Environmental control system with ejector-enhanced cooling

Patent metadata

Field	Value
Publication number	US-10408501-B2
Application number	US-201615386161-A
Country	US
Kind code	B2
Filing date	Dec 21, 2016
Priority date	Dec 21, 2016
Publication date	Sep 10, 2019
Grant date	Sep 10, 2019

Abstract

An environmental control system includes a primary heat exchanger operable to transfer heat from an air source to a refrigerant in a generator flow and output an air flow. An ejector is operable to produce an intermediate refrigerant flow based on receiving the generator flow as a motive fluid and drawing a vapor refrigerant flow as a suction fluid. A refrigerant condenser is operable to convert the intermediate refrigerant flow to a liquid refrigerant flow. A pump is operable to provide the refrigerant to the primary heat exchanger from a portion of the liquid refrigerant flow. An expansion device is operable to expand the liquid refrigerant flow prior to entering an evaporator. The evaporator is operable to convert the liquid refrigerant flow to the vapor refrigerant flow and produce a cooled evaporator air flow output based on the air flow.

First claim

What is claimed is:

1. An environmental control system for an aircraft, the environmental control system comprising:
a primary heat exchanger operable to transfer heat from an air source to a refrigerant in a generator flow and output an air flow;
an ejector in fluid communication with the primary heat exchanger and operable to produce an intermediate refrigerant flow based on receiving the generator flow as a motive fluid and drawing a vapor refrigerant flow as a suction fluid;
a refrigerant condenser in fluid communication with the ejector and operable to convert the intermediate refrigerant flow to a liquid refrigerant flow;
a pump operable to provide the refrigerant to the primary heat exchanger from a portion of the liquid refrigerant flow;
an expansion valve in fluid communication with the refrigerant condenser and an evaporator and operable to expand the liquid refrigerant flow prior to entering the evaporator; the evaporator in fluid communication with the ejector and the refrigerant condenser and operable to convert the liquid refrigerant flow to the vapor refrigerant flow and produce a cooled evaporator air flow output based on the air flow;
a turbine operable to produce a cooled air output based on the cooled evaporator air flow output, wherein the turbine is further operable to drive one or more ram air fans and/or an air compressor;
a second ejector, a second pump, a second expansion valve, and a second turbine, wherein a first refrigerant ejector cycle is formed between the primary heat exchanger, the ejector, a first section of the refrigerant condenser, the pump, the expansion valve, and the evaporator, and a second refrigerant ejector cycle is formed between the primary heat exchanger, the second ejector, a second section of the refrigerant condenser, the second pump, the second expansion valve, and the evaporator, and further wherein the turbine and the second turbine are configured to produce the cooled air output based on the cooled evaporator air flow output; and
a mixer operable to combine the cooled air output with a recirculated air flow to produce a supply air flow for the aircraft.

2. The environmental control system as in claim 1 , further comprising a secondary heat exchanger operable to cool the air flow prior to reaching the evaporator.

3. The environmental control system as in claim 2 , wherein a ram air flow is divided between the refrigerant condenser and the secondary heat exchanger.

4. The environmental control system as in claim 3 , further comprising a compressor operable to compress a portion of the ram air flow to produce the air source.

5. The environmental control system as in claim 2 , wherein a ram air flow received at the refrigerant condenser is passed in series to the secondary heat exchanger.

6. The environmental control system as in claim 1 , further comprising a pre-cooler operable to supply the air source to the primary heat exchanger as pre-cooled based on a ram air flow received at the refrigerant condenser and passed to the pre-cooler.

7. The environmental control system as in claim 1 , wherein a condensate is removed from the evaporator and moisture is selectively added to the air flow.

8. The environmental control system as in claim 1 , further comprising a moisture condenser in fluid communication with the evaporator and the turbine and operable to remove a condensate from the cooled evaporator air flow output.

9. A method of environmental control for an aircraft, the method comprising:
transferring heat in a primary heat exchanger from an air source to a refrigerant in a generator flow and outputting an air flow;
producing an intermediate refrigerant flow based on receiving the generator flow as a motive fluid and drawing a vapor refrigerant flow as a suction fluid by an ejector in fluid communication with the primary heat exchanger;
converting the intermediate refrigerant flow to a liquid refrigerant flow by a refrigerant condenser in fluid communication with the ejector;
providing the refrigerant to the primary heat exchanger at higher pressure from a portion of the liquid refrigerant flow by a pump;
expanding, by an expansion valve in fluid communication with the refrigerant condenser and an evaporator, the liquid refrigerant flow prior to entering the evaporator;
converting the liquid refrigerant flow to the vapor refrigerant flow by the evaporator in fluid communication with the ejector and the refrigerant condenser, and producing a cooled evaporator air flow output based on the air flow;
producing, by a turbine, a cooled air output based on the cooled evaporator air flow output, wherein a first refrigerant ejector cycle is formed between the primary heat exchanger, the ejector, a first section of the refrigerant condenser, the pump, the expansion valve, and the evaporator, and a second refrigerant ejector cycle is formed between the primary heat exchanger, a second ejector, a second section of the refrigerant condenser, a second pump, a second expansion valve, and the evaporator, and further wherein the turbine and a second turbine are configured to produce the cooled air output based on the cooled evaporator air flow output; and
combining the cooled air output with a recirculated air flow at a mixer to produce a supply air flow for the aircraft.

10. The method as in claim 9 , further comprising:
cooling, by a secondary heat exchanger, the air flow prior to reaching the evaporator.

11. The method as in claim 10 , further comprising:
dividing a ram air flow between the refrigerant condenser and the secondary heat exchanger.

12. The method as in claim 11 , further comprising:
compressing a portion of the ram air flow to produce the air source.

13. The method as in claim 10 , further comprising:
passing a ram air flow received at the refrigerant condenser in series to the secondary heat exchanger.

14. The method as in claim 9 , further comprising:
supplying the air source from a pre-cooler to the primary heat exchanger as pre-cooled based on a ram air flow received at the refrigerant condenser passed to the pre-cooler.

15. The method as in claim 9 , further comprising:
removing a condensate from the evaporator;
using condensate for evaporative precooling of ram air; and
selectively adding moisture to the air flow as needed.

16. The method as in claim 9 , further comprising:
removing a condensate from the cooled evaporator air flow output by a moisture condenser in fluid communication with the evaporator and the turbine.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Elsherbini Abdelrahman I
• St Rock Brian

Classifications

• F25B5/02

  arranged in parallel · CPC title

• B64D2013/0618

  with arrangements for reducing or managing bleed air, using another air source, e.g. ram air · CPC title

• B64D2013/0688

  with means for recirculating cabin air · CPC title

• B64D13/06

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

• B64D2013/0674

  comprising liquid subsystems · CPC title