Locking spacer assembly, corresponding blade assembly, method for installing a locking spacer

1. A locking spacer assembly configured to fill a final spacer slot in a disk groove between platforms of adjacent blades of a blade assembly comprising:

a first side piece;

a second side piece;

a mid piece configured to be disposed between an inner surface of the first side piece and an inner surface of the second side piece; and

a bolt configured to be disposed into the mid piece,

wherein the bolt is configured to position the mid piece in a radial position in an assembled state,

wherein the mid piece is configured to contact the first side piece and the second side piece in the assembled state to prevent an axial movement of the first side piece and an axial movement of the second side piece,

wherein the mid piece comprises a base and a hollow cylindrical body,

wherein the hollow cylindrical body radially penetrates through the base and radially extends upwardly from the base, and

wherein the bolt is threaded within the hollow cylindrical body.

2. The locking spacer assembly as claimed in claim 1 ,

wherein the base comprises two top surfaces axially extending out from a lower end of the hollow cylindrical body, and

wherein the two top surfaces contact a bottom surface of the first side piece and a bottom surface of the second side piece in the assembled state.

3. The locking spacer assembly as claimed in claim 1 ,

wherein the first side piece comprises a circular groove extending radially downwardly in an inner surface,

wherein the second side piece comprises a circular groove extending radially downwardly in an inner surface, and

wherein the hollow cylindrical body of the mid piece is disposed into the circular groove of the first side piece and the circular groove of the second side piece in the assembled state.

4. The locking spacer assembly as claimed in claim 1 , wherein the base comprises a dovetail shape.

5. The locking spacer assembly as claimed in claim 1 , wherein the first side piece comprises a tab extending from a top surface and protruding axially outwardly from the inner surface.

6. The locking spacer assembly as claimed in claim 5 , wherein the tab comprises a cutout.

7. The locking spacer assembly as claimed in claim 1 , wherein the second side piece comprises a recess formed at an edge of a top surface and the inner surface.

8. A blade assembly comprising:

a rotor disk comprising a disk groove;

a plurality of blades inserted in the disk groove, wherein each of the blades comprises a platform, and wherein a final spacer slot is formed in the disk groove between platforms of adjacent blades; and

a locking spacer assembly configured to fill the final spacer slot,

wherein the locking spacer assembly comprises:

a first side piece;

a second side piece;

a mid piece configured to be disposed between an inner surface of the first side piece and an inner surface of the second side piece; and

a bolt configured to be disposed into the mid piece,

wherein the bolt is configured to position the mid piece in a radial position in an assembled state,

wherein the mid piece is configured to contact the first side piece and the second side piece in the assembled state to prevent an axial movement of the first side piece and an axial movement of the second side piece,

wherein the mid piece comprises a base and a hollow cylindrical body,

wherein the hollow cylindrical body radially penetrates through the base and radially extends upwardly from the base, and

wherein the bolt is threaded within the hollow cylindrical body.

9. The blade assembly as claimed in claim 8 ,

wherein the base comprises two top surfaces axially extending out from a lower end of the hollow cylindrical body, and

wherein the two top surfaces contact a bottom surface of the first side piece and a bottom surface of the second side piece in the assembled state.

10. The blade assembly as claimed in claim 8 ,

wherein the first side piece comprises a circular groove extending radially downwardly in the inner surface,

wherein the second side piece comprises a circular groove extending radially downwardly in the inner surface, and

wherein the hollow cylindrical body of the mid piece is disposed into the circular groove of the first side piece and the circular groove of the second side piece in the assembled state.

11. The blade assembly as claimed in claim 8 , wherein the base comprises a dovetail shape.

12. The blade assembly as claimed in claim 8 , wherein the first side piece comprises a tab extending from a top surface and protruding axially outwardly from the inner surface.

13. The blade assembly as claimed in claim 12 , wherein the tab comprises a cutout.

14. The blade assembly as claimed in claim 8 , wherein the second side piece comprises a recess formed at an edge of a top surface and the inner surface.

15. A method for installing a locking spacer assembly into a final spacer slot in a disk groove between platforms of adjacent blades of a blade assembly, wherein the locking spacer assembly comprises a first side piece, a second side piece, a mid piece and a bolt, the method comprising:

disposing the bolt into the mid piece;

placing the mid piece and the bolt disposed within the mid piece into the disk groove;

placing the first side piece and the second side piece into the disk groove one after another such that the mid piece is disposed between an inner surface of the first side piece and an inner surface of the second side piece; and

positioning the mid piece in a radial position in an assembled state by the bolt such that the mid piece contacts the first side piece and the second side piece in the assembled state,

wherein the second side piece comprises a recess formed at an edge of a top surface and the inner surface, and wherein the first side piece and the second side piece are placed into the disk groove by overlapping the tab with the recess.

16. The method as claimed in claim 15 , further comprising axially moving the mid piece in the disk groove for aligning the mid piece with the first side piece and the second side piece prior to positioning the mid piece in the radial position.

17. The method as claimed in claim 15 , wherein the first side piece comprises a tab extending from a top surface and protruding axially outwardly from the inner surface.