INTERIOR TRIM COMPONENT FOR AN AIRCRAFT CABIN

An interior trim component (10) for an aircraft cabin comprises a supporting structure which is formed by a first chamber system (12) which is sealable against the outside atmosphere. The first chamber system (12) forming the supporting structure is adapted to be loaded with an internal pressure whi...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	VOELKLE, DIETMAR, FEILER, MARKUS, VEIHELMANN, BERND
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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