WINDOW FOR AN AIRCRAFT
First Claim
1. A window for an aircraft for a pressurised cabin, wherein in a frame an outer pane facing away from a cabin interior (I) when installed and an inner pane facing the cabin interior (I) are fixed, so that an intermediate space (Z) is formed between the outer and the inner pane,whereinat least one of the inner and the outer panes is provided with a transparent first layer of organic light-emitting diodes andwherein at least one of the inner and the outer panes is provided with an electrochromic second layer.
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Accused Products
Abstract
The invention relates to a window for an aircraft with a pressurised cabin, in which in a frame (1) is fixed an outer pane (3) facing away from a cabin interior (I) when installed and an inner pane (4) facing the cabin interior (I), so that an intermediate space (Z) is formed between the outer (3) and the inner pane (4). To create a lighting function, in accordance with the invention it is proposed that at least one of the inner (4) and the outer panes (3) is provided with a layer (5) of organic light-emitting diodes. In addition, one of the inner (4) and the outer panes (3) is provided with an electrochromic second layer (6).
13 Citations
9 Claims
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1. A window for an aircraft for a pressurised cabin, wherein in a frame an outer pane facing away from a cabin interior (I) when installed and an inner pane facing the cabin interior (I) are fixed, so that an intermediate space (Z) is formed between the outer and the inner pane,
wherein at least one of the inner and the outer panes is provided with a transparent first layer of organic light-emitting diodes and wherein at least one of the inner and the outer panes is provided with an electrochromic second layer.
Specification