The invention relates to a device (20) of simple design for measuring displacement between a first part (8) and a second part (10) that are substantially coaxial, preferably mounted on one another by an annular linear link, the device comprising: - a structure (22) for mounting the device on the part (8); - blades (26) secured to the structure (22) and bearing on an outer surface (34) of an intermediate member (32), the member (32) being mounted around the part (10); - at least one strain/deformation sensor (40) associated with each blade (26), the sensors being configured to transmit output signals dependent on the levels of deformation of the blades; and - a conversion unit (50) configured to deliver, from the output signals, at least one datum corresponding to the relative position of the parts (8, 10), preferably out of an azimuth angle, an elevation angle and an axial displacement.


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    Titel :

    DEVICE AND METHOD FOR MEASURING DISPLACEMENT BETWEEN TWO SUBSTANTIALLY COAXIAL PARTS, PREFERABLY FOR AIRCRAFT


    Weitere Titelangaben:

    DISPOSITIF ET PROCEDE DE MESURE DE LA DEFORMATION ENTRE DEUX PARTIES ESSENTIELLEMENT COAXIALES, NOTAMMENT POUR LES AERONEFS


    Beteiligte:
    BOISSON THOMAS (Autor:in)

    Erscheinungsdatum :

    2016-06-18


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01B MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS , Messen der Länge, der Dicke oder ähnlicher linearer Abmessungen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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