DEVICE FOR SUPPLYING LOADS IN THE OVERHEAD AREA OF A PASSENGER CABIN, IN PARTICULAR IN COMMERCIAL AIRCRAFT

Corresponding to reducing the number of components that need to be separately installed, in addition to a weight reduction and a reduction in the cable loom volume, improved system reliability is obtained if the loads relating to a seating space in a passenger cabin (12), in particular in an aircraf...

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Bibliographic Details
Main Authors KNOPP NORBERT, RENZ MARC, KLINGSEIS MARKUS, GRABMANN JUERGEN, VOLKLE DIETMAR, SCHMID FRANK, KUHNLA WOLF-DIETER
Format Patent
LanguageEnglish
Published 06.09.2012
Subjects
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS
PARACHUTES
PERFORMING OPERATIONS
TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
TECHNICAL SUBJECTS COVERED BY FORMER USPC
TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE
TRANSPORTING
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Summary:Corresponding to reducing the number of components that need to be separately installed, in addition to a weight reduction and a reduction in the cable loom volume, improved system reliability is obtained if the loads relating to a seating space in a passenger cabin (12), in particular in an aircraft, are combined on an overhead panel (17) which is connected, via line connections which are now only short, to a spatially associated supply module (19), which is operated in cutouts (20) in a stub frame (13), in order to anchor a hat rack (11) in the fuselage structure (16) of the cabin (12).
Bibliography:Application Number: US201113179794