(12) International Application Status Report

Received at International Bureau: 18 June 2007 (18.06.2007)

Information valid as of: Not available

Report generated on: 16 January 2021 (16.01.2021)

(10) Publication number: (43) Publication date: (26) Publication language:
WO 2007/14117613 December 2007 (13.12.2007) English (EN)

(21) Application number: (22) Filing date: (25) Filing language:
PCT/EP2007/05528631 May 2007 (31.05.2007) English (EN)

(31) Priority number(s): (32) Priority date(s): (33) Priority status:
10 2006 025 930.0 (DE)02 June 2006 (02.06.2006) Priority document received (in compliance with PCT Rule 17.1)
60/810,247 (US)02 June 2006 (02.06.2006) Priority document received (in compliance with PCT Rule 17.1)

(51) International Patent Classification:
B64C 1/14 (2006.01)

(71) Applicant(s):
AIRBUS DEUTSCHLAND GMBH [DE/DE]; Kreetslag 10 21129 Hamburg (DE) (for all designated states except US)
PAHL, Guenter [DE/DE]; Fuhlendorfweg 33g 22589 Hamburg (DE) (for US only)

(72) Inventor(s):
PAHL, Guenter; Fuhlendorfweg 33g 22589 Hamburg (DE)

(74) Agent(s):
PECKMANN, Ralf; Reinhard, Skuhra, Weise & Partner GbR Friedrichstrasse 31 80801 München (DE)

(54) Title (EN): FUSELAGE STRUCTURE AND METHOD FOR THE PRODUCTION OF A FUSELAGE STRUCTURE
(54) Title (FR): STRUCTURE DE FUSELAGE ET PROCÉDÉ DE FABRICATION D'UNE STRUCTURE DE FUSELAGE

(57) Abstract:
(EN): The present invention provides a method for the production of a fuselage structure, and a fuselage structure, in particular of an aircraft or spacecraft, with an inner shell arrangement (20) which has an upper inner shell (21) and a lower inner shell (22), the upper inner shell (21) being spaced apart at least in some sections from the lower inner shell (22) by a first gap (23) in order to form a window region; and a window band (41) which is arranged at least in the window region and has a pane device which comprises a grid structure (10) which absorbs fuselage forces.
(FR): La présente invention concerne un procédé de fabrication d'une structure de fuselage et une structure de fuselage, en particulier d'un aéronef ou d'un astronef, comportant un ensemble coque interne (20) composé d'une coque interne supérieure (21) et d'une coque interne inférieure (22), la coque interne supérieure (21) étant espacée, au moins dans certaines sections, de la coque interne inférieure (22) par un premier espace (23) de façon à former une région de hublot; et une bande de hublot (41) qui est située au moins dans la région de hublot et comporte un dispositif vitre qui comprend une structure en grille (10) absorbant les forces de fuselage.

International search report:
Received at International Bureau: 29 August 2007 (29.08.2007) [EP]

International Report on Patentability (IPRP) Chapter II of the PCT:
Not available

(81) Designated States:
AE, AG, AL, AM, AT, AU, AZ, BA, BB, BG, BH, BR, BW, BY, BZ, CA, CH, 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, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PG, PH, PL, PT, RO, RS, RU, SC, SD, SE, SG, SK, SL, SM, SV, SY, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
European Patent Office (EPO) : AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HU, IE, IS, IT, LT, LU, LV, MC, MT, NL, PL, PT, RO, SE, SI, SK, TR
African Intellectual Property Organization (OAPI) : BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, ML, MR, NE, SN, TD, TG
African Regional Intellectual Property Organization (ARIPO) : BW, GH, GM, KE, LS, MW, MZ, NA, SD, SL, SZ, TZ, UG, ZM, ZW
Eurasian Patent Organization (EAPO) : AM, AZ, BY, KG, KZ, MD, RU, TJ, TM