...由于爆震循环具有高热循环效率(可达49%)和压力增益(增压比可至20左右)特性,因此基于脉冲爆震燃烧室(Pulse Detonation Combustor,PDC)的混合式发动机引起了人们的特别关注,并被认为是未来高性能、轻重量、低成本航空发动机的潜在优良方案。
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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。
Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.
采用汽油和空气作为燃料和氧化剂，进行了脉冲爆震燃烧室(PDC)与涡轮相互作用的原理性模型试验装置的试验。
Experimental investigations of a principle model of interaction of pulse detonation combustor (PDC) with turbine were made by using gasoline and air as fuel and oxidizer.
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