Aircraft instrument systems

Communications: electrical – Aircraft alarm or indicating systems – Potential collision with other aircraft

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342 29, 364461, G08G 504

Patent

active

049806831

ABSTRACT:
An aircraft collision avoidance instrument system has a display located in the aircraft glareshield in the peripheral field of view of the pilot when the pilot is looking forwardly through the aircraft window. The display has a matrix array of LCD elements which is controlled to provide a continually changing image that is visible in the peripheral field of view of the pilot when a possible collision with another aircraft is likely. The changing image may be arrows moving up or down the display to indicate climb or decend, or a flashing horizontal line to indicate that present height must be maintained. An alphanumeric legend indicative of the collision avoidance action to be taken is also provided by the display. When no collision is likely, the display is used to present other information to the pilot.

REFERENCES:
patent: 3614728 (1971-10-01), Borrok et al.
patent: 3621210 (1971-11-01), Canning et al.
patent: 3699511 (1972-10-01), Fletcher et al.
patent: 3846746 (1974-11-01), Trageser et al.
patent: 4181405 (1980-01-01), Cohen
patent: 4403220 (1983-09-01), Donovan
patent: 4835537 (1989-05-01), Manion
"At the Crossroads in Air Traffic Control", IEEE Spectrum, Jul. 1970, pp. 69-83, Friedlander, Cl. 364-439.
"TCAS II Equipment", Aviation International News, 7-01-89, Tripp.

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