您要查找的是不是:
- An aircraft in which a turbojet is used. 涡轮喷气式飞机一种带涡轮发动机的飞行器
- A turbojet engine used todrive an external propeller. 涡轮螺旋桨发动机一种用于推动外部螺旋桨的涡轮喷气式发动机。
- The turboprop engine is very much like the turbojet. 涡轮螺桨发动机与涡轮发动机十分相似。
- The turboprop engine is very much like the turbojet . 涡轮螺桨发动机与涡轮发动机十分相似。
- A turbojet engine used to drive an external propeller. 涡轮螺旋桨发动机一种用于推动外部螺旋桨的涡轮喷气式发动机
- In 1939 the turbojet brought an entirely new method of propulsion. 1939年,涡喷发动机引入了一种全新的推力方法。
- The turbojet and the turboprop are much more satisfactory for airplanes. 涡轮喷气发动机和涡轮螺桨发动机更适用于飞机。
- The validation of method is demonstrated by one-spool turbojet engine. 单轴涡喷发动机的算例证明了方法的有效性。
- In the case of afterburning, the effective blockage of the EBMC flameholder , i.e. 加 力时,改变尾缘射流速度,可以改变它的有效堵塞比,实现加力比的 无级调节,是一种可变流阻系数(*的稳定器。
- A turbojet engine in which a fan supplements the total thrust by forcing air directly into the hot turbine exhaust. 涡轮风扇喷气发动机一种涡轮喷气发动机带有一个风扇,通过将空气直接压入热的涡轮排气管而补充总推力
- The J-10 adopts an adjustable, chin-mounted air intake that supplies air to the single Lyulka-Saturn AL-31FN afterburning turbofan jet engine. J-10采用了一个可调节机腹进气口为一台留里卡-土星设计局的AL-31FN加力燃烧涡轮风扇发动机提供空气。
- Dispersity of gas flow can be enhanced and afterburning efficiency can be improved by increasing primary nozzle numbers and nozzle expansion ratio. 增加一次喷嘴的数目和加大喷嘴的扩张比增加了燃气的分散性,提高了补燃效率。
- At this point, we very much look forward to working with you in good faith met together for your business carrier oil Afterburning Tim! 在此,我们非常期望与您真诚相识,共同为您的企业航母添油加力!
- First came the turbojet, now obsolete, then the turboprop, which is still found onboard small planes. 最开始的引擎是涡轮喷射式,目前已淘汰;然后是涡轮螺旋桨式引擎,现在仍可在小飞机上看到。
- Breathing can be divided into jet engine turbojet engine, turbo-fan jet engine and combustion ramjet engine. 如果按照这一定义,除远程巡航导弹外,各种飞航式反舰导弹和空地、空舰飞航式导弹也属于巡航导弹。
- The influence of afterburning chamber length on secondary combustion efficiency and flow field were analyzed based on direct-connected ground simulation test. 结合直连式地面模拟试验,分析了补燃室长度对掺混流场和二次燃烧效率的影响。
- The experimental result has practical significance for correctly using the twin-rotor turbojet. 实验结果对于正确使用该类型双转子涡喷发动机具有重要的现实意义。
- The proposed modeling methods can be extended to study other gas turbines with different types.For example, a twin-spool or with afterburning gas turbine system. 该文提出的建模方法可扩展应用于研究其他结构类型的燃机,如双轴的或带有回热器的燃气轮机系统。
- Chiang, H. D., and W. C. Ho, “Miniature Liquid Fueled Turbojet Engine”, U. S. Patent #5782079. 蒋小伟,何无忌,“超小型燃油气涡轮喷射引擎”中华民国第136677号专利。
- Smetana, F. O.,“Turbojet Engine Gas Path Analysis A Review,”AGARD Conference Proceedings, No. 165, 4-5 April, 1974. 陈大光;张赫然;“用气动热力参数对发动机故障进行诊断与定位的实用方法;”北京航空航天大学硕士论文第二章;1989年.