These steam conditions put new requirements on the steam turbine turbojet.
这些蒸汽工况对汽轮机涡轮喷气发动机提出了新的要求。
A turbojet, therefore, is more suitable at higher speed.
因此，涡喷发动机更适合更高速度的飞行。
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 improved and modification designs were conducted for a turbojet engine.
对某型涡轮喷气发动机进行了改进、改型设计。
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。
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。
Earlier this month it was feared that rust was eating through its four Rolls-Royce Olympus turbojet engines.
本月初，有人担心火神的四个罗尔斯·罗伊斯--奥林巴斯涡轮喷气发动机正被铁锈所腐蚀。
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。
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 response of turbojet engine to the turbulence-type of dynamic inlet total pressure distortion is discussed in this paper.
本文介绍涡喷发动机对湍流型动态畸变的响应。
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。
Driven by step motor, the metering valve can be used as fuel actuator in missile turbojet FADEC Full Autrority Digital Electronic...
燃油计量装置可用于弹用喷气发动机全权限数字电子控制系统。
Many off-design condition phenomena of a turbojet engine are related with the variation of incidence angles at front and rear compressor stages.
涡轮喷气发动机非设计状态下的许多现象都与共同工作时压气机前后各级攻角的变化有关。
A special instument is presented for monitoring the transient process in a turbojet engine, which is called "transient operating line indicator".
本文提出了一种测量涡喷发动机过渡过程的专用仪器——涡喷发动机过渡工作线显示仪。
The compressor's aerodynamic instability problem of a certain turbojet engine in the process of the throttling operation was experimentally studied.
对某型涡喷发动机节流过程中压气机的气动不稳定问题进行了分析研究。
Through noise data collection and power spectrum analysis of turbojet and turbofan, the main noise source and characteristics of noise are discussed.
通过对涡轮喷气及涡轮风扇发动机试车噪声的采集和声功率谱分析，讨论发动机的主要噪声源和噪声的特征。
The method of neural network incorporating a prior was given to recognize ignition time after analyzing ignition property of some missile turbojet burner.
在分析某弹用涡喷发动机燃烧室点火特性的基础上，提出利用结合先验知识的神经网络来识别发动机点火时刻的方法。
This paper presents the test plan, the results of the station parameters measurement for a typical turbojet engine and the analysis of measurement results.
本文介绍了一典型的涡轮喷气发动机全流程参数测量的试验方案、测试结果及分析。
This is the important research problem for starting of the jet engine in the sky. But it was researched for starting test of the small turbojet in the sky.
喷气发动机的空中起动是重要的研究课题，而小涡喷发动机的空中起动试验尚需探索。
Taking the certain small scaled turbojet as an example, the influence by mass injection and pre-cooled engine was calculated and analyzed along fly trajectory.
并以某小型涡喷发动机为例，沿飞行轨迹计算分析了射流预冷却对发动机性能的影响。
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。
He was familiar with the model. It was a Mobquet twin turbojet with a boosted Max airspeed. Mobquet Industries were known for their swoop bikes, not their speeders.
他很熟悉这种型号的飞船，这是Mobquet双胞胎公司的最大飞行马力涡轮喷气式飞船，Mobquet公司以他们的滑翔车著名，而不是飞船。
As an example, a robust control law is designed to the twin-spool turbojet engine system using the given method. The result shows that the given method is feasible.
文中以双转子涡喷发动机控制器设计为例，设计了基于LMI的鲁棒控制器，结果表明所给方法是可行的。
A brief view and results of tests for the effects of the inlet total pressure distortion on the performance and the stability of a two-spool turbojet engine are presented.
介绍进气总压畸变对双轴涡喷发动机性能和稳定性影响的试验及其结果。
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。
Meanwhile the pneumatic nozzle installed under left wall spray binder or coating liquid into turbojet material, in this way granule or successive even film can be obtained.
的气动喷嘴将粘合剂或包衣液喷入呈旋涡状的物料层，从而将粉体制成颗粒或获得连续均匀的衣膜。
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。
Based on experimental properties of compressor under inlet distortion, the performance of twin-spool turbojet engines is studied in this paper by means of numerical simulation.
基于畸变进气下压气机实验特性，数值模拟了畸变进气下双轴涡喷发动机的总体性能。
Rotor unbalancing is one of the main causes of vibration and noise in aero-engine, especially in micro-turbojet engine, which affects work performance and fatigue life directly.
航空发动机尤其是高速旋转的微型涡喷发动机，不平衡是造成转子振动过大以及产生噪音的主要原因之一，直接影响发动机的工作性能和使用寿命。
With a joint simulation flat of turbojet and its oil-supplied regulation system, three typical faults were simulated and evaluated with different model parameters and structure.
结果表明：供油调节系统故障对发动机正常工作有很大影响。
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