An aircraft flight attitude display device includes a central processing unit (CPU), a display unit electrically connected to the CPU for showing an aircraft image therein, a flight data receiver unit electrically connected to the CPU, a sky obstacle data receiver unit electrically to the CPU, a ground obstacle data receiver unit electrically connected to the CPU, and a power supply unit electrically connected to the CPU. With these arrangements, the aircraft flight attitude display device aids a pilot in making quick and correct judgment about the aircraft flight attitude relative to the sky and the ground, so as to upgrade the aviation safety.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT FLIGHT ATTITUDE DISPLAY DEVICE


    Contributors:

    Publication date :

    2020-12-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    AIRCRAFT FLIGHT ATTITUDE DISPLAY DEVICE

    LIN HUNG-HSIN | European Patent Office | 2022

    Free access

    Aircraft flight attitude simulation supporting device

    REN ZHONGCAI / NIE BOWEN / CEN FEI et al. | European Patent Office | 2022

    Free access

    Hoisting flight attitude adjustment throwing device for aircraft

    ZENG GUANNAN / ZHANG ZIJIAN / ZHOU LIYANG et al. | European Patent Office | 2021

    Free access

    Aircraft convenient for controlling flight attitude

    WANG ZHICHENG | European Patent Office | 2021

    Free access

    Synthetic Vision System Commercial Aircraft Flight Deck Display Technologies for Unusual Attitude Recovery

    Prinzel, Lawrence J., III / Ellis, Kyle E. / Arthur, Jarvis J. et al. | NTRS | 2017