| 摘要 |
1. Aircraft passenger seat [row]. 2. The invention relates to an aircraft passenger seat row having a) at least three seats ( 10, 12, 14 ), b) a seat frame ( 16 ) common to all seats and having a front transverse spar ( 18 ) and a rear transverse spar ( 20 ) in parallel with the front spar which spars are rigidly connected by means of seat pedestals ( 22 ) so as to be stationary in relation to each other, c) cushion carriers ( 26 ) supporting seat element cushions ( 24 ), d) seat dividers ( 28 ) supported by both transverse spars ( 18, 20 ) and mounted at the ends of the row of seats and between the seats, e) backrests ( 30 ) the inclined position of which may be adjusted and which are pivotably connected to the seat dividers ( 28 ), and f) arm rests ( 32 ), preferably at both ends of the row of seats and between the seats ( 10, 12, 14 ), the last-named arm rests ( 32 ) being pivotably mounted on at least one guide web ( 34 ) extending in parallel with the transverse spars ( 18, 20 ) and supported by seat dividers ( 28 ) mounted between the seats ( 10, 12, 14 ), a center seat ( 12 ) of a row of seats having between adjacent seats ( 10, 14 ) a separating element ( 36 ) which, when in a non-use position, is mounted at least partly in the area of the associated seat pedestals ( 22 ) for this center seat ( 12 ) and, when in a use position, is mounted at least partly above the seat dividers ( 28 ), and it being possible to move the separating element ( 36 ) between the positions named by means of a pivot mechanism ( 38 ).
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