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介绍了二种增加多用途飞机高温发动机寿命的优化控制方法。即通过综合控制压气机导向器叶片角度与喷管临界截面面积的快速变化推力法 ,和在此基础上增加可调涡轮导向器控制发动机的方法
Two kinds of optimal control methods to increase the life of multi-purpose aircraft high temperature engine are introduced. Namely through the comprehensive control of the compressor guide vane angle and the critical cross-sectional area of the nozzle rapidly changing thrust method, and on this basis, an adjustable turbo pilot control engine