System and method for in situ cleaning of internal components of a gas turbine engine and a related plug assembly

Patent metadata

Field	Value
Publication number	US-9951647-B2
Application number	US-201514972169-A
Country	US
Kind code	B2
Filing date	Dec 17, 2015
Priority date	Dec 17, 2015
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A system for in situ cleaning of internal components of a gas turbine engine may generally include a plug assembly defining a fluid passageway that is configured to be installed within an access port of the engine such that the fluid passageway defines a flow path between inner and outer casings of the engine. The plug assembly may include an inner sleeve at least partially defining the fluid passageway and an outer sleeve configured to receive a portion of the inner sleeve. The system may also include a fluid conduit configured to be coupled between a fluid source positioned external to the gas turbine engine and an inlet end of the plug assembly for supplying a cleaning fluid to the plug assembly. The cleaning fluid may be directed through the fluid passageway and may then be expelled from the plug assembly into the interior of the gas turbine engine.

First claim

What is claimed is:

1. A system for in situ cleaning of internal components of a gas turbine engine, the gas turbine engine including an outer casing and an inner casing, the system comprising:
a plug assembly defining a fluid passageway extending lengthwise between an inlet end and an outlet end, the plug assembly configured to be installed within an access port of the gas turbine engine such that the fluid passageway defines a flow path between the inner and outer casings for supplying a cleaning fluid within an interior of the gas turbine engine, the plug assembly including an inner sleeve at least partially defining the fluid passageway and an outer sleeve configured to receive a portion of the inner sleeve, the inner sleeve configured to be coupled to the inner casing and the outer sleeve configured to be coupled to the outer casing; and
a fluid conduit configured to be coupled between a fluid source positioned external to the gas turbine engine and the inlet end of the plug assembly for supplying the cleaning fluid to the plug assembly,
wherein the cleaning fluid supplied from the fluid conduit is directed through the fluid passageway from the inlet end to the outlet end and is expelled from the plug assembly into the interior of the gas turbine engine.

2. The system of claim 1 , wherein the outer sleeve defines an outer threaded area around an outer perimeter of the outer sleeve, the outer threaded area configured to engage a corresponding threaded portion of the access port defined through the outer casing.

3. The system of claim 1 , wherein the inner sleeve defines an inner threaded area around an outer perimeter of the inner sleeve, the inner threaded area configured to engage a corresponding threaded portion of the access port defined through the inner casing.

4. The system of claim 1 , wherein the inner sleeve is configured to move relative to the outer sleeve with variations in a radial distance defined between the inner and outer casings.

5. The system of claim 4 , wherein a biasing member is coupled between the inner and outer sleeves to allow the inner sleeve to move relative to the outer sleeve with variations in the radial distance.

6. The system of claim 1 , wherein a threaded end portion of the outer sleeve defines the inlet end of the plug assembly, the fluid conduit being configured to be coupled to the threaded end portion.

7. The system of claim 1 , wherein the system further comprises a removable cap configured to be coupled to the outer sleeve at the inlet end of the plug assembly.

8. The system of claim 7 , wherein the removable cap includes a cap portion configured to be coupled to the outer sleeve and a plug portion extending outwardly from the cap portion, the plug portion configured to extend lengthwise within the fluid passageway between the inlet and outlet ends of the plug assembly when the cap portion is coupled to the outer sleeve.

9. A gas turbine engine, comprising:
an outer casing, the outer casing defining an outer portion of an access port of the gas turbine engine;
an inner casing spaced radially inwardly from the outer casing by a radial distance, the inner casing defining an inner portion of the access port;
a plug assembly defining a fluid passageway extending lengthwise between an inlet end and an outlet end, the plug assembly being installed within the inner and outer portions of the access port such that the fluid passageway defines a flow path between the inner and outer casings for supplying a cleaning fluid within an interior of the gas turbine engine, the plug assembly including an inner sleeve at least partially defining the fluid passageway and an outer sleeve configured to receive a portion of the inner sleeve, the inner sleeve being coupled to the inner casing and the outer sleeve being coupled to the outer casing; and
a cap configured to be removably coupled to the outer sleeve at the outlet end of the plug assembly, the cap being configured to prevent fluid flow through the fluid passageway when the cap is installed onto the plug assembly.

10. The gas turbine engine of claim 9 , wherein the outer sleeve defines an outer threaded area around an outer perimeter of the outer sleeve, the outer threaded area configured to engage a corresponding threaded area of the outer portion of the access port defined by the outer casing.

11. The gas turbine engine of claim 9 , wherein the inner sleeve defines an inner threaded area around an outer perimeter of the inner sleeve, the inner threaded area configured to engage a corresponding threaded area of the inner portion of the access port defined by the inner casing.

12. The gas turbine of claim 9 , wherein the inner sleeve is configured to move relative to the outer sleeve with variations in the radial distance defined between the inner and outer casings.

13. The gas turbine engine of claim 12 , wherein a biasing member is coupled between the inner and outer sleeves to allow the inner sleeve to move relative to the outer sleeve with variations in the radial distance.

14. The gas turbine engine of claim 9 , wherein the cap includes a cap portion configured to be coupled to the outer sleeve and a plug portion extending outwardly from the cap portion, the plug portion configured to extend lengthwise within the fluid passageway between the inlet and outlet ends of the plug assembly when the cap portion is coupled to the outer sleeve.

15. A method for in situ cleaning of internal components of a gas turbine engine, the gas turbine engine include an inner casing and an outer casing, the method comprising:
accessing a plug assembly installed within an access port defined through the inner and outer casings of the gas turbine engine, the plug assembly defining a fluid passageway extending lengthwise between an inlet end and an outlet end such that the fluid passageway defines a flow path between the inner and outer casings, the plug assembly including an inner sleeve at least partially defining the fluid passageway and an outer sleeve configured to receive a portion of the inner sleeve;
coupling a fluid conduit between a fluid source positioned external to the gas turbine engine and an inlet end of the plug assembly; and
supplying a cleaning fluid from the fluid source through the fluid conduit to the plug assembly such that the cleaning fluid is directed through the fluid passageway defined by the plug assembly and is expelled from an outlet end of the plug assembly into an interior of the gas turbine engine.

16. The method of claim 15 , further comprising installing the plug assembly within the access port defined through the inner and outer casings of the gas turbine engine.

17. The method of claim 16 , wherein installing the plug assembly within the access port comprises:
coupling the outer sleeve of the plug assembly to the outer casing at an outer portion of the access port defined through the outer casing; and
coupling the inner sleeve of the plug assembly to the inner casing at an inner portion of the access port defined through the inner casing.

18. The method of claim 15 , further comprising removing a cap from the plug assembly prior to coupling the fluid conduit to the inlet end of the plug assembly, the cap including a cap portion configured to be coupled to the outer sleeve and a plug portion extending outwardly from the cap portion.

19. The method of claim 18 , further comprising reinstalling the cap relative to the plug assembly after the cleaning fluid has been supplied through the plug assembly such that the cap portion is coupled to t

Assignees

• Gen Electric

Inventors

• Rawson Lloyd Eric

Classifications

• F01D25/26

  Double casings; Measures against temperature strain in casings · CPC title

• F05D2230/60

  Assembly methods · CPC title

• F01D25/002 Primary

  Cleaning of turbomachines · CPC title

• B08B9/0321

  using pressurised, pulsating or purging fluid (E04F17/126 takes precedence) · CPC title

• F05D2220/32

  in gas turbines · CPC title