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Machine translation
1. (WO2011135214) NACELLE FOR AN AIRCRAFT ENGINE
Latest bibliographic data on file with the International Bureau   

Pub. No.:    WO/2011/135214    International Application No.:    PCT/FR2011/050506
Publication Date: 03.11.2011 International Filing Date: 14.03.2011
IPC:
B64D 29/06 (2006.01)
Applicants: AIRCELLE [FR/FR]; Route du Pont 8 F-76700 Gonfreville L'orcher (FR) (For All Designated States Except US).
BELLANGER, Alexandre [FR/FR]; (FR) (For US Only).
BOUILLON, Florent [FR/FR]; (FR) (For US Only).
DUBOIS, Laurent [FR/FR]; (FR) (For US Only).
ANFRAY, Emmanuel [FR/FR]; (FR) (For US Only)
Inventors: BELLANGER, Alexandre; (FR).
BOUILLON, Florent; (FR).
DUBOIS, Laurent; (FR).
ANFRAY, Emmanuel; (FR)
Agent: CABINET GERMAIN & MAUREAU; 8 Avenue du Président Wilson F-75016 Paris (FR)
Priority Data:
10/53343 29.04.2010 FR
Title (EN) NACELLE FOR AN AIRCRAFT ENGINE
(FR) Nacelle pour moteur d'aéronef
Abstract: front page image
(EN)The present invention relates to a support half structure for a nacelle of an aircraft engine, which half structure includes at least one longitudinal beam (1 a, 1 b) and a front half frame (3a, 3b), which are connected to each other and made at least partially from composite materials. Said half structure is characterized in that it includes a connecting hinge (13) arranged in the junction area of said beam (1 a, 1 b) and of said half frame (3a, 3b), said hinge (13) being made from composite materials arranged in such a manner that the fibers (16a, 16b) thereof are arranged as a continuation of the fibers (17) of the composite materials constituting said front half frame (3a, 3b).
(FR)Cette demi-structure de support pour nacelle de moteur d'aéronef, comprenant au moins une poutre longitudinale (1 a, 1 b) et un demi-cadre avant (3a, 3b) rel iés l 'un à l'autre et formés au moins en partie en matériaux composites, est remarquable en ce qu'elle comprend une charnière (13) de liaison disposée dans la zone de jonction de cette poutre (1 a, 1 b) et de ce demi-cadre (3a, 3b), cette charnière (1 3) étant formée par des matériaux composites agencés de manière que leurs fibres (16a, 16b) soient disposées dans la continuité des fibres (17) des matériaux composites formant ledit demi- cadre avant (3a, 3b).
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, 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, SD, SL, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Organization (AM, AZ, BY, KG, KZ, MD, 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: French (FR)
Filing Language: French (FR)