Damper of a gas turbine with a gap

Patent metadata

Field	Value
Publication number	US-10125987-B2
Application number	US-201514958386-A
Country	US
Kind code	B2
Filing date	Dec 3, 2015
Priority date	Dec 3, 2014
Publication date	Nov 13, 2018
Grant date	Nov 13, 2018

Abstract

A damper for a gas turbine combustion chamber as shown in FIG. 1 includes a damper volume wall and a main neck. The damper volume wall defines a damper volume inside the damper volume wall. The main neck includes a main neck wall defining a main neck volume inside the main neck wall. The main neck is associated with the damper volume for fluid communication between the damper volume and the gas turbine combustion chamber. In addition, the damper includes a gap between the main neck wall and the damper volume wall. The main neck defines a main neck axis. For example, the gap is a second neck, and in further embodiments, multiple damper volumes are provided.

First claim

The invention claimed is:

1. A damper for a gas turbine combustion chamber, comprising:
a damper volume wall defining a damper volume inside the damper volume wall;
a main neck, the main neck including a main neck wall defining a main neck volume inside the main neck wall, and the main neck being associated with the damper volume for fluid communication between the damper volume and a combustion chamber, wherein the main neck is mechanically connected to a wall of the combustion chamber; and
a gap between the main neck wall and the damper volume wall, such that the main neck is mechanically disconnected from the damper volume wall by the gap.

2. The damper of claim 1 , wherein comprising:
a second damper volume wall defining a second damper volume arranged outside the main neck wall; and
a second neck for fluid communication between the first damper volume and the second damper volume.

3. The damper of claim 1 , wherein the gap and the main neck are coaxial.

4. The damper of claim 1 , wherein the gap is disposed adjacent to the main neck.

5. The damper of claim 1 , wherein the full circumference of the main neck is surrounded by the gap.

6. The damper of claim 2 , comprising: a purge hole for providing a fluid to the second damper volume.

7. The damper of claim 1 , wherein the gap is partly defined by a flange.

8. A combustion chamber comprising the damper of claim 1 .

9. A gas turbine comprising the damper of claim 1 .

10. A method of operating a gas turbine, the gas turbine having a damper, the damper having a damper volume wall defining a damper volume inside the damper volume wall, and a main neck, the main neck having a main neck wall defining a main neck volume inside the main neck wall, and the main neck being associated with the damper volume for fluid communication between the damper volume and a combustion chamber of the gas turbine, the main neck mechanically connected to a wall of the combustion chamber, the damper including a gap between the main neck wall and the damper volume wall, such that the main neck is mechanically disconnected from the damper volume wall by the gap, the method comprising:
feeding a purging fluid through the gap between the main neck wall and the damper volume wall.

11. The method of claim 10 , comprising: feeding the purging fluid through the main neck from the damper volume into the combustion chamber.

12. The method of claim 10 , wherein the damper additionally includes a second damper volume wall defining a second damper volume arranged outside the main neck wall, and a second neck for fluid communication between the damper volume and the second damper volume, and the method comprises: feeding the purging fluid through a purge hole into the second damper volume.

Assignees

• Ansaldo Energia Switzerland AG

Inventors

• Tonon Devis
• Bothien Mirko Ruben

Classifications

• F23R2900/00014

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• F23M20/005 Primary

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• F16F15/02

  Suppression of vibrations of non-rotating, e.g. reciprocating systems; Suppression of vibrations of rotating systems by use of members not moving with the rotating systems ({F16F15/005 takes precedence } ; layered products B32B; suppression of vibration in ships B63; {relieving load on bearings, using magnetic means F16C39/06}) · CPC title

• F02C7/00 Primary

  Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) · CPC title