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Machine translation
1. (WO2010031960) REAR PART OF AN AIRCRAFT COMPRISING A STRUCTURE FOR SUPPORTING ENGINES, CONNECTED TO THE FUSELAGE BY AT LEAST ONE BLOCKING ELEMENT UNDER COMPRESSION LOADING
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2010/031960    International Application No.:    PCT/FR2009/051741
Publication Date: 25.03.2010 International Filing Date: 16.09.2009
IPC:
B64D 27/14 (2006.01), B64D 27/20 (2006.01), B64D 27/26 (2006.01)
Applicants: AIRBUS OPERATIONS (SOCIETE PAR ACTIONS SIMPLIFIEE) [FR/FR]; 316 Route de Bayonne F-31060 Toulouse (FR) (For All Designated States Except US).
LAFONT, Laurent [FR/FR]; (FR) (For US Only).
JOURNADE, Frédéric [FR/FR]; (FR) (For US Only)
Inventors: LAFONT, Laurent; (FR).
JOURNADE, Frédéric; (FR)
Agent: DU BOISBAUDRY, Dominique; Brevalex 95, rue d'Amsterdam F-75378 Paris Cedex 8 (FR)
Priority Data:
08 56300 18.09.2008 FR
Title (EN) REAR PART OF AN AIRCRAFT COMPRISING A STRUCTURE FOR SUPPORTING ENGINES, CONNECTED TO THE FUSELAGE BY AT LEAST ONE BLOCKING ELEMENT UNDER COMPRESSION LOADING
(FR) PARTIE ARRIERE D'AERONEF COMPRENANT UNE STRUCTURE DE SUPPORT DE MOTEURS RELIEE AU FUSELAGE PAR AU MOINS UN ELEMENT DE BLOCAGE SOLLICITE EN COMPRESSION
Abstract: front page image
(EN)The invention relates to a rear part of an aircraft (1) comprising a structure for supporting engines (14), passing through the fuselage, through a first opening and a second opening (18, 18). Said rear part comprises connection means connecting the support structure (14) to the fuselage (6), with first connection means connecting the structure (14) to a first casing (50) forming the first opening and second connection means connecting the structure (14) to a second casing (50) forming the second opening. According to the invention, the first and second connection means each comprise at least one blocking element (90, 92) of said support structure, under compression loading by being applied to the casing (50) and to the support structure (14).
(FR)L'invention se rapporte à une partie arrière d'aéronef (1) comprenant une structure de support des moteurs (14), traversant le fuselage au niveau d'une première et d'une seconde ouvertures (18, 18). Elle dispose de moyens d'attache raccordant la structure de support (14) au fuselage (6), comprenant des premiers moyens d'attache raccordant la structure (14) à un premier encadrement (50) formant la première ouverture et des seconds moyens d'attache raccordant la structure (14) à un second encadrement (50) formant la seconde ouverture. Selon l'invention, les premiers et seconds moyens d'attache comprennent chacun au moins un élément de blocage (90, 92) de ladite structure de support, sollicité en compression en étant en appui d'une part sur l'encadrement (50), et d'autre part sur la structure de support (14).
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IS, JP, KE, KG, KM, KN, KP, KR, KZ, LA, LC, LK, LR, LS, LT, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PE, PG, PH, PL, PT, RO, RS, RU, SC, SD, SE, SG, SK, SL, SM, ST, SV, 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, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, SE, SI, SK, SM, 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)