AIRCRAFT LAMP

WIPO Patent Application WO/2021/010270

A1

This aircraft lamp is provided with: a lamp outer case (4) in which the internal space is formed as a first placement space (5) and which is configured by a lamp housing (2) having an opening and a cover (3) attached to the lamp housing in a state of covering the opening; and a lamp unit (17) that is detachably attached to the lamp housing and that has a light source module (19) provided with a light source (33), an attaching base (18) to which the light source module is attached, and a power reception connector (21) which is attached to the attaching base and which is for supplying power to the light source, wherein an insertion hole (11a) in communication with the first placement space is formed in the lamp housing, a placement case (9) having a second placement space (10) opened to the outer surface side of the lamp housing is provided to the lamp housing, at least a part of the light source module is disposed in the first placement space in a state of being inserted in the through-hole, and the power reception connector is disposed in the second placement space.

JP6634303	A light source unit, manufacturing of the light source unit manufacturing method and a vehicle lamp
WO/2023/192495	LED RETROFIT LAMP FOR USE IN PROJECTOR TYPE AUTOMOTIVE HEADLIGHT SYSTEM
JP2024002551	Vehicle lights

NAKAMURA KAZUYOSHI (JP)
YODA TAKASHI (JP)
ISHIKIRIYAMA MASARU (JP)

PCT/JP2020/026816

January 21, 2021

July 09, 2020

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KOITO MFG CO LTD (JP)

F21S41/19; B64D47/06; F21S2/00; F21V19/00; F21V23/00; F21V23/06; F21V29/503; F21V29/76; F21W107/30; F21Y115/10

JP2013187081A	2013-09-19
JP2013054834A	2013-03-21
JP2015138742A	2015-07-30
JP2010033840A	2010-02-12
JP2010033841A	2010-02-12

See also references of EP 3998423A4

IWATA, Masanobu et al. (JP)

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