Turbine vane restoration system
View Patent ↗A system and method for reconfiguring a turbine vane. In at least one embodiment, the system may be used to straighten an airfoil of a turbine vane segment to remove lean, twist, or racking, or any combination thereof. The airfoil may be straightened by fixing portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane, restricting other portions of the forward and aft hooks of the inner and outer shrouds of the turbine vane to only move rotationally about a centerline of the inner or outer shrouds, and applying a load to various portions of the inner and outer shrouds and the airfoil to return the turbine vane to be within predetermined specifications.
1. A method for removing distortions from a turbine vane, comprising:
loading the turbine vane into a fixture, wherein the turbine vane is formed from an elongated airfoil having an inner shroud attached to a first end and an outer shroud attached to a second end opposite to the first end, wherein the outer shroud includes forward and aft outer hooks extending from the outer shroud away from the elongated airfoil;
locking the forward outer hook of the turbine vane to the fixture to substantially prevent movement of the forward outer hook;
restricting the aft outer hook of the turbine vane such that the aft outer hook may only rotate about an outer shroud centerline that is generally aligned with a line extending between a leading edge and trailing edge of the turbine vane; and
applying a force to the inner shroud.
2. The method of claim 1 , wherein the turbine vane is in a solution annealed state.
3. The method of claim 1 , applying an aging heat treatment to the turbine vane after applying the force to the turbine vane.
4. A method for removing distortions from a turbine vane comprising:
loading the turbine vane into a fixture, wherein the turbine vane is formed from an elongated airfoil having an inner shroud attached to a first end and an outer shroud attached to a second end opposite to the first end, wherein the outer shroud includes forward and aft outer hooks extending from the outer shroud away from the elongated airfoil;
locking the aft outer hook of the turbine vane to the fixture to substantially prevent movement of the aft outer hook;
restricting the forward outer hook of the turbine vane such that the forward outer hook may only rotate about an outer shroud centerline that is generally aligned with a line extending between a leading edge and trailing edge of the turbine vane; and
applying a force to the inner shroud.
5. The method of claim 4 , wherein the turbine vane is in a solution annealed state.
6. The method of claim 4 , applying an aging heat treatment to the turbine vane after applying the force to the turbine vane.
7. A method for removing distortions from a turbine vane comprising:
loading the turbine vane into a fixture, wherein the turbine vane is formed from an elongated airfoil having an inner shroud attached to a first end and an outer shroud attached to a second end opposite to the first end, wherein the inner shroud includes forward and aft inner hooks extending from the inner shroud away from the elongated airfoil;
locking the forward and aft inner hooks of the inner shroud of the turbine vane to the fixture to substantially prevent movement of the forward and aft inner hooks of the inner shroud;
fixing locking a forward outer hook to prevent rotation or axial movement; and
applying a force to an aft outer hook of the turbine vane to move the aft outer hook away from the inner shroud.
8. The method of claim 7 , wherein the turbine vane is in a solution annealed state.
9. The method of claim 7 , applying an aging heat treatment to the turbine vane after applying the force to the turbine vane.