A system which includes a first light beam locating sensor associated with a first position to be located on a wing of an aircraft. The first light beam locating sensor senses a first light beam at an identifiable position on the first light beam locating sensor. A processor is configured to receive a first signal from the first light beam locating sensor wherein the first signal includes a first identifiable position on the first light beam locating sensor. The processor is configured to determine a location of the first position on the wing and perform a first comparison of the location of the first position on the wing to a predetermined analyzed location of the first position on the wing.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SYSTEM AND METHOD FOR CORRECTING WING TWIST OF AN AIRCRAFT


    Weitere Titelangaben:

    SYSTEM UND VERFAHREN ZUR KORREKTUR DER SCHRÄNKUNG EINES FLÜGELS
    SYSTÈME ET PROCÉDÉ DE CORRECTION DE LA TORSION D'AILE D'UN AÉRONEF


    Beteiligte:
    PROVOST STEPHEN N (Autor:in) / PITT DALE M (Autor:in)

    Erscheinungsdatum :

    27.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    SYSTEM AND METHOD FOR CORRECTING WING TWIST OF AIRCRAFT

    STEPHEN N PROVOST / DALE M PITT | Europäisches Patentamt | 2018

    Freier Zugriff

    SYSTEM AND METHOD FOR CORRECTING WING TWIST OF AN AIRCRAFT

    PROVOST STEPHEN N / PITT DALE M | Europäisches Patentamt | 2018

    Freier Zugriff

    System and method for correcting wing twist of an aircraft

    PROVOST STEPHEN N / PITT DALE M | Europäisches Patentamt | 2018

    Freier Zugriff

    Wing-twist controlled aircraft

    UHLIG DANIEL / KAYS CORY A / ULECK KEVIN et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Wing-Twist Controlled Aircraft

    UHLIG DANIEL / KAYS CORY / ULECK KEVIN et al. | Europäisches Patentamt | 2019

    Freier Zugriff