afterburner

noun

1. （喷气发动机的）加力燃烧室，补燃室
   a device for increasing the power of a jet engine

1. Numerical Simulation of 3D and 2-Phase Chemical Reaction Flow for Afterburner
   加力燃烧室三维两相化学反应流数值模拟
2. Mechanism Investigation on Aircraft Afterburner Flameholder of High Efficiency 、 Low Drag and High Temperature Resistance; The addition of little Be can further improve the ignition temperature.
   高温、低阻、高效加力燃烧室火焰稳定器机理研究加入微量的铍能进一步提高含混合稀土的阻燃镁合金的起燃温度。
3. Speed density metering afterburner fuel control
   转速、密度燃油调节
4. The intensity of the gas backflow and axial swirl ond the dilution in the afterburner are enhanced by increasing the air-to-fuel ratio, and then the combustion efficiency is improved.
   提高空燃比，可增强补燃室中燃气的回流和轴向涡流强度，加大掺混力度，从而提高燃烧效率。
5. In the afterburner, the complicated temperature distribution has close relation with the dilution, combustion and flow of the air and gas.
   补燃室内复杂的温度分布和空气与燃气的掺混、燃烧及流动状态有密切关系。
6. Many jets have an afterburner.
   许多喷气机都有加力燃烧室。
7. The aircraft had 412 passengers on board, one of whom said he saw flames "like the afterburner of a fighter jet" from an engine.
   该机当时有412名乘客，其中一名乘客表示，他看到一台发动机喷火，“就像开了加力燃烧室的战斗机”。
8. The afterburner system is completely automatic and can be easily shut down when clean products are being fired.
   该重烧系统实现了完全自动化，并且当清洁产品烧制完成后，系统易于关闭。
9. This report discusses the study of detailed nonlinear real time performance simulation for a two spool turbofan engine with afterburner.
   本文就双轴加力涡扇发动机详细非线性实时仿真模型进行了研究。
10. Design and simulation of afterburner state control system of aero engine
    航空发动机加力状态控制系统设计与仿真
11. This airplane can go out to high subsonic speeds very easily without using afterburner. Residents have been complaining of the "boom" which is heard whenever a jet breaks through the sound barrier.
    这架飞机能够很轻松地在不打开加力的状态下飞到高亚音速。居民们一直抱怨喷气式飞机在作超音速飞行时所产生的音爆。
12. Afterburner fuel control pressure regulator service
    加力燃烧室供油调节调节压力的燃料气供给
13. New industries, speed up the afterburner; create the future, a blueprint reproduction.
    新兴产业，加速加力；创造未来，再现蓝图。
14. Research and development of afterburner control system for military aeroengine
    军用航空发动机加力控制系统的研究和发展
15. Numerical simulation of turbofan engine afterburner light-on process was presented.
    发展了一种低涵道比混合排气加力涡轮风扇发动机接通加力时的数值模拟方法。
16. The ignition system is applied to the afterburner structure with full inner cone for improving performance.
    这种点火系统特别适用于全锥加力燃烧室结构，以改进加力燃烧室性能；
17. Influence of low pressure on pressure and heat release fluctuations in Afterburner
    低压对加力燃烧室压力脉动和放热脉动的影响
18. Comprehensive Analysis of Low Pressure Condition Established with Ejection or Compressor Extraction for Afterburner Nozzle
    引射器引气与压气机抽气建立加力燃烧室喷口低压条件的综合分析
19. In order to show the effect of the simulation, the results of the simulation model calculated have been compared with the testing results. The compared result shows that the simulation model can simulate mixed flow turbofan engine with afterburner for ground starting effectively.
    为说明所建立的起动性能模型的模拟效果，将程序计算结果与试验结果进行了比较，结果表明该起动仿真模型能较准确地模拟混排加力涡扇发动机的地面起动过程。
20. Turbofan Afterburner and Multi-function Thrust Vectoring System
    涡扇加力和多功能推力矢量装置
21. The above experimental result is of value for the mechanism and suppression of low frequency combustion oscillation in an afterburner of a turbofan engine.
    上述结果对研究低频振荡燃烧机理和抑制技术有一定的参考价值。
22. This paper presents the combustion efficiency characteristics of an afterburner with bluff-body flame holders investigated with both numerical and experimental methods.
    本文对装有钝体火焰稳定器的加力燃烧室燃烧效率特性进行了数值分析和实验研究。
23. Cooling flow technique for designing afterburner heat shields
    气膜冷却技术在加力燃烧室隔热屏设计中的应用
24. Lastly, the main and afterburner fuel regulators were simulated under different conditions.
    最后在不同的给定条件下对主、加力燃油调节器进行了仿真研究。
25. The Flow Field and Combustion Efficiency Characteristics of Afterburner with Numerical Method
    数值分析加力燃烧室的燃烧效率和燃烧流场
26. Flight test research on static characteristics of afterburner fuel control system for turbojet engines
    涡喷发动机加力调节系统静特性试飞研究
27. It not only can control the engine at maximum-thrust and afterburner, but also gets over the disadvantage of common fuzzy controllers which cannot do real-time adjustments and control because of the fast dynamic response of the engine rev.
    其可以在最大和加力状态对发动机状态进行控制，克服了一般模糊控制器因发动机转速动态响应变化快而不能进行实时调整和控制的缺点。
28. Design improvement characteristics of EFE fan afterburner and nozzle system are particularly discussed.
    重点介绍了EFE型发动机的风扇加力燃烧室、喷管系统设计改进的特点。
29. Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.
    在涡扇发动机基础上，以脉冲爆震燃烧室代替普通加力燃烧室构成涡扇-脉冲爆震组合发动机。

noun

1. a device injects fuel into a hot exhaust for extra thrust