The invention discloses an aircraft total static pressure system tester calibration method, which comprises the following steps: enabling a standard flight parameter controller to generate pressure corresponding to flight parameters, and measuring a flight parameter indication error of an aircraft total static pressure system tester; the flight parameters comprise a total pressure parameter, a static pressure parameter, a height parameter, an air speed parameter and a Mach number parameter; enabling the aircraft total static pressure system tester to generate pressure corresponding to flight parameters, and measuring a flight parameter control stability error, a flight parameter control overshoot error and a flight parameter control callback error of the aircraft total static pressure system tester through a standard flight parameter controller; by increasing the flight parameter control stability error, the flight parameter control overshoot error and the flight parameter control callback error, the aircraft total static pressure system tester can be detected more comprehensively, and the detection precision is improved.

    本发明公开了一种飞机全静压系统试验器校准方法,使标准飞行参数控制器产生飞行参数对应的压力,测量飞机全静压系统试验器的飞行参数示值误差;飞行参数包括全压参数、静压参数、高度参数、空速参数和马赫数参数;使飞机全静压系统试验器产生飞行参数对应的压力,通过标准飞行参数控制器测量飞机全静压系统试验器的飞行参数控制稳定性误差、飞行参数控制超调量误差、飞行参数控制回调量误差;本发明通过增加飞行参数控制稳定性误差、飞行参数控制超调量误差、飞行参数控制回调量误差可以对飞机全静压系统试验器检测更加全面,提升检测精度。


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    Title :

    Aircraft total static pressure system tester calibration method


    Additional title:

    一种飞机全静压系统试验器校准方法


    Contributors:
    LI JUHUA (author)

    Publication date :

    2024-12-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    G01D MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE , Anzeigen oder Aufzeichnen in Verbindung mit Messen allgemein / 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 / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen



    Flight Calibration of Aircraft Static Pressure Systems

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    Flight Calibration of Aircraft Static Pressure Systems

    R. V. DeLeo / F. W. Hagen | NTIS | 1966


    Aircraft Electrical System Tester

    S. P. Mears | NTIS | 1979


    Aircraft Electrical System Tester

    S. P. Mears | NTIS | 1979