摘要
传统发动机加力燃烧室都采用V型火焰稳定器组织燃烧,自加力出现到第三代发动机,该方案一直得到了广泛应用。随着新一代歼击机性能指标的提高,发动机加力燃烧室需要新的突破才能满足更高推重比的要求。本文介绍了第三代、第四代发动机加力燃烧室的结构方案,并根据新一代加力燃烧室一体化设计思想,介绍了新颖加力燃烧室的结构方案。
V-shaped flame holder has been widely applied in aero-engine afterburner since the third generation aero-engine. Higher exhaust temperatures and survivability requirements for advanced aircraft have resulted in new creations in order to meet the increasing thrust-to-weight ratio development. This paper introduces the traditional configurations of afterburner and outlines one kind of new afterburner based on an integrative thought.
出处
《燃气涡轮试验与研究》
2008年第4期55-59,共5页
Gas Turbine Experiment and Research
