AVIC I develops and manufactures in series fighter, fighter bomber, bomber, transport, trainer aircraft, reconnaissance aircraft, turbojet engine, turbo fan engine, air-to-air missile and ground-to-air missile, etc. Major projects include F-10, FBC-1, FC-1, FTC-2000 aircraft and Taihang, Qingling, Kunlun Engines, which are well-known broadly. AVIC continuously broadens its product range.
中国一航系列发展歼击机、歼击轰炸机、轰炸机、运输机、教练机、侦察机与涡喷发动机、涡扇发动机和空空、地空导弹等，产品谱系日益丰富，其中包括已经部分公开的歼十、飞豹、枭龙、山鹰等飞机和太行、秦岭、昆仑等发动机。
Lead-acid battery and Zinc-silver battery have many limits in operarting environment and operating condition, The development of the aircraft Cd-Ni battery meet the motive requirements of the starting motor of the turbojet engine.
而铅酸蓄电池和锌银蓄电池在使用环境和使用条件上已有很多的限制，而镉镍航空蓄电池的发展满足了涡轮发动机起动马达动力要求。
The missile is roughly 3.5 m long and powered by a small turbojet/turbofan engine with an underslung intake.
导弹，大约是3.5米长，由一台小型涡喷/涡扇发动机用underslung摄入。
The design and test results of the new type high-subsonic speed submerged and semi-submerged intakes for cruise missile propelled by a turbojet engine have been introduced.
本文介绍了以涡轮喷气发动机为动力装置的飞航式战术导弹的一种新型高亚音速嵌入式、半嵌入式进气道的设计与试验研究结果。
The mathematical model of a turbojet engine and its control system was established.
研究了某型涡喷发动机及其控制系统的建模方法，并通过对燃油控制系统控制方程进
Turbojet engine is selected as propulsion system according to the practical situation.
其次，作为重要一环的推进系统，论文作了详细的论述与计算。
An airplane with an external propeller that is driven by a turbojet engine.
由涡轮螺桨发动机驱使的有额外推动器的飞机。
A design of a twin variable control system for Aero - turbojet engine
航空涡轮喷气发动机双变量控制系统设计
Simulations on the nonlinear model of the twin spool turbojet engine aerothermodynamics are conducted to verify the disturbance rejection and tracking performance.
所述方法在某型双转子涡喷发动机气动热力学非线性模型上对抗干扰性和目标跟踪进行了仿真验证。
Airplane powered by a turbojet engine.
由涡轮喷气发动机推动的飞机。
Experimental study of the flow field at the inlet of an engine in an altitude chamber experimental investigation of a rectifier for lowering the distortion of inlet air flow of turbojet engine in a higher altitude test facility
降低高空台涡喷发动机进气流场不均匀度装置的试验研究
An annular combustor with evaporation tubes was designed for certain micro-turbojet engine.
为某微型涡喷发动机设计了一个蒸发管环形燃烧室。
Experiments were performed to investigate surge problem of a single shaft axial flow turbojet engine during throttling.
对某型单轴涡喷发动机节流过程中的喘振故障进行了试验研究。
The turboprop engine is very much like the turbojet. It has an additional part, a propeller.
涡轮螺桨发动机与涡轮喷气发动机十分相似。它多了一个螺旋桨部件。
Meanwhile, the emphasis was placed on analysing the effect of inlet circumferential and radial pressure distortions on the performance and reliability of the twin-spool turbojet, the results of the analysis provide the experimental basis for matching between the engine and its intake.
重点分析了进口周向压力畸变和径向压力畸变对某型双转子涡喷发动机性能及可靠性的影响，为发动机/进气道的匹配提供试验依据。
Reducing Turbojet Engine Vibration by Optimizing Blade Arrangement Order on Rotor
采用转子叶片优化排序技术降低涡喷发动机的振动
Under the identical regime and inlet flow conditions, the performance of the twin spool turbojet engine was simulated respectively by real time model and non real time model.
该实时模型包括：线性化的压气机特性模型、简化的涡轮特性以及非线性方程组的降维处理。
A stage by stage mathematical model of the compressor in a turbojet engine is developed based on the control volume theory.
根据控制体理论，建立了涡喷发动机中压气机的逐级数学模型。
The process of loosing compressor aerodynamic stability in a turbojet engine was analyzed using the correlation integral method.
对某涡喷发动机压气机的气动失稳过程进行了相关积分分析。
This paper covers the designs of Hardware in the Loop Simulation (HILS) testing of minitype turbojet engine digital control regulator, and hardware and software configurations.
介绍了某小型涡喷发动机数控调节器的半实物仿真试验系统的设计，以及软件和硬件的试验配置。