afterburner

美 [ˈæftərbɜːrnər]英 [ˈɑːftəbɜːnə(r)]
  • n.(喷气发动机的)加力燃烧室,补燃室
afterburnerafterburner

noun

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

noun

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

数据来源:WordNet

  1. 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

  2. Feasibility Analysis of a New Inner Dumped Afterburner Concept

    新型内突扩加力燃烧室方案可行性分析

  3. 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

  4. 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

  5. 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

  6. 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

  7. Flow Field Calculation and Buckling Analysis for Afterburner

    隔热屏的流场计算及其屈曲分析

  8. 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

  9. Development of Side - Mounted , All - Time and Two - Phase Ignition System for Afterburner

    旁路式、长明灯两相加力点火系统的研制

  10. 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。

  11. 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

  12. 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。

  13. Large Eddy Simulation of Pollutant Performance in an Afterburner

    加力燃烧室污染特性的大涡模拟

  14. 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;

  15. The Investigation on Heat Transfer Characteristics of the Longitudinal Ripple Heat Shield Channel in Afterburner

    加力燃烧室纵向波纹隔热屏通道换热特性的试验研究

  16. 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

  17. 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。

  18. 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

  19. Numerical Simulation of the Cooling Performance of an Afterburner Air Blast Spraybar

    加力用气冷气动雾化喷油杆冷却性能数值模拟

  20. Large eddy simulation in turbulent combustion research Numerical simulation of the turbulent flow in a 3D afterburner

    湍流反应流研究中的大涡模拟三维加力燃烧室湍流流场的数值模拟

  21. An experimental investigation on infrared radiation characteristics of 2-D nozzles of turbofan engine afterburner

    无加力涡扇发动机二元喷管的红外辐射特性实验

  22. 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。

  23. Speed density metering afterburner fuel control

    转速、密度燃油调节

  24. Body-fitted coordinate systems for large-eddy simulation of the model Afterburner

    贴体坐标系下模型加力室的大涡模拟

  25. Numerical Simulation of Two phase Turbulent Combustion Flow in an Afterburner Under Generalized Nonorthogonal Curvilinear Coordinate Systems

    非正交曲线坐标系数值模拟加力燃烧室湍流两相流燃烧

  26. 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。

  27. 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。

  28. Aviation Vapor Core Pump is mainly applied in aviation engine afterburner system fuel pumps , also applied in main fuel systems .

    汽心泵主要应用于航空发动机加力燃油系统,也可应用于主燃油系统。

  29. Calculation of fuel concentration distribution in afterburner with V-shape flameholders

    带多圈环形V型稳定器的加力燃烧室两态燃油浓度分布计算

  30. The fluid fields in modelling afterburner are calculated using SIMPLE procedure , it is found difficult to make the calculation convergence .

    在用SIMPLE方法计算模型加力燃烧室的流场时,发现SIMPLE方法存在不易收敛的问题。