Thermal management systems and methods

Patent metadata

Field	Value
Publication number	US-10399683-B2
Application number	US-201615044523-A
Country	US
Kind code	B2
Filing date	Feb 16, 2016
Priority date	Feb 16, 2016
Publication date	Sep 3, 2019
Grant date	Sep 3, 2019

Abstract

A thermal management system includes at least one vapor control system (VCS) that is configured to cool portions of the vehicle. The VCS circulates a fluid therethrough to cool the portions of the vehicle through heat exchange. At least one reverse air cycle machine (RACM) couples to VCS through a first heat exchanger. The RACM is configured to receive ram air. The RACM expands the ram air. Heat from the fluid circulating through the VCS is transferred to the expanded ram air through the first heat exchanger.

First claim

What is claimed is:

1. A thermal management system that is configured to cool portions of a vehicle, the thermal management system comprising:
at least one vapor control system (VCS) that is configured to cool the portions of the vehicle, wherein the at least one VCS circulates a refrigerant therethrough to cool the portions of the vehicle through heat exchange, wherein the at least one VCS comprises a VCS compressor that compresses the refrigerant;
at least one reverse air cycle machine (RACM) that couples to the at least one VCS through a first heat exchanger, wherein the at least one RACM is configured to receive ram air, wherein the at least one RACM expands the ram air, and wherein heat from the refrigerant circulating through the at least one VCS after being compressed by the VCS compressor is transferred to the ram air that is expanded through the first heat exchanger, wherein the at least one RACM comprises a RACM compressor and one or more RACM valves, the one or more RACM valves disposed within a heat transfer circuit that includes conduits connected to the first heat exchanger, wherein the RACM compressor compresses the ram air after the heat from the refrigerant is transferred to the ram air, and wherein the ram air is exhausted from the vehicle after the RACM compressor compresses the ram air, and
a control unit operatively coupled to the one or more RACM valves, wherein the control unit selectively operates the one or more RACM valves to control a flow of the ram air through the heat transfer circuit and the first heat exchanger for regulating a temperature of the portions of the vehicle that are cooled by the at least one VCS.

2. The thermal management system of claim 1 , wherein the at least one RACM comprises a turbine, wherein the ram air at least partially powers the turbine.

3. The thermal management system of claim 1 , wherein the thermal management system refrains from utilizing bleed air from an engine of the vehicle.

4. The thermal management system of claim 1 , further comprising a second heat exchanger that couples the at least one VCS to a ram air conduit that connects to a ram air inlet, wherein heat from the refrigerant circulating through the at least one VCS is also transferred to the ram air flowing through the ram air conduit through the second heat exchanger.

5. The thermal management system of claim 1 , further comprising a second heat exchanger that couples the at least one VCS to a fuel line that connects a fuel tank to an engine of the vehicle, wherein heat from the refrigerant circulating through the at least one VCS is also transferred to fuel flowing through the fuel line through the second heat exchanger.

6. The thermal management system of claim 1 , wherein the at least one VCS comprises at least two parallel VCS.

7. The thermal management system of claim 1 , wherein the at least one RACM comprises at least two parallel RACMs.

8. The thermal management system of claim 1 , wherein the at least one VCS comprises one or more VCS valves, and the control unit is configured to selectively operate the one or more VCS valves to control a flow of the refrigerant through the at least one VCS.

9. A thermal management method of cooling portions of a vehicle, the thermal management method comprising:
cooling the portions of the vehicle with at least one vapor control system (VCS), wherein the cooling operation comprises circulating a refrigerant through the at least one VCS to cool the portions of the vehicle through heat exchange and compressing the refrigerant using a compressor of the at least one VCS;
receiving ram air with at least one reverse air cycle machine (RACM) that couples to the at least one VCS through a first heat exchanger, the at least one RACM including a compressor and one or more RACM valves, the one or more RACM valves disposed within a heat transfer circuit that includes conduits connected to the first heat exchanger;
expanding the ram air with the at least one RACM;
controlling a flow of the ram air, that is expanded, through the heat transfer circuit by selectively operating, via a control unit, the one or more RACM valves to regulate a temperature of the portions of the vehicle cooled by the at least one VCS;
transferring heat from the refrigerant circulating through the at least one VCS to the ram air, that is expanded, through the first heat exchanger;
using the compressor of the at least one RACM to compress the ram air after the heat from the compressed refrigerant is transferred to the ram air; and
exhausting the ram air from the vehicle after the compressor of the at least one RACM compresses the ram air.

10. The thermal management method of claim 9 , further comprising at least partially powering a turbine of the at least one RACM with the received ram air.

11. The thermal management method of claim 9 , further comprising using a second heat exchanger to transfer heat from the compressed refrigerant circulating through the at least one VCS to ram air within a conduit that connects to a ram air inlet.

12. The thermal management method of claim 9 , further comprising using a second heat exchanger to transfer heat from the compressed refrigerant circulating through the at least one VCS to fuel flowing through a fuel line.

13. The thermal management method of claim 9 , further comprising:
controlling a flow of the refrigerant through the at least one VCS by selectively operating, via the control unit, one or more VCS valves.

14. An aircraft comprising:
a fuselage defining one or more internal compartments;
wings extending from the fuselage;
an empennage extending from the fuselage;
one or more engines secured to one or more of the wings, the fuselage, or the empennage;
a fuel line that connects a fuel tank to an engine of the aircraft;
one or more electronic sub-systems; and
a thermal management system that cools a cabin or a load of the aircraft without using bleed air from the one or more engines, the thermal management system comprising:
at least one vapor control system (VCS) that circulates a refrigerant therethrough to cool the cabin or the load of the aircraft through heat exchange, wherein the at least one VCS comprises a VCS compressor that compresses the refrigerant;
at least one reverse air cycle machine (RACM) that couples to the at least one VCS through a first heat exchanger, wherein the at least one RACM receives ram air generated by motion of the aircraft, wherein the at least one RACM comprises a turbine, a RACM compressor, and one or more RACM valves, the one or more RACM valves disposed within a heat transfer circuit that includes conduits connected to the first heat exchanger, wherein the turbine expands the ram air and is at least partially powered by the ram air, and wherein heat from the refrigerant circulating through the at least one VCS is transferred within the first heat exchanger to the ram air that is expanded, wherein the RACM compressor compresses the ram air after the heat from the refrigerant is transferred to the ram air, and wherein the ram air is exhausted from the aircraft after the RACM compressor compresses the ram air;
a second heat exchanger that couples the at least one VCS to a ram air conduit that connects to a ram air inlet, wherein heat from the refrigerant circulating through the at least one VCS is transferred within the second heat exchanger to the ram air flowing through the ram air conduit;
a third heat exchanger that couples the at least one VCS to the fuel line, wherein heat from the refrigerant circulating through the at least one VCS is transferred within the third heat exchanger to fuel flowing through the fuel

Assignees

• Boeing Co

Inventors

• Behrens William Webster
• Tucker Andrew Richard

Classifications

• B64D2013/064

  comprising more than one system, e.g. dual systems · CPC title

• F02C6/08

  the gas being bled from the gas-turbine compressor · CPC title

• B64D2013/0674

  comprising liquid subsystems · CPC title

• B64D37/34

  Conditioning fuel, e.g. heating (during filling B64D37/18) · CPC title

• B64D13/06 Primary

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