Gas turbine fuel pipe comprising a damper

Patent metadata

Field	Value
Publication number	US-10323575-B2
Application number	US-201514975241-A
Country	US
Kind code	B2
Filing date	Dec 18, 2015
Priority date	Dec 19, 2014
Publication date	Jun 18, 2019
Grant date	Jun 18, 2019

Abstract

The invention concerns a gas turbine fuel pipe, having a fuel line, the fuel line having a fuel line volume, a fuel line outer wall and an opening in the fuel line outer wall, a damper having a damper volume and a damper outer wall and attached in fluid communication with the fuel line, wherein the damper covers the opening in the fuel line outer wall, and a perforated lining extending across at least part of the opening in the fuel line outer wall.

First claim

The invention claimed is:

1. A gas turbine fuel pipe, comprising:
a fuel line, the fuel line having a fuel line volume, a fuel line outer wall and an opening in the fuel line outer wall,
a damper having a damper volume and a damper outer wall and attached in fluid communication with the fuel line, wherein the damper covers the opening in the fuel line outer wall,
a perforated lining extending across at least part of the opening in the fuel line outer wall,
a baffle arranged across at least a part of the fuel line within a region of the gas turbine fuel pipe that is adjacent to the damper, and
the gas turbine fuel pipe additionally comprises: an inner fuel line inside the fuel line and the baffle is attached to the inner fuel line.

2. The gas turbine fuel pipe of claim 1 , in which the perforated lining extends all the way across the opening in the fuel line outer wall.

3. The gas turbine fuel pipe of claim 1 , in which a perforated lining extends across part of the opening and an imperforate lining extends across the rest of the opening in the fuel line outer wall.

4. The gas turbine fuel pipe of claim 1 , wherein the baffle is placed perpendicular to the longitudinal axis of the fuel line.

5. The gas turbine fuel pipe of claim 1 , in which the damper extends around the circumference of the fuel line.

6. The gas turbine fuel pipe of claim 1 , in which the gas turbine fuel pipe additionally comprises:
a centre body inside the fuel line, the centre body extending along a longitudinal axis of the fuel line at the point in the fuel line adjacent to the damper.

7. The gas turbine fuel pipe of claim 6 , wherein the centre body is an inner fuel line inside the fuel line.

8. The gas turbine fuel pipe of claim 1 , wherein the gas turbine fuel pipe describes at least one substantially right angle.

9. The gas turbine fuel pipe of claim 8 , wherein the damper is downstream of at least one 90° angle.

10. The gas turbine fuel pipe of claim 9 , wherein the damper is downstream of all the 90° angles.

11. A gas turbine comprising:
the gas turbine fuel pipe of claim 1 .

12. The gas turbine fuel pipe claim 1 , wherein the gas turbine fuel pipe describes at least two substantially right angles.

13. A method of operating a gas turbine, the gas turbine having a fuel line, the fuel line having a fuel line volume, a fuel line outer wall and an opening in the fuel line outer wall, a damper having a damper volume and a damper outer wall and attached in fluid communication with the fuel line, wherein the damper covers the opening in the fuel line outer wall, a perforated lining extending across at least part of the opening in the fuel line outer wall, a baffle arranged across at least a part of the fuel line within a region of the gas turbine fuel pipe that is adjacent to the damper, and the gas turbine fuel pipe additionally comprises: an inner fuel line inside the fuel line and the baffle is attached to the inner fuel line, the method comprising:
feeding fuel along the fuel line, and
damping vibrations and/or pulsations from a combustion chamber and from the fuel line.

Assignees

• Ansaldo Energia Switzerland AG

Inventors

• Wickström Anders Martin Axel
• Tonon Devis
• Bothien Mirko Ruben

Classifications

• F23R2900/00014

  Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators · CPC title

• F23D2210/00

  Noise abatement · CPC title

• F05D2220/32

  in gas turbines · CPC title

• F02C7/222 Primary

  Fuel flow conduits, e.g. manifolds · CPC title

• F23R3/28 Primary

  characterised by the fuel supply (burners F23D) · CPC title