Bypass valve system state indication

Patent metadata

Field	Value
Publication number	US-10378443-B2
Application number	US-201715422921-A
Country	US
Kind code	B2
Filing date	Feb 2, 2017
Priority date	Feb 2, 2017
Publication date	Aug 13, 2019
Grant date	Aug 13, 2019

Abstract

A fluid system may comprise a fluid passage comprising a passage inlet and a passage outlet, through which fluid may flow by entering the passage inlet as an inlet flow and exiting the passage outlet as an outlet flow; a bypass valve comprising a bypass inlet and a bypass outlet, the bypass inlet being in fluid communication with the passage inlet, wherein the bypass valve further comprises a piston coupled to a spring; and a position sensor coupled to the bypass valve and configured to detect a position of the piston in the bypass valve. The spring may retain the piston in a rest position, and the spring and the piston may be configured to block the fluid from passing through the bypass outlet in response to the inlet flow exerting a pressure below a bypass pressure threshold.

First claim

What is claimed is:

1. A fluid system, comprising:
a fluid passage comprising a passage inlet and a passage outlet, wherein the fluid passage is configured to allow a fluid to pass through the fluid passage by entering the passage inlet as an inlet flow and exiting the passage outlet as an outlet flow;
a bypass valve comprising a bypass inlet and a bypass outlet, the bypass inlet being in fluid communication with the passage inlet, wherein the bypass valve further comprises a piston coupled to a spring, wherein the spring retains the piston in a rest position, and the spring and the piston are configured to block the fluid from passing through the bypass outlet in response to the inlet flow exerting a pressure below a bypass pressure threshold, wherein the piston is in the rest position in the bypass inlet, wherein the bypass inlet comprises an inlet surrounding wall, wherein a portion of the inlet surrounding wall adjacent to the bypass outlet is a bypass slack area, wherein the piston is in the rest position at a slack area end furthest from the bypass outlet, and the piston is configured to move along the bypass slack area toward the bypass outlet in response to a pressure threshold being reached by the inlet flow in the passage inlet before allowing the fluid to pass through the bypass outlet;
a position sensor coupled to the bypass valve and configured to detect a position of the piston in the bypass valve; and
a control system in electronic communication with the position sensor, wherein the position sensor transmits the position of the piston to the control system, wherein the control system comprises a processor and is configured to determine an impending bypass flow through the bypass outlet in response to the piston being moved to a displaced position along the bypass slack area from the rest position without allowing the fluid to pass through the bypass outlet.

2. The fluid system of claim 1 , wherein the fluid passage is at least one of an oil filter, a fuel filter, or an air filter.

3. The fluid system of claim 1 , wherein the fluid passage is a heat exchanger.

4. The fluid system of claim 1 , wherein the bypass valve is configured to pass the fluid through the bypass outlet in response to the piston moving past the bypass slack area caused by the inlet flow reaching the bypass pressure threshold, and in response to the piston moving past the bypass slack area, the bypass outlet is in fluid communication with the bypass inlet.

5. The fluid system of claim 1 , wherein the control system is further configured to determine a bypass flow through the bypass outlet in response to the piston moving past the bypass slack area and allowing the fluid to pass through the bypass outlet.

6. The fluid system of claim 1 , wherein the position sensor is at least one of a proximity probe, a linear variable differential transformer, a sonar device, or a magnetic pickup.

7. The fluid system of claim 1 , wherein the bypass valve comprises a cap coupled to the spring, wherein the spring is disposed between the cap and the piston, and the position sensor is coupled to the cap.

8. An aircraft, comprising:
a gas turbine engine;
a fluid system at least one of coupled to, or in fluid communication with, the gas turbine engine, comprising:
a fluid passage comprising a passage inlet and a passage outlet, wherein the fluid passage is configured to allow a fluid to pass through the fluid passage by entering the passage inlet as an inlet flow and exiting the passage outlet as an outlet flow;
a bypass valve comprising a bypass inlet and a bypass outlet, the bypass inlet being in fluid communication with the passage inlet, wherein the bypass valve further comprises a piston coupled to a spring, wherein the spring retains the piston in a rest position, and the spring and the piston are configured to block the fluid from passing through the bypass outlet in response to the inlet flow exerting a pressure below a bypass pressure threshold, wherein the piston is in the rest position in the bypass inlet, wherein the bypass inlet comprises an inlet surrounding wall, wherein a portion of the inlet surrounding wall adjacent to the bypass outlet is a bypass slack area, wherein the piston is in the rest position at a slack area end furthest from the bypass outlet, and the piston is configured to move along the bypass slack area toward the bypass outlet in response to a pressure threshold being reached by the inlet flow in the passage inlet before allowing the fluid to pass through the bypass outlet;
a position sensor coupled to the bypass valve and configured to detect a position of the piston in the bypass valve; and
a control system in electronic communication with the position sensor, wherein the position sensor transmits the position of the piston to the control system, wherein the control system comprises a processor and is configured to determine an impending bypass flow through the bypass outlet in response to the piston being moved to a displaced position along the bypass slack area from the rest position without allowing the fluid to pass through the bypass outlet.

9. The aircraft of claim 8 , wherein the control system is further configured to determine a bypass flow through the bypass outlet in response to the piston moving past the bypass slack area and allowing the fluid to pass through the bypass outlet.

10. A method for monitoring a fluid passage, comprising:
passing a fluid through the fluid passage in a fluid system by the fluid entering a fluid inlet as an inlet flow and exiting through a fluid outlet as an outlet flow, wherein the fluid system comprises a bypass valve having a bypass inlet fluidly coupled to a passage inlet and a bypass outlet, wherein the bypass valve further comprises a piston in the passage inlet coupled to a spring, wherein the spring retains the piston in a rest position, and the spring and the piston are configured to block the fluid from passing through the bypass outlet in response to the inlet flow exerting a pressure below a bypass pressure threshold,
wherein the bypass inlet comprises an inlet surrounding wall, wherein a portion of the inlet surrounding wall adjacent to the bypass outlet is a bypass slack area, wherein the piston is in the rest position at a slack area end furthest from the bypass outlet of the bypass slack area, and the piston is configured to move along the bypass slack area toward the bypass outlet in response to the pressure threshold being reached by the inlet flow in the passage inlet before allowing the fluid to pass through the bypass outlet;
detecting, by a position sensor coupled to the bypass valve, a position of the piston in the passage inlet;
determining, by a processor, whether the piston has moved from the rest position; and
determining, by the processor, an impending bypass flow in response to determining that the piston has moved from the rest position to a displaced position along the bypass slack area.

11. The method of claim 10 , further comprising determining, by the processor, a bypass flow in response to determining that the piston has moved from the rest position to a bypass position, wherein the bypass position is when the piston has moved past the bypass slack area, causing the fluid to pass through bypass outlet.

Assignees

• United Technologies Corp

Inventors

• Clark Richard W
• Cué Javier A

Classifications

• F16K17/04

  spring-loaded · CPC title

• F16K37/0025

  Electrical or magnetic means (F16K37/0075 takes precedence) · CPC title

• Y02T50/675

  Cross-Sectional Technologies · mapped topic

• B01D35/1435

  with alarm means · CPC title

• F01D17/08

  responsive to condition of working-fluid, e.g. pressure · CPC title