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Method and apparatus for performing gas turbine engine maintenance

  • US 20070084210A1
  • Filed: 07/19/2005
  • Published: 04/19/2007
  • Est. Priority Date: 07/19/2005
  • Status: Active Grant
First Claim
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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:

  • 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.

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