Dual mode anticollision/recognition lamp for aircraft

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

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362240, 362251, 362276, 340981, 315 8461, 315315, B64D 4704

Patent

active

052933040

ABSTRACT:
A dual mode exterior lamp for an aircraft includes a higher intensity anticollision light, a lower intensity recognition light, a power supply for the lights, and means for activating the anticollision light when the aircraft is airborne and for activating the recognition light when the aircraft is on the ground. In the preferred embodiment the activating means is responsive to a landing gear position switch.

REFERENCES:
patent: 3619597 (1971-11-01), Adler
patent: 3676736 (1972-07-01), Starer
patent: 4011541 (1977-03-01), Fabry et al.
patent: 4185232 (1980-01-01), Ingalls et al.
patent: 4233652 (1980-11-01), Oswald
patent: 4346430 (1982-08-01), Holland
patent: 4554544 (1985-11-01), Task
patent: 5136481 (1992-08-01), Dietzsch et al.

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