Backflow prevention valve

Patent metadata

Field	Value
Publication number	US-10267430-B2
Application number	US-201715584714-A
Country	US
Kind code	B2
Filing date	May 2, 2017
Priority date	May 23, 2013
Publication date	Apr 23, 2019
Grant date	Apr 23, 2019

Abstract

A valve assembly includes an outer housing having a first opening in fluid communication with a first fluid, a second opening in fluid communication with a second fluid, a third opening in fluid communication with a third fluid and a fourth opening in fluid communication with a fourth fluid. The valve assembly includes a piston configured to slide within the outer housing into a first position at which the third opening is blocked from fluid communication with the fourth opening based on a fluid pressure of the first fluid being greater than a fluid pressure of the fourth fluid. The piston is further configured to slide within the outer housing into a second position at which the third opening is in fluid communication with the fourth opening based on the fluid pressure of the second fluid being greater than the fluid pressure of the fourth fluid.

First claim

What is claimed is:

1. An engine bleed-air system, comprising:
a bleed valve configured to receive as an input a first gas flow from an engine and a second gas flow from ambient air, and an electrical control signal configured to control a ratio of the first gas flow and the second gas flow to be output as a third gas flow;
a servo chamber including a first piston, the servo chamber configured to receive the third gas flow and to control a position of the first piston to control an output gas flow from the engine; and
a reverse-flow prevention valve in fluid communication with the first gas flow, the second gas flow, the third gas flow and a fourth gas flow, the reverse-flow prevention valve configured to expose the third gas flow to ambient air based on the fourth gas flow having a pressure greater than the pressure of the first gas flow, and the reverse-flow prevention valve configured to block the third gas flow from the ambient air based on the first gas flow having a pressure greater than the pressure of the fourth gas flow.

2. The engine bleed-air system of claim 1 , wherein the reverse-flow prevention valve comprises:
an outer housing having a first opening configured to be in fluid communication with the first gas flow, a second opening configured to be in fluid communication with the fourth gas flow, a third opening configured to be in fluid communication with the third gas flow, and a fourth opening configured to be in fluid communication with the ambient air; and
a second piston configured to slide within the outer housing, the second piston having a first end forming a seal with respect to the outer housing and being in contact with the first gas flow, a second end forming a seal with respect to the outer housing and being in contact with the second gas flow, a first recess in an outer radial surface of the second piston and a second recess in the outer radial surface of the second piston, the first recess in fluid communication with the second recess,
wherein the first recess is configured to be sealed off from the third opening when the second piston is in a first sliding position with respect to the outer housing, and the first recess is configured to be in fluid communication with the third opening, to transmit a gas between the third opening and the fourth opening, when the second piston is in a second sliding position with respect to the outer housing.

3. The engine bleed-air system of claim 2 , wherein the first recess and the second recess are annular recesses extending around the outer circumference of the second piston.

4. The engine bleed-air system of claim 2 , wherein the second piston includes a channel located radially-inward of the first and second recesses and connecting the first and second recesses.

5. The engine bleed-air system of claim 2 , further comprising:
a sealing structure located between the outer housing and the second piston along an entire length of the second piston, the second piston configured to slide with respect to the sealing structure, the sealing structure configured to seal the first opening from the second opening, the third opening and the fourth opening.

6. The engine bleed-air system of claim 2 , wherein the second piston includes a first cup-shaped recess at the first end to receive a first gas of the first gas flow and a second cup-shaped recess at the second end to receive a second gas of the fourth gas flow.

7. The engine bleed-air system of claim 2 , wherein an inner surface of the outer housing is cylindrical.

8. The engine bleed-air system of claim 1 , further comprising a first engine configured to emit the fourth gas flow,
wherein the first gas flow is a bleed gas flow that is bled from the fourth gas flow via a filter.

9. The engine bleed-air system of claim 8 , further comprising a second engine configured to emit a fifth gas flow, the fifth gas flow in fluid communication with the fourth gas flow via at least one control valve, the fourth gas flow and the fifth gas flow configured to be combined into sixth output gas flow downstream from the fourth and fifth gas flows.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Simpson Scott W

Classifications

• F16K31/122 Primary

  the fluid acting on a piston (F16K31/143, F16K31/163, F16K31/363, F16K31/383 take precedence) · CPC title

• F02C9/48

  Control of fuel supply conjointly with another control of the plant (with nozzle section control F02K1/17) · CPC title

• F02C9/18

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

• F01D17/105 Primary

  by passing part of the fluid · CPC title

• F05D2270/10

  to cope with, or avoid, compressor flow instabilities · CPC title