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90年代,推重比10一级加力式涡扇发动机研制成功,推重比15～20的发动机预研计划使航空工业进入一个崭新的发展阶段.推重比10一级发动机的涡轮进口温度已达到1580℃～1680℃.美国国防部开展的“综合高性能涡轮发动机技术”(IHPTET)计划和
In the 1990s, the thrust-weighted 10-stage afterburner turbofan engine was successfully developed, and the engine pre-research program with a thrust-weight ratio of 15 to 20 put the aviation industry in a completely new stage of development. The turbine inlet temperature of the 10- ℃ ~ 1680 ℃. The United States Department of Defense to carry out “integrated high-performance turbine engine technology” (IHPTET) plan and