generator with heat pipes." Applied Energy 290 (2021): 116586.5. IJV: Waltman, Sarah W., and Jacqueline F. Roen. "Thermal performance study of single-loop and dual-loop liquid flat plate solar collectors." International Journal of Energy Research 35.10 (2011): 847-859.请注意,这里提供的仅仅是一些例子,具体要根据您所参考的具体文献来确定正确的缩写。
多变量分析名词解释
1.variable變項:依不同數值或類別出現或變動的一種屬性,如性別(類別變動代表不同的性別)年齡、收入(依數值的變動代表不同的年齡與收入)。
2.independent variable自變項:指研究者能加以系統化操弄或安排變項,此種變項常是研究者懷疑造成某種事件或現象的「因」。
3.dependent variable依變項:指隨著自變項之改變發生改變,而無法加以操弄的變項,也是研究者所要觀察或蒐集之受試者的行為數據。
4.intervening variable中介變項:指介於自變項和依變項之間一切對依變項會產生作用的內在心理歷程而言,例如受訪者的意願、態度、動機與興趣等。
tent variable(潛在變項):6.measurement scale測量尺度:nominal variable, ordinal variable, internal variable andratio variable。
7.nominal variable名義變項:指利用名稱或數值來分辨人、事、物之類別的變項。
8.ordinal variable次序變項:指可利用數值或名稱來加以排序或賦予等第的變項。
9.internal variable等距變項:指可以賦予名稱(類別)並加以排序,且可以計算出其間差異之大小量的變項。
10.ratio variable等比變項:指可以賦予名稱、排序,並計算出差異大小量,還可找出某比率(倍數)等於某比率的變項。
11.variance變異數:一組數值離均差平方和之平均數。
12.control group控制組:指不接受實驗處理的受試者。
13.experimental group實驗組:指接受實驗處理的受試者。
14.randomization隨機化:指受試者被選中的機率是均等的。
15.matching比對配合:要設法使某兩組在實驗之前相同或相等的方法。
16.systematic bias系統性偏差:研究工具無法依目的正確的測量。
专题74 女航天员王亚平与中国航天人-备战2022中考英语阅读理解热点话题体裁分类训练
备战2022中考英语阅读理解热点话题+体裁分类训练(中考真题+各地模拟题)专题74 女航天员王亚平与中国航天人(2022·重庆南开中学一模)Wang Yaping, 41, became China’sfirst female spacewalker on Nov. 7th evening when she took part in the Shenzhou XIII mission’s first extravehicular activity (舱外活动) with Zhai Zhigang.The extravehicular operation began at 6:51 p.m. when Zhai opened a gate. By midnight, they had climbed up the station’s robotic arm and used it to practice extravehicular activity and rescue operations with Ye Guangfu remaining inside the station to control and support the spacewalk.The spacewalk was expected to further check the robotic arm’s capabilities (能力), examine the safety and performance of support devices (设施) in an extravehicular task and test a new type of extravehicular suit, because they would have one or two more spacewalks in the coming months.A native of Shandong province and mother of a 5-year-old girl, Wang Yaping joined the People’s Liberation Army Air Force in August 1997. In March 2012, she was part of the backup crew (后备人员) for the Shenzhou IX mission, and in June 2013, she took part in the Shenzhou X mission, which lasted nearly 15 days. She is the second Chinese woman to have flown in space.During the Shenzhou X flight, Wang gave China’s first space-based lecture inside the Tiangong I experimental module to more than 60 million Chinese students at about 80,000 schools across the country. Many students were encouraged after watching Wang’s lecture.▲ , they should experience a lot of pain that most people can’t stand and keep training all the time.She is such a great woman that people call her “the most beautiful astronaut”. Wish her together with the other astronauts to return safely in a few months.1.There are ________ astronauts in the Shenzhou XIII mission.A.two B.three C.four D.five 2.According to the passage we can know that ________.A.Wang and Ye went out of the spaceship on Nov. 7th eveningB.The extravehicular activity was for several reasonsC.Wang Yaping is the second woman to have flown in spaceD.Wang gave a space-based lecture during the Shenzhou XI flight3.Which of the following sentences can be put in the “▲”? A.However, to become an astronaut is not easyB.Because to give a lecture in space is coolC.So they want to become astronauts in the futureD.Though they may know nothing about space4.The best structure of this passage may be _________.A.B.C.D.(2022·湖南·长沙市北雅中学一模)Waving (向……挥手) her 5-year-old daughter goodbye, Wang Yaping, together with Zhai Zhigang and Ye Guangfu, went into space aboard the Shenzhou XIII on Oct. 16.The 41-year-old Wang became the first female astronaut to enter Tiangong space station. During their six-month stay, Wang, alongside Zhai and Ye, will do experiments and set up robotic arms. Wang will also do the first spacewalk by a Chinese woman, reported Xinhua. Wang’s space dream started in 2003, when China sent its first astronaut Yang Liwei into space. She told herself, “China now has a male astronaut. When will there be a female one?” At that time, Wang was a pilot in the Chinese army.After having safe flights for 1,600 hours over nine years, Wang was a strong candidate to become an astronaut in 2010. She pushed herself hard, getting the same training as men, including the pull-ups (引体向上) and barbells (杠铃). “The space environment won’t change because you are a woman,” she told Xinhua.The hardest part is the high-G training. Sitting in a spinning (旋转的) machine, Wang would become blind for a while because her brain was short of blood. “There’s a red button (按钮),” said Wang. “If you can’t bear it, you can press it to stop.” But Wang never used it. “There is no such red button in my heart.”That strong spirit finally led to realizing her dream in 2013. She joined the team for the Shenzhou X mission (任务).Wang said that as astronauts, women have their own advantages. “Women tend (倾向于) to be more patient and can better deal with loneliness. Women’s hearts are also easier to adapt to the weightless (失重的) environment, making them more suitable for long-term missions.”Retired NASA astronaut Catherine Coleman sent a greeting to Wang before the Shenzhou XIII trip. Coleman said, “When you look out the window and see the stars and the earth, billions of women will be looking out that window with you.” Wang carries the spirit of every young woman who dreams of something big.5.Wang won’t _______ during the six-month space stay.A.do experiments B.set up robotic arms C.look after her daughter 6.Which of the following is NOT TRUE according to the passage?A.Wang had few difficulties in the training.B.Wang is the first female astronaut to do the spacewalk in China.C.According to Coleman, Wang sets an example for women.7.According to the passage, the underlined word “candidate” in Paragraph 3 means_______.A.候选人B.参赛者C.考生8.According to Wang, a female astronaut has advantages of _______.a. more patienceb. less weightc. more problem-solving skillsd. better ability to deal with lonelinessA.ad B.cd C.bc9.What’s the best title of the passage?A.Long-term Space Missions B.The Space Dream C.Tiangong Space Station (2021·江苏无锡·九年级期末)On Nov 8, Wang Yaping, a female taikonaut of Shenzhou XIII mission, became China’s first and the world’s 16th female space walker. The expected six-month journey in space has left many curious about the differences between male and female astronauts, especially in terms of performing extravehicular (舱外的) activities (EV As). Despite (即使) physical challenges, female astronauts have unique (独一无二的) advantages.Understanding between astronauts is very important for carrying out EV As, which is based on excellent communication skills. Women are superior (更好的) in communication and language expression, and this helps female astronauts do extravehicular activities, according to Yang Yuguang, vice chair of Space Transportation Committee of the International Astronautical Federation.Men and women are different in body size, which also gives women unique advantages for spacewalks. “Their generally smaller size is an advantage, as women will be able to control their weight better and perform a wider variety of tasks,” Pang told China Daily.Women in general weigh less, eat less food, consume less oxygen (氧气), and therefore required less fuel (燃料) to get into space. A taikonaut must weigh between 55 kilograms and 70 kilograms to fit in the cabin of spacecraft and consume less fuel, according to CGIN.A different body shape requires a different spacesuit. A tailor-made spacesuit was prepared for Wang’s extravehicular activities, which was lighter than the males’. Designers optimized the pattern of this spacesuit in the lower limb (下肢) area to make it more suitable for astronauts with slimmer figures.According to Pang, many studies have found that female astronauts are more suitable for space missions, and have advantages over male astronauts in qualities such as attention to detail and thinking comprehensively (全面地).Men tend to excel in shorter-term, goal-oriented (目标导向的) situations while women are better in longer-term habitation-type (居住类) circumstances, according to National Geographic.Women’s participation in EV As is an integral (不可缺少的) part of space missions, and we are witnessing history thanks to Wang’s bravery, according to Yang.10.What do we know about Wang’s extravehicular activities?A.She is the first ever female space walker.B.The mission was planned to show gender equality.C.She performed some tasks that her male partners couldn’t do.D.The spacesuit she wore was specially designed.11.What does the underlined word “optimize” mean in this passage?A.make something better B.make something worseC.make something colourful D.make something colourless 12.Which of the following is an advantage females have over male astronauts? A.Females have better communication skills.B.Females deal with goal-oriented situations better than males.C.Female bodies are stronger and more flexible.D.Females can adapt to space more quickly.13.What’s the main idea of the article?A.The challenges female astronauts face during a spacewalk.B.The importance of females doing extravehicular activities.C.The advantages of females doing extravehicular activities.D.The preparations for the females to carry out space mission.(2022·安徽滁州·一模)Wang Yaping, 42, became China’s first female (女性的) spacewalker on the evening of Nov. 7th when she took part in the Shenzhou XIII mission’sfirst extravehicular activity (舱外活动) with Zhai Zhigang.The extravehicular activity began at 6:51 p.m. when Zhai opened a gate. By midnight, they had climbed up the station’s robotic arm and used it to practice extravehicular activity, with Ye Guangfu remaining inside the station to control and support the spacewalk.The spacewalk was expected to further check the robotic arm’s abilities, inspect the safety and performance of support devices (设备) in an extravehicular task and test a new type of extravehicular clothes, because they would have one or two more spacewalks in the coming months.As a native of Shandong Province and mother of a 6-year-old girl, Wang joined the Chinese People’s Liberation Army Air Force in August 1997. In June 2013, she took part in the Shenzhou X mission, which lasted nearly 15 days. She is the second Chinese woman to have flown in space.During the Shenzhou X fight, Wang gave China’s first space-based class inside the Tiangong-I to more than 60 million Chinese students across the country. Many students were encouraged after watching Wang’s class. However, ________.They have to experience a lot of pain that most people can’t stand and keep training all the time.She is such a great woman that people call her “the most beautiful astronaut”. 14.What does the underlined word “inspect” in Paragraph 3 mean in Chinese?A.训练B.检查C.经历D.购买15.What purpose isn’t included in the extravehicular task?A.To check the robotic arm’s abilities.B.To climb up the station’s robotic arm.C.To examine the safety of support devices.D.To test a new type of extravehicular clothes.16.Which of the following can be put into the “________”?A.it is not easy to be an astronautB.to give a class in space is coolC.students may know nothing about spaceD.students promise to be astronauts in the future17.What can we learn about Wang Yaping from the test?A.Wang is China’s first spacewalker to experience an extravehicular activity.B.Wang took part in the Shenzhou X mission in August 1997.C.Wang gave a space-based class inside the Tiangong-I in 2013.D.Wang took part in the Shenzhou XIII mission by herself.(2022·广东·珠海市文园中学一模)Three Chinese astronauts Wang Yaping, Zhai Zhigang and Ye Guangfu gave a space lecture on Dec. 9th 2021“Hello, everyone! Welcome to Tiangong Class.” With this greeting, a special lecture began on Tiangong space station about 400 kilometers above Earth on Dec. 9th 2021.Lasting for about an hour, the space lecture was broadcast live to millions of students. Three astronauts from the Shenzhou XIII crew hosted the lecture, introducing how they live and work on the space station and doing some interesting experiments that can only be done in space.This is the second live space lecture in China. In 2013, with the assistance of two other Shenzhou X crew members, Wang hosted the country’s first live space lecture to over 60 million schoolchildren across China.More space to teachCompared with the class eight years ago, this year’s space lecture is greatly different. The “classroom” is bigger. Instead of Tiangong I experimental module(实验舱), this year Wang had the space lecture in the Tianhe space core module(核心舱), which is the biggest spacecraft developed by China.Technological developmentThe quality of space to ground communication is also much improved.The space lecture eight years ago sometimes faced the challenges of the video freezing and an unclear picture, but this year’s lecture is different.With the help of China’s Tianlian satellites, the transmission(传输) speed has been highly increased and the whole live broadcast has run smoothly. These changes show that Chinese aerospace industry has made great progress in the past eight years.More coursesAlong with the technological progress, this year’s space lecture discussed more areas inscience. Eight years ago, students could watch the interesting phenomenon of weightlessness in space on TV. But this year, biology was added.Though these space lectures showed various topics, the aim behind the lectures has never changed. The space lectures aim to “spread knowledge about manned spaceflights and light up the interests for science among young people”. The spirit of science in the youth is an important driver of the progress of mankind. The space lecture makes young Chinese people take pride in our country as they see the rapid development of our space technology. 18.How far is Tiangong space station from the earth?A.2400 kilometers B.1800 kilometers C.400 kilometers D.600 kilometers 19.Who gave the space lecture on Dec 9th 2021?A.Wang Yaping, Zhai Zhigang and Ye GuangfuB.Wang Yaping, Yang Liwei and Liu yangC.Wang Yaping, Zhai Zhigang and Yang LiweiD.Wang Yaping, Zhai Zhigang and Nie Haisheng20.Which of the following is false according to the passage?A.The spacecraft where the astronauts gave the lecture on December 9th, 2021 is bigger than before.B.We could watch the whole live broadcast clearly on December 9th, 2021 because of technological development.C.Chinese aerospace industry has achieved a lot in the past eight years.D.We can learn as much knowledge as before from the space lecture.21.What’s the meaning of the underlined word “phenomenon”?A.原理B.数据C.现象D.表演22.What can we learn from the passage?A.The space lecture can not attract young people to study science.B.The purpose of the space lecture is to spread knowledge about manned spaceflights. C.All people in the world will be proud of being Chinese when they know the success of our country’s space technology.D.Wang Yaping hosted the country’s first live space lecture for the first time on December 9th 2021.(2022·山东济南·一模)“Hello, everyone! Welcome to Tiangong Class.” A special lecture began on Tiangong space station about 400 kilometers above Earth on Dec. 9, 2021.Lasting for about an hour, the space lecture was given to millions of students. Three astronauts, Zhai Zhigang, Wang Yaping and Ye Guangfu showed how they live and work on the space station and did some interesting experiments. This space lecture was greatly different from the one 8 years before. The “classroom” was bigger. It was China’s first extraterrestrial (地球外的) lecture series.Plants in space —The lab of the space station has many conditions that the Earth lab does not have, such as the weightless environment. The important jobs for astronauts included cell (细胞) observation and “feeding” plant life. In the lecture, Ye showed experiments about cell growth in a weightless environment. As early as 2016, Chinese scientists tried to grow rice on the Tiangong II space lab to study how plants grow without an Earth-like environment.Use it or lose it —The human body grows with the pull of Earth’s gravity (重力). But in space, our bones and muscles (肌肉) don’t need to support our body’s weight. This will cause bone and muscle loss. Astronauts can lose up to 20 percent of their muscles after a couple of weeks. That is dangerous for astronauts because they will be too weak to work.Astronauts have different ways to precent this. Zhai introduced a special uniform called “penguin suit”. Wearing it, astronauts use their muscles to stretch the bands in it. This keeps their muscles strong. Wang also showed students how she walked on a machine, and rode a bicycle. Astronauts exercise like that every day to prevent muscle loss.Young voices -Students were really interested in the lecture. A 13-year-old boy from Tianjin said, “The most exciting thing I learned is that astronauts “fly” all the time because there is no gravity.”Yin Peixin, an 11-year-old girl from Hubei said, “My favorite experiment is the one with the table tennis ball. Wang put the ball into a glass of water, but the ball didn’t float (漂浮). This was so magical!”Look! It was an eye-opening experience that would light up students’ interest in science, wasn’t it?23.What do we know about the 2021 space lecture from Paragraph 1?A.It was similar to the one 8 years before.B.It took place half a year ago.C.It showed astronauts’ life and work.D.It was given in a smaller classroom. 24.From Paragraph 2, what did Ye want to show the students?A.How cell grows on the space station.B.How rice is grown on the Tiangong lab.C.How to better grow space plants.D.How to study the rules of plant growth. 25.What does the part “Use it or lose it” mainly talk about?A.The reasons for muscle loss.B.Muscle loss in space and ways to stop it.C.The necessity of daily exercise.D.The advantages of “penguin suit”. 26.According to the article, which is NOT TRUE about the 2021 space lecture?A.The influence is far more than one hour.B.It showed the differences without gravity.C.It interested the kids with the experiments.D.It first introduced plant growth in space. 27.What’s the writer’s purpose of writing this article?A.To light up people’s interest in space experiments.B.To explain the importance of studying plants in space.C.To introduce the space lecture by Chinese astronauts.D.To make scientific knowledge popular among readers.(2022·重庆南开中学一模)Wang Yaping, together with Zhai Zhigang and Ye Guangfu, went into space aboard the Shenzhou XIII on October 16th, 2021. The 41-year-old Wang became the first Chinese female astronaut(女航天员)to enter Tiangong space station.Wang’s space dream started in 2003, when China sent its first astronaut Yang Liwei into space. At that time, Wang was a pilot in the Chinese army. After having safe flights for 1,600 hours over nine years, Wang was a strong candidate(候选人)to become an astronaut in 2010. She pushed herself hard, getting the same training as men. “The space environment won’t change because you are a woman,” she told Xinhua.The hardest part is the high-G training. Sitting in a spinning(旋转的)machine, Wang would become blind for a while because her brain was short of blood. “There’s a red button (按钮)”, said Wang. “If you can’t stand it, you can press it to stop.” But Wang never used it. “There is no such red button in my heart.” That strong spirit finally made her dream come true in 2013. She joined the team for the Shenzhou X mission(任务).Wang said that as astronauts, women have their own advantages(优势). “Women may be more patient and can better deal with loneliness. Women’s hearts are also easier to adapt to the weightless environment, making them more suitable for long-term missions.”Wang Yaping went a long way before becoming the first woman to enter the Tiangongspace station. She sets a good example for all women who dream of going to space. 28.Wang’s words mean _________ in Paragraph 2.A.The space environment is easy to change.B.Only men can go to space station in the world.C.Both male and female astronauts can go to space.D.Men and women will face the same difficulties in space.29.The underlined word “adapt” in the fourth paragraph probably means ________ . A.合适B.改编C.适应D.接受30.Which of the following is TRUE?A.Wang is the first female astronaut in the world.B.Wang dreamed of being an astronaut in 2003.C.It was a short time before Wang made her dream come true.D.Wang pressed the red button when she became blind after the high-G training. 31.What advantages does a female astronaut have according to Wang?a. More patience.b. Less weight.c. More problem-solving skills.d. Better ability to deal with loneliness.A.ad B.ab C.bc D.bd (2022·广东·红岭中学八年级期末)Wang Yaping, together with Zhai Zhigang and Ye Guangfu, went into space aboard the Shenzhou XIII on October 16th. The 41-year-old Wang became the first female astronaut (女航天员) to enter Tiangong space station.Wang’s space dream started in 2003, when China sent its first astronaut Yang Liwei into space. At that time, Wang was a pilot in the Chinese army. After having safe flights for 1,600 hours over nine years, Wang was a strong candidate to become an astronaut in 2010. She pushed herself hard, getting the same training as men. “The space environment won’t change because you are a woman,” she told Xinbua.The hardest part is the high-G training. Sitting in a spinning (旋转的) machine, Wangwould become blind for a while because her brain was short of blood. “There’s a red button (按钮), said Wang.” If you can’t bear it, you can press it to stop.” But Wang never used it. “There is no such red button in my heart.” That strong spirit finally made her dream come true in 2013. She joined the team for the Shenzhou X mission.Wang said that as astronauts, women have their own advantages (优势). “Women may be more patient and can better deal with loneliness. Women’s hearts are also easier to adapt (适应) to the weightless environment, making them more suitable for long-term missions.”Wang Yaping went a long way before becoming the first woman to enter the Tiangong space station. She sets a good example for all women who dream of going to space. 32.What do Wang’s words mean in Paragraph 2?A.The space environment is easy to change.B.Only men can go to space.C.Men and women will face the same difficulties in space.D.Both male and female astronauts can go to space.33.What does the underlined word candidate in the second paragraph probably mean? A.成员B.伙伴C.候选人D.飞行员34.Which of the following is TRUE?A.Wang is the first female astronaut in the world.B.Wang dreamed of being an astronaut in 2003.C.It was a short time before Wang made her dream come true.D.Wang pressed the red button when she became blind after the high-G training. 35.What advantages does a female astronaut have according to Wang?a. More patience.b. Less weight.c. More problem-solving skills.d. Better ability to deal with loneliness.A.ad B.ab C.bc D.bd36.What can we learn from Wang’s story?A.Never too old to learn.B.Well begun is half done.C.Old habits die hard.D.Nothing is difficult if you put your heart into it.(2022·辽宁沈阳·七年级期末)“I feel great!” said Wang Yaping when she came out of the Tiangong space station, waving back to Earth.On Nov. 7, the 41-year-old made history. She became China’s first woman space-walker! Wang, together with astronaut (宇航员) Zhai Zhigang did a 6.5-hour spacewalk. Since 1984, only 16 women(including Wang) around the world have ever done spacewalks, according to Global Times. But woman space-walkers are very important to space. “Humans may live on other planets someday. If we don’t let women take part in this, we can’t prepare well. We need to study how women’s bodies change in space. That’s why Wang’s spacewalk is important,” a scientist told Global Times.Women are more patient and careful. Women can better deal with loneliness. Women have better skills to talk with others. It’s easier for women’s hearts to work well in the environment without gravity. So it’s easier for them to stay longer in space.37.How did Wang Yaping feel when she walked out of the station?A.Cold.B.Tired.C.Great.D.Worried. 38.What can we learn about the spacewalk on Nov. 7?A.It was the world’s first woman spacewalk.B.It lasted for more than 6 hours. C.Wang Yaping did the spacewalk alone.D.It made Wang Yaping very sick. 39.Women astronauts help us _________.A.live better on EarthB.know more about men astronautsC.better prepare for the future lifeD.study how men astronauts’ bodies change in space40.What is the last paragraph (段落) mainly about?A.Why Wang’s spacewalk is important.B.When humans can live on other planets.C.Why astronauts do spacewalks.D.How woman bodies change in space.(2021·山东青岛·九年级期末)Chinese astronauts Zhai Zhigang, Wang Yaping and Ye Guangfu gave a science lecture(讲座) from China’s space station to students on Earth on December 9th, 2021. The class began at 3:40 p.m., with a total of 1,420 students attending the lecture from five classrooms across China. The primary classroom is in China Science and Technology Museum. Classrooms have also been set up in Nanning, Wenchuan, Hong Kong and Macao. Tens of millions of students across China watched the hour long televised event.Shenzhou-13 members gave the students a tour of the living and working areas of thespace station. They showed the students how to increase their strength with their exercise equipment(设备), introduced a specially designed spacesuit and performed experiments. Ye, who is on his first spaceflight, showed how he moved in the weightless environment. They also answered questions from students during the lecture.It was the first lecture of the Tiangong Class. More lectures will be held and presented by Chinese astronauts. Such activities are held to spread knowledge and encourage a love for science among young people.Shi Yi, a physics teacher in Beijing, said the space lecture was an eye-opening experience that would ignite(点燃) students’ interest in science.Wang Yihan, a fifth-grade student, said, “The experiments really surprised me. I have great interest in spaceflight and would like to take part in our country’s space program in the future.”Vincent Wong, headmaster of Hong Kongs Pui Kiu College, said the event gave Hong Kong students an opportunity to communicate with the astronauts. “It also helped to strengthen their national identity(认同) as they saw the rapid development of our country’s space technology,” he said.41.The astronauts held the live class ______.A.at the television stationB.in five classrooms across ChinaC.on China’s space stationD.in China Science and Technology Museum42.What can we know about the astronauts from the second paragraph?A.They design a special spacesuit.B.They take exercise to lose weight. C.They are in space for the first time.D.They show how they live and work. 43.The underlined word “presented” in paragraph 3 means ______.A.given B.driven C.gifted D.watched 44.Why does the writer mention the three viewers in the last three paragraphs?A.To spread knowledge to readers.B.To show that the class is meaningful. C.To voice viewers different ideas.D.To explain why viewers attend the class. 45.Where is the passage probably from?A.A science fiction.B.A history book.C.An art magazine.D.A news website.参考答案:1.B2.C3.A4.D【解析】【导语】本文是一篇说明文。
换热器热力学计算中平均温差计算方法
路广遥等:换热器热力学计算中平均温差计算方法
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在小流量时应尽量避免使用 LMTD 法; 随着雷诺 数的增加,二者区别越来越小,在紊流区,水平 流动时,z>98.1%;竖直流动时,z>96.9%,二者 相差不大,所以大流量时采用两种数据处理方法 所得结果相近。孙中宁[7]通过计算分析也认为, 大流量时,当进出口温差相差一倍,对数平均温 差与算术平均温差相差 3.82%。其计算结果与本 实验结果接近。从图 2、图 3 可以看出,在大流 量时采用这两种数据处理方法相差不大,其差别 在工程中完全可以忽略。 由于壁温测量比较繁琐, LMTD 较简单易行,所以,在工程计算中可以采 用 LMTD 来分析紊流区内的对流换热特性。 Ram[9]在进行理论分析的基础上得出了对数 平均温差的近似算法:
1 引
言
换热器是工业领域中应用十分广泛的热量交 换设备,在换热器的热工计算中,常常利用传热 方程和传热系数方程联立求解传热量、 传热面积、 [1 , 2] 分离换热系数和污垢热阻等参数 。温差计算 经常采用对数平均温差法(LMTD)和效能-传热单 元数法 (ε-NTU) ,二者原理相同。不过,使用 LMTD 方法需要满足一定的前提条件;如果不满 足这些条件,可能会导致计算误差。刘凤珍对低 温工况下结霜翅片管换热器热质传递进行分析, 从能量角度出发,由换热器的对数平均温差引出 对数平均焓差,改进了传统的基于对数平均温差 的结霜翅片管换热器传热、传质模型[3]。Shao 和 Granryd 通 过 实 验 和 理 论 分 析 认 为 , 由 于 R32/R134a 混合物温度和焓值为非线性关系,采 用 LMTD 法会造成计算误差;当混合物的组分 不同时,所计算的换热系数可能偏大,也可能偏 小[4],他们认为,采用壁温法可使计算结果更精 确。王丰利用回热度对燃气轮机内流体的对数平 均温差和换热面积进行计算[5]。Ziegler 定义了温 度梯度、驱动平均温差、热力学平均温差,认为 判定换热效率用热力学平均温差,用对数平均温 差判定传热成本的投入,而算术平均温差最易计 算;当温度梯度足够大时,对数平均温差、算术
小试实验阶段 英语
小试实验阶段英语The Importance of the Pilot Experiment Stage.The pilot experiment stage is often overlooked in the scientific process, yet it plays a crucial role in the overall success of a research project. This phase serves as a critical bridge between theory and practical application, allowing researchers to test their hypotheses under controlled conditions before embarking on larger, more costly experiments.The primary purpose of the pilot experiment is to assess the feasibility and validity of the proposed research methodology. This includes evaluating the effectiveness of the chosen experimental design, measuring instruments, and data collection techniques. Through this stage, researchers can identify potential weaknesses in their methods and make necessary adjustments to ensure the reliability and accuracy of their findings.Moreover, the pilot experiment allows researchers to estimate the resources required for the full-scale study. This includes everything from materials and equipment to personnel and time. By carefully monitoring the resources used during the pilot stage, researchers can develop a more accurate budget and timeline for their larger experiment.Additionally, the pilot experiment provides valuable insights into potential ethical and safety considerations. This is particularly important in fields such as medicine and biotechnology, where experiments can have significant implications for human health and safety. By conducting a pilot study, researchers can identify any potential risks and develop appropriate safety measures to protect both their subjects and themselves.The data collected during the pilot experiment also serves as a valuable source of information for refining the research question and hypotheses. As researchers analyze the data, they may identify new patterns or trends that suggest modifications to their original research questions. These insights can lead to a more focused and targetedfull-scale study.Furthermore, the pilot experiment stage is an opportunity for researchers to gain practical experience with their methodology. This hands-on experience can be invaluable in helping researchers identify and correct any mistakes they may have made in their theoretical planning. By conducting the pilot study, researchers can gain confidence in their methods and feel more prepared for the challenges of the larger experiment.In summary, the pilot experiment stage is a crucial component of the scientific process. It allows researchers to test their hypotheses under controlled conditions, estimate the resources required for the full-scale study, identify potential ethical and safety considerations, refine their research questions and hypotheses, and gain practical experience with their methodology. By investing the time and resources necessary to conduct a thorough pilot study, researchers can increase the likelihood of success in their larger experiment and make a significant contribution to their field of study.。
电气控制英文参考文献(精选120个最新)
改革开放以来,随着我国工业的迅速发展和科学技术的进步,电气控制技术在工业上的运用也越来越广泛,对于一个国家的科技水平高低来说,电气控制技术水平是一项重要的衡量因素.电气控制技术主要以电动机作为注重的对象,通过一系列的电气控制技术,买现生产或者监控的自动化.下面是搜索整理的电气控制英文参考文献,欢迎借鉴参考。
电气控制英文参考文献一: [1]Laiqing Xie,Yugong Luo,Donghao Zhang,Rui Chen,Keqiang Li. Intelligent energy-saving control strategy for electric vehicle based on preceding vehicle movement[J]. Mechanical Systems andSignal Processing,2019,130. [2]F.N. Tan,Q.Y. Wong,W.L. Gan,S.H. Li,H.X. Liu,F. Poh,W.S. Lew. Electric field control for energy efficient domain wallinjection[J]. Journal of Magnetism and Magnetic Materials,2019,485. [3]N. Nursultanov,W.J.B. Heffernan,M.J.W.M.R. van Herel,J.J. Nijdam. Computational calculation of temperature and electrical resistance to control Joule heating of green Pinus radiata logs[J]. Applied Thermal Engineering,2019,159. [4]Min Cheng,Junhui Zhang,Bing Xu,Ruqi Ding,Geng Yang. Anti-windup scheme of the electronic load sensing pump via switchedflow/power control[J]. Mechatronics,2019,61. [5]Miles L. Morgan,Dan J. Curtis,Davide Deganello. Control of morphological and electrical properties of flexographic printed electronics through tailored ink rheology[J]. 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Delou,Julia P.A. de Azevedo,Dinesh Krishnamoorthy,Maurício B. de Souza,Argimiro R. Secchi. Model Predictive Control with Adaptive Strategy Applied to an Electric Submersible Pump in a Subsea Environment[J]. IFACPapersOnLine,2019,52(1). [12]Unal Yilmaz,Omer Turksoy,Ahmet Teke. Intelligent control of high energy efficient two-stage battery charger topology forelectric vehicles[J]. Energy,2019,186. [13]Qiuyi Guo,Zhiguo Zhao,Peihong Shen,Xiaowen Zhan,Jingwei Li. Adaptive optimal control based on driving style recognition forplug-in hybrid electric vehicle[J]. Energy,2019,186. [14]Leonid Lobanov,Nikolai Pashсhin. Electrodynamic treatment by electric current pulses as effective method of control of stress-strain states and improvement of life of welded structures[J]. Procedia Structural Integrity,2019,16. [15]Evangelos Pournaras,Seoho Jung,Srivatsan Yadhunathan,Huiting Zhang,Xingliang Fang. Socio-technical smart grid optimization via decentralized charge control of electric vehicles[J]. Applied Soft Computing Journal,2019,82. [16]Guoming Huang,Xiaofang Yuan,Ke Shi,Xiru Wu. A BP-PID controller-based multi-model control system for lateral stability of distributed drive electric vehicle[J]. Journal of the Franklin Institute,2019,356(13). [17]Ioannis Kalogeropoulos,Haralambos Sarimveis. Predictive control algorithms for congestion management in electric power distribution grids[J]. Applied Mathematical Modelling,2020,77. [18]Junjun Zhu,Zhenpo Wang,Lei Zhang,David G. Dorrell.Braking/steering coordination control for in-wheel motor drive electric vehicles based on nonlinear model predictive control[J]. Mechanism and Machine Theory,2019,142. [19]Jiechen Wu,Junjie Hu,Xin Ai,Zhan Zhang,Huanyu Hu. Multi-time scale energy management of electric vehicle model-based prosumers by using virtual battery model[J]. Applied Energy,2019,251. [20]G. Coorey,D. Peiris,T. Usherwood,L. Neubeck,J. Mulley,J. Redfern. An Internet-Based Intervention Integrated with the Primary Care Electronic Health Record to Improve Cardiovascular Disease Risk Factor Control: a Mixed-Methods Evaluation of Acceptability, Usage Trends and Persuasive Design Characteristics[J]. Heart, Lung and Circulation,2019,28. [21]Félice Lê-Scherban,Lance Ballester,Juan C. Castro,Suzanne Cohen,Steven Melly,Kari Moore,James W. Buehler. Identifying neighborhood characteristics associated with diabetes and hypertension control in an urban African-American population usinggeo-linked electronic health records[J]. Preventive Medicine Reports,2019,15. [22]Yuekuan Zhou,Sunliang Cao. Energy flexibility investigation of advanced grid-responsive energy control strategies with thestatic battery and electric vehicles: A case study of a high-rise office building in Hong Kong[J]. Energy Conversion and Management,2019,199. [23]D. Aravindh,R. Sakthivel,B. Kaviarasan,S. MarshalAnthoni,Faris Alzahrani. Design of observer-based non-fragile load frequency control for power systems with electric vehicles[J]. ISA Transactions,2019,91. [24]Augusto Matheus dos Santos Alonso,Danilo IglesiasBrandao,Tommaso Caldognetto,Fernando Pinhabel Maraf?o,Paolo Mattavelli. A selective harmonic compensation and power control approach exploiting distributed electronic converters inmicrogrids[J]. International Journal of Electrical Power and Energy Systems,2020,115. [25]Hay Wong,Derek Neary,Eric Jones,Peter Fox,Chris Sutcliffe. Benchmarking spatial resolution in electronic imaging for potential in-situ Electron Beam Melting monitoring[J]. Additive Manufacturing,2019,29. [26]Yunfei Bai,Hongwen He,Jianwei Li,Shuangqi Li,Ya-xiong Wang,Qingqing Yang. Battery anti-aging control for a plug-in hybrid electric vehicle with a hierarchical optimization energy management strategy[J]. Journal of Cleaner Production,2019,237. [27]N. Samartin-Veiga,A.J. González-Villar,M.T. Carrillo-de-la-Pe?a. Neural correlates of cognitive dysfunction in fibromyalgia patients: Reduced brain electrical activity during the execution ofa cognitive control task[J]. NeuroImage: Clinical,2019,23. [28]Masato Nakaya,Shinta Watanabe,Jun Onoe. Control of electric, optical, thermal properties of C 60 films by electron-beam irradiation[J]. Carbon,2019,152. [29]R. Saadi,M.Y. Hammoudi,O. Kraa,M.Y. Ayad,M. Bahri. A robust control of a 4-leg floating interleaved boost converter for fuel cell electric vehicle application[J]. Mathematics and Computers in Simulation,2019. [30]Frederik Banis,Daniela Guericke,Henrik Madsen,Niels Kj?lstad Poulsen. Supporting power balance in Microgrids with Uncertain Production using Electric Vehicles and Indirect Control ? ? This work has been supported by ENERGINET.DK under the project microgrid positioning - uGrip and the CITIES project.[J]. IFAC PapersOnLine,2019,52(4). 电气控制英文参考文献二: [31]Huijuan Luo,Jinpeng Yu,Chong Lin,Zhanjie Liu,Lin Zhao,Yumei Ma. Finite-time dynamic surface control for induction motors with input saturation in electric vehicle drive systems[J]. Neurocomputing,2019. [32]Peter K. Joseph,D. Elangovan,G. Arunkumar. Linear control of wireless charging for electric bicycles[J]. Applied Energy,2019,255. [33]Yu Congyang,Zhu Dequan,Wang Chaoxian,Zhu Lin,Chu Tingting,Jen Tien-Chien,Liao Juan. Optimizing Electric Adjustment Mechanism Using the Combination of Multi-body Dynamics and Control[J]. Procedia Manufacturing,2019,35. [34]Hussein Termous,Xavier Moreau,Clovis Francis,Hassan Shraim. Effect of fractional order damping control on braking performancefor electric vehicles ? ? This work was supported by the Lebanese research program and the AUF-CNRSL-UL program.[J]. IFAC PapersOnLine,2019,52(5). [35]Manuel Schwartz,Florian Siebenrock,S?ren Hohmann. Model Predictive Control Allocation of an Over-actuated Electric Vehicle with Single Wheel Actuators[J]. IFAC PapersOnLine,2019,52(8). [36]Di Wu,Nikitha Radhakrishnan,Sen Huang. A hierarchical charging control of plug-in electric vehicles with simpleflexibility model[J]. Applied Energy,2019,253. [37]Abhishek Nayak,Rubi Rana,Sukumar Mishra. Frequency Regulation by Electric Vehicle during Grid Restoration using Adaptive Optimal Control[J]. IFAC PapersOnLine,2019,52(4). [38]Nicolò Robuschi,Mauro Salazar,Pol Duhr,FrancescoBraghin,Christopher H. Onder. Minimum-fuel Engine On/Off Control for the Energy Management of a Hybrid Electric Vehicle via Iterative Linear Programming ? ? We thank Ferrari S.p.A. for supporting this project.[J]. IFAC PapersOnLine,2019,52(5). [39]Anas A. Ahmed,M.R. Hashim,Marzaini Rashid. Control of the structural, electrical and optical properties of spin coated NiO films by varying precursor molarity[J]. Thin Solid Films,2019,690. [40]Wilco van Harselaar,Niels Schreuders,Theo Hofman,Stephan Rinderknecht. Improved Implementation of Dynamic Programming on the Example of Hybrid Electric Vehicle Control[J]. IFACPapersOnLine,2019,52(5). [41]Jose A. Matute,Mauricio Marcano,Sergio Diaz,Joshue Perez. Experimental Validation of a Kinematic Bicycle Model Predictive Control with Lateral Acceleration Consideration ? ? This project has received funding from the Electronic Component Systems for European Leadership Joint Undertaking under grant agreement No 737469 (AutoDrive Project). This Joint Undertaking receives support fromthe European Union Horizon 2020 research and innovation programmeand Germany, Austria, Spain, Italy, Latvia, Belgium, Netherlands, Sweden, Finland, Lithuania, Czech Republic, Romania,[J]. IFAC PapersOnLine,2019,52(8). [42]Vladislav S. Gromov,Oleg I. Borisov,Sergey S. Shavetov,AntonA. Pyrkin,FatimatB. Karashaeva. Modeling and Control of Robotic Systems Course: from Fundamentals to Applications ? ? 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《化学工程与工艺专业英语》课文翻译-Unit 3 Typical Activities of Chemical Engineers
Unit 3 Typical Activities of Chemical Engineers化学工程师的例行工作The classical role of the chemical engineer is to take the discoveries made by the chemist in the laboratory and develop them into money--making, commercial-scale chemical processes. The chemist works in test tubes and Parr bombs with very small quantities of reactants and products (e.g., 100 ml), usually running “batch”, constant-temperature experiments. Reactants are placed in a small container in a constant temperature bath. A catalyst is added and the reactions proceed with time. Samples are taken at appropriate intervals to follow the consumption of the reactants and the production of products as time progresses.化学工程师经典的角色是把化学家在实验室里的发现拿来并发展成为能赚钱的、商业规模的化学过程。
化学家用少量的反应物在试管和派式氧弹中反应相应得到少量的生成物,所进行的通常是间歇性的恒温下的实验,反应物放在很小的置于恒温水槽的容器中,加点催化剂,反应继续进行,随时间推移,反应物被消耗,并有生成物产生,产物在合适的间歇时间获得。
SPBCN小学中级组三四年级词汇(1800)
SPBCN拼词大赛小学中级组词汇INTERMEDIATE GROUP WORD LIST(1800)小中组是指三年级至四年级的学生组别。
小中组单词主要由6大部分组成,分别是原SPBCN词库单词,人教版英语教材单词,外研版英语教材单词,美国较为通用的词汇学习教材单词,根据蓝思分级阅读体系精选的经典英文名著中的单词,以及CEFR分级下的词汇。
其中,人教版英语教材主要包括五至六年级词汇和部分七至九年级词汇,外研版英语教材五至六年级词汇,美国通用词汇学习教材四年级至六年级少量词汇,精选蓝思指数在670-800L范围的经典英文名著中的词汇,以及CEFR分级下A1-A2的部分高频词汇,本组别共包含1800个单词备注:带有小蜜蜂标记的为本组别核心词汇,主要用于复赛备赛参考。
对于其他赛段本组别的所有单词都应予以参考。
本组别共包含600个核心词汇。
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脓毒症患者脂蛋白及其代谢失调的研究进展
脓毒症患者脂蛋白及其代谢失调的研究进展【摘要】高密度脂蛋白与脓毒症关系最为密切,通过减毒、抗炎、抗氧化、抗血栓形成等参与调节免疫反应。
在脓毒症患者中,脂酶和脂质转运蛋白发生结构和功能上的改变,导致脂蛋白代谢失调,高密度脂蛋白功能障碍(dysHDL)和氧化型低密度脂蛋白(oxLDL)蓄积,造成炎症消退失败、组织损伤和器官功能障碍。
脓毒症患者远期预后较差,与持续性炎症、免疫抑制和分解代谢综合征(PICS)有关,PICS主要机制与骨髓来源的抑制性细胞持续性扩增相关。
本文究高密度脂蛋白在脓毒症中的作用及代谢变化的研究进展作一综述,期望对脓毒症的病情评估和治疗提供新思路。
【关键词】脓毒症脂蛋白代谢持续性炎症免疫抑制与分解代谢综合征(PICS)脓毒症是机体对感染免疫失调而导致的一种危及生命的器官功能障碍疾病,具有高发病率、高死亡率、高治疗费用等特点[1]。
脂蛋白除了在新陈代谢中具有重要作用外,还对免疫系统有多效性作用[2]。
研究证实,脂蛋白在早期能引起炎症反应有利于病原体清除,后期也可作为载体对细菌死亡碎片进行清除,在组织损伤恢复过程发挥重要作用,其中高密度脂蛋白(High density lipoprotein,HDL)与脓毒症关系最密切[3]。
Tanaka S等[2, 4]研究表明,HDL通过减毒、抗炎、抗氧化、抗血栓形成等功能在调节免疫反应和保护内皮细胞功能中发挥重要作用,但氧化后的HDL缺乏执行以上功能的能力。
脂蛋白在脓毒症急性反应期发生结构和功能改变,其含量也相应改变,如HDL、低密度脂蛋白(LDL)水平降低[5];HDL的主要组成载脂蛋白AI (apoAI)、载脂蛋白AⅡ(apoAⅡ)等含量降低,血清淀粉样蛋白A(SAA)、脂多糖结合蛋白(LBP)含量增加[6]。
同时,脂蛋白代谢有关的脂酶和转运蛋白也发生着变化,如卵磷脂胆固醇乙酰基转移酶(LCAT)、胆固醇酯转移蛋白(CETP)、对氧磷酶-1(PON1)降低,磷脂转移蛋白(PLTP)、磷脂酶A2(PLA2)增多[7],从而导致HDL功能上的改变,造成组织损伤、器官功能障碍。
雪橇飞机AEROCET 1500 CC11-160 ELSA 水上浮筒补充手册说明书
9.1 AEROCET 1500 AMPHIBIOUS FLOATS LOG OF REVISIONSINTENTIONALLY LEFT BLANK9.1.1 GENERALThis supplement must be attached to the Pilot’s Operating Handbook when floats are installed. The information contained herein supplements or supersedes the Pilot’s Operating Handbook only in the areas listed in this supplement. For limitations, procedures and performance information not contained in this supplement, consult Section 2 of the Pilot’s Operating Handbook. It should be noted that these floats are “experimental” and as such there is no warranty to their compliance to either the ASTM or Part 23 Standards. 9.1.2 FUEL QUANTITY INDICATORSTo determine the fuel quantity when equipped with floats, use the fuel quantity indication for level flight. Fuel indications in the water will vary depending on the angle at which the aircraft is floating. Generally, using the markings for level flight will ensure that the amount of fuel available is greater than what is shown on the gauges. 9.1.3 BILGE PUMPThere is a bilge pump stowed in a float locker. Any water that has accumulated in the floats may be emptied out by removing the rubber plugs and using the pump to draw the water out. Make sure that no one is standing in the way of the water stream.9.1.4 FLOAT COMPARTMENTSThere are 6 water tight compartments on each float, 1 of which is a storage locker on each float.Figure 9-1-1 View of the Aircraft with FloatsFigure 9-1-2 View of Floats9.1.5 LIMITATIONS9.1.5.1 GENERALThis section provides the recommended operating limitations, instrument markings, color-coding and basic placards for operation that are specific to the Cub Crafters' CC11-160 when equipped with floats. By ELSA classification, the owner may establish his/her own limitations, etc., but may not fly above the established ELSA weight requirement.Please refer to Section 2 of the aircraft flight manual for the complete list of operating limitations, instrument markings, color-coding and basic placards for operation that are common to the landplane and seaplane. AIRSPEED LIMITATIONSINDICATED AIRSPEED (IAS) MPH KNOTS Never exceed speed (V NE) 141 12397 84 Operating maneuvering speed (V A)(at 1430 lb)Maximum Flap Speed (V FE flaps 50°) 81 7071 62 Best Rate of Climb Speed (V Y)(at 1430 lb)Best Angle of Climb Speed (V X)50 43(at 1430 lb)Maximum Demonstrated Crosswind Velocity.......... 11 kts Maximum Demonstrated Wave Height ........................ 1 ft9.1.5.2 CENTER OF GRAVITY▪Position of Datum............ 60 inches ahead of wing leading edge▪Maximum Gross Weight ........................ 1430 lb.▪Maximum Float Baggage 80lb./each float locker Center of Gravity Limits at 1430 lb.▪Forward .................................73.0 in. aft of datum ▪Aft .........................................78.5 in. aft of datum Center of Gravity Limits at 1100 lb. or less▪Forward ................................70.5 in. aft of datum▪Aft ........................................78.5 in. aft of datum9.1.5.3 PLACARDSLocate near water rudder retraction handle stowage hook:Or"WATER RUDDERALWAYS UPEXCEPTWATER TAXIING"On hydraulic hand pump cover at gear selector handle:9.1.6 EMERGENCY PROCEDURES9.1.6.1 GENERALThis section provides the procedures recommended when encountering an emergency or a critical situation as related specifically to operations when the floats are installed. It is highly r ecommended to establish one’s own numbers for emergency conditions in lieu of the ELSA (experimental) classification. Again, this is a recommendation only. For all other emergency procedures outside of float operations, refer to Section 3 of the regular flight manual.This section is divided into two parts. The first contains emergency procedure checklists. The second part amplifies the items listed in the checklists and includes information that is not readily adaptable to a checklist format or which the pilot could not be expected to refer to in an emergency situation. This information should be reviewed regularly.Pilots must familiarize themselves with the procedures in this section and must be prepared to take appropriate action should an emergency arise.It is stressed that the procedures outlined in this section are recommendations only. They are not a substitute for sound judgment and common sense and may have to be adjusted depending on the circumstances prevailing at the time of the emergency. It is important that the pilot be thoroughly familiar with the aircraft. He/She must review and practice as many of these procedures as are safe to perform as part of his/her training. Above all, in any emergency situation, MAINTAIN CONTROL OF THE AIRCRAFT.AIRSPEEDS FOR EMERGENCY OPERATIONSSTALL SPEEDS (1430 lb)INDICATED AIRSPEED (IAS) MPH KNOTS Flaps up (V S1).................................. 40 35Flaps down (50°) (V S0)...................... 32 28 BEST GLIDE (V G)Flaps up (1430 lb.)............................. 68 59 9.1.6.2 EMERGENCY CHECKLIST9.1.6.2.1 Emergency Landing on Water withoutEngine PowerINDICATED AIRSPEED (IAS) MPH KNOTS ▪ Approach (flaps up).................. V G68 59 ▪Seat Belts Tight and secure When landing area assured:▪Flaps...................................................... A s required ▪Gear ................................. Up(ck lights and mirrors) ▪Door................................................................ Open ▪ELT ............................................................. Activate ▪Touchdown .......................................Slightly tail low ▪Control Stick ..... Progress to full aft after touchdown When aircraft comes to a stop:▪Magnetos/Ignition ............................................... Off ▪Master Switch ..................................................... Off ▪Fuel Selector ...................................................... Off If time permits, check GPS or charts for airports in the immediate vicinity. If possible, notify your difficulty and intentions by radio on 121.50 and/or squawk 7700.9.1.6.2.2 Emergency Landing on Land withoutEngine PowerINDICATED AIRSPEED (IAS) MPH KNOTS ▪ Approach (flaps up).................. V G68 59 ▪Seat Belts ...................................... T ight and secure ▪Flaps ..................................................... As required ▪Gear ............................ Down (ck lights and mirrors) ▪Door ............................................................... Open ▪ELT ............................................................ Activate ▪Touchdown ......................................... Level attitude ▪Control Stick ..... Progress to full aft after touchdown When aircraft comes to a stop:▪Magnetos/Ignition ............................................... Off ▪Master Switch ..................................................... Off ▪Fuel Selector ...................................................... Off If time permits, check GPS or charts for suitable landing areas in the immediate vicinity. If possible, notify your difficulty and intentions by radio on 121.50 and/or squawk 7700.9.1.6.2.3 Landing Gear Fails to Retract or ExtendIf possible, cycle the gear to address the problem. If the problem is unable to be corrected, leave the gear lever in the down position and allow time for the gear to deploy by gravity. Reducing speed will help the main gear to come down. Always land on land and never on water under these conditions.9.1.6.3 AMPLIFIED EMERGENCY PROCEDURES9.1.6.3.1 Total Loss of Engine Power in FlightThe aircraft with floats will glide approximately 1.1 nautical miles for every 1000 feet of altitude loss. The rate of descent will be approximately 890 feet per minute. Most GPS devices have a “Direct to” function that shows the closest airports. Use charts to assess the topography of airports in the immediate vicinity.9.1.6.3.2 Emergency Landing on Land withoutEngine PowerWhen having to make an emergency landing on land the pilot should use his/her best judgment to find the most suitable surface for landing. Touchdown should be level attitude if gear is up and slightly tail low if gear is down.9.1.7 NORMAL PROCEDURES9.1.7.1 INTRODUCTIONThis section describes the procedures recommended for the pilot to follow during normal operations of the aircraft on floats. It is divided into two parts. The first has abbreviated checklists; these are in a format suitable for reference in the cockpit. The second part amplifies the information given in the checklists. It provides the pilot with detailed descriptions that will help him/her understand the procedures and techniques. This section contains complete checklists so that the pilot can carry out these activities without having to turn back and forth in this manual.9.1.7.2 AIRSPEEDS FOR NORMAL OPERATIONSThe speeds in this section are based on a maximum weight of 1430 lb, under standard conditions, at sea level.9.1.7.3 MAXIMUM WAVE HEIGHTMaximum Demonstrated Wave Height ........................... 1 ft 9.1.7.4 NORMAL PROCEDURES CHECKLISTFor ease of operation, this supplement will provide the complete checklist.9.1.7.4.1 Cockpit Preflight▪Flight Controls ............... Free and correct operation ▪Trim .................. C heck operation and set for takeoff ▪Fuel Selector ................................................... Both ▪Flaps............................................. Proper operation ▪Fuel Gauges ...........Sufficient fuel for intended flight (Use level flight indications for float operation) ▪Mixture .................................................... Idle cut-off ▪Carburetor Heat ............................................... Cold ▪Magnetos/Ignition ............................................... Off ▪Ignition Backup Battery ................................ Normal ▪Electrical Switches .............................................. Off ▪Landing Gear Selector ......................... U p for WaterDown for Land (Check for firm pressure on the pump handle) ▪Water Rudders ................. Check operation and set(Up for land- ensure handle is stowed)(Down for Water) ▪Master Switch ..................................................... On ▪Navigation/Strobe Lights ................ Check operation ▪Landing Light ................................. Check operation ▪Stall Warning Horn......................... Check operation ▪Master Switch ..................................................... Off ▪Circuit Breakers ......................................... Check in ▪Windows ......................................................... Clear ▪Documentation .......................................... Onboard If passenger seat unoccupied▪Passenger Seat Harness ..............................Secure9.1.7.4.2 Preflight Right Fuselage, Wing, and Float▪Right Fuselage .............................................. C heck ▪Fuel Sump ...................................................... Drain ▪Flap Surface ................................... C heck condition ▪Flap Hinges ................................................... C heck ▪Aileron Surface ............................... C heck condition ▪Aileron Hinges ............................................... C heck ▪Wing Tip and Light......................................... C heck ▪Vortex Generators ......................................... C heck ▪Fuel Cap Vent ............................................... C heck ▪Fuel Tank ........... C heck supply and cap for security ▪Water Rudder and Cables............................. C heck, Extend- retract ▪Main (45psi) and Nose Gear (70psi) (Amphibious Only).............................................................. C heck ▪Float ..... C heck for damage and water accumulation(Use bilge pump as necessary)▪Bilge Rubber Plugs ......................................Secure ▪Oar ................................. Check stowed and secure ▪Float Hatches .... Cargo secure and hatches latched9.1.7.4.3 Preflight Nose Section▪Oil Door .......................................................... O pen ▪Oil Quantity .......................... Check and cap secure ▪Engine Condition .......................................... Check ▪Oil Door ......................................................... Close ▪Propeller and Spinner ................................... Check ▪Air Inlets ....................................................... Check ▪Fuel Strainer (in front of firewall on left) .......... Drain ▪Fuel Drain (behind firewall on left) ................. D rain* *For aircraft S/N 00264 and on only9.1.7.4.4 Preflight Left Fuselage, Wing, and Float▪Float Hatches ... .Cargo secure and hatches latched ▪Main (45psi) and Nose Gear (70psi) (Amphibious Only) ............................................................. Check ▪Float .....Check for damage and water accumulation(Use bilge pump as necessary)▪Bilge Rubber Plugs ...................................... Secure ▪Fuel Tank ...........Check supply and cap for security ▪Fuel Cap Vent ............................................... Check ▪Landing Light ................................. Check condition ▪Pitot Tube ...................................... Check condition ▪Stall Warning Vane ........................ Check condition ▪Wing Tip and Light ......................... Check condition ▪Vortex Generators ........................................ Check▪Aileron Hinges ............................................... C heck ▪Aileron Surface ............................... C heck condition ▪Flap Hinges ................................................... C heck ▪Flap Surface ................................... C heck condition ▪Water Rudder and Cables ............................. C heck ▪Left Fuselage................................................. C heck 9.1.7.4.5 Empennage▪Bracing Wires .............................. Check for tension ▪Hinges ........................................................... C heck ▪Surfaces ........................................................ C heck 9.1.7.4.6 Preflight GeneralCheck that all wings and other external surfaces are free from frost, ice or snow.9.1.7.4.7 Startup and Taxi▪Preflight Inspection ................................... C omplete ▪Pilot Seat ................................................... Adjusted ▪Seat Belts ................................................. Fastened ▪Passenger Briefing ................................... C omplete ▪Door ............................................................. C losed ▪Fuel Selector ................................................... Both ▪Avionics Master Switch ....................................... Off ▪Water Rudders ................................ Down for water ▪Landing Gear....................................... Up for WaterDown for Land ▪Propeller Area ................................................ Clear 9.1.7.4.8 Starting Engine▪Battery Master Switch ........................................ .On ▪Check Gear Advisory…. Cancel any advisory audio ........................................Press Test to check lights ▪Strobes ............................................................... On ▪Magneto/Ignition Switches ...........................Both on ▪Mixture ....................................................... Full rich▪Primer ...................Apply (3 times if cold, omit if hot) ▪Throttle ..............................................Open 1/2 inch ▪Starter......................................................... Engage After engine has started:▪Oil Pressure .................................................. Check ▪Throttle .............................................Set 1000 RPM ▪Lights .................................................... As required ▪Avionics Master Switch ....................................... O n 9.1.7.4.9 Starting Engine When Flooded▪Magneto/Ignition Switches .......................... Both on ▪Mixture .................................................... Idle cut-off ▪Throttle ..................................................... Full open ▪Starter......................................................... Engage When engine fires:▪Mixture ............................................................. Rich ▪Throttle ................................... Retard to 1200 RPM ▪Oil Pressure .................................................. Check ▪Lights .................................................... As required ▪Avionics Master Switch ....................................... O n 9.1.7.4.10 Warm up▪Throttle ...................................... 1000 to 1200 RPM9.1.7.4.11 Taxiing▪Taxi Area ........................................................ Clear ▪Throttle ................................................ Apply slowly 9.1.7.4.12 Before Takeoff▪Flight Instruments ......................................... Check ▪Magnetos/Ignition ............................................ Both ▪Carburetor Heat ........................................ Off (cold) ▪Trim ................................................................... Set ▪Landing Gear ........................................ Up for LandDown for Land(Ck for firm pressure on pump handle) ▪Flaps ......................................... S econd notch (35º) ▪Controls ........................ Free and proper movement ▪Doors............................................................ C losed ▪Strobes and Lights................................. A s required ▪Seat Belts ....................................... Check fastened ▪Throttle .................................................. 1700 RPM* ▪Mixture ............................................................. Set* ▪Magnetos/Ignition .................................. C heck both▪Carburetor Heat .... Hot, note RPM drop and remove ▪Primer.......................................................... Locked ▪Engine Instruments........................................ C heck* Lean at high altitudes for peak RPM.9.1.7.4.13 Takeoff▪Water Rudders .............................................. Check Up ▪Landing Gear ............................................ Up for WaterDown for Land ▪Control Stick ....................................................... F ull Aft ▪Throttle ...................... ...............................................Full ▪Control Stick ............................................ Move forward On water, when the nose stops rising to attain the planing attitude (on the step). ▪Accelerate to flying speed (depending on aircraft weight)▪Control Stick ................................ Gentle back pressure ▪Landing Gear ............................................ Up for WaterDown for Land ▪Flaps ...................................... Retract slowly after liftoff9.1.7.4.14 ClimbINDICATED AIRSPEED (IAS) MPH KNOTS ▪Best Rate..................................... 71 62▪ Best Angle.................................... 50 43▪Mixture .................................................................. Rich As required, LEAN to obtain maximum RPM:▪Carburetor Heat .......................................... As required 9.1.7.4.15 Cruise▪Power .................................................................. A djust ▪Mixture ................................................................ A djust ▪Carburetor Heat ........................... Cold, use as required 9.1.7.4.16 Descent▪Power .................................................................. A djust ▪Mixture ............................................ R ichen as required ▪Carburetor Heat .......................................... As required 9.1.7.4.17 Approach▪Fuel Selector ......................................................... Both ▪Seat Belts ....................................................... F astened ▪Mixture .................................................................... Set ▪Flaps ....................................................................... Set INDICATED AIRSPEED (IAS) MPH KNOTS Maximum speed first notch flaps (15°) 85 74Maximum speed (>15°) 81 70 ▪Trim ............................................................ As required ▪Speed ......................................................... As required(1.3 full flaps stall speed at gross weight is 42 mph or37 knots IAS)9.1.7.4.18 Landing▪Water Rudders ............................................... C heck up ▪Landing Gear ............................................ Up for Water Down for Land (cancel condition on advisory) ▪Control Stick ................................ H old full aft as aircraft decelerates to taxi speed9.1.7.4.19 Cross Wind Landing▪Fuel Selector ......................................................... Both ▪Seat Belts ....................................................... Fastened ▪Mixture .................................................................... Set ▪Flaps .............................................. Set below white arc INDICATED AIRSPEED (IAS) MPH KNOTS Maximum speed first notch flaps (15°) 85 74Maximum speed (>15°) 81 70 ▪Trim ............................................................. A s required ▪Speed ......................................................... A s required (A higher speed than normal is recommended)▪Water Rudders ............................................... Check up ▪Landing Gear ............................................ Up for WaterDown for Land ▪Ailerons-Rudder ....................................... O n short final Use ailerons to keep upwind wing lowRudder to hold landing area alignment▪Touchdown ........................ Do not touch down in a slip ▪Landing Roll ..................... Use ailerons to keep upwind wing down, rudder to keep directional control asappropriate, water rudders down (water only)9.1.7.4.20 Go-Around▪Throttle ......................................................... Full power ▪Airspeed ................................................. A bove 52 mphor 45 Knots ▪Landing Gear..................................................... Retract ▪Flaps .......................................................Retract slowly ▪Trim ............................................................ As required 9.1.7.4.21 Stopping Engine▪Flaps ................................................................. Retract ▪Electrical Equipment ................................................. O ff ▪Avionics Master Switch ............................................. O ff ▪Throttle .................................................................... I dle ▪Mixture ......................................................... Idle cut off ▪Magnetos/Ignition ..................................................... O ff ▪Master Switch ........................................................... O ff9.1.8 WEIGHT AND BALANCE9.1.8.1 INTRODUCTIONThis section provides the position of the center of gravity relative to the datum. It also describes how to calculate the empty weight of the aircraft based on data for the landplane. Should it be necessary to weigh the aircraft on floats, please consult the maintenance manual.9.1.8.2 PERTINENT INFORMATION FOR WEIGHTAND BALANCE OF THE CC11-100 AIRCRAFTEQUIPPED WITH FLOATSPosition of Datum ...................................... 60 inches aheadof wing leading edgeMaximum Gross Weight ......................................... 1430 lb. Maximum Float Baggage .................. 80lb./each float locker ..................................................................... (160 lb. Total)Center of Gravity Limits at 1430 lb. Forward................................................ 73.0 in. aft of datum Aft ........................................................ 78.5 in. aft of datum Center of Gravity Limits at 1100 lb. or less Forward................................................ 70.5 in. aft of datum Aft ........................................................78.5 in. aft of datum9.1.8.3 DETERMINATION OF EMPTY WEIGHTThe empty weight and the position of the center of gravity are recorded in Section 6 of this manual.The weight and moments of the floats are given in Table 9-1-1. If there is any difficulty or concern in values listed, performing an actual weight and balance is recommended.Table 9-1-1 - Weight of Amphibious Floats9.1.8.4 WEIGHT AND BALANCE DETERMINATIONFOR FLIGHTIn order to calculate the weight and balance of the aircraft:1. Insert the respective loads in Table 9-1-3 or Table9-1-4.2. Multiply each load by its respective arm and notethe moment.3. Add the loads to calculate the takeoff weight.4. Add the moments to compute the total moment.5. Divide the moment by the takeoff weight. This isthe final position of the center of gravity.6. Plot the point on Figure 9-1-2. If it is within theweight and balance envelope, the aircraft is withinthe approved envelope.Table 9-1-1 –Weight and Balance Loading Form with FloatsTable 9-1-2 –Weight and Balance Loading Form with FloatsExtended Cargo CompartmentFigure 9-1-2 - Weight and Balance Envelope with Floats70717273747576777879Inches Aft of DatumW e i g h t (l b )9.1.9 PERFORMANCEThese floats are “experimental” and as such there is no warranty to their compliance to either the ASTM or Part 23 Standards. Therefore, performance information is not required and is not available at this time. Pilots are advised that takeoff and landing rolls will be increased from standard landing gear due to additional weight.All values listed are at gross weight under standard sea level conditions. The charts below should be filled in by the owner in order to establish working numbers for the aircraft. Propeller, engine capability, etc. are all variables unique to each aircraft.9.1.9.1 CLIMB9.1.9.2 Takeoff/Landing-Wheels9.1.9.3 Takeoff/Landing-Water。
空难英语作文
空难英语作文In the realm of modern transportation, air travel stands as a symbol of efficiency and speed. However, the occasional air disaster serves as a stark reminder of the potential risks involved in flying. This essay delves into the impact of air disasters on aviation safety, examining the measures taken to prevent such tragedies and the psychological effects on the public and industry.Air disasters, while rare, have a profound impact on the aviation industry. Each incident triggers a thorough investigation by organizations such as the National Transportation Safety Board (NTSB) in the United States orthe equivalent bodies worldwide. These investigations aim to identify the cause of the accident, whether it be mechanical failure, human error, or a combination of factors. Thefindings are then used to improve safety protocols and regulations, ensuring that the likelihood of a similarincident is minimized in the future.One of the most significant outcomes of air disasters is the technological advancements they inspire. For instance, the introduction of the black box, a flight data recorder, was a direct result of the need for better crash investigation methods. Today, black boxes are standard equipment on all commercial aircraft, providing crucial data that helps investigators piece together the events leading up to a crash.Moreover, air disasters have led to the implementation of rigorous training programs for pilots and crew members. Simulation training, which allows pilots to experience and respond to various emergency scenarios in a controlled environment, has become an integral part of a pilot's education. This training enhances their ability to handle crises, thereby increasing the chances of averting a disaster.The psychological impact of air disasters should not be underestimated. For the families of the victims, the loss is immeasurable. For the public, such incidents can lead to a temporary decrease in air travel, as fear of flying becomes more pronounced. Airlines and governments often respond by offering reassurances about the safety of air travel, highlighting the industry's impressive safety record and the low probability of an accident.In conclusion, while air disasters are tragic and have far-reaching consequences, they also serve as catalysts forchange within the aviation industry. They prompt a reassessment of safety measures, drive technological innovation, and reinforce the importance of comprehensive training. Despite the challenges, the aviation industry's commitment to learning from these incidents has led to continuous improvements in safety, making flying one of the safest modes of transportation today.。
油田新型示踪剂的研究与应用的开题报告
油田新型示踪剂的研究与应用的开题报告1. 研究背景和意义石油是世界上一种非常重要的能源资源,其采集和开发对于国家的经济发展以及能源安全都具有至关重要的作用。
油田示踪剂是一种在油田开采中被广泛使用的技术,它可以追踪油田内的流体运动,为油田开发提供了重要的技术支持。
随着油田开采的不断进行以及对示踪剂技术的不断研究,研制出新型示踪剂具有重大的意义。
其一方面可以提高油井采油率、延长油井寿命,并减轻环境污染的风险;另一方面还可以促进我国化工产业的发展。
2. 研究目的本研究旨在研究新型油田示踪剂,并应用于实践中。
通过分析新型示踪剂的特性,优点和不足,确定适用范围,并与传统示踪剂进行比较,验证其在应用中的优越性。
3. 研究内容(1)介绍新型示踪剂的背景、意义和研究现状;(2)对新型示踪剂进行理化性质、毒性评价以及在实验室条件下的追踪实验;(3)通过对实验数据的分析,评价新型示踪剂在油井开采中的特性和优势,与传统示踪剂进行比较;(4)结合实践应用,论证新型示踪剂的可行性和效果,并对其应用进行优化和改进。
4. 研究方法(1)文献调研法:从理论上研究新型示踪剂的研究,目的是分析国内外新型示踪剂的应用现状和进展;(2)实验方法:选取适当的实验模型,比较传统示踪剂和新型示踪剂的性能,例如比较示踪剂的可追踪性、环境友好性等;(3)统计分析方法:对实验数据进行分析,统计新型示踪剂的性能。
5. 预期成果(1)研究新型油田示踪剂的理论特性,明确其适用范围和优越性;(2)对新型示踪剂进行实验研究和分析,并在实际应用中验证其有效性;(3)论证新型示踪剂的应用前景和市场发展。
6. 研究拟定时间表(1)文献调研和理论分析:2个月;(2)实验设计和数据采集:3个月;(3)数据分析和结果撰写:2个月;(4)论文修改和准备答辩:1个月。
7. 研究的经费来源研究经费主要通过学校和科研项目申请来获得,同时也可以适度通过企业支持等方式解决。
具体费用分配如下:(1)实验材料和设备费用:20000元;(2)差旅和交通费用:5000元;(3)书籍和文献资料费用:3000元;(4)其他杂项支出费用:2000元。
可降解和不可降解输尿管支架在家犬输尿管中的病理学变化
可降解和不可降解输尿管支架在家犬输尿管中的病理学变化王炜;李牧;刘绍虔;徐缓;李虹【摘要】背景:目前临床应用的输尿管支架主要由不能在人体内降解的硅酮、聚氨甲酸乙酯等为原料制成,置入体内一段时间后必须通过有创的侵入性操作拔除,增加了患者的痛苦.目的:比较可降解材料消旋聚乳酸输尿管支架和聚氨甲酸乙酯支架在家犬输尿管内的组织病理学变化.方法:经开放手术分别将消旋聚乳酸支架和聚氨甲酸乙酯支架置于19只家犬左右两侧输尿管内,术后每2周取出支架4次,同时切取输尿管组织在光镜下观察输尿管组织病理改变.结果与结论:术后第2周和第4周两侧输尿管有明显的上皮脱落、固有层水肿和肌层结构紊乱,第6周仅发现固有层小血管充血,第8周输尿管全层组织基本恢复正常.结果证实消旋聚乳酸输尿管支架具有良好的组织相容性.【期刊名称】《中国组织工程研究》【年(卷),期】2010(014)029【总页数】4页(P5321-5324)【关键词】降解;输尿管;支架;病理学;消旋聚乳酸;生物相容性【作者】王炜;李牧;刘绍虔;徐缓;李虹【作者单位】东莞市人民医院泌尿外科,广东省东莞市,523000;东莞市人民医院泌尿外科,广东省东莞市,523000;东莞市人民医院泌尿外科,广东省东莞市,523000;四川大学华西医院病理科,四川省,成都市,610041;四川大学华西医院泌尿外科,四川省,成都市,610041【正文语种】中文【中图分类】R3180 引言聚乳酸是一种安全、可靠、生物相容性良好的可降解材料。
聚乳酸及其共聚/聚合物已广泛应用于外科缝线、纱布、药物控释体系、骨科内固定和组织修复材料等领域。
在泌尿外科,以聚乳酸共聚/聚合物制成的可降解尿道支架已经直接应用于尿道狭窄以及前列腺增生等疾病的治疗,并且在特定患者人群中取得一定的效果[1-10]。
迄今为止,以聚乳酸为主要材料的可降解输尿管支架仍未有直接应用于临床的报道,大多数研究仍然停留于动物试验阶段,而且,大部分可降解输尿管支架的动物试验仅仅观察了支架本身的降解性能以及降解过程变化,对输尿管的组织病理学变化报道不多[11-15]。
基于PIV测量的柔性壁减阻试验
基于PIV测量的柔性壁减阻试验顾建农;晏欣;张志宏;赵昕【摘要】为了解不同性能的柔性壁对湍流边界层的减阻效果,利用粒子图像测速技术( PIV)对刚性壁面与4种材料的柔性壁面的湍流边界层流向速度分量进行测量.从边界层速度分布求得壁面切应力的分布,并由此得到柔性壁与刚性平板的平均摩擦阻力系数.实验结果表明,柔性壁面的边界层速度分布在对数律上有所平移,具有特定性能的柔性壁具有一定的减阻作用.%For understanding the effect of compliant walls on drag reduction in turbulent boundary layer,the velocity profile in turbulent boundary layer over a rigid wall and six compliant walls is measured with the particle image velocimetry( PIV) . First,the shear stress profile alone the wall is calculated from the velocity profile in bounday layer, then the average skin friction coefficient of the rigid wall and compliant wall is calculated from the shear stress profile. The experimental result shows that, in boundary layer of turbulent flows over a compliant wall, compared with that over a rigid wall, the velocity profiles in log law region is extended further away from the wall. The experimental result confirms the effect of drag reduce for the special compliant coating surface of turbulent boundary layer.【期刊名称】《舰船科学技术》【年(卷),期】2012(034)011【总页数】5页(P82-85,121)【关键词】减阻;柔性壁;PIV;边界层【作者】顾建农;晏欣;张志宏;赵昕【作者单位】海军工程大学理学院,湖北武汉430033;海军工程大学理学院,湖北武汉430033;海军工程大学理学院,湖北武汉430033;武汉大学水利水电学院,湖北武汉430021【正文语种】中文【中图分类】O3571 概述柔性壁减阻的设想最早是由 Kramer[1](1957)提出的,其减阻原因通常被解释为粘弹性材料的柔性壁可以提高层流边界层的稳定性,从而推迟边界层的转捩。
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Chemical Engineering Science58(2003)4695–4703/locate/cesExperimental investigation of a pilot-scale jet bubbling reactorfor wet ue gas desulphurisat ionYuanjing Zheng,S ren Kiil∗,Jan E.JohnssonDepartment of Chemical Engineering,Technical University of Denmark,Building229,DK-2800,Kgs.Lyngby,DenmarkReceived22August2002;received in revised form17February2003;accept ed21July2003AbstractIn the present work,an experimental parameter study was conducted in a pilot-scale jet bubbling reactor for wet ue gas desulphurisation (FGD).The pilotplantis downscaled from a limest one-based,gypsum producing full-scale wetFGD plant.Import antprocess paramet ers, such as slurry pH,inlet ue gas concentration of SO2,reactor temperature,and slurry concentration of Cl−have been varied.The degree of desulphurisation,residual limestone content of the gypsum,liquid phase concentrations,and solids content of the slurry were measured during the experimental series.The SO2removal e ciency increased from66.1%to71.5%when the reactor slurry pH was changed from3.5to5.5.Addition of Cl−(in the form of CaCl2·2H2O)to the slurry(25g Cl−=l)increased the degree of desulphurisation to above99%,due to the onset of extensive foaming,which substantially increased the gas–liquid contact area.An increase in the inlet ue gas SO2concentration from502 to991ppmv led to a decrease in the SO2removal e ciency from80.1%to69.4%.A temperature increase from296to323K caused a reduction in the degree of desulphurisation from69.4%to68.1%,but this result is almost within the experimental uncertainty.The residual limestone level in the gypsum formed increased with increasing values of reactor slurry pH,inlet ue gas SO2concentration,and slurry concentration of Cl−.?2003Elsevier Ltd.All rights reserved.Keywords:Wet FGD;Jet bubbling reactor;Absorption;Dissolution;Slurries;SO21.IntroductionCombustion of sulphur-containing fossil fuels,such as coal and oil,results in sulphur dioxide(SO2)emissions. The SO2is known to have detrimental e ects on human health and the environment,and as a consequence,many countries have imposed stringent regulations on coal-ÿred power plants over the past two decades(Soud,2000).In Denmark,for instance,an environmental levy of20Danish Kroner(equivalent to US$2.5)/kg sulphur emitted to the atmosphere was introduced on January1st2000(Frandsen, 2000).Consequently,reductions in SO2emissions are es-sential for the economy of power plants and research in desulphurisation technologies,in order to further optimise the processes,is needed.In the past10years, ue gas desulphurisation(FGD) technology has made considerable progress in terms of∗Corresponding author.Tel.:+45-4525-2827;fax:+45-4588-2258.E-mail address:sk@kt.dtu.dk(S.Kiil).e ciency,reliability(deÿned here as FGD operating hours divided by the boiler operating hours in a given period) and costs(Soud,2000).Presently,there are several ways of reducing SO2emissions from coal utilisation.Wet scrub-bers,especially the limestone-gypsum process,are the front-running FGD technologies.There are four main types of wet scrubbers,the spray scrubber,the packed tower, the jet bubbling reactor(JBR),and the double-loop reactor (Takeshita&Soud,1993).Fundamental studies have focused on the spray scrub-ber(e.g.Agrawal&Rochelle,1993;Brogren&Karlsson, 1997;Eden&Luckas,1998)and the packed tower(Kiil, Michelsen,&Dam-Johansen,1998;Frandsen,Kiil,& Johnsson,2001;Kiil,Nygaard,&Johnsson,2002;Zheng, Kiil,Johnsson,&Zhong,2002).However,few fundamen-tal studies on the JBR system have been reported.The in-vestigations(e.g.Gilbert,Kogawa,Sawahata,&Kumagai, 1987;Someshwar,Bhagat,&Hopke,1989;Yanagioka &Uchida,1993;Burford,Pearl,&Stevens,1994;Burford, 1997)consist of full-scale measurements where the0009-2509/$-see front matter?2003Elsevier Ltd.All rights reserved. doi:10.1016/j.ces.2003.07.0024696Y.Zheng et al./Chemical Engineering Science58(2003)4695–4703Fig.1.Schematic illustration of a full-scale jet bubbling reactor.After Burford(1997).performance of the commercial Chiyoda Thoroughbred121 (CT-121)process has been tested.These studies involved, for instance,the e ects of JBR slurry pH and pressure drop on the SO2removal and limestone utilization.Krasnopoler, Shields,and Shoji(1991)have explored the advantages of the CT-121process as a throwaway FGD system.These conditions,however,are only relevant for American wet FGD plants.In most European and Japanese plants the by-productmustbe high-qualit y gypsum,useful for wall-board manufacture.Kovacs and Fulop(1998)conducted SO2absorption experiments in a JBR using water and lime (as opposed to limestone)suspensions.Recently,Yoo and Kim(1998)presented some experimental results obtained using fairly low SO2concentrations(¡400ppmv).Their results showed the e ect of HCl in the ue gas on the degree of desulphurisation.Due to the increased importance of the JBR for wet FGD in Europe there is a need to increase the JBR process knowledge.A schematic drawing of a full-scale JBR is shown in Fig.1.The central feature of the JBR process is the absorber (reactor),in which the ue gas is blown into a limestone slurry,thereby forming aÿne bubble bed where SO2can be absorbed.The dissolved SO2dissociates to HSO−3,which is subsequently oxidised to SO2−4by injected air.Finally,SO2−4 ions combine with Ca2+ions,originating from dissolved limestone,and crystallise as gypsum.The overall reaction in the plant can be written asCaCO3(s)+SO2(g)+1=2O2(g)+2H2O(l)→CaSO4·2H2O(s)+CO2(g):(1) The JBR process eliminates the use of large recycle pumps and spray heads,making it less complex than conventional spray tower systems.However,the pressure drop in the JBR is signiÿcantly higher than that of the spray tower(Takeshita &Soud,1993).One major di erence between the JBR and other FGD absorption vessels is the gas–liquid contacting pattern.The ue gas enters the JBR through the gas-cooling duct where it is cooled and saturated with water by injection of water and slurry.The ue gas is then distributed through a large number of gas sparging tubes,which are immersed 12–18cm below the surface of the gypsum slurry(Burford, 1997).This injection of gas into the slurry creates a froth layer,which promotes absorption of SO2from the ue gas. The froth zone provides a very high gas–liquid interfacial area for SO2mass transfer to the slurry,as well as capture of y ash residuals(Yanagioka&Uchida,1993).The bub-bles in the froth zone are continuously collapsing and re-forming thereby generating new interfacial area and trans-port of reaction products away from the froth zone to the bulk slurry solution(Chiyoda Corporation,2000).Another major di erence between the JBR system and conventional FGD units is the operating slurry pH.The JBR system typ-ically operates between a pH of3.5and4.5in the slurry tank,whereas most conventional limestone systems operate ata holding t ank pH of5.0and above(Behrens&Delleney, 1981).In the JBR process the ue gas passes through a con-tinuous liquid phase.Conventional wet FGD plants,using spray towers,have ue gas as the continuous phase.The former enhances the mass transfer of SO2by providing a large gas–liquid contact area.Hence,a high SO2removal e ciency can be gained ata lower pH,leading t o a very low residual limestone content of the gypsum produced. To gain a deeper understanding of the JBR process,a limest one-based wetFGD pilotplant,downscaled from a full-scale JBR plant,has been constructed.A number of experiments,at di erent operating conditions,have been conducted.2.Experimental equipment and procedure2.1.JBR wet FGD pilot plantThe JBR pilotplantis downscaled from a full-scale wet FGD plantcleaning t he ue gas from a285MW e coal-ÿred power plant.A typical ue gas ow rate from the full-scale power plantis285N m3=s and the number of sparging tubes in the full-scale JBR is about2000.The diameter of the JBR is17m and the volume of the gypsum slurry is1300m3.A schematic illustration of the pilot plant is shown in Fig.2.The main components are the JBR,the feed and product tanks,and the natural gas burner.All pipes and vessels are made of PVC or stainless steel to avoid cor-rosion.The absorber is a stirred vessel with continuous feeding of both gas and liquid phases.The reactor tem-perature is controlled by means of a heat exchanger.The reactor vessel is a cylinder with an inner diameter of 52cm,and a height of101cm,ÿtted with four vertical ba es,a pH probe and a oating contact system for slurry level control.To avoid plugging,the level control was ushed with N2for30s every10min.An axial four-blade stirrer(diameter of20cm),with adjustable speed from 0to1420rpm,creates a high degree of mixing in the liquid phase.Y.Zheng et al./Chemical Engineering Science 58(2003)4695–47034697Gas from burnerTo stackGas sample boardDistilled water Pure SO 2Product tankFeed tankCompressed airSlurry pumpHeating water bathJet bubbling reactorWaterHeat exchanger Fig.2.Schematic illustration of the experimental pilot-scale JBR appa-ratus.The feed gas is supplied from either a natural gas burner or as compressed air.The gas mixture enters the heat ex-changer where it is cooled from burner temperatures to 74◦C.The gas enters the JBR through the gas-cooling duct where the temperature is reduced further to 50◦C and the gas is saturated by injection of distilled water.It was not possible to have a slurry quench zone upstream the reactor like in the full-scale absorber (Fig.1),as there was no water cleaning system in the gas distribution box.Keeping the gas distribu-tion box and sparger tubes free of solids is critical to ensure continuous performance of the system.In the experiments at room temperature,compressed and saturated air at 23◦C was used instead of burner ue gas.The low temperature (as opposed to the pertinent temperature of 50◦C)was used due to practical limitations of the temperature control at the high ue gas ow rates employed.However,as shown later in Section 3the degree of desulphurisation is practically in-dependent of reactor temperature in the range studied.In order to simulate a coal combustion ue gas,SO 2is added to the saturated gas just before it enters the absorber.The ue gas is then distributed through nine gas sparger tubes (Fig.3)with an internal diameter of 27:2mm and a length of 436mm.The tubes are immersed 5cm below the stag-nant surface of the gypsum/limestone slurry,and the injec-tion of gas into the slurry creates a froth layer,which pro-motes absorption of SO 2from the ue gas.The treated ue gas ÿnally ows to the stack.Air is introduced into the reactor through a probe to ox-idize HSO −3o SO 2−4.The SO 2−4ions combine with Ca 2+,originating from the dissolved limestone,and crystallize as gypsum.The addition of fresh limestone slurry is controlled by maintaining the holding tank pH at a constant value (typically 4.5).The changing weight of the feed tank over time is recorded and allows the feed consumption rate to be calculated.The feed slurry is prepared by mixing distilled water and a required amount of commercial limestone.JBR orificeGasdistribution boxFlue gasFig.3.Photo of gas distribution box with nine sparger tubes.A product stream of JBR slurry is withdrawn intermittently to the product tank.To study the e ect on the performance of the pilot plant from Cl,which is released during coal combustion as HCl and subsequently absorbed in the slurry in the full-scale plant,Cl was added to the feed tank in the form of CaCl 2·2H 2O(s)in one experiment.A steady-state concentration level of 25g Cl −=l,typical for a Danish wet FGD plant,was used (Frandsen etal.,2001).2.2.AnalysesThe amountof residual limest one in gypsum samples was determined by acid titration.Solids content (gypsum with residual limestone)of the slurry samples were determined by evaporation (9days at 40◦C)and subsequentweighing.Particle size distributions (PSDs)of limestone and gypsum samples were measured on a Malvern analyser,employ-ing laser di raction (Rawle,1997),and using ethanol as dispersant.2.3.Dimensional analysisA dimensional analysis for the volumetric mass transfer coe cientwas carried outin t he process of downscaling from full-to pilot-scale (Riber,2001).The reason for fo-cusing on this particular variable in the downscaling is that it contains the mass transfer and chemical reaction charac-teristics of the wet FGD plant and as such all the essential process parameters.It was chosen to have nine gas sparging tubes in the pilot plant to include possible interaction among the gas outlet streams of the various tubes.The dimensional analysis showed that in order to establish complete similarity between the pilot-and full-scale plants (at the same tempera-ture and pressure),the values of the following dimensionless numbers should be identical:Re =ud g =Ág ,Fr =u 2=(gd ),4698Y.Zheng et al./Chemical Engineering Science58(2003)4695–4703Table1Numerical values of the dimensionless numbers in three cases(each one ensuring that one particular dimensionless number is identical for the pilot-and full-scale plant)Scale of plant Re Fr l=(du2 g) Full35,89414460.0048 Pilot(case1)35,8941:2×1080.0001 Pilot(case2)10,8461:7×1050.0048 Pilot(case3)416214460.084The values of the dimensionless numbers for the full-scale plant are determined by the process parameters,which areÿxed in the analysis.and l=(du2 g),for nomenclature,see list of symbols.Here, it should be noted that similarity for the dimensionless num-ber(p2−p1)=(u2 g)=5,also appearing in the analysis, could be established by an adequate choice of immersion depth of gas sparging tubes(the latter being proportional to the total pressure drop in the pilot plant,p2−p1).Itwas not possible,due to the appearance of the same parameters in more t han one dimensionless number and pilotplant ow rate limitations,to obtain complete similarity for Re,Fr,and l=(du2 g)at the same time.In Table1the numerical val-ues for three cases(each having one of the three dimension-less numbers identical for pilot-and full-scale)are shown. The Froude number,Fr,physically represents the ratio of the initial jet momentum ow to the buoyant force(Bird, Stewart,&Lightfoot,1960)and is very important for the transition between jet stream and bubble formation,and so for the performance of the JBR.It was chosen to have the same Froude number in t he pilotand full-scale plantand relax on the other dimensionless parameters(i.e.case3in Table1).An additional argument,supporting this choice, was that the Re number was of the same order of magni-tude when keeping Fr constant,while a constant Re num-ber would cause a deviation of a factor of as much as105 between the Froude number in the pilot and full-scale plant (see Table1).The reason for this di erence is to be found in the way the various physical parameters appear in the di-mensionless numbers.Also,the ratio of ue gas ow rate to reactor slurry volume of the pilot plant is identical to that of the full-scale plant(=0:265s−1).In summary,itis not possible to obtain complete similarity between the pilot-and full-scale plantand one mustrely on physical knowledge of the process to make an adequate choice of downscaling(i.e. the design of a representative pilot plant).3.Results and discussionTo investigate the e ects of important process parame-ters,four experimental series were conducted in the pilot plant.Experimental parameters for a selected Base Case are presented in Table2.The other experiments involved per-turbations from the Base Case with respect to reactor pH, inlet ue gas concentration of SO2,reactor temperature,and Table2Experimental parameters of the Base CaseParameter ValueFlue gas ow rate(m3=s STP)0.0275Inlet ue gas concentration of SO2(ppmv)991 Limestone content of feed stream(wt%)10 Temperature(K)296Slurry level in the reactor(m)0.585 Oxidation air rate to reactor(m3=s STP)1:07×10−4 Pressure in plant(Pa)1:013×105 Reactor pH 4.5 Limestone type Faxe limestone Slurry concentration of Cl−0.0 Chemical analysis of Faxe limestone is provided in Kiil etal.(1998).slurry concentration of Cl−.Other parameters in Table2 such as ue gas ow rate,and oxidation air rate,deviated a few percentage points among experiments.The most essen-tial parameter for a wet FGD plant is the degree of desul-phurisation.However,for plants employing the forced oxi-dation mode(most European and Japanese plants),another essential parameter is the amount of residual limestone in the gypsum.There are two reasons for this:(1)good utilisation of limestone and(2)a saleable gypsum product(i.e.less than about3wt%residual limestone,(Ib k,1996)).More recently several wet FGD plants in the USA have converted their wet lime/limestone/waste plants to gypsum producing facilities,and the trend is continuing(Soud,2000).How-ever,the majority of wet FGD plants in the USA produce a mixture of calcium sulphite and gypsum as opposed to commercial quality gypsum.In Europe the wet FGD plants are designed and built to produce gypsum suitable for wall-board utilisation rather than disposal(Clarke,1993).Con-sequently,the degree of desulphurisation and the amount of residual limestone in the gypsum were analyzed for each experiment.3.1.E ects of reactor slurry pHFig.4shows the SO2removal e ciency atdi erentpH values with an SO2inlet concentration of991ppmv.The SO2removal e ciency appears to increase almost linearly from66.1%to71.5%when increasing the reactor pH in a range from3.5to5.5.At a higher pH,the dissociation reaction of SO2:SO2+H2O HSO−3+H+(2) is shifted to the right,leading to an increase in the enhance-ment factor and thereby in the degree of desulphurisation. Zhong(1998)did some wet FGD experiments in the falling ÿlm pilotplantdescribed in Kiil etal.(1998)at50◦C,with an inletSO2concentration of about1000ppmv.In this case, the SO2removal e ciency also increased approximately lin-early when increasing the holding tank pH in a range of pH of4.5–6.1(Fig.4).The results also agree well with YooY.Zheng et al./Chemical Engineering Science 58(2003)4695–4703469936Slurry pH value020406080100S O 2 r e m o v a l e f f i c i e n c y %5parison of pH e ects on SO 2removal e ciency between JBRs and a falling ÿlm pilot plant.The JBR of this work was run at 23◦C,the ue gas inletSO 2concentration was 991ppmv,and other parameters are given in Table 2.The falling ÿlm pilotplantwas run at50◦C,with a ue gas inlet SO 2concentration of 1000ppmv.The inlet SO 2concentration of Yoo and Kim’s JBR was about 300ppmv with a reactor pressure drop of about 1100Pa.All experimental results were obtained at steady state operation of the pilot plants.Error bars are shown on the ÿgure.and Kim’s (1998)JBR experiment s.Itis notpossible t o extrapolate directly the SO 2removal e ciency for the ÿrst two processes to full-scale plants using the results in Fig.4,because in both cases the full-scale plant has additional SO 2removal.In a packed tower there is a spray section above the falling ÿlm section and a gas–liquid contact zone below.In the JBR process there is injection of slurry into the ue gas before it enters the bubbling reactor (Fig.1).Only the trend in the dependence of removal e ciency with pH is provided in Fig.4.The total e ciency of a full-scale plant cannotbe seen.However,in bot h cases itcan be seen t hat a substantial desulphurisation takes place.The reason for a higher SO 2removal e ciency in Yoo and Kim’s exper-iments,which also did not include a desulphurisation zone prior to the JBR,may be due to a di erent setup and ex-perimental conditions.In their case the reactor has a diam-eter of 220mm and a height of 500mm.The diameter of the sparger tube is about 6mm and the oriÿce diameter is 2mm.The inletSO 2concentration is only about 300ppmv and there is also a deeper sparger immersing length corre-sponding to a reactor pressure drop of about 1100Pa.In our case the reactor pressure drop is only about 600Pa.Fig.5shows the residual limestone level in the gypsum atdi erentpH values wit h an SO 2inlet concentration of 991ppmv.The residual limestone level of the gypsum in-creases with increasing pH values.These results are in good agreement with full-scale results of Gilbertetal.(1987)and Someshwar etal.(1989).In the wet FGD process,the pH value of the slurry is very important because pH a ects the dissolution rate of limestone,the relative concentrationdistribution of HSO −3and SO −3,and the dissolution equi-346Slurry pH value00.40.81.21.62R e s i d u a l l i m e s t o n e i n g y p s u m w t %Fig.5.The residual limestone in the gypsum at di erent pH values.Parameters are given in Table 2.The experimental results were obtained at steady state operation of the pilot plant.Error bars are shown on the ÿgure.librium of SO 2(Eq.(2)).Low pH favors the dissolutionrate of limestone.A decrease in pH of 2corresponds to a 100-fold increase in hydrogen ion concentration and almost the same in limestone dissolution rate (Kiil,Johnsson,&Dam-Johansen,1999).The operation at lower pH ranges has a smaller risk of scaling and plugging (Burford,1997).The JBR process is designed to operate in a pH range of 3–5where the driving force for limestone dissolution is high,resulting in nearly complete reagent utilisation.At low pH,the prevailing sulfurous species is bisulphite (HSO −3)as op-posed to sulÿte ion (SO 2−3).HSO −3is more easily oxidizedo SO 2−4than SO 2−3(Takeshita &Soud,1993).Thus,itis advant ageous t o run a wetFGD plantatlow values of pH from a limestone utilization and gypsum production point of view.However,the degree of desulphurisation decreases atlower pH,as seen in Fig.4.A transient mass balance calculation for total S or Ca over the JBR,assuming mixed ow for the slurry phase,provides an equation for the time,t ,it takes to obtain a given concentration (total S or Ca)in the slurry (Fogler,1986)t =− ln 1−CC o;(3)where is the space time (i.e.the slurry volume divided by the volumetric feed rate)and C o is the steady-state concen-tration in the JBR.The time it takes the e uent concentration to reach 99%of its steady-state value is found by inserting C =0:99C o in Eq.(3).This gives t =4:6 =4:6×35:5=163h,i.e.about7days.Itcan be seen in Fig.6that experimental data suggests that the time to reach the steady-state value is about 9days (216h)rather than 7.However,taking into account the uncertainties of the measurements and the as-sumption of perfect mixing in the above calculation the agreement seems reasonable.The solids concentration in the Base Case experimentwas used as an indicat ion of when4700Y.Zheng et al./Chemical Engineering Science 58(2003)4695–4703246810Running time (days)S o l i d s c o n c e n t r a t i o n w /w %Fig.6.Solids concentration levels of the Base Case experiment as a function of time.Parameters are given in Table 2.Error bars are shown on the ÿgure.Table 3Degree of desulphurisation,residual limestone in the gypsum,and solids concent rat ion atdi erent ue gas inletSO 2concentrations InletSO 2concentration (ppmv)991502Degree of desulphurisation (%)69.480.1Residual limestone in the gypsum (wt%)0.660.30Time to reach steady state (h)163260Solids concentration (wt%)27.232.3Parameters are given in Table 2.the system had reached a steady state.In the pilot plant the steady-state concentration is in uenced by the limestone concentration in the feed tank.In full-scale systems,on the other hand,the level of solids concentration at steady state is determined by the water balance.However,it should be mentioned that the advantages of operating the scrubber at low slurry concentrations include reduced plugging and reduced wear of JBR internals.There is also more risk for the sparger tubes to be plugged when the solids concentra-tions become high (¿24%)(Burford,1997).In the experi-mentatpH 5.5,aboutone-t hird of t he cross sect ion of each sparger tube was plugged after a running time of 5days.3.2.E ects of inlet SO 2concentrationTable 3shows the degree of desulphurisation,residual limestone in the gypsum,and solids concentrations at dif-ferentinletSO 2concentrations at a pH of 4.5.The e ect of inletSO 2concentration on SO 2removal e ciency is quite signiÿcant.An increase in inlet SO 2concentration leads to a decrease in SO 2removal e ciency ata given setof scrubber operating conditions.This drop in SO 2removal e ciency is a result of the lower enhancement factor for absorption of SO 2,which may be evidenced by comparing with the sim-ulations of Kiil etal.(1998).Table 4Cl −e ects on SO 2removal e ciency,and residual limestone in the gypsumInletSO 2concentration (ppmv)502605Cl −concentration (g/l)025Degree of desulphurisation (%)80.199¡Residual limestone in the gypsum (wt%)0.3 3.6Parameters are given in Table 2.The limestone utilisation increased with a decrease in in-letSO 2concentration.At a lower SO 2concentration,less limestone is needed to maintain the same pH of the holding tank,and the limestone slurry feed rate is decreased,result-ing in an increase in JBR solids residence time.It took a longer time to reach a steady state in the case of a lower inletSO 2concentration because the feed rate of limestone slurry was lower.To make sure a steady state was reached,the mass balances of Ca 2+and S were calculated.In the Base Case,the balance deviation of Ca 2+and S was −5:5%and 2.2%,respectively.Most of the deviations were within ±7%.The time needed for the system to reach a steady state at di erent conditions was also estimated.At an inletSO 2concentration of 991ppmv it should take 163h for the system to reach a steady state and at an inlet SO 2concentration of 501ppmv the value was 260h (these esti-mated values may,due to the assumption of perfect mixing made in the calculations,be somewhat lower than the actual values as discussed in the previous paragraph).The mean residence time of limestone slurry increased from 35.5to 56:5h.The reason for this increase in residence time is that the limestone slurry feed rate dropped from 3.5to 2:2kg =h because the limestone concentration in the feed tank was the same in all experiments.3.3.E ects of Cl −Table 4illustrates the e ects of Cl −on SO 2removal ef-ÿciency and residual limestone level of the gypsum.The addition of Cl −enhances the SO 2removal e ciency from about80%t o above 99%.This is in good agreementwit h Yoo and Kim’s results (1998).They also found that the SO 2removal e ciency showed a maximum value (about99%)in the range of 10–30g Cl −=l when Cl −was added to the slurry in the form of CaCl 2.The main reason for this e ect is assumed to be an increase in the gas–liquid surface area due to foaming.The addition of Cl −caused the slurry level to rise 8cm higher in the reactor and extensive foaming was observed.The gas/liquid interfacial area is expected to in-crease accordingly as the slurry level above the sparger tube is increased (Riber,2001).Other reasons for the very low outlet concentration of SO 2measured could be a sampling error because of fouling of the sample line or because of an increased level of residual limestone in the gypsum.As the free space above the liquid surface is 41cm and the slurry level only rose 8cm,it is unlikely that foam could penetrateY.Zheng et al./Chemical Engineering Science58(2003)4695–47034701 Table5Degree of desulphurisation at di erent reactor temperaturesReactor temperature(K)Degree of desulphurisation(%)29669.432368.1Parameters are given in Table2.the sampling system and impair the SO2measurement.Theaddition of Cl−to the slurry elevates the content of residuallimestone from about0.3to3:6wt%.This is because of alower limestone dissolution rate due to the increased con-centration of Ca2+(Frandsen etal.,2001).One could argue that the large excess of CaCO3content may contribute to the high SO2removal rate rather than the foaming.However,in our previous work on a fallingÿlm column the removal ef-ÿciency was only83%with a residual limestone content of 4:6wt%,using the same Cl−level.In these earlier exper-iments,an SO2removal increase with the addition of Cl−was also observed(Frandsen,2000;Frandsen etal.,2001). The mechanism through which Cl−modiÿes the froth ten-dency of the slurry is unknown.Probably,the increase in ionic strength of the slurry(as a result of an elevated con-centration of Cl−)modiÿes the surface tension and thereby the foaming capacities of the slurry,but this could not be conÿrmed.Detailed measurements of the slurry surface ten-sion as a function of Cl−concentration is needed.3.4.E ects of reactor temperatureTable5shows the e ect of reactor(i.e.absorber and ue gas)temperature on the degree of desulphurisation.The SO2 removal e ciency decreased from69.4%to68.1%when the reactor temperature was increased from296to323K. These experimental results are so close(¡1:5%di erence) that the e ect of experimental errors cannot be excluded. However,a lower degree of desulphurisation with increas-ing temperature is indeed expected due to the lower water solubility of SO2at higher temperatures(Kiil etal.,1998). Itshould be ment ioned t hatt he experimentat323K did not reach a steady-state solids concentration level due to a poor long-term performance of the burner at high temper-ature.However,previous experiments have shown that the degree of desulphurisation is practically insensitive to the solids content of the slurry and the results seem credible. Obviously,the residual limestone level of the gypsum could not be estimated for this particular experiment.3.5.Particle size distributions of gypsumFig.7shows that the PSD of gypsum varied only slightly with changing values of slurry pH and inlet SO2con-centration.For all the experiments,the volume moment mean(i.e.equivalentvolume mean diamet er,deÿned in Rawle,1997)of the gypsum particles are in the range of0.010.11101001000Particle diameter, µm20406080100Cumulativevolumefraction,%limestonepH=4.5pH=5.5pH=3.5502 ppmvFig.7.Particle size distributions of gypsum and Faxe limestone.Process parameters are given in Table2.The502ppmv in the legend refers to the inlet ue gas SO2concentration.The experimental results were obtained at steady state operation of the pilot plant.42–50 m.In the Base Case experiment,about50vol% is smaller than44 m and about90vol%are smaller t han 94 m.According to results obtained at Georiga Yates plant,a particle size distribution displaced towards smaller part icles was found athigher inletSO2concentrations and slurry pH values(Burford,1997).The author stated that this was probably because of lower solids residence time at higher inletSO2concentrations and slurry pH values.How-ever,this tendency was not found in our experiments.The secondary nucleation of gypsum in a JBR system may be less than that in a common spray tower.The latter employs large centrifugal pumps to move reacted slurry,probably causing crystal attrition and secondary nucleation.It was also found that the gypsum particle size was reduced when y ash was present during an elevated ash-loading test at Georiga Yates plant(Burford,1997).However,there was no y ash addition in our experiments,only limestone im-purities.Notice,that the mean limestone particle size(about 30 m)is signiÿcantly smaller than that of the gypsum particles(42–50 m).4.ConclusionsAn experimental parameter study with a pilot-scale jet bubbling reactor for wet ue gas desulphurisation was con-ducted.Parameters varied were ue gas SO2inletconcen-tration,slurry pH,reactor temperature,and concentration of Cl−.They all a ect,to various extents,the degree of SO2 removal,limestone utilisation,and gypsum quality.The presence of Cl−can decrease the purity of the gypsum sig-niÿcantly.Running the system at a lower pH value or remov-ing Cl−before the reactor can reduce the residual limestone level in the gypsum.There is,however,a trade-o between the limestone utilization,gypsum production and the de-gree of desulphurisation.In future work,experiments with。