A warning system 10 that warns of saturation of the control capability for the moving surface such as an elevator 4 and a rudder 8 of an aircraft has a determination section 31 that determines whether or not the control capability for the moving surface is saturated, and a display 50 that issues a warning when the determination section 31 determines that the control capability for the moving surface is saturated. The determination section 31 determines that the control capability for the elevator 4 is saturated, when a control target position of the elevator 4 by, for example, a control stick (column) is larger than a first reference position indicating an operation limit of the elevator 4, and a present position of the column is smaller than a second reference position indicating an operation limit of the column.


    Access

    Download


    Export, share and cite



    Title :

    WARNING SYSTEM OF AIRCRAFT AND AIRCRAFT


    Contributors:

    Publication date :

    2015-06-25


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    Warning system for aircraft, and aircraft

    MAEDA NAOTO / MIYOSHI MASAYA | European Patent Office | 2016

    Free access

    AIRCRAFT WARNING SYSTEM

    NIZOV SERGEJ NIKOLAEVICH | European Patent Office | 2018

    Free access

    Warning system of aircraft and aircraft

    MIYOSHI MASAYA | European Patent Office | 2015

    Free access

    AIRCRAFT COLLISION WARNING

    SHENFELD URI / ROSENFELD SAMUEL | European Patent Office | 2017

    Free access

    Aircraft collision warning

    SHENFELD URI / ROSENFELD SAMUEL | European Patent Office | 2019

    Free access