Inlet guide vane removal tools and methods

Patent metadata

Field	Value
Publication number	US-11022147-B2
Application number	US-201616349104-A
Country	US
Kind code	B2
Filing date	Nov 15, 2016
Priority date	Nov 15, 2016
Publication date	Jun 1, 2021
Grant date	Jun 1, 2021

Abstract

An inlet guide vane removal assembly includes a support frame with a support plate. At least one force device is coupled to the support plate. A puller bracket is attached to the at least one force device. The puller bracket has an open-ended slot defined therethrough, and a plurality of flanges positioned to engage an installed inlet guide vane. When the force device is actuated, the puller bracket is displaced relative to the support frame to facilitate removing the inlet guide vane.

First claim

What is claimed is:

1. An inlet guide vane removal assembly comprising:
a support frame comprising a support plate;
a pair of force devices coupled to said support plate, each force device of said pair of force devices comprising an actuator and an engaging rod slidably coupled thereto; and
a puller bracket coupled to each said engaging rod of said each force device, said puller bracket comprising:
an open-ended slot defined therethrough; and
a plurality of flanges positioned to engage an installed inlet guide vane such that, when at least one force device of said pair of force devices is actuated, said puller bracket is displaced relative to said support frame to facilitate removal of the inlet guide vane.

2. An inlet guide vane removal assembly in accordance with claim 1 , wherein said support plate comprises an open-ended slot defined therein and configured to receive an airfoil portion of the inlet guide vane.

3. An inlet guide vane removal assembly in accordance with claim 1 , wherein said support frame further comprises a guide plate spaced from said support plate.

4. An inlet guide vane removal assembly in accordance with claim 3 , wherein said support plate comprises an open-ended slot defined therein and configured to receive an airfoil portion of the inlet guide vane.

5. An inlet guide vane removal assembly in accordance with claim 3 , wherein said guide plate comprises an open-ended slot defined therein and configured to receive an airfoil portion of the inlet guide vane.

6. An inlet guide vane removal assembly in accordance with claim 3 , wherein said support frame comprises a positioning plate releasably coupled to said guide plate, said positioning plate configured to couple to said guide plate in a first positioned configured to facilitate installing said inlet guide vane removal assembly in a rotor in orientation, and a second positioned configured to facilitate installing said inlet guide vane removal assembly in a rotor out orientation.

7. An inlet guide vane removal assembly in accordance with claim 6 , wherein said positioning plate comprises an open-ended slot defined therein and configured to receive an airfoil portion of the inlet guide vane.

8. An inlet guide vane removal assembly in accordance with claim 1 , wherein said at least one force device is one or more of the following: a hydraulic ram, a lead screw and drive assembly, and an air cylinder.

9. An inlet guide vane removal assembly in accordance with claim 1 further comprising a half ring bridge configured to couple to a casing of a turbine assembly, said half ring bridge comprising a support beam and a half ring segment configured to receive said support frame.

10. A method for removing an inlet guide vane from a turbine assembly, said method comprising:
at least partially disassembling a casing of the turbine assembly to provide access to the inlet guide vane;
engaging the inlet guide vane using an inlet guide vane removal assembly;
applying a force to a puller bracket of the inlet guide vane removal assembly using at least one force device of a pair of force devices, such that the inlet guide vane is displaced within the turbine assembly, to facilitate removing a drive gear from the inlet guide vane, wherein each force device of said pair of force devices comprises an actuator and an engaging rod slidably coupled thereto, and wherein the puller bracket is coupled to each said engaging rod of said each force device; and
removing the inlet guide vane from the turbine assembly.

11. A method in accordance with claim 10 , wherein engaging the inlet guide vane comprises engaging a cylindrical shaft of the inlet guide vane with the puller bracket.

12. A method in accordance with claim 11 , wherein applying the force to the puller bracket comprises applying the force substantially axially to the cylindrical shaft of the inlet guide vane.

13. A method in accordance with claim 10 , wherein applying the force to the puller bracket comprises applying the force to the puller bracket via each engaging rod of the pair of force devices.

14. A method in accordance with claim 10 further comprising:
coupling a half ring bridge to the at least partially disassembled casing; and
coupling the inlet guide vane removal assembly to the half ring bridge.

15. A method in accordance with claim 10 , wherein engaging the inlet guide vane using the inlet guide vane removal assembly further comprises positioning an airfoil of the inlet guide vane in an open-ended slot formed in a guide plate of the inlet guide vane removal assembly.

16. A method in accordance with claim 15 , wherein positioning the airfoil of the inlet guide vane in the open-ended slot comprises:
coupling a positioning plate to the guide plate in a rotor in orientation; and
engaging the inlet guide vane with the inlet guide vane removal assembly in the rotor in orientation.

17. A method in accordance with claim 15 , wherein positioning the airfoil of the inlet guide vane in the open-ended slot comprises:
coupling a positioning plate to the guide plate in a rotor out orientation; and

engaging the inlet guide vane with the inlet guide vane removal assembly in the rotor out orientation.

18. An inlet guide vane removal assembly comprising:
a support frame comprising a support plate;
at least one force device coupled to said support plate;
a half ring bridge configured to couple to a casing of a turbine assembly, said half ring bridge comprising a support beam and a half ring segment configured to receive said support frame; and
a puller bracket coupled to said at least one force device, said puller bracket comprising:
an open-ended slot defined therethrough; and
a plurality of flanges positioned to engage an installed inlet guide vane such that, when said at least one force device is actuated, said puller bracket is displaced relative to said support frame to facilitate removal of the inlet guide vane.

Assignees

• Gen Electric
• Haier Us Appliance Solutions Inc

Inventors

• Wojciechowski Piotr Hubert
• Herbold John William
• Perkowski Szymon

Classifications

• F05D2260/4031

  as in toothed gearing · CPC title

• F05D2230/68

  using auxiliary equipment for lifting or holding · CPC title

• F05D2230/70

  Disassembly methods · CPC title

• F01D25/285

  Temporary support structures, e.g. for testing, assembling, installing, repairing; Assembly methods using such structures · CPC title

• B23P19/04

  for assembling or disassembling parts · CPC title