Spring loaded sleeve valve with controlled closing force
11703128 ยท 2023-07-18
Assignee
Inventors
Cpc classification
F16K31/1221
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/42
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/38
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/141
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/46
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/606
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F01D17/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/123
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/0215
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C9/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K1/126
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/65
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D27/023
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/44
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2270/101
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05D2260/52
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16K1/12
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C6/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02C9/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
A sleeve valve includes an inlet port and an outlet port. A sleeve is movable to close flow from the inlet port to the outlet port. The sleeve valve has a sleeve biased to an open position at which it allows flow from the inlet port to the outlet port by a spring. Pressure in a pressure chamber urges the sleeve to a closed position at which it blocks flow from the inlet port to the outlet port. A line pressure conduit communicates the fluid chamber into the pressure chamber. Pressurized air is supplied to the pressure chamber through a selectively closed valve. The selectively closed valve is opened to allow the flow of high pressure air from a pressure source into the pressure chamber to move the sleeve to a closed position. A bleed air system for a gas turbine engine is also disclosed.
Claims
1. A sleeve valve comprising: an inlet port and an outlet port, with a fluid chamber connecting the inlet port to the outlet port; a sleeve valve movable to close flow from the inlet port to the outlet port, the sleeve valve having a sleeve being biased by a spring to an open position at which it allows flow from the inlet port to the outlet port, and the sleeve moving within a housing, and having a pressure chamber on an opposed side of the sleeve from the spring, such that pressure in the pressure chamber urges the sleeve to a closed position at which it blocks flow from the inlet port to the outlet port; a line pressure conduit communicates the fluid chamber into the pressure chamber; pressurized air supplied to the pressure chamber through a selectively closed valve, the selectively closed valve being opened to allow the flow of high pressure air from a pressure source through a high pressure conduit into the pressure chamber to move the sleeve to a closed position; a control valve controls the high pressure air through the high pressure conduit into the pressure chamber when it is open, and a check valve provided on the line pressure conduit to block flow of the high pressure air moving back outwardly into the fluid chamber; the control valve is a solenoid valve; and the solenoid valve controls a position of a pressure relay valve, with the solenoid valve received on a first control conduit, and the pressure relay valve blocking flow through the high pressure conduit into the pressure chamber.
2. The sleeve valve as set forth in claim 1, wherein the control valve and the check valve are separate valves.
3. The sleeve valve as set forth in claim 1, wherein a spring chamber is defined on a side of the sleeve receiving the spring, and the spring chamber communicating with a tap to a pressure source.
4. The sleeve valve as set forth in claim 3, wherein the pressure source is an ambient pressure.
5. The sleeve valve as set forth in claim 3, wherein the tapped pressure is above an ambient pressure.
6. The sleeve valve as set forth in claim 1, wherein an electric control is programmed to control the solenoid to achieve the flow of high pressure air into the pressure chamber based upon system conditions.
7. The sleeve valve as set forth in claim 1, wherein a spring chamber is defined on a side of the sleeve receiving the spring, and the spring chamber communicating with a tap to a pressure source, wherein the pressure source is an ambient pressure.
8. The sleeve valve as set forth in claim 1, wherein a spring chamber is defined on a side of the sleeve receiving the spring, and the spring chamber communicating with a tap to a pressure source, wherein the tapped pressure is above an ambient pressure.
9. A bleed air system for a gas turbine engine comprising: a compressor, the compressor having a bleed conduit bleeding into a bleed valve; the bleed valve having an inlet port and an outlet port, with a fluid chamber connecting the inlet port to the outlet port; the bleed valve also having a sleeve movable to close flow from the inlet port to the outlet port, the sleeve valve having a sleeve being biased to an open position at which it allows flow from the inlet port to the outlet port by a spring, and the sleeve moving within a housing, and having a pressure chamber on opposed side of the sleeve from the spring, such that pressure in the pressure chamber urges the sleeve to a closed position at which it blocks flow from the inlet port to the outlet port; a line pressure conduit communicates the fluid chamber into the pressure chamber; pressurized air supplied to the pressure chamber through a selectively closed valve, the selectively closed valve being opened to allow the flow of high pressure air from a pressure source through a high pressure conduit into the pressure chamber through a high pressure conduit to move the sleeve to a closed position; and a control valve controls the high pressure air through the high pressure conduit into the pressure chamber when it is open, and a check valve provided on the line pressure conduit to block flow of the high pressure air moving back outwardly into the fluid chamber, and the control valve is separate from the check valve; where in the control valve controls the position of the selectively closed valve.
10. The bleed air system as set forth in claim 9, wherein a spring chamber is defined on a side of the sleeve receiving the spring, and the spring chamber communicating with a tap to a pressure source.
11. The bleed air system as set forth in claim 10, wherein the pressure source is an ambient pressure.
12. The bleed air system as set forth in claim 10, wherein the tapped pressure is above an ambient pressure.
13. The bleed air system as set forth in claim 9, wherein the control valve is a solenoid valve.
14. The bleed air system as set forth in claim 13, wherein an electric control is programmed to control the solenoid to achieve the flow of high pressure air into the pressure chamber based upon system conditions.
15. The bleed air system as set forth in claim 9, wherein a spring chamber is defined on a side of the sleeve receiving the spring, and the spring chamber communicating with a tap to a pressure source, wherein the pressure source is an ambient pressure.
16. The bleed air system as set forth in claim 9, wherein a spring chamber is defined on a side of the sleeve receiving the spring, and the spring chamber communicating with a tap to a pressure source, wherein the tapped pressure is above an ambient pressure.
17. A bleed air system for a gas turbine engine comprising: a compressor, the compressor having a bleed conduit bleeding into a bleed valve; the bleed valve having an inlet port and an outlet port, with a fluid chamber connecting the inlet port to the outlet port; the bleed valve also having a sleeve movable to close flow from the inlet port to the outlet port, the sleeve valve having a sleeve being biased to an open position at which it allows flow from the inlet port to the outlet port by a spring, and the sleeve moving within a housing, and having a pressure chamber on opposed side of the sleeve from the spring, such that pressure in the pressure chamber urges the sleeve to a closed position at which it blocks flow from the inlet port to the outlet port; a line pressure conduit communicates the fluid chamber into the pressure chamber; pressurized air supplied to the pressure chamber through a selectively closed valve, the selectively closed valve being opened to allow the flow of high pressure air from a pressure source through a high pressure conduit into the pressure chamber through a high pressure conduit to move the sleeve to a closed position; a control valve controls the high pressure air through the high pressure conduit into the pressure chamber when it is open, and a check valve provided on the line pressure conduit to block flow of the high pressure air moving back outwardly into the fluid chamber; the control valve is a solenoid valve; and wherein the solenoid valve controls a position of a pressure relay valve, with the solenoid valve received on a first control conduit, and the pressure relay valve blocking flow through the high pressure conduit into the pressure chamber.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
(4)
(5)
(6)
DETAILED DESCRIPTION
(7)
(8) A sleeve 32 is movable within the housing 29. As shown in the
(9) Further shown is high pressure conduit 50 communicating into the chamber 44 through a solenoid 52 to selectively communicate air from a high pressure source 54. A control 200 controls the solenoid 52.
(10) As further shown in
(11) In
(12) As known, a bleed valve is to close when the compressor 22 pressure exceeds a particular value. The function of the bleed valve is to bleed air at lower pressure operation. To continue to bleed air would cause efficiency losses to the associated gas turbine engine.
(13) Thus, in
(14) The control 200 has the ability to control the position and operation of the valve 25. As such, the control 200 may move the valve to a closed position such as shown in
(15)
(16) As shown in
(17) This embodiment has the additional feature that the conduit 156/157 may be larger in area than could be the case if the solenoid 52 alone controls flow of the control high pressure air. That is, by having the relay valve 210, a greater airflow may be sent into the chamber 44 to move the sleeve 32 to the closed position more rapidly.
(18)
(19) The control 200 may be a standalone controller, or it may be incorporated into a full authority digital electronic controller for the engine associated with compressor 22. The control 200 would be programmed as appropriate to achieve the control as disclosed in this application.
(20) Although embodiments of this disclosure have been shown, a worker of ordinary skill in this art would recognize that modifications would come within the scope of this disclosure. For that reason, the following claims should be studied to determine the true scope and content of this disclosure.