Bleed valve resonance augmentations

Patent metadata

Field	Value
Publication number	US-9879611-B2
Application number	US-201514754298-A
Country	US
Kind code	B2
Filing date	Jun 29, 2015
Priority date	Jul 22, 2014
Publication date	Jan 30, 2018
Grant date	Jan 30, 2018

Abstract

Bleed valve assemblies in a gas turbine engine are disclosed herein. A bleed valve assembly in a low pressure compressor may include a bleed valve and a resonator chamber. A manifold may allow passage of air from a bleed duct into the resonator chamber. The resonator chamber may alter resonation properties of the bleed duct in order to prevent damage to components in the low pressure compressor.

First claim

The invention claimed is:

1. A bleed valve assembly comprising:
a bleed valve including an axial span bounding an aperture;
a manifold located at least partially within the aperture;
a chamber body assembly coupled to the manifold, wherein the manifold comprises a passage configured to fluidly connect the chamber body assembly to a bleed duct, wherein the chamber body assembly comprises a forward chamber and an aft chamber, wherein a depth of the forward chamber is less than a depth of the aft chamber;
a resonator cover coupled to the chamber body assembly; and
an actuator configured to open and close the bleed valve.

2. The bleed valve assembly of claim 1 , wherein the chamber body assembly comprises a chamber body and a chamber flange.

3. The bleed valve assembly of claim 2 , wherein the chamber flange comprises one or more female threads located within the chamber body.

4. The bleed valve assembly of claim 2 , wherein the chamber flange comprises an alignment peg.

5. A low pressure compressor (“LPC”) case comprising:
a first bleed duct; and
a first bleed valve assembly configured to seal the first bleed duct, the first bleed valve assembly comprising a first resonator chamber and an actuator configured to open and close the bleed valve assembly,
wherein the first resonator chamber comprises a forward chamber and an aft chamber, wherein a depth of the forward chamber is less than a depth of the aft chamber,
wherein the first bleed valve assembly comprises a manifold, the manifold comprising a passage fluidly connecting the first resonator chamber to the bleed duct.

6. The LPC case of claim 5 , further comprising a second bleed duct and a second bleed valve assembly configured to seal the second bleed duct, the second bleed valve assembly comprising a second resonator chamber.

7. The LPC case of claim 6 , wherein a height of the first resonator chamber is greater than a height of the second resonator chamber.

8. The LPC case of claim 7 , wherein a volume of the first resonator chamber is equal to a volume of the second resonator chamber.

9. The LPC case of claim 5 , wherein the first bleed valve assembly comprises a bleed valve, a manifold, a chamber body assembly, and a resonator cover.

10. A gas turbine engine comprising:
a low pressure compressor;
a bleed duct configured to release bleed air from the low pressure compressor;
a first bleed valve assembly configured to seal the bleed duct;
an actuator configured to open and close the first bleed valve assembly; and
a resonator chamber in fluid communication with the bleed duct via a passage in a manifold of the first bleed valve assembly,
wherein the resonator chamber comprises a forward chamber and an aft chamber, wherein a depth of the forward chamber is less than a depth of the aft chamber.

11. The gas turbine engine of claim 10 , further comprising a second bleed valve assembly.

12. The gas turbine engine of claim 11 , wherein a volume of the first bleed valve assembly is equal to a volume of the second bleed valve assembly.

13. The gas turbine engine of claim 12 , wherein a height of the first bleed valve assembly is greater than a height of the second bleed valve assembly.

Assignees

• United Technologies Corp

Inventors

• Morin Bruce L
• Topol David A
• Boyer Mark
• Desfosses Brian
• Quin W Marshall
• Holchin John
• Little Jonathan D
• Roseberry Bryan

Classifications

• F04D27/0215

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

• F02C3/13

  having variable working fluid interconnections between turbines or compressors or stages of different rotors {(controlling flow ratio between different flows of multi-flow jet-propulsion plant, e.g. ducted fan F02K3/075)} · CPC title

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• F02C9/18 Primary

  by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages {(F02C3/113 takes precedence)} · CPC title

• F04D29/665

  by means of resonance chambers or interference · CPC title