Aircraft illumination device

Illumination – Vehicle steering mechanism or element moves pivoted lamp or... – Tie rod element controlled

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Details

340946, 362 34, B64D 4702

Patent

active

054166721

ABSTRACT:
A system for illuminating parts of an aircraft, such as a helicopter, including three low-intensity position lights (10) mounted on the aircraft, with two of the position lights mounted in a forward location and spaced laterally from the center of the aircraft and a third position light mounted in an aft location centrally positioned on the aircraft. The three position lights provide a triangular light formation that indicates the position of the aircraft during tactical, covert operations. The position lights include a chemiluminescent light source (12) and a housing (22) for carrying the chemiluminescent light source. Each housing is secured to a part of the aircraft by means of a bracket (52) and a pair of band clamps (60). The chemiluminescent light source is visible from within the housing within a limited range of the aircraft. Preferably, the chemiluminescent light source creates an infrared light that is detectable by means of night vision goggles worn by pilots of nearby flying aircraft.

REFERENCES:
patent: 2365038 (1944-12-01), Adler, Jr.
patent: 4916581 (1990-04-01), Authier

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