SEAT, IN PARTICULAR AN AIRCRAFT SEAT

The invention relates to a seat (S), in particular an aircraft seat, comprising- a seat support structure (1) comprising at least one seat surface (1.1) with a seat surface frame (1.1.1) and a backrest (1.2) with a backrest frame (1.2.1) being pivotable relative to the seat surface (1.1),- a base su...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	DECH, Jannik, REICHEL, Uwe, RENNO, Stefan, PUGH, Samuel David, RUESS, Georg, BURGEY, Daniel
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:	The invention relates to a seat (S), in particular an aircraft seat, comprising- a seat support structure (1) comprising at least one seat surface (1.1) with a seat surface frame (1.1.1) and a backrest (1.2) with a backrest frame (1.2.1) being pivotable relative to the seat surface (1.1),- a base support element (2) supporting the seat support structure (1), and- a seat adjustment arrangement (3),- which comprises at least one coupling unit (4) movable relative to the base support element (2), the coupling unit (4) is configured to connect the seat surface frame (1.1.1) and the backrest frame (1.2.1) to one another and which is provided with at least one bearing element (5), and- which comprises at least one guide element (6) in which the bearing element (5) is movably guided,wherein the seat adjustment arrangement (3) is adapted to transfer the seat support structure (1) into a sitting position (P1), a comfort and/or lying position (P2) by displacing the bearing element (5) along the guide element (6).