System and method for cleaning a gas turbine engine and related wash stand

Patent metadata

Field	Value
Publication number	US-12228041-B2
Application number	US-202217886384-A
Country	US
Kind code	B2
Filing date	Aug 11, 2022
Priority date	Jan 20, 2016
Publication date	Feb 18, 2025
Grant date	Feb 18, 2025

Abstract

A system for cleaning a gas turbine engine may generally include a wash stand having a base frame and a plurality of fluid injection nozzles configured to be supported by the base frame relative to the gas turbine engine. The nozzles may be configured to inject a cleaning fluid through an inlet of the fan casing of the engine as the fan blades are being rotated in a rotational direction such that the cleaning fluid is directed past the rotating fan blades and into a compressor inlet of the engine. Additionally, each nozzle may be oriented at a positive tangential angle defined relative to the rotational direction of the plurality of fan blades. The system may also include a fluid source in flow communication with the wash stand for supplying the cleaning fluid to the plurality of fluid injection nozzles.

First claim

What is claimed is:

1. A cleaning system for a gas turbine engine comprising:
a washer including a first set of nozzles locatable adjacent to a gas turbine engine, the first set of nozzles arranged about a centerline;
a cleaning fluid in fluid communication with the first set of nozzles for discharge into a gas turbine engine as a plurality of fan blades rotate in a rotational direction relative to the centerline, the cleaning fluid being supplied at a pressure; and
each nozzle of the first set of nozzles being upstream of the plurality of fan blades of the gas turbine engine and oriented at a first positive tangential angle defined relative to a rotational direction of the plurality of fan blades, the first positive tangential angle having a first axial component along the centerline and a first rotational component relative to a rotational direction of a plurality of fan blades, the first positive tangential angle and/or the pressure being determined from a rotational speed of the plurality of fan blades during cleaning such that at least a majority of the cleaning fluid passes through the plurality of fan blades unbated by the plurality of fan blades into a compressor inlet of the gas turbine engine while the plurality of fan blades are rotating.

2. The cleaning system of claim 1 wherein the first positive tangential angle ranges from greater than zero degrees to 60 degrees.

3. The cleaning system of claim 1 wherein each nozzle of the first set of nozzles is oriented radially inwardly relative to the centerline.

4. The cleaning system of claim 1 wherein the cleaning fluid is in fluid communication with the first set of nozzles at a pressure ranging from 60 psi to 900 psi.

5. The cleaning system of claim 1 wherein the washer further comprises a base frame and the first set of nozzles being coupled to the base frame to form an annular array about the centerline.

6. The cleaning system of claim 5 wherein the first set of nozzles is coupled to the base frame via a ring-shaped nozzle manifold.

7. The cleaning system of claim 1 wherein the first positive tangential angle of at least one of the nozzles of the first set of nozzles is adjustable.

8. The cleaning system of claim 1 wherein the first positive tangential angle of at least one of the nozzles of the first set of nozzles is adjustable based on the rotational speed of a gas turbine engine.

9. The cleaning system of claim 1 wherein the washer is moveable to align the centerline with a rotational axis of a gas turbine engine.

10. The cleaning system of claim 1 wherein the cleaning fluid is heated.

11. The cleaning system of claim 1 wherein the cleaning fluid is supplied from a mobile source.

12. The cleaning system of claim 1 comprising a second set of nozzles being interchangeable with the first set of nozzles, each nozzle of the second set of nozzles having a second positive tangential angle defined relative to a rotational direction of a plurality of fan blades being different than the first tangential angle of the first set nozzles, the second positive tangential angle having a second axial component along the centerline and a second rotational component relative to a rotational direction of a plurality of fan blades.

13. A cleaning system for a gas turbine engine comprising:
a washer including a plurality of nozzles locatable adjacent to a gas turbine engine, the plurality of nozzles arranged about a centerline;
a cleaning fluid in fluid communication with the plurality of nozzles for discharge into a gas turbine engine as a plurality of fan blades rotate in a rotational direction relative to the centerline; and
each nozzle being upstream of the plurality of fan blades of the gas turbine engine and oriented at a positive tangential angle defined relative to a rotational direction of a plurality of fan blades, at least one of a tangential orientation or a radial orientation of at least one of the plurality of nozzles being adjustable relative to the centerline, the positive tangential angle being determined from a rotational speed of the plurality of fan blades during cleaning such that at least a majority of the cleaning fluid passes through the plurality of fan blades unbated by the plurality of fan blades into a compressor inlet of the gas turbine engine while the plurality of fan blades are rotating.

14. The cleaning system of claim 13 wherein at least one of the tangential orientation or the radial orientation of at least one of the plurality of nozzles being adjustable relative to the centerline based on a speed of rotation of a plurality of fan blades.

15. The cleaning system of claim 13 wherein at least one of the tangential orientation or the radial orientation of at least one of the plurality of nozzles being adjustable relative to the centerline while cleaning fluid is being discharged from the plurality of nozzles.

16. The cleaning system of claim 13 wherein at least one of the tangential orientation or the radial orientation of at least two of the plurality of nozzles being different.

17. The cleaning system of claim 13 wherein the positive tangential angle ranges from greater than zero degrees to 60 degrees.

18. The cleaning system of claim 13 wherein each nozzle of the plurality of nozzles is oriented radially inwardly relative to the centerline.

19. The cleaning system of claim 13 wherein the cleaning fluid is in fluid communication with the plurality of nozzles at a pressure ranging from 60 psi to 900 psi.

Assignees

• Gen Electric

Inventors

• Rawson Lloyd Eric
• Wallace Thomas Tracy

Classifications

• F04D29/38

  Blades {(for axial flow compressors F04D29/324)} · CPC title

• B08B5/02

  Cleaning by the force of jets, e.g. blowing-out cavities {(airguns or nozzles per se B05B1/005)} · CPC title

• B08B3/10

  with additional treatment of the liquid or of the object being cleaned, e.g. by heat, by electricity or by vibration · CPC title

• B08B3/003

  Cleaning involving contact with foam · CPC title

• B08B3/02

  Cleaning by the force of jets or sprays · CPC title