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 | , , |
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Format | Patent |
Language | English |
Published |
17.05.2016
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Subjects | |
Online Access | Get full text |
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