Missile Turbofan Engine Starter Electrical System Design, Technical Studies,

The thrust of power equipment must be increased greatly on the basis of great thrust level of the prime cruise missle according to the technical requirement of the developing cruise missle. The engines which have come into use and research cannot meet the need of the developing cruise missle. The starting electrical system design for the missle turbofan engine in double harness with the key technical research and test of great thrust level of the missle turbofan engine.The demonstration of the design technology of the main accessories and the general technology must be completed.This thesis just aims at these problems and carries through the starting electrical system design for the missle turbofan engine as a basis for the unique manufacture rule and short life and low cast of the missle engine.In this design the technology and cartridge starter used by the missle engine in-country are utilized.The key accessories such as powder starter, cartridge starter and starting control box will be designed.The sticking technology can be brought through simulation test and debugging test. It can obtain the ways of starting control of the missle turbofan engine and the technology and the practical experience of resisting disturb in order to establish the base of designed engines and achieve the requirement of the missle launch scheduling.