The invention belongs to the technical field of aircraft wing fuel tank balance design, and particularly relates to an aircraft wing fuel tank fuel quantity automatic balance method which is implemented based on an aircraft wing fuel tank fuel quantity automatic balance system, a balance monitor automatically carries out balance according to set logic, manual work is not needed, and the balance efficiency is improved. The fuel quantity in three wing fuel tanks can be rapidly controlled within the average fuel quantity M +/-300kg in real time, the fuel quantity in the other wing fuel tank can be controlled within the average fuel quantity M +/-900kg, the precision can be controlled by adjusting the balance adjusting threshold H and the balance control threshold I, and the precision requirements of different airplanes for fuel imbalance control are met.

    本申请属于飞机机翼油箱平衡设计技术领域,具体涉及一种飞机机翼油箱内燃油量自动平衡方法,基于飞机机翼油箱内燃油量自动平衡系统实施,由平衡监控器根据设定的逻辑,自动进行平衡,不需要人工,能够快速实时的将其中三个机翼油箱内燃油量控制在平均燃油量M±300kg以内,另一个机翼油箱内燃油量控制在平均燃油量M±900kg以内,并可通过调整平衡调节阈值H、平衡控制阈值I,来控制精度,满足不同飞机对燃油不平衡控制的精度需求。


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    Title :

    System and method for automatically balancing fuel quantity in aircraft wing fuel tank


    Additional title:

    一种飞机机翼油箱内燃油量自动平衡系统及其方法


    Contributors:
    QIAN YI (author) / ZHANG YIN (author) / JI XINGCHANG (author) / SHEN NANA (author)

    Publication date :

    2025-01-14


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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