Patent ID: 8297811
Filing Date: 2012-10-30
Classification: B60Q,B64D,F21V,F21W,F21Y

Abstract:
1. An aircraft lamp comprising: a housing capable of being attached to a body of an aircraft; a discharge lamp; a reflector which reflects visible light from the discharge lamp; a light transmissive cover which transmits reflected light from the reflector to a front side of the housing; a lamp socket connected electrically to the discharge lamp and an igniter which activates the discharge lamp; and a high-voltage electrical power line that electrically connects the lamp socket with the igniter, wherein the discharge lamp, the reflector, the light transmissive cover, the lamp socket, and the igniter are provided within the housing, wherein a heat insulating air layer is provided between the lamp socket and the igniter, wherein the high-voltage electrical power line is provided so as to pass through the heat insulating air layer, wherein the reflector is attached to the lamp socket, wherein a supporting surface of the lamp socket and an attaching surface of the igniter are disposed so as to be substantially at right angles to a direction in which the reflector is attached in the housing, and wherein the air layer is formed between the supporting surface and the attaching surface.