FLASH TANK ELIMINATOR
A flash tank for use in a vapor compression system includes a flash tank housing, an inlet, a vapor outlet, a liquid outlet, and an eliminator. The eliminator is fluidically positioned between the inlet and the vapor outlet. The eliminator includes either a plurality of blades or a piccolo tube connected to the vapor outlet.
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The present invention relates to vapor compression systems, and in particular, to a flash tank for use in a vapor compression system.
Vapor compression systems commonly compress and expand a refrigerant for use in refrigeration applications. Some vapor compression systems make use of a flash tank. As liquid refrigerant passes through an orifice or valve into a relatively low pressure flash tank, the liquid refrigerant flashes into a combination of liquid and gaseous or vapor refrigerant. Some flash tanks have both a liquid outlet and a vapor outlet. It can be undesirable to flow refrigerant in the wrong phase through the wrong outlet. For example, flowing liquid refrigerant through the vapor outlet can increase power consumption and reduce cooling performance of the vapor compression system.
SUMMARYAccording to the present invention, a flash tank for use in a vapor compression system includes a flash tank housing, an inlet, a vapor outlet, a liquid outlet, and an eliminator. The eliminator is fluidically positioned between the inlet and the vapor outlet. The eliminator includes either a plurality of blades or a piccolo tube connected to the vapor outlet.
Another embodiment of the present invention is a method for operating a vapor compression system. The method includes flowing refrigerant from a condenser to a flash tank, separating liquid refrigerant from vapor refrigerant via an eliminator that includes a plurality of blades, flowing vapor refrigerant from the eliminator through a vapor outlet to a compressor, and flowing liquid refrigerant from the eliminator, through a liquid outlet, to an evaporator.
Liquid refrigerant in flash tank 12 flows through passage 20A to evaporator 14, where the refrigerant is heated and evaporated into a vapor. The vapor refrigerant then flows from evaporator 14 through passage 20B to compressor 16 for the cycle to be repeated. In the illustrated embodiment, thermal expansion valve (TXV) 32 is positioned along passage 20A. TXV 32 is controlled according to inputs received from temperature sensor 34 and pressure sensor 36. Suction pressure regulation valve 38 is positioned along passage 20B. Suction pressure regulation valve 38 can be substantially adjacent to an inlet to compressor 16 and can be part of a common assembly with compressor 16. TXV 32 and suction pressure regulation valve 38 are actuated to control the pressure and temperature of refrigerant leaving evaporator 14 and entering compressor 16. In an alternative embodiment, TXV 32 can be replaced with an electronic expansion valve (EXV), and suction pressure regulation valve 38 can be omitted.
Vapor refrigerant in flash tank 12 flows through passage 20F to economizer port 40 of compressor 16. Flash tank pressurization valve 42 is positioned along passage 20F to control pressure in flash tank 12. Thus, compressor 16 is connected to and receives a flow of vapor refrigerant both from flash tank 12 and from evaporator 14.
Quench trap 44 is positioned along passage 20D between condenser 18 and flash tank 12. Compressor over-temp valve 46 is positioned along passage 20E, which connects passage 20D to passage 20F. When temperature of compressor 16 is sensed to exceed a threshold, compressor over-temp valve 46 can be actuated to supply cooled liquid refrigerant from quench trap 44, through passages 20E and 20F, and to economizer port 40 of compressor 16 to cool compressor 16. During normal operation, compressor over-temp valve 46 can remain substantially closed.
Condenser 18 is a heat exchanger connected to coolant loop 48, which is connected to power electronics cooling system (PECS) 50 of an aircraft (not shown). This allows PECS 50 to cool the refrigerant in condenser 18 of SCU 10.
Evaporator 14 is a heat exchanger connected to coolant loop 52, which is connected to integrated cooling system (ICS) 54 of the aircraft. Integrated cooling system 54 includes one or more aircraft systems that require cooling, such as a galley refrigeration system and a cabin air temperature control system. This allows SCU 12 to cool coolant of ICS 54 in evaporator 14.
Droplets or a mist of liquid refrigerant can be entrained in the vapor refrigerant flowing through eliminator 70. Eliminator 70 separates the liquid refrigerant from the vapor refrigerant by collecting the droplets of liquid refrigerant, which adheres to blades 74. The liquid refrigerant that adheres to blades 74 then flows down blades 74 toward bottom support 78, and then drips from bottom support 78 to collect at bottom 60 of flash tank 12. Vapor refrigerant flows through vapor outlet 64.
In further alternative embodiments, eliminators 70, 170, and 270 can have blades 74, 174, and 274 arranged in alternative shapes, such as an arc.
Thus, the various embodiments of eliminators 70, 170, 270, 370, and 470 provide effective and reliable mechanisms for separating liquid refrigerant from vapor refrigerant in flash tanks 12, 112, and 212. This allows for a reduction in the amount of liquid refrigerant supplied to economizer port 40 of compressor 16, thus increasing efficiency and reducing power consumption of compressor 16.
While the invention has been described with reference to exemplary embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Therefore, it is intended that the invention not be limited to the particular embodiments disclosed, but that the invention will include all embodiments falling within the scope of the appended claims. For example, flash tank 12 can be part of a vapor compression system having different components than those illustrated in
Claims
1. A flash tank for use in a vapor compression system, the flash tank comprising:
- a flash tank housing;
- an inlet;
- a vapor outlet;
- a liquid outlet; and
- an eliminator fluidically positioned between the inlet and the vapor outlet, wherein the eliminator comprises a plurality of blades.
2. The flash tank of claim 1, and further comprising:
- a condenser fluidically connected to the inlet;
- a compressor fluidically connected to the vapor outlet; and
- an evaporator fluidically connected to the liquid outlet.
3. The flash tank of claim 2, wherein the compressor is fluidically connected to the flash tank via a first passage, fluidically connected to the evaporator via a second passage, and connected to the condenser via a third passage.
4. The flash tank of claim 1, and further comprising:
- a piccolo tube connected to the inlet.
5. The flash tank of claim 1, wherein the flash tank housing has a top and a bottom, wherein the inlet and the vapor outlet are each positioned at the top, and wherein the liquid outlet is positioned at the bottom.
6. The flash tank of claim 5, wherein the inlet and the liquid outlet are positioned on a first side of the eliminator and the vapor outlet is positioned on a second side of the eliminator.
7. The flash tank of claim 1, wherein the plurality of blades are substantially vertically aligned between a top support and a bottom support.
8. The flash tank of claim 1, wherein each of the plurality of blades has at least one bend such that a flow path between the blades has at least one turn.
9. The flash tank of claim 1, wherein each of the plurality of blades has at least two bends such that a flow path between the blades has at least two turns.
10. The flash tank of claim 1, wherein the plurality of blades are spaced such that there is no straight line flow path from the inlet to the vapor outlet.
11. The flash tank of claim 1, wherein the plurality of blades are arranged in a single linear row.
12. The flash tank of claim 1, wherein the plurality of blades are arranged in at least a first linear row and a second linear angled with respect to the first linear row.
13. A flash tank for use in a vapor compression system, the flash tank comprising:
- a flash tank housing;
- an inlet;
- a vapor outlet;
- a liquid outlet; and
- an eliminator fluidically positioned between the inlet and the vapor outlet, wherein the eliminator comprises a first piccolo tube connected to the vapor outlet.
14. The flash tank of claim 13, and further comprising:
- a second piccolo tube connected to the inlet.
15. The flash tank of claim 14, wherein the flash tank housing has a top and a bottom, wherein the first and second piccolo tubes are each positioned at the top, and wherein the liquid outlet is positioned at the bottom.
16. The flash tank of claim 14, and further comprising:
- a fitting rigidly connected to the first and second piccolo tubes, wherein the inlet is a fitting inlet, wherein the vapor outlet is a fitting outlet, and wherein the fitting has a fitting interface for connecting to the flash tank housing.
17. A method for operating a vapor compression system, the method comprising:
- flowing refrigerant from a condenser to a flash tank;
- separating liquid refrigerant from vapor refrigerant via an eliminator that comprises a plurality of blades;
- flowing vapor refrigerant from the eliminator through a vapor outlet, to a compressor; and
- flowing liquid refrigerant from the eliminator, through a liquid outlet, to an evaporator.
18. The method of claim 17, and further comprising:
- flowing refrigerant from the evaporator to the compressor; and
- flowing refrigerant from the compressor to the condenser.
19. The method of claim 17, wherein the liquid refrigerant adheres to the plurality of blades as it passes through channels between the plurality of blades and subsequently flows down the plurality of blades to collect at a bottom of the flash tank.
20. The method of claim 17, and further comprising:
- cooling the refrigerant in the condenser via coolant of an aircraft power electronics cooling system; and
- cooling coolant of an aircraft integrated cooling system via refrigerant in the evaporator.
Type: Application
Filed: Mar 30, 2012
Publication Date: Oct 3, 2013
Applicant: Hamilton Sundstrand Corporation (Windsor Locks, CT)
Inventor: Sung-Han Jung (Glastonbury, CT)
Application Number: 13/435,399
International Classification: F25B 1/00 (20060101); F25D 11/00 (20060101);