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1)  gas engine
燃气发动机
1.
Development of Model WT615.00LPG Gas Engine;
WT615.00LPG燃气发动机
2.
Calculation and analysis of the primary energy ratio for gas engine-driven heat pumps;
燃气发动机驱动热泵一次能源利用系数的计算和分析
2)  rocket motor exhaust
发动机燃气
3)  gas engine-driven
燃气发动机驱动
1.
A combined air-conditioning system composed of gas engine-driven refrigerating unit and rotary dehumidification system is introduced, and the reasons influencing its extended application are discussed.
 介绍了燃气发动机驱动制冷机组复合转轮除湿空调系统的组成,探讨了影响其推广的原因。
4)  lean burn engine emission
贫燃发动机尾气
5)  LPG fueled engine
LPG燃气发动机
1.
In 2 periods of road test(more than 30,000 kilometers mileage)on a Santana 99 new model taxi,it is verified that the anti-oxidation, abrasion resistance,and oil changing mileage of this type of oil can meet the application requirements of LPG fueled engine.
长城润滑油分公司针对LPG燃气发动机的需求,推出了燃气发动机润滑油Ⅱ型。
6)  gas turbine engine
燃气涡轮发动机
1.
The development history of aviation engine oil is briefly described , and the trend of future aviation gas turbine engine oil is predicted.
简述了航空燃气涡轮发动机油的发展历史,预测了未来航空燃气涡轮发动机油的发展动向。
2.
This paper aims at developing an interactive CAD system for a gas turbine engine using the ANSYS finite element analysis software.
开发了基于大型有限元分析软件Ansys的燃气涡轮发动机辅助设计系统,该系统将CAD参数建模技术、工程有限元数值计算方法、经典强度计算理论与现代优化设计技术相结合,实现了涡轮盘、机匣和涡轮轴典型零件的参数优化设计的完整设计流程,建立了结构优化设计平台;并通过机匣的结构优化设计实例,验证了燃气涡轮发动机辅助设计系统的有效性。
3.
The gas turbine engine windmilling is a state that when the engine doesn t work,the rotors temporarily operate at a sub-steady rotating speed due to the airflow ram and the co-work of aerodynamics,rotor inertia and drag torque.
由于很多燃气涡轮发动机都缺乏计算风车特性必需的低转速状态的部件特性,给计算发动机风车状态的特性带来了很大的困难。
补充资料:航空发动机推重比(见航空发动机推力)


航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine

  hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
  
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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