Thermal management system for future vertical lift aircraft

Patent metadata

Field	Value
Publication number	US-12552541-B2
Application number	US-202318506775-A
Country	US
Kind code	B2
Filing date	Nov 10, 2023
Priority date	Nov 10, 2023
Publication date	Feb 17, 2026
Grant date	Feb 17, 2026

Abstract

A thermal management system for an aircraft includes a liquid loop, a vapor compression cycle loop, and an air loop. The liquid loop includes a pump to deliver a working fluid a cold sink for cooling a heat load with the working fluid. The vapor compression cycle loop is fluidly coupled to the liquid loop by a separator. The separator is configured to separate a two-phase form of the working fluid into a vapor form of the working fluid for delivery to a compressor of the vapor compression cycle loop and a liquid form of the working fluid for delivery to the liquid loop. The air loop in thermal communication with the working fluid and configured to provide cooling or heating air for an aircraft cabin.

First claim

The invention claimed is:

1 . A thermal management system for an aircraft, the thermal management system comprising:
a liquid loop comprising:
a pump to deliver a working fluid; and
a cold sink for cooling a heat load with the working fluid;
a vapor compression cycle loop fluidly coupled to the liquid loop by a separator, the separator configured to separate a two-phase form of the working fluid into a vapor form of the working fluid for delivery to a compressor of the vapor compression cycle loop and a liquid form of the working fluid for delivery to the liquid loop; and an air loop in thermal communication with the working fluid and configured to provide cooling or heating air for an aircraft cabin.

2 . The thermal management system of claim 1 , wherein the vapor compression cycle loop comprises:
a first heat exchanger configured to be fluidly coupled to the compressor in a first mode of operation; and a second heat exchanger configured to be fluidly coupled to the compressor in a second mode of operation, wherein the second heat exchanger is disposed to place the working fluid in thermal communication with the air loop.

3 . The thermal management system of claim 2 and further comprising:
a first valved fluid line configured to operatively couple the compressor to the first heat exchanger; and
a second valved fluid line configured to operatively couple the compressor to the second heat exchanger.

4 . The thermal management system of claim 3 , wherein the first mode of operation is a cooling mode and the second mode of operation is a heating mode; and
wherein the first valved fluid line is configured to be open to flow of the working fluid and the second valved fluid line is configured to be closed to flow of the working fluid in a cooling mode of operation; and wherein the second valved fluid line is configured to be open to flow of the working fluid and the first valved fluid line is configured to be closed to flow of the working fluid in a heating mode of operation.

5 . The thermal management system of claim 4 , wherein the first heat exchanger is configured to function as a condenser in the cooling mode of operation and the second heat exchanger is configured to function as an evaporator in the cooling mode of operation.

6 . The thermal management system of claim 5 , wherein the vapor compression cycle loop is configured, in the cooling mode of operation, to deliver the working fluid from the separator to the compressor, to the first heat exchanger, to an expansion valve, to the second heat exchanger, and back to the separator.

7 . The thermal management system of claim 4 , wherein the first heat exchanger is configured to function as an evaporator in the heating mode of operation and the second heat exchanger is configured to function as a condenser in the heating mode of operation.

8 . The thermal management system of claim 7 , wherein the vapor compression cycle loop is configured, in the heating mode of operation, to deliver the working fluid from the separator to the compressor, to the second heat exchanger, to an expansion valve, to the first heat exchanger, and back to the separator.

9 . The thermal management system of claim 7 , and further comprising a third valved fluid line configured to fluidly connect the cold sink of the liquid loop to the separator and a fourth valved fluid line configured to connect the cold sink to the second heat exchanger.

10 . The thermal management system of claim 9 , wherein the third valved fluid line is open and the fourth valved fluid line is closed during each of the cooling mode of operation and the heating mode of operation.

11 . The thermal management system of claim 10 , wherein the third valved fluid line is closed and the fourth valved fluid line is open during an alternate heating mode of operation.

12 . The thermal management system of claim 11 , wherein the compressor is off during the alternate heating mode of operation.

13 . The thermal management system of claim 4 , wherein each of the first valved fluid line and the second valved fluid line comprises a three-way electronically controlled switchable valve.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Mandel Raphael
• Turney Joseph E
• Ranjan Ram
• Pess Matthew L

Classifications

• F25B2400/0411

  for expansion valves or capillary tubes · CPC title

• F25B2400/23

  Separators · CPC title

• F25B41/42

  Arrangements for diverging or converging flows, e.g. branch lines or junctions · CPC title

• F25B2400/0409

  for evaporators · CPC title

• F25B2400/0403

  for condensers · CPC title