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1. (WO2017064646) STRINGER-LESS FUSELAGE STRUCTURE AND METHOD OF MANUFACTURE
Latest bibliographic data on file with the International Bureau    Submit observation

Pub. No.: WO/2017/064646 International Application No.: PCT/IB2016/056142
Publication Date: 20.04.2017 International Filing Date: 13.10.2016
IPC:
B64C 1/06 (2006.01) ,B64C 1/12 (2006.01)
Applicants: BOMBARDIER INC.[CA/CA]; 400 Côte Vertu Road West Dorval, Québec H4S 1Y9, CA
SHORT BROTHERS PLC[IE/IE]; Airport Road Belfast BT3 9DZ, IE (MT)
Inventors: MAROUZE, Jean-Philippe; CA
Agent: NORTON ROSE FULBRIGHT CANADA LLP / S.E.N.C.R.L.; Suite 2500, 1 Place Ville Marie Montreal, Québec H3B 1R1, CA
Priority Data:
62/242,49516.10.2015US
Title (EN) STRINGER-LESS FUSELAGE STRUCTURE AND METHOD OF MANUFACTURE
(FR) STRUCTURE DE FUSELAGE SANS LISSE ET PROCÉDÉ DE FABRICATION
Abstract: front page image
(EN) Stringer-less fuselage structures and associated methods of manufacturing are disclosed. In some embodiments, a fuselage structure includes a composite fuselage skin (24) including a plurality of tear straps (32) formed in the composite fuselage skin where each tear strap extends generally along a longitudinal axis of the composite fuselage skin. The fuselage structure also includes a plurality of frames (28) supporting an interior of the composite fuselage skin where the frames are spaced apart along the longitudinal axis of the composite fuselage skin.
(FR) L'invention concerne des structures de fuselage sans lisse et des procédés de fabrication associés. Dans certains modes de réalisation, une structure de fuselage comprend une enveloppe de fuselage composite (24) comprenant une pluralité de sangles de déchirure (32) formées dans l'enveloppe de fuselage composite où chaque sangle de déchirure s'étend généralement le long d'un axe longitudinal de l'enveloppe de fuselage composite. La structure de fuselage comprend également une pluralité de cadres (28) soutenant l'intérieur de l'enveloppe de fuselage composite où les cadres sont espacés le long de l'axe longitudinal de l'enveloppe de fuselage composite.
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, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JP, KE, KG, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, 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, SA, 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 (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (EPO) (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, KM, ML, MR, NE, SN, TD, TG)
Publication Language: English (EN)
Filing Language: English (EN)