Abstract: The invention relates to a method for producing fibre-reinforced hollow bodies comprising integrally formed elements in a hollow mould. A fibre mat is laminated in two halves of the hollow mould, which respectively form the negative mould for the fibre-reinforced hollow bodies comprising integrally formed elements to be produced, and, once the two halves of the thus lined hollow mould have been connected, the fibre mat is pressed into the hollow mould under pressure in a form-fitting manner. The invention also relates to products produced according to the inventive method.

Abstract: Disclosed is a passenger seat, especially an airline passenger seat, comprising seat components such as a seat part, a backrest, and an armrest (3), at least one of which is movably disposed relative to the other seat components to adjust the position, and a partition (9, 11) that can be transferred between an operational position in which the same extends in a lateral shielding area of the seat and a non-operational position in which the same unblocks the shielding area. The partition is composed of several wall parts (9, 11) which extend in the shielding area in the operational position and interact via a guiding device (43, 45) such that the movement of one wall part (9) during the transfer between the non-operational and the operational position entrains another wall part (11).

Abstract: Disclosed is a passenger seat, especially an airline passenger seat, comprising seat components such as a seat part, a backrest, and an armrest (3), at least one of which is movably disposed relative to the other seat components to adjust the position, and a partition (9, 11) that can be transferred between an operational position in which the same extends in a lateral shielding area of the seat and a non-operational position in which the same unblocks the shielding area. The partition is composed of several wall parts (9, 11) which extend in the shielding area in the operational position and interact via a guiding device (43, 45) such that the movement of one wall part (9) during the transfer between the non-operational and the operational position entrains another wall part (11).

Abstract: In the case of a locking device for a tray table system in a seat, in particular an aircraft passenger seat, with a first (3) and a second tray table part (5) that can be moved around swivel axes (25 or 37), different from one another, between horizontal use positions and non-use or stowed positions, closing parts (43, 47) are assigned to the two tray table parts (3, 5) and can be adjusted relative to one another in an active position, in which they close with respect to one another to keep them from raising a tray table part (3) in a use position.