| 1. | Structural design study of a micro - turbojet engine
微型涡喷发动机结构设计研究 |
| 2. | Experimental study on the inlet total pressure distortion of a turbojet engine
某型涡喷发动机进气总压畸变的试验研究 |
| 3. | General specification of turbojet engines and turbofan engines for aircraft
飞行器用涡轮喷气及涡轮风扇发动机通用规范 |
| 4. | Failure mechanism and improvement measures of high - temperature and high - speed ball bearings for turbojet engine
涡喷发动机高温高速轴承失效机理及改进措施 |
| 5. | 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。 |
| 6. | Turbojet engine is selected as propulsion system according to the practical situation . the work of this part ranges from design to characteristic analysis . the characteristic curves of engine in various situation are shown , which provides preparation for trajectory computation
并对涡喷发动机从设计到特性分析做了大量的工作，给出发动机在不同工作状态下的特性曲线，为进一步研究弹道设计提供了前期的准备工作。 |
| 7. | Since delays are often encountered in engineering systems , ecology systems , electricity systems , management systems and control systems such as the turbojet engine , microwave oscillator , nuclear reactor , controlability of systems and optimal control , etc . the phenomena of delays are investigated by more and more scientists
在工业工程、生态系统、电力系统、管理系统、控制系统等实际系统中常常遇到很多时滞问题，如涡轮喷气发动机、微波振子、核反应、系统的可控性和最优控制等问题，所以时滞现象越来越受到众多科学家的广泛关注。 |
| 8. | By adjusting many variable geometry components of the engine , bypass ratio can be changed during large range ( the most 0 . 25 of military fighter ) . the high specific thrust characteristic of turbojet engine and the low specific fuel consumption characteristic of the turbofan engine can be realized during different flight phase by the usage of vce technology
变几何变循环发动机是应用于第四代多用途战斗机的理想动力装置，通过多个部件几何的调节在较大范围内改变涵道比，能够使发动机在不同航段分别实现涡喷发动机的高单位推力性能和涡扇发动机的低油耗性能。 |
