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Machine translation
1. (WO2007012735) DEVICE FOR TESTING A FUSELAGE STRUCTURE WITH LONGITUDINAL AND CIRCUMFERENTIAL CURVATURE
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2007/012735    International Application No.:    PCT/FR2006/001790
Publication Date: 01.02.2007 International Filing Date: 21.07.2006
IPC:
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)
Applicants: AIRBUS FRANCE [FR/FR]; 316, route de Bayonne, F-31060 Toulouse (FR) (For All Designated States Except US).
SAVES-SAINT-GERMES, Cyrille [FR/FR]; (FR) (For US Only).
DECRAECKER, Patrick [FR/FR]; (FR) (For US Only).
MIGNON, Olivier [FR/FR]; (FR) (For US Only).
LANVERS, Benoît [FR/FR]; (FR) (For US Only)
Inventors: SAVES-SAINT-GERMES, Cyrille; (FR).
DECRAECKER, Patrick; (FR).
MIGNON, Olivier; (FR).
LANVERS, Benoît; (FR)
Agent: SANTARELLI; 14, Avenue de la Grande-Armée, B.P. 237, F-75822 PARIS CEDEX 17 (FR)
Priority Data:
0507957 26.07.2005 FR
Title (EN) DEVICE FOR TESTING A FUSELAGE STRUCTURE WITH LONGITUDINAL AND CIRCUMFERENTIAL CURVATURE
(FR) DISPOSITIF D'ESSAIS D'UNE STRUCTURE DE FUSELAGE A COURBURE LONGITUDINALE ET CIRCONFERENTIELLE
Abstract: front page image
(EN)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.
(FR)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.
Designated States: AE, AG, AL, AM, AT, AU, AZ, BA, BB, BG, BR, BW, BY, BZ, CA, CH, CN, CO, CR, CU, CZ, DE, DK, DM, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LV, LY, MA, MD, MG, MK, MN, MW, MX, MZ, NA, NG, NI, NO, NZ, OM, PG, PH, PL, PT, RO, RS, RU, SC, SD, SE, SG, SK, SL, SM, SY, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW.
African Regional Intellectual Property Organization (BW, GH, GM, KE, LS, MW, MZ, NA, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, MD, RU, TJ, TM)
European Patent Office (AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HU, IE, IS, IT, LT, LU, LV, MC, NL, PL, PT, RO, SE, SI, SK, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, ML, MR, NE, SN, TD, TG).
Publication Language: French (FR)
Filing Language: French (FR)