G - Physics – 01 – M
Patent
G - Physics
01
M
G01M 7/04 (2006.01) G01M 5/00 (2006.01) G01M 7/06 (2006.01) G01N 3/04 (2006.01) G01N 3/06 (2006.01) G01N 3/08 (2006.01)
Patent
CA 2615279
The invention concerns a device for testing a fuselage structure (10) with longitudinal and circumferential curvature, comprising a set of means for applying forces (80) on the fuselage structure. It comprises a central shaft (20) extending in the longitudinal direction and at the center of the fuselage structure and adapted to be secured to the fuselage structure (10). The set of force applying means is mounted between the fuselage structure and supporting means (70, 90) integral with the central shaft (20). The invention is particularly useful for performing tests on an aircraft fuselage.
Le dispositif d'essais d'une structure de fuselage (10) à courbure longitudinale et circonférentielle, comprend un ensemble de moyens d'application de forces (80) sur la structure de fuselage. Il comprend un arbre central (20) s'étendant dans la direction longitudinale et au centre de la structure de fuselage et adapté à être solidarisé à la structure de fuselage (10). L'ensemble des moyens d'application de forces est monté entre la structure de fuselage et des moyens de support (70, 90) solidaires de l'arbre central (20). Utilisation notamment pour réaliser des essais sur un fuselage d'un avion.
Decraecker Patrick
Lanvers Benoit
Mignon Olivier
Saves-Saint-Germes Cyrille
Airbus France
Airbus Operations Sas
Riches Mckenzie & Herbert Llp
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