The invention relates to a window unit W for aircraft cabins, comprising an outer window frame 1, an inner window frame 3, a window pane 2 lying between them, and possibly having a sun-visor 4, a roller blind 34 or the like arranged between the inner window frame 3 and a possible covering frame 5, t
The invention relates to a window unit W for aircraft cabins, comprising an outer window frame 1, an inner window frame 3, a window pane 2 lying between them, and possibly having a sun-visor 4, a roller blind 34 or the like arranged between the inner window frame 3 and a possible covering frame 5, the window unit W being insertable into the opening 7 in a side-wall panel 6 or the like in the aircraft cabin. In order to make it possible for the window unit W to be rapidly and simply installed and removed, the invention makes provision for the window unit W to have a centering device and at least two snap fastenings 13, advantageously with locking devices, to detachably connect it to the side-wall panel 6, or to components connected thereto, the side-wall panel 6, or components connected thereto, having any necessary mating parts for the centering device for the snap fastenings 13. The centering device is advantageously arranged corresponding to a clock position of 6 o'clock, and two snap fastenings 13 are advantageously arranged on the circumference of the window unit (W) corresponding to a clock position of 10 and 2 o'clock.
대표청구항▼
[ We claim:] [1.]1. Window unit (W) for an aircraft having a cabin, a hull and a pressure window component, comprising: an outer window frame (1), an inner window frame (3), a window pane (2) lying between the outer window frame (1) and the inner window frame (3), the window unit (W) being insertabl
[ We claim:] [1.]1. Window unit (W) for an aircraft having a cabin, a hull and a pressure window component, comprising: an outer window frame (1), an inner window frame (3), a window pane (2) lying between the outer window frame (1) and the inner window frame (3), the window unit (W) being insertable into an opening (7) in a side-wall panel (6) in the aircraft cabin, the window unit (W) having a centering device and at least two snap fastenings (13) to detachably connect the window unit (W) to the side-wall panel (6) or to components connected thereto, the side-wall panel (6) or components connected thereto having any necessary mating parts for the centering device and for the at least two snap fastenings (13), said connection of the window unit (W) to the side-wall panel, or components connected thereto, being independent of said hull or pressure window component.
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이 특허에 인용된 특허 (11)
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