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1. WO2007141291 - AIRCRAFT FUSELAGE STRUCTURE AND METHOD FOR ITS PRODUCTION

Publication Number WO/2007/141291
Publication Date 13.12.2007
International Application No. PCT/EP2007/055556
International Filing Date 06.06.2007
IPC
B64C 1/00 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces, or the like
CPC
B64C 1/061
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
06Frames; Stringers; Longerons ; ; Fuselage sections
061Frames
B64C 1/18
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
1Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
18Floors
Y10T 29/49622
YSECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
10TECHNICAL SUBJECTS COVERED BY FORMER USPC
TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
29Metal working
49Method of mechanical manufacture
49616Structural member making
49622Vehicular structural member making
Y10T 29/49826
YSECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
10TECHNICAL SUBJECTS COVERED BY FORMER USPC
TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
29Metal working
49Method of mechanical manufacture
49826Assembling or joining
Applicants
  • AIRBUS DEUTSCHLAND GMBH [DE]/[DE] (AllExceptUS)
  • ROMING, Thorsten [DE]/[DE] (UsOnly)
  • SCHROEER, Thorsten [DE]/[DE] (UsOnly)
Inventors
  • ROMING, Thorsten
  • SCHROEER, Thorsten
Agents
  • PECKMANN, Ralf
Priority Data
10 2006 026 168.206.06.2006DE
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) AIRCRAFT FUSELAGE STRUCTURE AND METHOD FOR ITS PRODUCTION
(FR) STRUCTURE DE FUSELAGE D'AÉRONEF ET PROCÉDÉ DESTINÉ À SA PRODUCTION
Abstract
(EN)
An aircraft fuselage structure with frames (11) running transversely with respect to the longitudinal direction of the fuselage, and main deck cross members (14) is disclosed. The aircraft fuselage structure contains premanufactured integral units (10) which each comprise at least the lower region of the fuselage frame (11) and the main deck cross member (14), the fuselage frame (11) and a region (14a) of the main deck cross member (14) that spans at least an essential part of the width of the main deck and merges on both sides into the fuselage frame (11) being premanufactured in the form of an integral component.
(FR)
La présente invention concerne une structure de fuselage d'aéronef avec des cadres (11) s'étendent transversalement par rapport au sens longitudinal du fuselage et des barres transversales de pont principal (14). La structure de fuselage d'aéronef comporte des unités préfabriquées monoblocs (10) dont chacune comprend au moins la région inférieure du cadre de fuselage (11) et la barre transversale de pont principal (14). Par ailleurs, le cadre de fuselage (11) et une région (14a) de la barre transversale de pont principal (14) qui recouvre au moins une majeure partie de la largeur du pont principal et épouse de part et d'autre le cadre du fuselage (11), sont préfabriqués pour présenter la forme d'un élément constitutif monobloc.
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