Ducted gas turbine engine stability bleed valve with passive and active shutoff

Patent metadata

Field	Value
Publication number	US-10626802-B2
Application number	US-201816137874-A
Country	US
Kind code	B2
Filing date	Sep 21, 2018
Priority date	Sep 21, 2018
Publication date	Apr 21, 2020
Grant date	Apr 21, 2020

Abstract

A bleed air valve comprises a piston that moves along a guide, where the piston includes a first surface and an opposing second surface. A pressure divider network includes a divider network inlet having an inlet cross sectional area in fluid communication with a fluid passage, a divider network outlet having an outlet cross sectional area in fluid communication with ambient pressure, and a network chamber in fluid communication with the divider network inlet and the divider network outlet. The network chamber has a pressure value between pressure at the divider network inlet and pressure at the divider network outlet. A shuttle valve includes a shuttle inlet and a shuttle outlet, where the shuttle outlet is in fluid communication with the first surface. An electromechanical valve receives a command signal and in response provides compressed air to an electromechanical valve output that is in fluid communication with the shuttle inlet.

First claim

What is claimed is:

1. A bleed air valve, comprising:
a housing that includes an inlet at a first end, an outlet at a second end, and a center portion between the inlet and the outlet to selectively provide a pneumatic flow path between the inlet and the outlet via a passage in the center portion;
a piston that moves along a center guide, where the piston includes a first piston surface and an opposing second piston surface, and the piston moves along the center guide in response to forces applied to the first piston surface and the second piston surface, where the piston is spring biased to an open position such that the inlet and the outlet are in fluid communication;
a pressure divider network that includes a divider network inlet having an inlet cross sectional area in fluid communication with the passage, a divider network outlet having an outlet cross sectional area in fluid communication with ambient pressure, and a network chamber in fluid communication with the divider network inlet and the divider network outlet, where the network chamber has an intermediate pressure value between pressure at the divider network inlet and pressure at the divider network outlet and based upon the inlet cross sectional area and the outlet cross sectional area;
a shuttle valve that includes a shuttle valve inlet and a shuttle valve outlet, where the shuttle valve outlet is in fluid communication with the piston first surface;
a solenoid valve that receives a command signal and in response provides compressed air to a solenoid valve output that is in fluid communication with the shuttle valve inlet; and
a spring that applies a force to the second piston surface to spring bias the bleed air valve to the open position.

2. The bleed air valve of claim 1 , where the cross sectional area of the divider network outlet is greater than the cross sectional area of the divider network inlet.

3. The bleed air valve of claim 1 , where the solenoid valve receives gas turbine engine compressor discharge pressure such that when the solenoid valve that receives the command signal to close the solenoid valve provides the compressor discharge pressure to the solenoid valve output.

4. The bleed air valve of claim 3 , where the cross sectional area of the divider network inlet is less than 50% of the cross sectional area of the divider network outlet.

5. The bleed air valve of claim 1 , where the center guide is axially aligned with the housing inlet and the housing outlet.

6. The bleed air valve of claim 3 , where the shuttle valve also includes a second shuttle valve inlet in fluid communication with the network chamber.

7. The bleed air valve of claim 6 , where the shuttle valve is integral with the housing.

8. A bleed air valve, comprising:
a housing that includes an inlet at a first end, an outlet at a second end, and a center portion between the inlet and the outlet to selectively provide a pneumatic flow path between the inlet and the outlet via a passage in the center portion;
a piston that moves along a center guide, where the piston includes a first piston surface and an opposing second piston surface, and the piston moves along the center guide in response to forces applied to the first piston surface and the second piston surface, where the piston is spring biased to an open position such that the housing inlet and the housing outlet are in fluid communication;
a pressure divider network that includes a divider network inlet having an inlet cross sectional area in fluid communication with the passage, a divider network outlet having an outlet cross sectional area in fluid communication with ambient pressure, and a network chamber in fluid communication with the divider network inlet and the divider network outlet, where the network chamber has an intermediate pressure value between pressure at the divider network inlet and pressure at the divider network outlet;
a valve that includes a valve inlet and a valve outlet, where the valve outlet is in fluid communication with the piston first surface; and
a control valve that receives a command signal and in response provides compressed air to a control valve output that is in fluid communication with the valve inlet.

9. The bleed air valve of claim 8 , further comprising a spring that applies a force to the second piston surface.

10. The bleed air valve of claim 9 , where the network chamber has an intermediate pressure value is dependent on the inlet cross sectional area and the outlet cross sectional area.

11. The bleed air valve of claim 10 , where the valve also includes a second valve inlet in fluid communication with the network chamber.

12. The bleed air valve of claim 11 , where the cross sectional area of the divider network inlet is less than 50% of the cross sectional area of the divider network.

13. The bleed air valve of claim 12 , where the control valve comprises an electromechanical valve.

14. The bleed air valve of claim 13 , where the valve comprises a shuttle valve.

15. An aircraft gas turbine engine bleed air valve, comprising:
a housing that includes an inlet at a first end, an outlet at a second end, and a center portion between the inlet and the outlet to selectively provide a pneumatic flow path between the inlet and the outlet via a passage in the center portion;
a piston that axially moves along a center guide, where the piston includes a first piston surface and an opposing second piston surface, and the piston axially moves along the center guide in response to forces applied to the first piston surface and the second piston surface, where the piston is spring biased to an open position such that the inlet and the outlet are in fluid communication;
a pressure divider network that includes a divider network inlet having an inlet cross sectional area in fluid communication with the passage, a divider network outlet having an outlet cross sectional area in fluid communication with ambient pressure, and a network chamber in fluid communication with the divider network inlet and the divider network outlet, where the network chamber has an intermediate pressure value between pressure at the divider network inlet and pressure at the divider network outlet;
a shuttle valve that includes a shuttle valve inlet and a shuttle valve outlet, where the shuttle valve outlet is in fluid communication with the piston first surface;
an electromechanical valve that receives a command signal and in response provides compressed air to an electromechanical valve output that is in fluid communication with the shuttle valve inlet; and
a spring that applies a force to the second piston surface to spring bias the aircraft gas turbine engine bleed air valve to the open position to bleed compressor air to ambient.

16. The bleed air valve of claim 15 , where the network chamber intermediate pressure value is dependent on the inlet cross sectional area and the outlet cross sectional area.

17. The bleed air valve of claim 16 , where the shuttle valve also includes a second shuttle valve inlet in fluid communication with the network chamber.

Assignees

• United Technologies Corp

Inventors

• Goodman Robert B
• Greenberg Michael D

Classifications

• 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

• F01D17/105

  by passing part of the fluid · CPC title

• F04D27/0215

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

• F05D2270/301

  Pressure · CPC title

• F01D17/145

  by means of valves, e.g. for steam turbines (valves in general F16K) · CPC title