PROBLEM TO BE SOLVED: To deal with restrictions on engine mode change by a latch in a case of restarting an engine that stops during flight.SOLUTION: A FADEC 10 for controlling an aircraft engine 11 in response to a mode includes: a latch activation unit 32 for latching the mode; and a ground/flight determination unit 34 for determining whether an aircraft is on a ground or on a flight off the ground. The latch activation unit 32 is activated if the ground/flight determination unit 34 determines that the aircraft is on the ground, and is not activated if the ground/flight determination unit 34 determines that the aircraft is on a flight.

    【課題】飛行中に停止したエンジンを再始動させる場合、ラッチによってエンジンのモード変更が制限されることに対処すること。【解決手段】航空機のエンジン11をモードに応じて制御するFADEC10は、モードをラッチするラッチ発動部32と、航空機が地上にいるのか、地上から離れて飛行しているのかを判別する駐機中・飛行中判別部34と、を備える。ラッチ発動部32は、駐機中・飛行中判別部34により航空機が地上にいると判断される場合に発動し、航空機が飛行していると判断される場合には発動しない。【選択図】図4


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    Title :

    AIRCRAFT ENGINE CONTROL COMPUTER AND AIRCRAFT


    Additional title:

    航空機のエンジン制御コンピュータ、および航空機


    Contributors:

    Publication date :

    2015-06-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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