Device for testing a fuselage structure with longitudinal...

G - Physics – 01 – M

Patent

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Details

G01M 7/04 (2006.01) G01M 5/00 (2006.01) G01N 3/00 (2006.01) G01N 3/06 (2006.01) G01N 3/08 (2006.01)

Patent

CA 2615277

The invention concerns a device for testing a fuselage structure (10) with longitudinal and circumferential curvature comprising means for applying forces (30, 40) on the fuselage structure (10). It comprises support means (50) for supporting the fuselage structure (10) and the set of force applying means (30, 40). The set of force applying means (30, 40) is mounted between the support means (50) and force introducing means (7) integral with the fuselage structure (10), and is adapted to apply collinear forces to the fuselage structure (10). 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 moyen d'application de forces (30, 40) sur la structure de fuselage (10). Il comprend des moyens de support (50) adaptés à supporter la structure de fuselage (10) et l'ensemble des moyens d'application de forces (30, 40). L'ensemble des moyens d'application de forces (30, 40) est monté entre les moyens de support (50) et des moyens d'introduction de forces (70) solidaires de la structure de fuselage (10), et est adapté à appliquer des forces colinéaires à la structure de fuselage (10). Utilisation notamment pour réaliser des essais sur un fuselage d'un avion.

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