The invention belongs to an aero-engine control system, and particularly relates to an aero-engine digital electronic controller airborne system which comprises an EEC system, an engine power generation system, an airborne power source, an aircraft control system and an engine subsystem. The EEC system is installed on an aircraft engine, and the engine power generation system and the airborne power supply are mutually backed up to supply power to the EEC system; monitoring signals and control instructions of all subsystems of the engine are transmitted and gathered to the EEC system through cables, the EEC system is connected with an aircraft control system through a bus, the integrity of the engine serving as a product is improved, and independence and integrity of the structure and the function of the engine are achieved.

    本申请属于航空发动机控制系统,特别涉及一种航空发动机数字电子控制器机载系统,EEC系统、发动机发电系统、机载电源、飞机控制系统、发动机各个子系统;所述EEC系统安装在飞机发动机上,发动机发电系统与机载电源相互备份对EEC系统供电;发动机各个子系统的监控信号和控制指令通过电缆传输汇总到EEC系统,EEC系统通过总线与飞机控制系统连接,提高了发动机作为一个产品的整体性,实现了发动机结构和功能的独立完整。


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    Title :

    Airborne system of digital electronic controller of aero-engine


    Additional title:

    一种航空发动机数字电子控制器机载系统


    Contributors:
    LI JIAN (author) / CAO MAOGUO (author) / KA JI-WON (author) / YANG RANSHENG (author) / MAO XIAOQI (author) / LIANG JING (author) / SUN JIAWEI (author) / YANG YONGHUA (author) / LU WENRUI (author) / DENG RUTAN (author)

    Publication date :

    2024-10-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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