AIRCRAFT SEATING CONFIGURATION

There is a seating assembly adapted to be positioned in an aircraft cabin. The seating assembly comprises a first seat having a first seat back and a first seat bottom and defining a first longitudinal axis, and a second seat having a second seat back and a second seat bottom and defining a second l...

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Bibliographische Detailangaben
Hauptverfasser:	JIN, ZHAO, ORSON, BEN
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 TRANSPORTING
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Beschreibung
Zusammenfassung:	There is a seating assembly adapted to be positioned in an aircraft cabin. The seating assembly comprises a first seat having a first seat back and a first seat bottom and defining a first longitudinal axis, and a second seat having a second seat back and a second seat bottom and defining a second longitudinal axis. The first and second seats are positioned adjacent to one another. The seating assembly comprises a third longitudinal axis that is approximately parallel with a longitudinal axis defined by the aircraft cabin when the seating assembly is positioned in an aircraft cabin. The first seat faces fore and is positioned such that the first longitudinal axis forms an angle with the third longitudinal axis that is between about 1° and about 44° and the second seat faces fore and is positioned such that the second longitudinal axis forms an angle with the third longitudinal axis that is between about 1° and about 44°. The first and second seats each face away from each other and away from the third longitudinal axis.