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1. (WO2007000544) AIRCRAFT JET ENGINE PYLON SUSPENSION ATTACHMENT
Latest bibliographic data on file with the International Bureau

Pub. No.: WO/2007/000544 International Application No.: PCT/FR2006/050467
Publication Date: 04.01.2007 International Filing Date: 22.05.2006
IPC:
B64C 27/18 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
27
Rotorcraft; Rotors peculiar thereto
04
Helicopters
12
Rotor drives
16
Drive of rotors by means, e.g. propellers, mounted on rotor blades
18
the means being jet-reaction apparatus
Applicants:
AIRBUS FRANCE [FR/FR]; 316, route de Bayonne F-31060 Toulouse, FR (AllExceptUS)
DIOCHON, Lionel [FR/FR]; FR (UsOnly)
SARRATO, Michael [FR/ES]; ES (UsOnly)
CHARTIER, David [FR/FR]; FR (UsOnly)
PETRISSANS, Isabelle [FR/FR]; FR (UsOnly)
Inventors:
DIOCHON, Lionel; FR
SARRATO, Michael; ES
CHARTIER, David; FR
PETRISSANS, Isabelle; FR
Agent:
DU BOISBAUDRY, Dominique; Brevalex 3, rue du Docteur Lancereaux F-75008 Paris, FR
Priority Data:
055133123.05.2005FR
Title (EN) AIRCRAFT JET ENGINE PYLON SUSPENSION ATTACHMENT
(FR) MAT D'ACCROCHAGE DE TURBOREACTEUR POUR AERONEF
Abstract:
(EN) The invention relates to an aircraft jet engine pylon suspension attachment comprising a rigid structure (10) provided with a central longitudinal caisson (22). According to said invention, the rigid structure also comprises two side caissons (24a, 24b) fixed to the front part of the central caisson (22), the pylon is provided with first (6a) and second (6b) front engine fasteners which are constructed in such a way that they pick up loads produced in the longitudinal direction (X) of the pylon, wherein said first and second fasteners are connected to the two side caissons, respectively.
(FR) L'invention se rapporte à un mât d'accrochage de turboréacteur pour aéronef, le mât disposant d'une structure rigide (10) comportant un caisson central longitudinal (22). Selon l'invention, la structure rigide comprend en outre deux caissons latéraux (24a, 24b) solidaires d'une partie avant dudit caisson central (22), le mât comportant également une première (6a) et une seconde attache moteur avant (6b) conçues de manière à reprendre des efforts s'exerçant selon une direction longitudinale (X) du mât, ces première et seconde attaches étant respectivement agencées sur les deux caissons latéraux.
front page image
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, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, 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, RU, SC, SD, SE, SG, SK, SL, SM, SY, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, YU, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (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)
Also published as:
EP1883578JP2008542090RU02400401BRPI0609810US20080191088CN101180211
CA2608940FR2885877