Angle of attack display
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United States of America Patent
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-
Nov 24, 2015
Grant Date -
Mar 26, 2015
app pub date -
Sep 20, 2013
filing date -
Sep 20, 2013
priority date (Note) -
In Force
status (Latency Note)
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Abstract
An aircraft safety system includes a Stall/Spin Warning & Recovery Computer, an angle of attack sensor, a side slip sensor and an angle of attack display. The Stall/Spin Warning and Recovery Computer detects whether the aircraft is in a safe condition or an unsafe condition. The angle of attack display includes a first configuration that displays information indicative of safe aircraft condition when the orientation detector detects a safe condition and a second configuration that displays information indicative of unsafe aircraft condition when the computer detects an unsafe condition. The display may transition from the first configuration to the second configuration when the orientation detector detects an unsafe condition and then to a third configuration, which may include visual control-input instructions that enable recovery to a safe condition.
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