关键词: 航空发动机;发动机控制;防喘控制+

Abstract: The design and development of engine surge control system,especially the parameters of heat disturbance when the fighter launches a missile,were discussed in this paper.Four heat disturbance parameters(inlet relative average temperature increment(δT);temperature rising rate(dT/dt);equivalent heat region angle(Φ_e);continuous time of heat disturbance(t_B)) were introduced and the criterion for optimal design of a engine surge control system is provided by means of tests and data analysis.A flight test with this engine surge control system has completed and it is shown that the method of design and development for engine surge control system introduced is successful.

Key words: Aircraft engine;Aeroengine control;Engine surge control~+