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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;
High speed micro-turbomachinery such as micro gas turbine and micro turbojet engine has an apparent feature that they have light weight and high speed rotor with complex structure. 微型高速透平机械如微型燃气轮机和微型喷气发动机的一个显著特点是都具有结构复杂，重量轻的高速转子。
micro turbojet engine 微小型涡喷发动机
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。
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
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。
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
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。
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.
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。
The rocket sled test can imitate the dynamic conditions of missile launching, it is very important for missile turbojet engine design. 火箭橇试验能够真实的模拟导弹发射条件,它对于弹用涡轮喷气发动机研究具有十分重要的意义。
The rocket sled test was carried out for overall investigatingthe 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。
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。
Turbomeca company, a subsidiary of micro-turbine engine company, is the largest missile in Europe, UAV and auxiliary power unit (APU) turbojet engine manufacturers. 透博梅卡公司的子公司微型涡轮发动机公司，是欧洲最大的导弹、无人机和辅助动力装置（APU）涡喷式发动机的生产商。
A testing instrument is described for the box against pant of some turbojet engine used for checking the breakdown within the electric circuit and for adjusting the whole machine functions, while the box against pant is being examined. 摘要某涡喷发动机防喘盒检测仪用于该型发动机防喘盒检修时的内部电路故障检测和整机性能调试。
The particle trajectory is calculated with certain amoune of selected control rules by establishing mathematical mod els such as whole missile mass calculation model,aerodynamic estimation model and turbojet engine performance interpolation. 通过建立全弹质量计算模型、气动估算模型和涡喷发动机性能插算等数学模型 ;选取一定的控制规律进行了质点弹道计算 .
Making its first flight on 18 October 1966, the KM was powered by a whopping 10 turbojet engines and weighed up to 540 tons. 他第一次飞行是在1966年10月18日，KM装有10台非常巨大的涡轮喷气引擎，最大起飞重量达到540吨。
Chinese media said last year that the PLA had finally developed an indigenous turbojet engine called the WS-10A, or "Taihang", as it is known commercially, and had started installing it in the J-10. 中国媒体曾报道，去年人民解放军已研发出名为WS-10A的自主涡轮喷气式发动机，其商业用名为“太行”，并且已经开始安装入J-10战机中。
As an example,the method provided was adopted to rectify the parameters in the simulation model of a given twin-spool reheated turbojet engine,and the simulation achieved satisfactory accuracy. 应用本文方法对某型双转子加力涡喷发动机仿真模型进行校正，获得了满意的仿真精度。