Dual action check valve with combined return and bypass passages

Patent metadata

Field	Value
Publication number	US-10144518-B2
Application number	US-201313743373-A
Country	US
Kind code	B2
Filing date	Jan 17, 2013
Priority date	Jan 17, 2013
Publication date	Dec 4, 2018
Grant date	Dec 4, 2018

Abstract

A combination includes a selectively driven fan and a bypass flow passage for bypassing the fan. The bypass flow passage communicates with a first check valve to allow air to flow from the bypass passage to a downstream location. A second check valve allows air driven by the fan to pass into a return passage and return to an inlet of the fan in the event that the discharge pressure from the fan overcomes a spring force associated with the second check valve. A heat exchanger pack and an environmental control system for use on an aircraft, and a method are all also disclosed.

First claim

The invention claimed is:

1. A fan and bypass combination comprising:
a selectively driven fan and a bypass flow passage for bypassing said fan, said bypass flow passage communicating with a first check valve selectively movable to a bypass position to allow air to flow from said bypass flow passage to a downstream location;
a second check valve movable to a return position for allowing air driven by said fan to pass into a return passage, and return to an inlet of said fan in the event that a discharge pressure from said fan overcomes a spring force associated with said second check valve;
wherein said return passage is said bypass flow passage;
wherein said second check valve is associated with said first check valve, and moves with said first check valve when said first check valve moves to said bypass position; and
wherein said first check valve moves away from a first valve plate in said bypass position, and said second check valve moves away from said check valve when in said return position.

2. A heat exchanger pack comprising:
at least one heat exchanger associated with a cooling air flow, and said at least one heat exchanger being positioned intermediate a cooling air inlet and a fan, and a check valve;
said fan being selectively driven to move cooling air over said at least one heat exchanger, and a bypass flow passage for bypassing said fan, said bypass flow passage communicating with a first check valve selectively movable to a bypass position to allow air to flow from said bypass flow passage to a downstream location, a second check valve movable to a return position for allowing air driven by said fan to pass into a return passage, and return to an inlet of said fan in the event that a discharge pressure from said fan overcomes a spring force associated with said second check valve;
wherein said return passage is said bypass flow passage;
wherein said second check valve is associated with said first check valve, and moves with said first check valve when said first check valve moves to said bypass position; and
wherein said first check valve moves away from a first valve plate in said bypass position, and said second check valve moves away from said first check valve when in said return position.

3. An environmental control system for use on an aircraft comprising:
an air cycle machine for delivering air to uses on an aircraft, and said air cycle machine passing air through at least one heat exchanger;
said at least one heat exchanger associated with a cooling air flow, and said at least one heat exchanger being positioned intermediate a cooling air inlet and a fan, and a check valve;
said fan being selectively driven to move cooling air over said at least one heat exchanger, and a bypass flow passage for bypassing said fan, said bypass flow passage communicating with a first check valve selectively movable to a bypass position to allow air to flow from said bypass flow passage to a downstream location, a second check valve movable to a return position for allowing air driven by said fan to pass into a return passage, and to an inlet of said fan in the event that the discharge pressure from said fan overcomes a spring force associated with said second check valve;
wherein said return passage is said bypass flow passage;
wherein said second check valve is associated with said first check valve, and moves with said first check valve when said first check valve moves to said bypass position; and
wherein said first check valve moves away from a first valve plate in said bypass mode, and said second check valve moves away from said first check valve when in said return position.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Hipsky Harold W

Classifications

• B64D13/06 Primary

  the air being conditioned (pressurising B64D13/02) · CPC title

• G05D7/01

  without auxiliary power · CPC title

• F04D27/009

  by bleeding, by passing or recycling fluid · CPC title

• F16K15/035

  with a plurality of valve members · CPC title

• F16K17/196

  spring-loaded · CPC title