SYSTEM AND METHOD TO PREVENT UNINTENDED AIRCRAFT ENGINE SHUTDOWN

Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver...

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Bibliographische Detailangaben
Hauptverfasser:	RUHAN, Desmond, MARTIN, Andrew, ZIOLKOWSKI, Craig, ABLER, Todd
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	Flight control systems, flight control methods, and aircraft are provided. An aircraft including a system and a method for receiving (510), via a fuel switch (260, 450), a first control signal indicative of an off position on a fuel switch (260, 450), determining (520) a throttle (270, 410) resolver angle of a throttle (270, 410) controller in response to the first control signal, comparing (530) the throttle (270, 410) resolver angle to a threshold throttle (270, 410) angle, and generating (540) a pilot warning in response to the first control signal and the throttle (270, 410) resolver angle exceeding the threshold throttle (270, 410) angle.