elemento de armaÇço, sistema de montagem de componentes de aeronave, e, mÉtodo de montar um componente em uma aeronave

The frame element (10) which is attachable to an aircraft structure has a fastening device for fastening aircraft interior component or insulation pack to the frame element. The connecting struts (16,18) of the frame element are provided with recesses (26,28,30,32) for receiving the ribs of the airc...

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Bibliographic Details
Main Authors MICHAEL AUBURGER, CHRISTIAN KOEFINGER, JOACHIM METZGER
Format Patent
LanguagePortuguese
Published 24.09.2013
Subjects
AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The frame element (10) which is attachable to an aircraft structure has a fastening device for fastening aircraft interior component or insulation pack to the frame element. The connecting struts (16,18) of the frame element are provided with recesses (26,28,30,32) for receiving the ribs of the aircraft structure when the frame element is attached to the aircraft structure. An independent claim is included for method of fitting aircraft interior component in an aircraft.
Bibliography:Application Number: BR2007PI15734