Excessive sink rate warning system for aircraft
AssigneeSundstrand Data Control, Inc.
InventorCharles Donald Bateman
Life of this patent
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AssigneeSundstrand Data Control, Inc.
InventorCharles Donald Bateman
Estimating the term…
In an aircraft ground proximity warning system that compares the rate of descent of an aircraft with its altitude above the terrain and in response thereto generates a warning signal when the aircraft's sink rate exceeds a predetermined limit for a particular altitude, a first type of advisory voice warning is generated for combinations of lesser descent rates and greater altitudes and a second type of imperative voice warning is generated for greater sink rates at lower altitudes where the danger of the aircraft impact with the terrain is more significant. In addition, the repetition rate of the advisory warning is increased as a function of increasing descent rate and the amplitude of the advisory warning can similarly be increased as function of increasing descent rate in order to call attention to an increasing undesirable operating condition.
A warning system for use in aircraft having a source of signals representing the aircraft's barometric rate of descent and a source of signals representing the aircraft's altitude above terrain, comprising:
A warning system for use in aircraft having a barometric altimeter and a radar altimeter comprising:
An excessive descent rate warning system for use in aircraft having a source of signals representing the aircrafts barometric descent rate and a radio altimeter, comprising:
A warning system for use in aircraft having a source of signals representing the aircraft's barometric rate of descent and a source of signals representing the aircraft's altitude above terrain, comprising:
A warning system for use in aircraft having a source of signals representing the aircraft's altitude above terrain, comprising:
Dependencies are inferred from the claim text.