OPERATING AIRCRAFT PROPULSION SYSTEM DURING ENGINE-INOPERATIVE EVENT

A method is provided for operating an aircraft having a first propulsion unit and a second propulsion unit. During this method a propulsion unit-inoperative event is identified where the first propulsion unit is inoperative and the second propulsion unit is operative. A trimmed parameter for the sec...

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Bibliographische Detailangaben
Hauptverfasser:	GATES, PATRICK, PAPILLON, MELANIE
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A method is provided for operating an aircraft having a first propulsion unit and a second propulsion unit. During this method a propulsion unit-inoperative event is identified where the first propulsion unit is inoperative and the second propulsion unit is operative. A trimmed parameter for the second propulsion unit is converted to an actual parameter for the second propulsion unit. The actual parameter is monitored over a period of time the second propulsion unit operates during the propulsion unit-inoperative event. An action is performed in response to determining that the second propulsion unit has operated for at least a time threshold with the actual parameter being equal to or greater than a parameter threshold.