加力燃油控制系统的研究和发展  

Research and Development of Afterburner' s Fuel Control System

作　　者：朴英 张绍基 

出　　处：《国际航空》1995年第11期43-45,共3页International Aviation

摘　　要：对高性能战斗机,其发动机加力燃油控制系统性能十分重要.50多年来,各国一直在竞相研究和发展军用发动机加为燃烧室及其燃油控制系统,并形成了两种典型风格:即欧美风格和俄国风格.军用发动机加力燃油控制系统主要包括:加力燃油泵、加力调节器、加力计量装置及燃油分配装置.随着发动机数控技术的研究和发展以及新型复合材料的应用,使加为燃油控制系统逐步向数字电子化、小型化、一体化方向发展,大大改善了军用发动机的性能.It is very important to improve the performance of the afterburner ' s fuel control system for the advanced military engine . The US, British , French and Russia have being researched and developed the afterburner and its fuel control system for many years. The fuel control system includes mainly the fuel pump, controller , fuel flow meter and fuel flow divider . With the development of the FADEC and the application of the new composite , the fuel control system tends to electrical , small-scale and integrative direction , which will improve significantly the performance of the military engine .

关 键 词：军用飞机 发动机 加力燃油泵 燃油控制系统 

分 类 号：V228.1[航空宇航科学与技术—飞行器设计]