AIRPLANE SEAT DEVICE

The invention relates to an airplane seat device, comprising at least one stand unit (12a; 12b; 12c), at least one backrest (24a; 24b; 24c; 24d) which is coupled to the stand unit (12a; 12b; 12c), at least one seat base (28a; 28b; 28c; 28d) which is coupled to the stand unit (12a; 12b; 12c) and/or t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser:	KUGLER, Kai-Uwe
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:	The invention relates to an airplane seat device, comprising at least one stand unit (12a; 12b; 12c), at least one backrest (24a; 24b; 24c; 24d) which is coupled to the stand unit (12a; 12b; 12c), at least one seat base (28a; 28b; 28c; 28d) which is coupled to the stand unit (12a; 12b; 12c) and/or the backrest (24a; 24b; 24c; 24d), and at least one kinematic module (34a; 34b), which is designed to adjust the backrest (24a; 24b; 24c; 24d) and/or the seat base (28a; 28b; 28c; 28d) between at least one normal substantially upright seating position and a comfort position. The kinematic module (34a; 34b) is designed to adjust the backrest (24a; 24b; 24c; 24d) and/or the seat base (28a; 28b; 28c; 28d) into an additional special upright position, which differs from the upright seating position and in which the backrest (24a; 24b; 24c; 24d) is set forwards at least in a sub-region and/or the seat base (28a; 28b; 28c; 28d) is at least pivoted, in at least one operating state.