Damper check valve

Patent metadata

Field	Value
Publication number	US-10794283-B2
Application number	US-201715634303-A
Country	US
Kind code	B2
Filing date	Jun 27, 2017
Priority date	Jun 27, 2017
Publication date	Oct 6, 2020
Grant date	Oct 6, 2020

Abstract

A gas turbine engine includes a fan, a compressor, a combustor, a turbine, a bypass duct, and a bearing compartment assembly. The bearing compartment assembly includes a fluid pump, a compartment, a fluid line between the fluid pump and the compartment, and a damper check valve located in the fluid line. The damper check valve is a unitary, monolithic component that is configured to restrict a reverse flow from the compartment to the fluid pump substantially more than the damper check valve restricts a standard flow from the fluid pump to the compartment.

First claim

The invention claimed is:

1. A gas turbine engine comprising:
a fan;
a compressor downstream of the fan;
a combustor downstream of the fan;
a turbine downstream of the fan;
a bypass duct downstream of the fan and radially outward of the compressor; and
a bearing compartment assembly comprising:
a fluid pump;
a compartment;
a fluid line extending between the fluid pump and the compartment; and
a damper check valve located in the fluid line, the damper check valve being
a unitary, monolithic component that is configured to restrict a reverse flow from the compartment to the fluid pump substantially more than the damper check valve restricts a standard flow from the fluid pump to the compartment, wherein the damper check valve comprises:
an inlet portion with a straight inner shape comprising a length and a diameter along the length, wherein the length is between one to five times the diameter of the straight inner shape;
a converging portion downstream of the inlet portion;
a diverging portion downstream of the converging portion, and a constriction between the converging portion and the diverging portion; wherein
the diverging portion comprises:
a full-width portion in contact with an interior of the fluid line; and
a reentrant protrusion downstream of the full-width portion that is spaced apart from the interior of the fluid line;
wherein the reentrant protrusion comprises:
 a protrusion length measured from a downstream end of the full-width portion to an exit diameter of the reentrant protrusion, and wherein the protrusion length is less than the length of the inlet portion.

2. The gas turbine engine of claim 1 , wherein the damper check valve is configured to restrict reverse flow fifteen times more than the damper check valve is configured to restrict standard flow.

3. The gas turbine engine of claim 1 , wherein the damper check valve is configured to restrict reverse flow twenty times more than the damper check valve is configured to restrict standard flow.

4. The gas turbine engine of claim 1 , wherein the fan is driven through a gearbox.

5. The gas turbine engine of claim 1 , wherein:
the compressor comprises a low pressure compressor rotor and a high pressure compressor rotor;
the turbine comprises a high pressure turbine rotor connected to the high pressure compressor rotor by a high shaft and a low pressure turbine rotor connected to the low pressure compressor rotor by a low shaft; and
the bearing compartment assembly supports the low shaft.

6. The gas turbine engine of claim 1 , wherein the fluid pump is an oil pump and the fluid line is an oil line.

7. The gas turbine engine of claim 1 , wherein the converging portion comprises:
a primary convergence downstream of the inlet portion with a frusto-conical inner shape.

8. The gas turbine engine of claim 7 , wherein the converging portion further comprises a secondary convergence downstream of the primary convergence and upstream of the constriction.

9. A bearing compartment assembly comprising:
a fluid pump;
a compartment;
a fluid line extending between the fluid pump and the compartment; and
a damper check valve located in the fluid line, the damper check valve being a unitary, monolithic component that is configured to restrict a reverse flow from the compartment to the fluid pump substantially more than the damper check valve restricts a standard flow from the fluid pump to the compartment, wherein the damper check valve comprises:
an inlet portion with a straight inner shape comprising a length and a diameter along the length, wherein the length is between one to five times the diameter of the straight inner shape;
a primary convergence with a frusto-conical inner shape downstream of the inlet portion;
a diverging portion downstream of the primary convergence; and
a constriction between the primary convergence and the diverging portion;
wherein the diverging portion comprises:
a full-width portion downstream of the primary convergence in contact with an interior of the fluid line; and
a reentrant protrusion downstream of the full-width portion that is spaced apart from the interior of the fluid line
wherein the reentrant protrusion comprises:
a protrusion length measured from a downstream end of the full-width portion to an exit diameter of the reentrant protrusion, and wherein the protrusion length is less than the length of the inlet portion.

10. The damper check valve of claim 9 , wherein the protrusion length is one to five times as long as the exit diameter of the reentrant protrusion.

11. A damper check valve that is a unitary, monolithic component comprising:
an inlet portion with a straight inner shape comprising a length and a diameter along the length, wherein the length is between one to five times the diameter of the straight inner shape; and
a primary convergence downstream of the inlet portion with a frusto-conical inner shape;
a diverging portion downstream of the primary convergence, the diverging portion comprising:
a full-width portion in contact with an interior of the fluid line; and
a reentrant protrusion downstream of the full-width portion that has a reduced outer shape that is spaced apart from the interior of the fluid line, wherein the reentrant protrusion comprises:
a protrusion length measured from a downstream end of the full-width portion to an exit diameter of the reentrant protrusion, and wherein the protrusion length is less than the length of the inlet portion; and

a constriction between the primary convergence and the diverging portion, the constriction being a smallest inner diameter of the damper check valve;
wherein the damper check valve is configured to restrict a reverse flow from the compartment to the fluid pump substantially more than the damper check valve restricts a standard flow from the fluid pump to the compartment.

12. The damper check valve of claim 11 , further comprising a secondary convergence downstream of the primary convergence and upstream of the constriction.

13. The damper check valve of claim 11 , wherein the protrusion length is one to five times as long as the exit diameter of the reentrant protrusion.

Assignees

• United Technologies Corp

Inventors

• Sheridan William G

Classifications

• F01D25/20 Primary

  using lubrication pumps · CPC title

• F16N2270/60

  Pressure · CPC title

• F01M1/16

  Controlling lubricant pressure or quantity (rendering machines or engines inoperative or idling on lubricant pressure failure F01M1/22) · CPC title

• F05D2260/60

  Fluid transfer · CPC title

• F16N2280/00

  Valves · CPC title