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DEVELOPMENT OF ELECTRONIC CONTROL UNIT FOR THE SPEED CONTROL OF LOW PRESSURE COMPRESSOR ROTOR OF AERO-ENGINE OF MILITARY CLASS AIRCRAFT PARTICULAR TO AL31FP ENGINE
DEVELOPMENT OF ELECTRONIC CONTROL UNIT FOR THE SPEED CONTROL OF LOW PRESSURE COMPRESSOR ROTOR OF AERO-ENGINE OF MILITARY CLASS AIRCRAFT PARTICULAR TO AL31FP ENGINE
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机译：电子控制单元的开发，用于AL31FP发动机特有的军用飞机的航空发动机低压压缩机转子的速度控制
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摘要
The electronic engine control unit [EECU] is a part of electronic hydro-mechanical system for the adjustment and control of aero- engine parameters of military class aircraft at all the regimes of operation. The unit adjusts the engine parameters and gives signals for other control units, warning systems and flight data recorders. The present engine controller for the control of Low Pressure Compressor Rotor rpm (N1) of the aero-engine involves the development of an electronic module, PCB for the control of N1 and actuation of other hydro-mechanical systems, warning units and Flight data recorders.
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