Fixture for compressor stator chord restoration repair

1. A fixture assembly for retaining a workpiece during a coining process, wherein the workpiece includes an airfoil portion, a platform, and feet extending from the platform opposite the airfoil portion, the feet configured to engage a retention slot in a gas turbine engine, wherein each one of the feet defines a substantially arcuate engagement surface, the assembly comprising: a workpiece that includes an airfoil portion, a platform, and feet extending from the platform opposite the airfoil portion, wherein each one of the feet defines a substantially arcuate engagement surface; a mounting block for releasably engaging the feet, wherein the mounting block comprises: a first portion defining opposite first and second lateral edges; a slot defined in the first portion between the first and second lateral edges and having an exposed front face to provide access to the slot; and first and second retaining structures positioned adjacent to the first and second lateral edges, respectively, of the first portion, wherein each of the first and second retaining structures overhangs the slot and defines an engagement surface facing the slot, such that during engagement of the workpiece the substantially arcuate engagement surfaces of the feet contact the engagement surfaces of the first and second retaining structures to provide a pivotable engagement.

2. The assembly of claim 1 and further comprising: a first portion of a coining die fixed adjacent to the mounting block to engage the airfoil portion of the workpiece during the coining process, wherein the engagement of the mounting block to the workpiece permits pivotal movement of the workpiece relative to the first portion of the coining die between pre-coining and post-coining positions.

3. The assembly of claim 2 , wherein the first portion of the coining die is positioned substantially horizontally, and wherein the mounting block has a non-horizontal orientation.

4. The assembly of claim 1 , wherein the engagement surfaces of the first and second retaining structures are each substantially planar.

5. The assembly of claim 1 , the mounting block further comprising: attachment structures for removably securing the mounting block to a base, wherein the attachment structures comprise fasteners secured to the first portion of the mounting block.

6. The assembly of claim 1 and further comprising: a biased retaining pin extending from the first portion of the mounting block through at least a portion of the slot for biasing the workpiece relative to the first and second retaining structures.

7. The assembly of claim 6 , wherein the biased retaining pin is oriented substantially perpendicular to the planar surface of the first retaining structure, and is configured to contact the workpiece at a face of the platform opposite the airfoil portion.

8. A fixture assembly for retaining a workpiece, wherein the workpiece includes an airfoil portion, a platform, and feet extending from the platform opposite the airfoil configured to engage a retention slot in a gas turbine engine, wherein each one of the feet defines a substantially arcuate engagement surface, the assembly comprising: a workpiece that includes an airfoil portion, a platform, and feet extending from the platform opposite the airfoil, wherein each one of the feet defines a substantially arcuate engagement surface;

a first mounting surface configured to engage a first foot of the workpiece at the respective substantially arcuate engagement surface; a second mounting surface configured to engage a second foot of the workpiece at the respective substantially arcuate engagement surface; a third substantially planar mounting surface positioned adjacent to both the first and second mounting surfaces and configured to contact both first and second feet of the workpiece, wherein the first and third mounting surfaces can maintain engagement with respect to two datum surfaces at the feet of the workpiece while allowing pivoting movement of the workpiece.

9. The assembly of claim 8 , wherein the first and second mounting surfaces are each cylindrical.