Aircraft engine repair tool and method for removal and installation of a rotor in an aircraft engine
Methods and tools for facilitating the installation and/or removal of a rotor on a shaft of a gas turbine engine are provided. The tool includes a stabilizer attachable to the shaft and including a first guide counterpart. The tool also includes a holder attachable to the rotor and including a second guide counterpart for engagement with the first guide counterpart of the stabilizer. Engagement of the first and second guide counterparts guides movement of the holder relative to the stabilizer along a guide axis and prevents movement of the holder relative to the stabilizer transverse to the guide axis.
1 . A method for installing a rotor on a shaft of a gas turbine engine, or removing the rotor from the gas turbine engine, the method comprising:
attaching a stabilizer to a flange of the shaft of the gas turbine engine;
movably engaging a rotor holder with the stabilizer to permit movement of the rotor holder relative to the stabilizer along a rotation axis of the shaft and substantially prevent movement of the rotor holder relative to the stabilizer transverse to the rotation axis of the shaft;
with the rotor attached to the rotor holder, the rotor released from the shaft and the rotor holder engaged with the stabilizer, moving the rotor holder and the rotor together along the rotation axis of the shaft toward or away from an installed position of the rotor along the shaft; and
after moving the holder and the rotor along the rotation axis of the shaft, either:
attaching the rotor to the shaft when the rotor holder and the rotor have been moved toward the installed position of the rotor; or
removing the rotor from the gas turbine engine when the rotor holder and the rotor have been moved away from the installed position of the rotor.
2 . The method as defined in claim 1 , wherein the gas turbine engine is a turbofan engine and the method includes:
removing a fan from a fan interface of the shaft; and
attaching the stabilizer to the flange of the shaft.
3 . The method as defined in claim 2 , wherein the rotor is part of a compressor boost module including a stator and the method includes moving the rotor holder and the compressor boost module together as a unit along the rotation axis of the shaft.
4 . The method as defined in claim 1 , comprising moving the rotor holder and the rotor away from the installed position with the rotor holder engaged to the stabilizer at least until the rotor has axially cleared a rotor mounting interface disposed on the shaft.