# US 11,306,609 B2 · Retractable washing device

> Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt

- Number: US 11,306,609 B2
- Document ID: US11306609B2
- Status: Granted
- Kind: B2
- Application number: 16/577,540
- Filed: 2019-09-20
- Published: 2021-03-25
- Granted: 2022-04-19
- Earliest claimed: 2019-09-20
- Assignees: Pratt & Whitney Canada Corp.
- Applicants: Pratt & Whitney Canada Corp.
- Inventors: Richard Ivakitch
- Web page: https://patentgrep.com/patent/US11306609B2

## CPC

- F01D 25/002: {Cleaning of turbomachines}
- B08B 3/02: Cleaning by the force of jets or sprays
- B08B 3/08: the liquid having chemical or dissolving effect
- B08B 9/00: Cleaning hollow articles by methods or apparatus specially adapted thereto
- F02C 7/30: Preventing corrosion {or unwanted deposits} in gas-swept spaces
- F05D 2220/32: in gas turbines
- F05D 2230/72: Maintenance
- F05D 2260/95: Preventing corrosion
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- B08B: CLEANING IN GENERAL; PREVENTION OF FOULING IN GENERAL
- F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00)
- F05D: INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS

## Abstract

A gas turbine engine having an engine core defining a core flow path delimited by an engine casing, a washing device having a spraying member defining a conduit in fluid communication with a source of washing fluid, the spraying member having a spraying section for outputting the washing fluid from the conduit, the spraying member movable relative to the engine casing from a retracted position in which the spraying section is flush with a surface of the engine casing defining said core flow path, and an expanded position in which the spraying section protrudes beyond the surface of the engine casing into the core flow path

## Claims

### Claim 1

A gas turbine engine comprising an engine core defining a core flow path delimited by an engine casing extending annularly around a central axis, a washing device having a spraying member defining a conduit in fluid communication with a source of washing fluid, the spraying member having a spraying section for outputting the washing fluid from the conduit, the spraying member movable relative to the engine casing along a direction having a radial component relative to the central axis from a retracted position in which the spraying section is flush with a surface of the engine casing defining said core flow path, and an expanded position in which the spraying section protrudes beyond the surface of the engine casing into the core flow path.

### Claim 2 (depends on 1)

The gas turbine engine of claim 1, wherein the spraying member is slidably received within a housing, the housing secured to the engine casing and defining a cavity fluidly connected to the source of washing fluid and to the conduit of the spraying member.

### Claim 3 (depends on 2)

The gas turbine engine of claim 2, wherein a biasing member is in engagement with the spraying member and the housing and exerts a biasing force on the spraying member such that the spraying member is biased in the retracted position when the washing device is not in operation, the biasing force less than a fluid force exerted on the spraying member by a pressure of the washing fluid when the washing device is in operation.

### Claim 4 (depends on 1)

The gas turbine engine of claim 1, wherein the engine casing defines an aperture for receiving the spraying member, a size of the aperture corresponding to that of the spraying member.

### Claim 5 (depends on 2)

The gas turbine engine of claim 2, wherein the engine casing defines an aperture, a size of the aperture corresponding to that of the housing, the housing being flush with the engine casing, the spraying section contained within the cavity when the spraying member is in the retracted position.

### Claim 6 (depends on 1)

The gas turbine engine of claim 1, wherein the spraying section defines at least one spraying aperture for outputting the washing fluid, the at least one spraying aperture oriented in a downstream direction relative to air circulating in the core flow path.

### Claim 7 (depends on 2)

The gas turbine engine of claim 2, further comprising an anti-rotation feature between the housing and the spraying member for maintaining a relative circumferential position of the spraying member relative to the housing at least when the spraying member is in the expanded position.

### Claim 8 (depends on 7)

The gas turbine engine of claim 7, wherein the anti-rotation feature includes at least one tab defined by one of the housing and the spraying member and at least one slot defined by the other of the housing and the spraying member, the at least one slot slidably receiving the at least one tab.

### Claim 9 (depends on 1)

The gas turbine engine of claim 1, including a compressor section having a low-pressure compressor and a high-pressure compressor, the washing device located between the low-pressure compressor and a high-pressure compressor.

### Claim 10 (depends on 1)

The gas turbine engine of claim 1, wherein the washing device is removably securable to the engine casing.

### Claim 11 (depends on 2)

The gas turbine engine of claim 2, wherein the washing device includes a quick connect fitting secured to the housing for selectively connecting the washing device to the source of washing fluid.

### Claim 12 (depends on 2)

The gas turbine engine of claim 2, further comprising a sleeve located within the housing and surrounding the spraying member, the spraying member in a sliding engagement with the sleeve.

### Claim 13

A washing device for a gas turbine engine, comprising: a housing securable to a casing of the gas turbine engine and defining a cavity fluidly connectable to a source of washing fluid; a spraying member slidably received within the cavity of the housing and defining a conduit in fluid communication with the cavity for receiving the washing fluid, the spraying member having a spraying section for outputting the washing fluid from the conduit, the spraying member movable from a retracted position in which the spraying section is entirely contained within the cavity and an expanded position in which the spraying section protrudes outside the cavity; and a biasing member in engagement with both of the housing and the spraying member, the biasing member exerting a biasing force on the spraying member such that the spraying member is biased in the retracted position when the washing device is not in operation, the biasing force less than a fluid force exerted on the spraying member by a pressure of the washing fluid when the washing device is in operation.

### Claim 14 (depends on 13)

The washing device of claim 13, wherein an end of the spraying section is axially aligned with an end of the housing in the retracted position.

### Claim 15 (depends on 13)

The washing device of claim 13, wherein the biasing member is a spring disposed within the cavity and around the spraying member.

### Claim 16 (depends on 13)

The washing device of claim 13, wherein the spraying section defines at least one spraying aperture for outputting the washing fluid in a direction being at least partially radial relative to an axis of the washing device.

### Claim 17 (depends on 13)

The washing device of claim 13, further comprising an anti-rotation feature between the housing and the spraying member for maintaining a relative circumferential position of the spraying member relative to the housing at least when the spraying member is in the expanded position.

### Claim 18 (depends on 13)

The washing device of claim 13, wherein the washing device includes a quick connect fitting secured to the housing for selectively connecting the washing device to the source of washing fluid.

### Claim 19 (depends on 13)

The washing device of claim 13, further comprising a sleeve located within the housing and surrounding the spraying member, the spraying member in a sliding engagement with the sleeve.