英语释义

• jet engine in which a turbine drives air to the burner

• airplane powered by a turbojet engine

片语

ool turbojet铜管式涡轮喷气发动机

turbojet cycle涡轮喷气发动机循环

turbojet nozzle涡轮喷气发动机喷口

turbojet engine涡轮式喷射引擎；[航] 涡轮喷气发动机；喷气涡轮机

turbojet eng涡轮喷气发动机

nuclear turbojet核涡轮喷气发动机

bypass turbojet旁通涡喷发动机

turbojet inlet涡轮喷气发动机进气道

turbojet fighter[军]

leaky turbojet超低旁通比涡喷发动机

英汉例句

• 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。

• the rocket sled test was carried out for overall investigating the dynamic process of missile turbojet engine starting and accelerating.

  为了研究弹用涡轮喷气发动机动态启动加速过程，开展了发动机火箭橇试验研究。

• although multiple engines could possibly be synchronized to fire in a manner that reduces vibration levels, they will still be significantly greater than those generated by turbojet or rocket motors.

  从它的发动机和机身的构造材料，虽然多引擎也可能会被同步到火灾的方式，降低振动水平，但仍将大大高于由涡喷发动机或火箭发动机产生的。

• 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。

• 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 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。

• 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。

• 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。

• 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蹤进行了仿真验证。

• 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。

• stimulation to the pilotless aircraft turbojet engine proves several advantages of this controlling method, such as good robustness, sensitive response, and minimal stable error.

  对某型无人机涡喷发动机控制系统的仿真结果表明此控制方式具有鲁棒性好、响应速度快、稳态误差小等优点。

• the validation of the method is demonstrated by the identification examples of turbojet engine.

  以涡喷发动机辨识算例证明了该方法的有效性。

• 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。

• the turbojet is far more sensitive to dynamic inlet distortion than to steady inlet distortion.

  发动机对动态畸变流场的敏感度远高于稳态畸变。

• 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。

• 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。

• 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。

• a model for 100n class micro turbojet engine is established. software and hardware system design of the controller is accomplished by using robust control algorithm.

  建立了100n推力级微小型涡喷发动机模型，应用鲁棒控制算法进行了控制器软、硬件系统开发设计；

• this method was applied to designing the steady state controller of a two spool turbojet aeroengine with success.

  该方法被用于某型双转子涡喷航空发动机稳态控制器的设计，并取得了良好效果。

• 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。

• the results indicate that the circled simulation flat is of high reliability, and it can reflect the actual working process of the turbojet and its oil supplied regulating system.

  结果表明仿真平台具有较好的可信度，能够反映发动机及其供油调节系统真实的工作过程。

• 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。