The invention discloses an airplane ground flight verification system. The airplane ground flight verification system comprises a load simulation computer (1), a temperature control computer (2), a hydraulic pump drive computer (3), a main control computer (4), a network switch (5) and a conditioning node computer (6). The network switch (5) is connected with the load simulation computer (1), the temperature control computer (2), the hydraulic pump drive computer (3), the main control computer (4) and the conditioning node computer (6). The load simulation computer is used for managing a load simulation system and simulating a front undercarriage and a rear undercarriage. The temperature control computer is used for adjusting the temperature of the system and preventing accidents caused by excessively-high temperature of the system. The hydraulic pump drive computer is used for managing a hydraulic system and controlling the rotating speed of a main pump and an auxiliary pump on an airplane.


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    Title :

    Airplane ground flight verification system


    Contributors:
    PAN TENGFEI (author) / HOU WENLI (author) / WU LIANG (author) / XUELINXI (author) / LIQUAN (author)

    Publication date :

    2015-11-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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    Berner, A. E. / Manning, M. K. / Society of Flight Text Engineers | British Library Conference Proceedings | 1997



    Ground versus flight tests of airplane engine installations

    Kendrick, J.B. | Engineering Index Backfile | 1942


    Ground versus flight tests of airplane engine installations

    Kendrick, J.B. | Engineering Index Backfile | 1942


    GROUND Versus FLIGHT TESTS of Airplane Engine Installations

    KENDRICK, JAMES B. | SAE Technical Papers | 1942