Aircraft maneuver envelope warning system

Communications: electrical – Aircraft alarm or indicating systems – Nonalarm flight indicator

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340945, 340978, G01C 2100

Patent

active

053593260

ABSTRACT:
A maneuver envelope warning system for an aircraft having operating limits, operating condition sensors and an indicator driver. The indicator driver has a plurality of visual indicators. The indicator driver determines a relationship between sensed operating conditions and the operating limits; such as, a ratio therebetween. The indicator driver illuminates a number of the indicators in proportion to the determined relationship. The position of the indicators illuminated represents to a pilot in an easily ascertainable manner whether the operational conditions are approaching operational limits of the aircraft, and the degree to which operational conditions lie within or exceed operational limits.

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