Anti-rotation assembly

Patent metadata

Field	Value
Publication number	US-10598015-B2
Application number	US-201715794676-A
Country	US
Kind code	B2
Filing date	Oct 26, 2017
Priority date	Oct 26, 2017
Publication date	Mar 24, 2020
Grant date	Mar 24, 2020

Abstract

An anti-rotation assembly may include a first shaft, a second shaft, and a locking sprocket. The first shaft may have a first crenelated end rim, the second shaft may have a second crenelated end rim, and the locking sprocket may be configured to engage the first crenelated end rim and the second crenelated end rim to anti-rotatably couple the first shaft to the second shaft. That is, the locking sprocket may be configured to prevent relative rotation between the two shafts. The anti-rotation assembly may further include an axial retaining ring configured to axially retain the locking sprocket.

First claim

What is claimed is:

1. An anti-rotation assembly comprising:
a first shaft comprising a first crenelated end rim defining a plurality of first crenels;
a second shaft comprising a second crenelated end rim defining a plurality of second crenels;
a locking sprocket comprising a body and a plurality of teeth extending from the body, wherein the body of the locking sprocket locking sprocket is disposed radially inward of the first crenelated end rim and the second crenelated end rim, wherein the locking sprocket is configured to engage the first crenelated end rim and the second crenelated end rim to anti-rotatably couple the first shaft to the second shaft, wherein the plurality of teeth are configured to extend into the plurality of first crenels and the plurality of second crenels to prevent relative rotation between the first shaft and the second shaft; and
an axial retaining ring configured to axially retain the locking sprocket.

2. The anti-rotation assembly of claim 1 , wherein an inner radius of the body of the locking sprocket is the same as an inner radius of the first shaft and the second shaft.

3. The anti-rotation assembly of claim 1 , wherein:
the plurality of first crenels are defined between a plurality of first merlons of the first crenelated end rim;
the plurality of second crenels are defined between a plurality of second merlons of the second crenelated end rim;
the plurality of first merlons are aligned with the plurality of second merlons; and
the plurality of first crenels are aligned with the plurality of second crenels.

4. The anti-rotation assembly of claim 3 , wherein the plurality of first merlons collectively define a circumferential groove configured to receive the axial retaining ring.

5. The anti-rotation assembly of claim 4 , wherein the first crenelated end rim is axially longer than the second crenelated end rim.

6. The anti-rotation assembly of claim 4 , wherein the circumferential groove is disposed at an axial midpoint between first closed ends of the plurality of first crenels of the first crenelated end rim and second closed ends of the plurality of second crenels of the second crenelated end rim.

7. The anti-rotation assembly of claim 1 , wherein the first shaft comprises first threads disposed on a first radially outward surface of the first shaft and the second shaft comprises second threads disposed on a second radially outward surface of the second shaft.

8. The anti-rotation assembly of claim 1 , wherein
the first shaft and second shaft are shafts of a gas turbine engine.

9. The anti-rotation assembly of claim 8 , wherein the first shaft is a first stage turbine shaft and the second shaft is a second stage turbine shaft.

10. The anti-rotation assembly of claim 8 , wherein the first shaft is a turbine shaft and the second shaft is a compressor shaft.

11. A method of assembling a gas turbine engine, the method comprising:
engaging a locking sprocket on a first crenelated end rim of a first shaft;
positioning a second shaft so that a second crenelated end rim of the second shaft is juxtaposed with the first crenelated end rim;
axially moving the locking sprocket to engage the first crenelated end rim and the second crenelated end rim; and
engaging an axial retaining ring in a circumferential groove defined in the first crenelated end rim to retain the locking sprocket in place;
wherein:
the first crenelated end rim defines a plurality of first crenels;
the second crenelated end rim defines a plurality of second crenels;
the locking sprocket comprises a body and a plurality of teeth extending from the body;
the body of the locking sprocket is disposed radially inward of the first crenelated end rim and the second crenelated end rim; and
axially moving the locking sprocket to engage the first crenelated end rim and the second crenelated end rim comprises inserting the plurality of teeth to extend into the plurality of first crenels and the plurality of second crenels to prevent relative rotation between the first shaft and the second shaft.

12. The method of claim 11 , wherein engaging the locking sprocket on the first crenelated end rim of the first shaft comprises engaging the axial retaining ring in the circumferential groove.

13. The method of claim 12 , further comprising removing the axial retaining ring from the circumferential groove before axially moving the locking sprocket.

14. The method of claim 13 , further comprising replacing the axial retaining ring into the circumferential groove after axially moving the locking sprocket.

15. The method of claim 11 , wherein positioning the second shaft comprises aligning a plurality of first merlons of the first crenelated end rim with a plurality of second merlons of the second crenelated end rim.

16. An anti-rotation assembly comprising:
a first shaft comprising a first crenelated end rim defining a plurality of first crenels, wherein the plurality of first crenels are defined between a plurality of first merlons of the first crenelated end rim;
a second shaft comprising a second crenelated end rim defining a plurality of second crenels, wherein the plurality of second crenels are defined between a plurality of second merlons of the second crenelated end rim;
a locking sprocket comprising a plurality of teeth, wherein the locking sprocket is configured to engage the first crenelated end rim and the second crenelated end rim to anti-rotatably couple the first shaft to the second shaft, wherein the plurality of teeth are configured to extend into the plurality of first crenels and the plurality of second crenels to prevent relative rotation between the first shaft and the second shaft; and
an axial retaining ring configured to axially retain the locking sprocket;
wherein
the plurality of first merlons are aligned with the plurality of second merlons and the plurality of first crenels are aligned with the plurality of second crenels;
the plurality of first merlons collectively define a circumferential groove configured to receive the axial retaining ring; and
the circumferential groove is disposed at an axial midpoint between first closed ends of the plurality of first crenels of the first crenelated end rim and second closed ends of the plurality of second crenels of the second crenelated end rim.

17. The an anti-rotation assembly of claim 16 , wherein a body of the locking sprocket, from which the plurality of teeth extends, is disposed radially inward of the first crenelated end rim and the second crenelated end rim.

18. The anti-rotation assembly of claim 17 , wherein an inner radius of the body of the locking sprocket is the same as an inner radius of the first shaft and the second shaft.

19. The anti-rotation assembly of claim 16 , wherein the first crenelated end rim is axially longer than the second crenelated end rim.

Assignees

• United Technologies Corp

Inventors

• Oren Nicholas Waters
• Wilson Ross

Classifications

• F01D5/026 Primary

  Shaft to shaft connections · CPC title

• F05D2250/182

  crenellated, notched · CPC title

• F02C3/073

  the compressor and turbine stages being concentric · CPC title

• Y10T403/5773

  Interfitting · CPC title

• F05D2240/60

  Shafts · CPC title