Method and apparatus for performing gas turbine engine maintenance
First Claim
1. A method for performing maintenance on a gas turbine engine assembly that includes a gas turbine engine including at least one variable stator vane assembly, at least one variable bypass valve, a hydromechanical unit that includes a first servo motor coupled to the at least one variable stator vane assembly and a second servo motor coupled to the at least one variable bypass valve, and an engine control unit configured to couple to the first and second servo motors, said method comprises:
- unplugging a first connector from a first socket, the first connector electrically coupled to the engine control unit, the first socket electrically coupled to the hydromechanical unit;
plugging a second connector into the first socket, the second connector electrically coupled to a driver simulator; and
operating the driver simulator to reposition at least one of the variable stator vane assembly and the variable bypass valve from a first operational position to a second operational position that is different than the first operational position.
1 Assignment
0 Petitions
Accused Products
Abstract
A method for performing maintenance on a gas turbine engine assembly includes unplugging a first connector from a first socket, the first connector electrically coupled to the engine control unit, the first socket electrically coupled to the hydromechanical unit, plugging a second connector into the first socket, the second connector electrically coupled to a driver simulator, cranking the engine core to a low speed value, and operating the driver simulator to reposition at least one of the variable stator vane assembly and the variable bypass valve from a first operational position to a second operational position that is different than the first operational position.
17 Citations
20 Claims
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1. A method for performing maintenance on a gas turbine engine assembly that includes a gas turbine engine including at least one variable stator vane assembly, at least one variable bypass valve, a hydromechanical unit that includes a first servo motor coupled to the at least one variable stator vane assembly and a second servo motor coupled to the at least one variable bypass valve, and an engine control unit configured to couple to the first and second servo motors, said method comprises:
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unplugging a first connector from a first socket, the first connector electrically coupled to the engine control unit, the first socket electrically coupled to the hydromechanical unit;
plugging a second connector into the first socket, the second connector electrically coupled to a driver simulator; and
operating the driver simulator to reposition at least one of the variable stator vane assembly and the variable bypass valve from a first operational position to a second operational position that is different than the first operational position. - View Dependent Claims (2, 3, 4, 5)
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6. A driver simulator for performing maintenance on a gas turbine engine assembly that includes a gas turbine engine including at least one variable stator vane assembly, at least one variable bypass valve, a hydromechanical unit that includes a first servo motor coupled to the at least one variable stator vane assembly and a second servo motor coupled to the at least one variable bypass valve, said driver simulator comprising:
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a first system coupled to the hydromechanical unit and configured to reposition the variable stator vane assembly from a first operational position to a second operational position; and
a second system coupled to the hydromechanical unit and configured to reposition the variable bypass valve from a first operational position to a second operational position. - View Dependent Claims (7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20)
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Specification