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The cabin individual lighting for an aircraft, with a light source (10) provided for one or for a group of passengers, has an anti-glare device (20) with a number of light-directing units each with a light entry opening, a light exit opening, and a wall which connects the light entry opening and lig...

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Bibliographische Detailangaben
Hauptverfasser:	VOGEL, CARSTEN, BUDINGER, TILO
Format:	Patent
Sprache:	ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMSTHEREOF HEATING INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21Sand F21V, RELATING TO USESOR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS LIGHTING MECHANICAL ENGINEERING NON-PORTABLE LIGHTING DEVICES PARACHUTES PERFORMING OPERATIONS STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHERARTICLES, NOT OTHERWISE PROVIDED FOR SYSTEMS THEREOF TRANSPORTING VEHICLE LIGHTING DEVICES SPECIALLY ADAPTED FOR VEHICLEEXTERIORS WEAPONS
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Beschreibung
Zusammenfassung:	The cabin individual lighting for an aircraft, with a light source (10) provided for one or for a group of passengers, has an anti-glare device (20) with a number of light-directing units each with a light entry opening, a light exit opening, and a wall which connects the light entry opening and light exit opening, wherein the light-directing units allow a dispersion of a light which is emitted from the light source basically only to the passengers allocated to the light source. An independent claim is included for an aircraft with cabin individual lighting.