Aircraft engine assembly for controlling engine oil flow during fire conditions and method for using same
AssigneePratt & Whitney Canada Corp.
InventorsKashif Mohammed, Vivek Bhat
Life of this patent
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AssigneePratt & Whitney Canada Corp.
InventorsKashif Mohammed, Vivek Bhat
Estimating the term…
An assembly for an aircraft includes an aircraft housing, an auxiliary power unit (APU), an oil system, a door actuator, and a controller. The aircraft housing forms a compartment. The aircraft housing includes an intake door. The intake door is movable between a closed position, an open position, and intermediate positions between the closed position and the open position. The APU is disposed within the compartment. The APU includes an engine. The engine includes an air inlet and a rotational assembly. The oil pump is operatively connected to the rotational assembly. The door actuator is operatively connected to the intake door. The door actuator is operable to position the intake door in the closed position, the open position, and the intermediate positions to control an ambient air flow to the air inlet. The controller is operatively connected to the door actuator. The controller is configured to identify a fire condition within the compartment, identify a fire position of the intake door, and control the door actuator to position the intake door in the fire position. The fire position is one of the open position or the intermediate positions.
An assembly for an aircraft, the assembly comprising:
A method for controlling an oil flow rate for an oil system of an auxiliary power unit (APU) for an aircraft, the method comprising:
An assembly for an aircraft, the assembly comprising:
Dependencies are inferred from the claim text.