This application relates to a sleeve valve which has a first mode for closing the valve when a line pressure exceeds a predetermined force, and also has a controlled closing mode.
Sleeve valves are known, and typically include a sleeve which is biased in one direction by a spring to an open position. A pressure force acts against the spring force and may close the sleeve when the pressure force exceeds the spring force.
One application for a sleeve valve is as an aircraft compressor system bleed valve. As known, in a gas turbine engine, the compressor has issues with stability at startup and other low power conditions. Thus, at low pressure a bleed valve opens to allow some of the compressed air to bleed outwardly. It is typical to have the valve in different passive positions at different engine operating conditions. As mentioned, it is open at low power for stability reasons. On the other hand, it is typically closed at high power to preserve efficiency.
A sleeve valve includes an inlet port and an outlet port. A fluid chamber connects the inlet port to the 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. The sleeve moves within a housing, and has a pressure chamber on opposed side of the sleeve from the spring. 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 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 is also disclosed.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
A sleeve 32 is movable within the housing 29. As shown in the
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.
As further shown in
In
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.
Thus, in
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
As shown in
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.
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.
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.
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| Number | Date | Country |
|---|---|---|
| 3726032 | Oct 2020 | EP |
| Entry |
|---|
| European Search Report for EP Application No. 22197803.4 dated Feb. 22, 2023. |
| Number | Date | Country | |
|---|---|---|---|
| 20230109588 A1 | Apr 2023 | US |