AIRCRAFT LAMP

An aircraft lamp of the present disclosure includes a plurality of LEDs, an inner lens that diffuses light of the LED in a lamp longitudinal direction, and a light scattering and transmitting member (outer lens 4) that scatters and transmits the light that transmits the inner lens. The inner lens is...

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Bibliographische Detailangaben
1. Verfasser:	YODA, Takashi
Format:	Patent
Sprache:	eng
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 THEFORM OR THE KIND OF THE LIGHT SOURCES OR OF THE COLOUR OF THELIGHT EMITTED INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21Sand F21V, RELATING TO USESOR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS STRUCTURAL COMBINATIONS OF LIGHTING DEVICES WITH OTHERARTICLES, NOT OTHERWISE PROVIDED FOR TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An aircraft lamp of the present disclosure includes a plurality of LEDs, an inner lens that diffuses light of the LED in a lamp longitudinal direction, and a light scattering and transmitting member (outer lens 4) that scatters and transmits the light that transmits the inner lens. The inner lens is a cylindrical lens, and convex portions are formed along a lamp transverse direction. In addition, the convex portions are formed in parallel in a lamp longitudinal direction.