Frame element, aircraft component assembly system and method of fitting a component in an aircraft
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United States of America Patent
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May 17, 2016
Grant Date -
Nov 5, 2009
app pub date -
Feb 23, 2009
filing date -
Aug 22, 2006
priority date (Note) -
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Abstract
A frame element (10; 10′) for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at least one insulation pack (52) to the frame element (10; 10′). An aircraft component assembly system (46) comprises a plurality of such frame elements (10; 10′). In a method of fitting a component (34, 52) in an aircraft, a frame element (10; 10′) is provided. At least one interior component (34) or at least one insulation pack (52) is fastened to the frame element (10; 10′). Then the frame element (10; 10′) having the at least one interior component (34) or the at least one insulation pack (52) fastened thereto is attached to an aircraft structure (36).
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