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Internal arrangement of the walls of the fuselage of an aircraft
   
Document Number
US Patent 7461816
Issued Date
December 9, 2008
Link
Inventors
Schwartz; Bruno (Tournefeuille,FR)
Tanguy; Richard (Tournefeuille,FR)
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Abstract
An internal arrangement of aircraft fuselage walls supports two longitudinal auxiliary passage ducts at the upper part of the fuselage and on each side of its longitudinal plane of symmetry. The arrangement includes a longitudinal central element forming a dome connecting the structural ducts, an interior ceiling panel situated under the dome and facing toward the cabin, and two lateral cover panels. A lower edge of each lateral panel is articulated with respect to the fuselage so that it may occupy a raised position in which it is connected to a respective one of the structural ducts near an upper edge of the structural duct and a lowered position in which it is distant from the structural duct. Also, the upper edge of each lateral panel is extended, in the raised position, beyond the structural duct to cover the corresponding longitudinal edges of the dome and the ceiling panel.
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Number of Claims:
9
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Owner
Eads Sogerma Services (Merignac,FR)
Published
December 9, 2008
Application Number
11/109,677
Filed
April 20, 2005
US Classification
244/117R   244/119
Int'l Classification
B64C   1/00   (20060101)  
Examiner
Attorney/Law Firm
Priority Data
Apr 27, 2004 [FR] 04 04435
USPTO Field of Search
244/117R   244/118.5   244/119   244/120   105/397   105/344   105/329.1  
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