FRAME COMPONENT WITH VARIABLE WALL THICKNESS

Described is a frame component for a passenger seat assembly. The frame includes a tubular frame component having a first portion and a second portion. The bent portion bends the frame at a non-zero angle within a plane. The tubular frame component includes a variable inner diameter such that the fi...

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Bibliographische Detailangaben
Hauptverfasser:	TRANIER, Romain, PARKER, Charles Michael, MANSOURI, Reza
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS SEATS SPECIALLY ADAPTED FOR VEHICLES TRANSPORTING VEHICLE PASSENGER ACCOMMODATION NOT OTHERWISE PROVIDEDFOR VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	Described is a frame component for a passenger seat assembly. The frame includes a tubular frame component having a first portion and a second portion. The bent portion bends the frame at a non-zero angle within a plane. The tubular frame component includes a variable inner diameter such that the first portion of the tubular frame component has a first wall thickness and the bent portion of the tubular frame component has a second wall thickness that is different from the first wall thickness.