A load testing apparatus can include a plurality of vertical load structures arranged on a flight control surface to provide torque on the control surface and reacted by a control rod of the flight control surface. The load testing apparatus can also include a plurality of fore/aft load structures arranged to provide tensile and/or compressive force in a direction intersecting a hinge line of the flight control surface. Each of the plurality of fore/aft load structure can include a first rubber pad having a surface extending in a first plane that is arranged to contact a lower surface of the flight control surface. Each of the plurality of fore/aft load structures can also include a first rubber pad having a surface extending in a second plane that is arranged to contact an upper surface of the flight control surface, wherein the first plane and the second plane are non-parallel planes.


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    Titel :

    Load testing for flight control surface


    Beteiligte:
    PERRY PAULINE (Autor:in)

    Erscheinungsdatum :

    2022-10-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01N Untersuchen oder Analysieren von Stoffen durch Bestimmen ihrer chemischen oder physikalischen Eigenschaften , INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES / B64C AEROPLANES , Flugzeuge / 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




    APPARATUS BEING POSSIBLE TO APPLY FLIGHT LOAD AND CONTROL ATTITUDE FOR TESTING WING OF FLIGHT VEHICLE

    KIM JONG HEON / KIM GYOUNG BEOM / KIM HEE JUNG et al. | Europäisches Patentamt | 2018

    Freier Zugriff

    Flight Testing a Modern Flight Control System

    Smith, T. D. / SAE / AIAA | British Library Conference Proceedings | 1997



    Flight Testing a Modern Flight Control System

    Smith, Terry D. | SAE Technical Papers | 1997