Air-liquid heat exchanger assembly having a bypass valve

Patent metadata

Field	Value
Publication number	US-9745069-B2
Application number	US-201313746073-A
Country	US
Kind code	B2
Filing date	Jan 21, 2013
Priority date	Jan 21, 2013
Publication date	Aug 29, 2017
Grant date	Aug 29, 2017

Abstract

An air-liquid heat exchanger assembly for an environmental control system of an aircraft includes a heat exchanger, a controller, and a bypass valve. The heat exchanger includes a first chamber and a second chamber. The first chamber has a first inlet that is provided a liquid and a first end that is provided air. The second chamber is arranged adjacent the first chamber. The bypass valve is operably coupled to the controller. The bypass valve having an inlet coupled to a first outlet of the first chamber, a first outlet coupled to a second inlet of the second chamber, and a second outlet coupled to a bypass conduit. The controller adjusts a position of the bypass valve to control the flow of liquid through the second chamber and the bypass conduit.

First claim

What is claimed is:

1. An air-liquid heat exchanger assembly for an environmental control system of an aircraft comprising:
a heat exchanger that includes:
a first chamber having a first inlet, a first outlet, and a first end, the first inlet being configured to receive a liquid and the first end being configured to receive air, and
a second chamber having a second inlet and a second outlet, the second chamber arranged adjacent to the first chamber, the second outlet coupled to a bypass conduit, wherein the air passes over the first chamber and subsequently passes over the second chamber;

a controller that monitors the operating conditions of the heat exchanger; and
a bypass valve operably coupled to the controller, the bypass valve having an inlet directly coupled to the first outlet of the first chamber by a first conduit, the bypass valve having a first outlet directly coupled to the second inlet of the second chamber by a second conduit, and the bypass valve having a second outlet directly coupled to the bypass conduit wherein the controller adjusts a position of the bypass valve to control a flow of the liquid through both the second chamber and the bypass conduit in response to a signal received from the controller that is based on the operating conditions.

2. The air-liquid heat exchanger assembly according to claim 1 , wherein the first chamber is positioned adjacent to the second chamber and is separated therefrom by an insulation gap.

3. The air-liquid heat exchanger assembly according to claim 1 , wherein the liquid is a coolant.

4. The air-liquid heat exchanger assembly according to claim 1 , wherein the first chamber has a single pass, cross-flow core arrangement.

5. The air-liquid heat exchanger assembly according to claim 1 , wherein the operating conditions includes at least one of an altitude of the aircraft, a liquid flow rate, an air flow rate, a temperature of the liquid entering the first inlet of the first chamber, and a temperature of the liquid within the bypass conduit.

6. The air-liquid heat exchanger assembly according to claim 1 , wherein the second chamber has a cross-counter flow core arrangement.

7. The air-liquid heat exchanger assembly according to claim 6 , wherein the second chamber has a multiple pass core arrangement.

8. The air-liquid heat exchanger assembly according to claim 1 , further comprising:
a first temperature sensor operably coupled to the controller, the first temperature sensor positioned to measure a temperature of a remixed liquid resulting from the liquid that bypasses the second chamber via the bypass valve via the bypass conduit and the liquid that exits the second outlet of the second chamber via a conduit that is attached to the second outlet of the second chamber at a first end and the conduit is connected at a second end to the bypass conduit bypass conduit.

9. The air-liquid heat exchanger assembly according to claim 8 , further comprising:
a second temperature sensor operably coupled to the controller, the second temperature sensor arranged adjacent the first inlet of the first chamber, the second temperature sensor positioned to measure a temperature of the liquid entering the first chamber.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Shea Brian R

Classifications

• B64D2013/0666

  with means for preventing icing within the ECS components · CPC title

• F28D2021/0021

  for aircrafts or cosmonautics · CPC title

• F28F27/02 Primary

  for controlling the distribution of heat-exchange media between different channels ({static flow control means in header boxes F28F9/026}; arrangements of guide plates or guide vanes F28F9/22, F28F25/12) · CPC title

• F28F2250/06

  Derivation channels, e.g. bypass · CPC title

• B64D2013/0674

  comprising liquid subsystems · CPC title