Warning system having low intensity wind shear enhancements

Communications: electrical – Aircraft alarm or indicating systems – Flight alarm

Patent

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Details

340970, 340967, G08B 2300

Patent

active

051535882

ABSTRACT:
A ground proximity warning system for aircraft having flight path angle based warning criteria generates a warning in the event of an excessively steep flight path angle during an approach to a landing. The warning criteria are altered to provide an earlier warning upon the occurrence of a low intensity wind shear or a below glideslope condition. A below glideslope warning system that is biased as a function of decreasing performance shear is also provided. A descent rate based warning system usable above a predetermined altitude may also be provided to supplement the flight path angle warning system.

REFERENCES:
patent: 4684948 (1987-08-01), Bateman
patent: 4947164 (1990-08-01), Bateman

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