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Machine translation
1. (WO2013113650) SYSTEM AND METHOD FOR MOUNTING AIRCRAFT SYSTEM COMPONENTS IN THE CROWN AREA OF AN AIRCRAFT
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2013/113650    International Application No.:    PCT/EP2013/051559
Publication Date: 08.08.2013 International Filing Date: 28.01.2013
IPC:
B64F 5/00 (2006.01), B64D 11/00 (2006.01)
Applicants: AIRBUS OPERATIONS GMBH [DE/DE]; Kreetslag 10 21129 Hamburg (DE)
Inventors: BREUER, Matthias; (DE).
TUAN, Wei-Chung; (DE).
KLEPKA, Frank; (DE)
Agent: SCHICKER, Silvia; Schweigerstrasse 2 81541 München (DE)
Priority Data:
10 2012 001 797.9 30.01.2012 DE
61/592,014 30.01.2012 US
Title (EN) SYSTEM AND METHOD FOR MOUNTING AIRCRAFT SYSTEM COMPONENTS IN THE CROWN AREA OF AN AIRCRAFT
(FR) SYSTÈME ET PROCÉDÉ POUR MONTER DES COMPOSANTS DE SYSTÈME D'AÉRONEF DANS LA ZONE EN COURONNE D'UN AÉRONEF
Abstract: front page image
(EN)A system (10) for mounting aircraft system components (28, 58) in the crown area of an aircraft comprises a first longitudinal carrier element (12), a second longitudinal carrier element (14) and a bridging element (16) which connects said first longitudinal carrier element (12) to said second longitudinal carrier element (14). The system is mountable in the crown area of an aircraft in such a way that the first and the second longitudinal carrier element (12, 14) extend substantially parallel to the longitudinal axis (L) of the aircraft. A plurality of cable ducts (26) for accommodating electrical lines (28) is provided on the first and/or the second longitudinal carrier element (12, 14).
(FR)L'invention porte sur un système (10) pour monter des composants de système d'aéronef (28, 58) dans la zone en couronne d'un aéronef, lequel système comprend un premier élément de support longitudinal (12), un second élément de support longitudinal (14) et un élément de raccordement (16) qui relie ledit premier élément de support longitudinal (12) audit second élément de support longitudinal (14). Le système peut être monté dans la zone en couronne d'un aéronef de telle manière que le premier et le second élément de support longitudinal (12, 14) s'étendent sensiblement parallèlement à l'axe longitudinal (L) de l'aéronef. Une pluralité de conduites de câble (26) pour recevoir des lignes électriques (28) sont disposées sur le premier et/ou sur le second élément de support longitudinal (12, 14).
Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, 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, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW.
African Regional Intellectual Property Organization (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (AL, 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, RS, 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: English (EN)
Filing Language: English (EN)