The invention provides an aircraft structure dynamic loading testing device, including a nozzle 141, 142, an attachment mechanism comprising a first portion 124 attached to the nozzle such that a nozzle force direction 141c is constrained at a set orientation and a second portion 125 for attaching to the aircraft structure 110 and configured to be constrained at a given orientation with respect to the aircraft structure, and a length of conduit 121, 123, wherein, in use, fluid is supplied along the length of conduit to the nozzle and ejected from the nozzle such that the nozzle exerts a dynamic force on the aircraft structure in the direction of the nozzle force direction. The invention also provides a dynamic loading testing device, a kit of parts and methods of dynamic load testing of a structure.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    AN AIRCRAFT STRUCTURE DYNAMIC LOADING TESTING DEVICE


    Weitere Titelangaben:

    VORRICHTUNG ZUM PRÜFEN DER DYNAMISCHEN BELASTUNG VON FLUGZEUGSTRUKTUREN
    DISPOSITIF DE TEST DE CHARGEMENT DYNAMIQUE DE STRUCTURE D'AÉRONEF


    Beteiligte:

    Erscheinungsdatum :

    02.11.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    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



    AIRCRAFT STRUCTURE DYNAMIC LOADING TESTING DEVICE

    GAMBIOLI FRANCESCO / LÜEBKE VERENA ALICE / JETZSCHMANN CHRISTINA et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    An aircraft structure dynamic loading testing device

    Europäisches Patentamt | 2021

    Freier Zugriff

    An aircraft structure dynamic loading testing device

    FRANCESCO GAMBIOLI / VERENA LÜBKE / CHRISTINA JETZSCHMANN et al. | Europäisches Patentamt | 2022

    Freier Zugriff

    Loading systems for aircraft structural testing

    Pickering, R.C. | Tema Archiv | 1976


    Dynamic Loading of Aircraft Structures

    Bronstein, M. / Geier, M. / Tekhniyon, Makhon tekhnologi le-Yisra'el | British Library Conference Proceedings | 2013