Bleed valve assembly with valve shims for varying bleed flow in gas turbine engine compressors and method for operating

Patent metadata

Field	Value
Publication number	US-12264685-B1
Application number	US-202418640404-A
Country	US
Kind code	B1
Filing date	Apr 19, 2024
Priority date	Apr 19, 2024
Publication date	Apr 1, 2025
Grant date	Apr 1, 2025

Abstract

A bleed valve assembly includes a manifold coupled to a case of a compressor of a gas turbine engine to control a flow of bleed air exiting the compressor, a valve housing coupled with the manifold, a piston configured to move selectively relative to the valve housing and the manifold, and one or more shims located between the valve housing and the piston.

First claim

What is claimed is:

1. A method for operating a bleed valve assembly for a gas turbine engine, the method comprising
providing a bleed valve assembly including a manifold coupled to a case of a compressor of the gas turbine engine to control a flow of bleed air, a valve housing coupled with the manifold, and a piston received in the valve housing, wherein the manifold includes an outer surface defining an air passageway formed in the manifold for the bleed air to exit the compressor through the manifold, the air passageway defining a central axis of the bleed valve assembly,
locating one or more shims between an upper surface of the piston and an inner surface of the valve housing,
moving the piston to an open position in which the upper surface of the piston engages the one or more shims and a bottom surface of the piston is spaced a first axial distance apart from the outer surface of the manifold so that the bleed air exiting the compressor exits the compressor at a first predetermined rate,
removing at least one shim of the one or more shims from between the upper surface of the piston and the inner surface of the valve housing, and
moving the piston to the open position in which the upper surface of the piston engages the one or more shims and the bottom surface of the piston is spaced a second axial distance apart from the outer surface of the manifold so that the bleed air exiting the compressor exits the compressor at a second predetermined rate, the second axial distance being greater than the first axial distance and the second predetermined rate being greater than the first predetermined rate.

2. The method of claim 1 , further comprising removing the one or more shims from between the upper surface of the piston and the inner surface of the valve housing and moving the piston to the open position in which the upper surface of the piston engages the inner surface of the valve housing and the bottom surface of the piston is spaced a third axial distance apart from the outer surface of the manifold so that the bleed air exiting the compressor exits the compressor at a third predetermined rate, the third axial distance being greater than the first and second axial distances and the third predetermined rate being greater than the first and second predetermined rates.

3. The method of claim 2 , further comprising changing the bleed valve assembly between a reduced flow configuration in which the bottom surface of the piston is spaced the first axial distance from the outer surface of the manifold when the piston is moved to the open position, a maximum flow configuration in which the bottom surface of the piston is spaced the third axial distance from the outer surface of the manifold when the piston is moved to the open position, and at least one intermediate-flow configuration in which the piston is spaced an axial distance between the first axial distance and the third axial distance from the outer surface of the manifold when the piston is moved to the open position.

4. The bleed valve assembly of claim 2 , wherein the third axial distance is about or equal to the axial distance between the bottom surface of the valve housing that outer surface of the manifold.

5. The method of claim 1 , wherein the first axial distance less than the axial distance between a bottom surface of the valve housing and the outer surface of the manifold.

6. The bleed valve assembly of claim 1 , wherein an axial height of a first shim of the one or more shims is equal to an axial height of a second shim of the one or more shims.

7. A bleed valve assembly for a gas turbine engine, the bleed valve assembly comprising
a manifold coupled to a case of a compressor of the gas turbine engine to control a flow of bleed air exiting the compressor, the manifold having an outer surface defining an air passageway formed in the manifold for the bleed air to exit the compressor through the manifold, wherein the air passageway defines a central axis of the bleed valve assembly,
a valve housing coupled with the manifold and configured to receive pressurized air, and
a piston received in the valve housing and configured to move selectively relative to the valve housing and the manifold in response to the valve housing receiving the pressurized air to close the air passageway of the manifold, wherein the piston is movable between an open position in which a bottom surface of the piston is spaced apart from the manifold to open the air passageway and a closed position in which the piston closes the air passageway,
wherein the bleed valve assembly is changeable, via addition or removal of one or more shims, between a reduced-flow configuration in which an upper surface of the piston engages the one or more shims located between the upper surface of the piston and an inner surface of the valve housing and the bottom surface of the piston is spaced a first axial distance from the outer surface of the manifold when the piston is in the open position so that the bleed air passes through the bleed valve assembly at a first predetermined rate, and a maximum-flow configuration in which the upper surface of the piston engages the inner surface of the valve housing and the bottom surface of the piston is spaced a second axial distance from the outer surface of the manifold so that the bleed air passes through the bleed valve assembly at a second predetermined rate, wherein the second axial distance is greater than the first axial distance and the second predetermined rate is greater than the first predetermined rate.

8. The bleed valve assembly of claim 7 , wherein the bleed valve assembly is further changeable between the reduced-flow configuration, the maximum-flow configuration, and at least one intermediate-flow configuration in which an upper surface of the piston engages one or more shims located between the upper surface of the piston and an inner surface of the valve housing and the bottom surface of the piston is spaced a third axial distance from the outer surface of the manifold so that the bleed air passes through the bleed valve assembly at a third predetermined rate, wherein the third axial distance is greater than the first axial distance and less than the second axial distance, and the third predetermined rate is greater than the first predetermined rate and less than the second predetermined rate.

Assignees

• Rolls Royce Nam Tech Inc
• Rolls Royce Corp

Inventors

• Lighty Kerry J
• Acker Jonathan P
• Kremer Douglas J
• Mazur Steven
• Whitlock Mark E

Classifications

• F04D27/023

  Details or means for fluid extraction · CPC title

• F04D27/0215 Primary

  Arrangements therefor, e.g. bleed or by-pass valves · CPC title