Interior panel of an aircraft cabin integrating an air duct

The device (1) has a covering panel (2) bearing a system formed of an air circulation pipe i.e. air pipe (3) and an electric cable, where the air pipe is fastened to an exterior face (6) of the panel. A lower end i.e. upstream end (26), of the pipe is equipped with a quick disconnect type connection...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SABADIE, LIONEL, BERTANDEAU, LAURENT, BANIS, CHRISTIAN, BERNABE, THOMAS, TOMASI, MARC
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION HELICOPTERS INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINEDOPTICAL AND ELECTRIC CABLES OR LINES PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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