METHOD AND DEVICE FOR STABILISATION OF GEOMETRICAL PARAMETERS OF AIRCRAFT LANDING SYSTEM INDICATING LIGHTS Russian patent published in 2009 - IPC B64F1/18 

Abstract RU 2350517 C1

FIELD: transport.

SUBSTANCE: apart from traditional stabilisation of indicating lights unit, in aircraft swinging of prime importance is influence of air medium parameters on the indicating lights propagation direction and geometrical parameters in the zone of formation of the above lights. With due allowance for the above fact, air medium parameter pickups and indicating light stabilisation unit are installed in the aforesaid zone and heat radiation effects brought about by the indicating light unit are ruled out. Indicating floodlight can be replaced with white-radiation laser and modulator of brightness, color and laser beam 3D position. Note here that all heat radiating elements are located outside the laser beam formation zone, while the 3D modulator is installed at landing strip start.

EFFECT: reduced influence of medium on parameters of color zone created by indicating lights in landing aircraft of ship deck.

2 cl, 1 dwg

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RU 2 350 517 C1

Authors

Narver Valerij Naumovich

Narver Vadim Valerievich

Patrushev Vladimir Viktorovich

Dates

2009-03-27Published

2007-08-06Filed