Interface Element, Aircraft Interior Equipment Component And Method For Installing An Aircraft Interior Equipment Component

An interface element (10) for connecting a first section of an aircraft supply system, which is provided on an aircraft interior equipment component (12), to a second section of the aircraft supply system includes a carrier structure (14) which is fastenable to the aircraft interior equipment compon...

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Bibliographische Detailangaben
Hauptverfasser:	KNOEPFLE STEFAN, PLADECK GERRIT, STUETZER JOERG, KOWALSKI REMIGIUSZ, STROEBELE DIETMAR
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COMBINED OPERATIONS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS MACHINE TOOLS METAL-WORKING NOT OTHERWISE PROVIDED FOR OTHER WORKING OF METAL PARACHUTES PERFORMING OPERATIONS TRANSPORTING UNIVERSAL MACHINE TOOLS
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Beschreibung
Zusammenfassung:	An interface element (10) for connecting a first section of an aircraft supply system, which is provided on an aircraft interior equipment component (12), to a second section of the aircraft supply system includes a carrier structure (14) which is fastenable to the aircraft interior equipment component (12). Further, the interface element (10) includes a connector element (26, 52) which is connectable to the first section of the aircraft supply system provided on the aircraft interior equipment component (12) and which is mounted on the carrier structure (14) by way of a bearing means (24, 50). The bearing means (24, 50) includes at least one resilient bearing element (40, 58) which enables the connector element (26, 52) to be mounted such that it is movable in all three spatial directions.