Control device of microminiature turbojet and starting control method thereof
A technology of turbojet and control device, which is applied in the fuel control of turbine/propulsion device, engine components, and turbine/propulsion fuel delivery system, etc. Lightweight, simplified controls, easy-to-operate effects
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 The present invention will be further described in detail below in conjunction with the accompanying drawings.
 The amount of oil required for a micro turbojet engine is 0.1kg / h. According to the design requirements and characteristics of the turbojet engine control device, the aeroengine can run stably and reliably under any environmental conditions and any working conditions, and its performance benefits can be fully utilized. The realization of fuel supply quantitative and good starting control of the engine directly affects the performance of the engine, and is related to whether the engine can run reliably and efficiently in the expected working state. Aiming at the micro turbojet engine, the present invention proposes a novel control device which uses a fuel gear pump to independently complete the dual functions of establishing oil pressure and regulating oil volume and a control method suitable for starting the micro turbojet engine.
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