Multifunction positioning lock washer

1. A gas turbine engine section comprising:

a rotatable shaft;

axially adjacent stationary and rotating components located on the rotatable shaft and separated by an axial separation distance;

a nut configured to thread onto the rotatable shaft to hold one of the axially adjacent stationary and rotating components in compression;

a multifunction positioning lock washer with antirotation geometry configured to prevent the nut from tightening or loosening, wherein an axial length of the multifunction positioning lock washer is adjusted by removing material based on measurement of the axial separation distance to define the axial separation distance by spacing the stationary component relative to the rotating component.

2. The gas turbine engine section of claim 1 , wherein the rotating component is supported on a non-rotating structure via a bearing assembly and a rotating shaft, and wherein the multifunction positioning lock washer takes in tolerances by adjusting the position of the rotating shaft relative to the bearing assembly.

3. The gas turbine engine section of claim 2 , wherein the rotatable shaft has a radial shoulder adjacent the multifunction positioning lock washer.

4. The gas turbine engine section of claim 1 , wherein the rotating component comprises a rotor with airfoil blades, and wherein the stationary component comprises a stator with stationary vanes.

5. The gas turbine engine section of claim 1 , wherein the antirotation geometry comprises washer antirotation geometry configured to antirotate the multifunction positioning lock washer relative to the rotatable shaft, and nut antirotation geometry configured to antirotate the nut relative to the multifunction positioning lock washer, thereby preventing the nut from tightening or loosening.

6. The gas turbine engine section of claim 5 , wherein the washer antirotation geometry comprises a polygonal inner surface of the multifunction positioning lock washer configured to mate with a complementary polygonal surface of the shaft.

7. The gas turbine engine section of claim 6 , wherein the washer antirotation geometry comprises a plurality of axially-extending tabs configured to mate with complementary slots on the shaft.

8. The gas turbine engine section of claim 6 , wherein the nut antirotation geometry comprises a plurality of radially outward-extending crenellations or tabs configured to mate with the nut.

9. The gas turbine engine section of claim 8 , wherein the nut has a plurality of lugs, slots, grooves, or tabs configured to mate with the nut antirotation geometry of the multifunction positioning lock washer.

10. A method for assembling a gas turbine engine section, the method comprising:

measuring an axial separation distance between axially adjacent components;

removing material to reduce the axial length of a multifunction positioning lock washer with antirotation geometry, so as to modify the axial separation distance;

inserting the multifunction positioning lock washer between a shaft and a nut, such that the antirotation geometry of the multifunction positioning lock washer prevents the nut from tightening or loosening, and the axial length of the multifunction positioning lock washer adjusts the separation distance.

11. The method of claim 10 , wherein the axially adjacent components are adjacent rotating and stationary structures, and wherein the axial length of the multifunction positioning lock washer defines the separation distance by spacing rotating structures relative to rotating structures.

12. The method of claim 11 , wherein the rotating structure is supported on a non-rotating structure via a bearing assembly and a rotating shaft, and wherein the multifunction positioning lock washer defines the separation distance between adjacent rotating and nonrotating structures by adjusting the position of the rotating shaft relative to the bearing assembly.

13. The method of claim 12 , wherein the rotating shaft has a radial shoulder, and wherein inserting the multifunction positioning lock washer comprises inserting the multifunction positioning lock washer between the radial shoulder of the rotating shaft and the bearing assembly, such that the multifunction positioning lock washer abuts and is axially retained by the radial shoulder.

14. The method of claim 11 , wherein the nut holds the rotating structure in compression.

15. The method of claim 10 , wherein the antirotation geometry comprises washer antirotation geometry configured to antirotate the multifunction positioning lock washer relative to the shaft, and nut antirotation geometry configured to antirotate the nut relative to the multifunction positioning lock washer, thereby preventing the nut from tightening or loosening.

16. The method of claim 10 , wherein the antirotation geometry comprises a polygonal surface of the multifunction positioning lock washer configured to mate with a complementary polygonal surface of the shaft or nut.

17. The method of claim 10 , wherein the antirotation geometry comprises a plurality of axially-extending tabs configured to mate with complementary slots on the shaft or nut.

18. The method of claim 10 wherein the nut antirotation geometry comprises a plurality of radially outward-extending crenellations or tabs configured to mate with the shaft or nut.

19. The method of claim 10 , wherein measuring the axial separation distance between axially adjacent components comprises assembling the gas turbine engine section prior to removing material from the multifunction positioning lock washer, and recording the resulting axial separation distance between axially adjacent components.