G - Physics – 01 – S
Patent
G - Physics
01
S
343/15
G01S 1/08 (2006.01)
Patent
CA 1128627
ABSTRACT OF THE DISCLOSURE By utilizing a radio altimeter in conjunction with a measure of the aircraft speed, landing gear position and flap position, an aircraft terrain warning system is made possible which provides a voice warning indicating that the aircraft is too low with respect to the terrain when the aircraft is above a predetermined speed. For aircraft speeds below the predetermined speed, a voice warning is provided when the aircraft is below predetermined altitude with the landing gear up indicating that the aircraft is too low with the gear up and when the gear is down and the flaps are not in a landing position and the aircraft descends below a second predetermined altitude a voice warning is generated indicating that the aircraft is too low with flaps up.
369115
George H. Riches And Associates
Sundstrand Data Control Inc.
LandOfFree
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