Circumferential row of vanes for a gas turbine engine and having non-uniform vane spacing

Patent metadata

Field	Value
Publication number	US-12410722-B2
Application number	US-202318335591-A
Country	US
Kind code	B2
Filing date	Jun 15, 2023
Priority date	Jun 15, 2023
Publication date	Sep 9, 2025
Grant date	Sep 9, 2025

Abstract

A circumferential row of vanes for a gas turbine engine, the circumferential row of vanes has non-uniform spacing. The circumferential row of vanes includes a plurality of stator vanes arranged circumferentially about an inner ring. The plurality of stator vanes include a first group of stator vanes having a first spacing between adjacent stator vanes of the first group of stator vanes and a second group of stator vanes having a second spacing between adjacent stator vanes of the second group of stator vanes. The second spacing is from two percent to eleven percent greater than a nominal uniform vane spacing or from two percent to eleven percent lesser than the nominal uniform vane spacing, the nominal uniform vane spacing being defined by a total number of the plurality of stator vanes. An engine includes the circumferential row of vanes.

First claim

The invention claimed is:

1. A circumferential row of vanes for a gas turbine engine, the circumferential row of vanes having non-uniform vane spacing and comprising:
a plurality of stator vanes arranged circumferentially about an inner ring, the plurality of stator vanes comprising:
a first group of stator vanes having a first spacing between adjacent stator vanes of the first group of stator vanes; and
a second group of stator vanes having a second spacing between adjacent stator vanes of the second group of stator vanes, wherein the second spacing is from two percent to eleven percent lesser than a nominal uniform vane spacing or from two percent to eleven percent greater than the nominal uniform vane spacing, the nominal uniform vane spacing being defined by a total number of the plurality of stator vanes.

2. The circumferential row of vanes of claim 1 , wherein the first spacing is uniform between the plurality of stator vanes in the first group of stator vanes and is based on the second spacing.

3. The circumferential row of vanes of claim 1 , wherein the plurality of stator vanes comprises only the first group of stator vanes and the second group of stator vanes.

4. The circumferential row of vanes of claim 1 , wherein a number of stator vanes in the first group of stator vanes is equal to the total number of the plurality of stator vanes minus the number of stator vanes in the second group of stator vanes.

5. The circumferential row of vanes of claim 1 , wherein a number of stator vanes in the second group of stator vanes is from twenty percent to forty percent of the total number of the plurality of stator vanes.

6. The circumferential row of vanes of claim 5 , wherein the number of stator vanes in the second group of stator vanes is about one-third of the total number of the plurality of stator vanes.

7. The circumferential row of vanes of claim 1 , wherein the second spacing is from two percent to eleven percent lesser than the nominal uniform vane spacing.

8. The circumferential row of vanes of claim 7 , wherein the second spacing is from four percent to six percent lesser than the nominal uniform vane spacing.

9. The circumferential row of vanes of claim 8 , wherein the second spacing is 4.3 percent lesser than the nominal uniform vane spacing.

10. The circumferential row of vanes of claim 1 , wherein the second spacing is from two percent to eleven percent greater than the nominal uniform vane spacing.

11. The circumferential row of vanes of claim 10 , wherein the second spacing is from four percent to six percent greater than the nominal uniform vane spacing.

12. The circumferential row of vanes of claim 11 , wherein the second spacing is 5.2 percent greater than the nominal uniform vane spacing.

13. The circumferential row of vanes of claim 1 , wherein the plurality of stator vanes provide a harmonic response defined by the total number of the plurality of stator vanes, the first spacing, and the second spacing.

14. The circumferential row of vanes of claim 13 , wherein the second spacing is selected to bias the harmonic response to one or more harmonics above or below a uniform main driving harmonic defined by a uniformly spaced circumferential row of vanes.

15. The circumferential row of vanes of claim 13 , wherein the harmonic response is biased to one or more harmonics above a uniform main driving harmonic defined by a uniformly spaced circumferential row of vanes.

16. The circumferential row of vanes of claim 15 , wherein the harmonic response is biased above the uniform main driving harmonic due to the second spacing being from two percent to eleven percent lesser than the nominal uniform vane spacing.

17. The circumferential row of vanes of claim 15 , wherein the harmonic response includes a main driving harmonic that occurs at the uniform main driving harmonic, a first harmonic one lower than the main driving harmonic, and the one or more harmonics, and wherein an amplitude of the harmonics below the first harmonic are less than an amplitude of at least one of the one or more harmonics.

18. The circumferential row of vanes of claim 13 , wherein the harmonic response is biased to one or more harmonics below a uniform main driving harmonic defined by a uniformly spaced circumferential row of vanes.

19. The circumferential row of vanes of claim 18 , wherein the harmonic response is biased below the uniform main driving harmonic due to the second spacing being from two percent to eleven percent greater than the nominal uniform vane spacing.

20. The circumferential row of vanes of claim 18 , wherein the harmonic response includes a main driving harmonic that occurs at the uniform main driving harmonic, a first harmonic one higher than the main driving harmonic, and the one or more harmonics, and wherein an amplitude of the harmonics above the first harmonic are less than an amplitude of at least one of the one or more harmonics.

Assignees

• Gen Electric

Inventors

• Phillips Julia Elizabeth
• Chapman Brandon

Classifications

• F05D2220/32

  in gas turbines · CPC title

• F05D2250/37

  circumferential · CPC title

• F01D9/041 Primary

  using blades (F01D5/148 takes precedence) · CPC title