Frame element, aircraft component assembly system and method of fitting a component in an aircraft

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...

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Main Authors KOEFINGER CHRISTIAN, AUBURGER MICHAEL, METZGER JOACHIM
Format Patent
LanguageEnglish
Published 17.05.2016
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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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).
AbstractList 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).
Author AUBURGER MICHAEL
METZGER JOACHIM
KOEFINGER CHRISTIAN
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RelatedCompanies AUBURGER MICHAEL
METZGER JOACHIM
KOEFINGER CHRISTIAN
AIRBUS DEUTSCHLAND GMBH
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Snippet 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...
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SubjectTerms AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
Title Frame element, aircraft component assembly system and method of fitting a component in an aircraft
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