B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/06 (2006.01)
Patent
CA 2650509
An aircraft fuselage structure is described with frames running in the circumferential direction, stringers running in the longitudinal direction and a skin which is arranged thereon and outwardly seals the aircraft fuselage in a compression-proof manner. According to the invention, it is provided that the aircraft fuselage structure contains prefabricated integral units (10) which each run in the circumferential direction of a fuselage segment and in which the frame (11) of a fuselage segment and connecting elements (17, 18) for connection to skin elements (20) comprising stringers (22) and skin (21) are formed.
L'invention concerne une structure de fuselage d'aéronef possédant des cadres s'étendant dans le sens circonférentiel, des lisses s'étendant dans le sens longitudinal et un revêtement plaqué contre et rendant étanche à l'extérieur le fuselage d'aéronef d'une manière lui permettant de résister à la pression. Selon l'invention, la structure de fuselage d'aéronef comporte des unités préfabriquées monoblocs (10) s'étendant chacune dans le sens circonférentiel d'un compartiment de fuselage, unités dans lesquelles sont formées le cadre (11) d'un compartiment de fuselage, ainsi que des éléments de raccordement (17, 18) pour le raccordement aux éléments du revêtement (20) comprenant les lisses (22) et le revêtement (21).
Airbus Deutschland Gmbh
Airbus Operations Gmbh
Sim & Mcburney
LandOfFree
Aircraft fuselage structure and method for producing it does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Aircraft fuselage structure and method for producing it, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Aircraft fuselage structure and method for producing it will most certainly appreciate the feedback.
Profile ID: LFCA-PAI-O-1634479