Vibration damping system for turbine blade or nozzle, retention system therefor, and method of assembly

Patent metadata

Field	Value
Publication number	US-11519276-B1
Application number	US-202217574092-A
Country	US
Kind code	B1
Filing date	Jan 12, 2022
Priority date	Jan 12, 2022
Publication date	Dec 6, 2022
Grant date	Dec 6, 2022

Abstract

A vibration damping element for a vibration damping system for a turbine nozzle or blade includes an elongated body and a wire mesh member that surrounds the elongated body. The wire mesh member has a first outer dimension in an inoperative state and a second, larger outer dimension in an operative state. In the operative state, the wire mesh member frictionally engages with an inner surface of a body opening in the turbine nozzle or blade to damp vibration. In the inoperative state, the wire mesh member slides freely in the body opening in the turbine nozzle or blade. A retention system includes a retention member on the elongated body that fixes the wire mesh member relative to a length of the elongated body in the operative state in the body opening of the turbine nozzle or blade.

First claim

What is claimed is:

1. A vibration damping element for a vibration damping system for a turbine nozzle or blade, comprising:
an elongated body;
a wire mesh member surrounding the elongated body and having a first outer dimension in an inoperative state and a second, larger outer dimension in an operative state, wherein in the operative state, the wire mesh member frictionally engages with an inner surface of a body opening in the turbine nozzle or blade to damp vibration, and in the inoperative state, the wire mesh member slides freely in the body opening in the turbine nozzle or blade; and
a retention member on the elongated body to fix a first section of the wire mesh member relative to a length of the elongated body in the operative state in the body opening of the turbine nozzle or blade.

2. The vibration damping element of claim 1 , wherein the retention member includes a protrusion on a first portion of an outer surface of the elongated body, the protrusion engaging within an inner dimension of a mesh opening in the first section of the wire mesh member to create the second, larger outer dimension on the wire mesh member in the operative state.

3. The vibration damping element of claim 2 , wherein the elongated body includes a second portion on the outer surface thereof, wherein the mesh opening in a second section of the wire mesh member different than the first section slides freely relative to the second portion.

4. The vibration damping element of claim 1 , wherein the retention member includes a threaded section on a first portion of an outer surface of the elongated body, the threaded section having an outer dimension larger than an inner dimension of a mesh opening in the first section of the wire mesh member to create the second, larger outer dimension on the wire mesh member in the operative state.

5. The vibration damping element of claim 4 , wherein the retention member includes a non-threaded section on a second portion on the outer surface of the elongated body, wherein the inner dimension of the mesh opening in a second section of the wire mesh member different than the first section slides freely relative to the second portion.

6. A vibration damping system for a turbine nozzle or blade, comprising:
a body opening extending through a body of the turbine nozzle or blade between a tip end and a base end thereof; and
a vibration damping element disposed in the body opening, the vibration damping element including:
an elongated body having a first, free end and a second end fixed relative to one of the base end and the tip end;
a wire mesh member surrounding the elongated body and having a first outer dimension in an inoperative state and a second, larger outer dimension in an operative state, wherein in the operative state, the wire mesh member frictionally engages with an inner surface of the body opening in the turbine nozzle or blade to damp vibration and in the inoperative state, the wire mesh member slides freely in the body opening in the turbine nozzle or blade; and
a retention member on the elongated body configured to fix a first section of the wire mesh member relative to a length of the elongated body in the operative state in the body opening of the turbine nozzle or blade.

7. The vibration damping system of claim 6 , wherein the retention member includes a protrusion on a first portion of an outer surface of the elongated body, the protrusion engaging with an inner dimension of a mesh opening in the first section of the wire mesh member to create the second, larger outer dimension on the wire mesh member in the operative state.

8. The vibration damping system of claim 7 , wherein the retention member includes a second portion on the outer surface of the elongated body, wherein the inner dimension of the mesh opening in a second section of the wire mesh member different than the first section slides freely relative to the second portion.

9. The vibration damping system of claim 6 , wherein the retention member includes a threaded section on a first portion of an outer surface of the elongated body, the threaded section having an outer dimension larger than an inner dimension of the first section of the wire mesh member to create the second, larger outer dimension on the wire mesh member in the operative state.

10. The vibration damping system of claim 9 , wherein the elongated body includes a non-threaded section on a second portion on the outer surface of the elongated body, wherein the inner dimension of the mesh opening in a second section of the wire mesh member different than the first section slides freely relative to the second portion.

11. The vibration damping system of claim 6 , wherein the second end of the elongated body is fixed relative to the tip end of the body, and the first, free end extends towards the base end.

12. The vibration damping system of claim 6 , wherein the second end of the elongated body is fixed relative to the base end of the body of the turbine nozzle or blade, and the first, free end extends towards the tip end.

13. The vibration damping system of claim 6 , wherein the wire mesh member includes a plurality of wire mesh members spaced along the elongated body, each wire mesh member engaging with a different portion of the inner surface of the body opening.

14. A method of assembling a vibration damping system in a turbine nozzle or blade, the method comprising:
positioning a wire mesh member in a body opening extending through a body of the turbine nozzle or blade between a tip end and a base end thereof, the wire mesh member having a mesh opening therein having an inner dimension and a first outer dimension that slides freely in the body opening in the turbine nozzle or blade in an inoperative state;
positioning an elongated body in the body opening and within the mesh opening of the wire mesh member, wherein a retention member on the elongated body fixes a first section of the wire mesh member relative to a length of the elongated body in an operative state in the body opening of the turbine nozzle or blade by creating a second, larger outer dimension in the wire mesh member that frictionally engages with an inner surface of the body opening in the turbine nozzle or blade; and
fixing the elongated body relative to one of the base end and the tip end such that the elongated body has a first, free end and a second end fixed relative to the one of the base end and the tip end.

15. The method of claim 14 , wherein the retention member includes a protrusion on a first portion of an outer surface of the elongated body, and the positioning of the elongated body includes engaging the protrusion within the inner dimension of the mesh opening in the first section of the wire mesh member to create the second, larger outer dimension on the wire mesh member.

16. The method of claim 15 , wherein the retention member includes a second portion on the outer surface of the elongated body, wherein the inner dimension of the mesh opening in a second section of the wire mesh member different than the first section slides freely relative to the second portion.

17. The method of claim 14 , wherein the retention member includes a threaded section on a first portion of an outer surface of the elongated body, the threaded section having an outer dimension larger than the inner dimension of the mesh opening in the first section of the wire mesh member, and wherein the positioning of the elongated body includes threading the first portion into the mesh opening to create the second, larger outer dimension on the wire mesh member.

Assignees

• Gen Electric

Inventors

• Snider Zachary John
• Delvaux John Mcconnell

Classifications

• F05D2300/614

  Fibres or filaments · CPC title

• F05D2300/613

  Felt · CPC title

• F05D2250/71

  curved · CPC title

• F05D2250/241

  spherical · CPC title

• F05D2250/232

  conical · CPC title