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US2931190A - Jet refrigeration system - Google Patents

Jet refrigeration system Download PDF

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US2931190A
US2931190A US662360A US66236057A US2931190A US 2931190 A US2931190 A US 2931190A US 662360 A US662360 A US 662360A US 66236057 A US66236057 A US 66236057A US 2931190 A US2931190 A US 2931190A
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fluid
motive fluid
jet
heat
refrigerant
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Dubitzky Michael
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Coleman Co Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B1/00Compression machines, plants or systems with non-reversible cycle
    • F25B1/06Compression machines, plants or systems with non-reversible cycle with compressor of jet type, e.g. using liquid under pressure
    • F25B1/08Compression machines, plants or systems with non-reversible cycle with compressor of jet type, e.g. using liquid under pressure using vapour under pressure
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2341/00Details of ejectors not being used as compression device; Details of flow restrictors or expansion valves
    • F25B2341/001Ejectors not being used as compression device
    • F25B2341/0015Ejectors not being used as compression device using two or more ejectors

Definitions

  • a refrigeration system employing jet pumps in a heatoperated cycle possesses a distinct advantage over conventional refrigeration systems in being able to operate without the need for electrical power. Further, such refrigeration systems operate noiselessly and can be provided through the use of relatively simple equipment and at low cost.
  • the jet, heat-operated refrigeration systems heretofore available have been characterized by an unacceptably low efliciency, or, more precisely, coeflicient of performance.
  • the coeflicient of performance of a refrigeration system (hereinafter designated COP) is defined as the ratio of effective refrigeration to the total heat energy input.
  • COP coeflicient of performance of a refrigeration system
  • a much investigated fluid jet refrigeration system employed the use of steam as the fluid.
  • the factor of low efliciency referred to above is particularly applicable to steam jet refrigeration which, at normal air conditioning temperatures, has a COP of about 0.25 to about 0.35. Even advances in the design of ejectors (jet pumps) have not contributed significantly to the achievement of higher COPs.
  • the binary jet refrigeration cycle employing this invention has two fluids to accomplish the cooling efiect atent by means of heat.
  • the primary or motive fluid acts very much like steam in a power plant: emerges from a boiler as a vapor at high temperature and pressure, expands in an ejector to a lower pressure and temperature, and after it is condensed by external means, it is pumped and fed back to the boiler.
  • the refrigeration or secondary fluid goes through a conventional vapor refrigeration cycle of expansion, evaporation, compression, and condensationexcept that it is compressed in the ejector by the expanding motive fluid.
  • Such a fluid jet refrigeration system employing two fluids operates between three temperatures: the boiler temperature, the condensing temperature, and the refrigerant evaporating temperature.
  • the two latter temperatures are defined by the application.
  • the refrigerant evaporating temperature depends upon the level at which refrigeration is desired. In air conditioning, for example, this level normally is between 35 and 45 F.
  • the condensing temperature depends upon the external cooling means available, and is generally between and F. for water-cooled units, and between and F. for air-cooled units.
  • the boiler temperature is somewhat more flexible, but is subject to the practical limitations of materials used and boiler efliciency desired. A temperature of about 500 F. is usually found reasonable.
  • FIG. 1 is a flow diagram showing a fluid jet refrigeration cycle having two boilers and two heat-exchangers
  • Fig. 2 is a flow diagram showing a fluid jet refrigeration cycle having one boiler and one heat-exchanger
  • Fig. 3 is a representation of the thermodynamic cycle for a typical motive fluid of this invention.
  • Figs. 1 and 2 are typical of cycles which may be used to embody the process of this invention.
  • Figs. 1 and 2 differ in the number of boilers and heat exchangers used.
  • Fig. 1 shows a boiler and a. heat exchanger for each jetpump, while
  • Fig. 2 shows one boiler and one heat exchanger serving both jet pumpsl
  • a separator 10 in which the motive fluid and refrigerant are physically separated by gravity or other means as indicated hereinafter. From this separator 10, each of the fluids is drawn off to enter its own part of the cycle. The following description will trace first the refrigerant and then the motive fluid, for the sake of simplicity.
  • the refrigerant is taken from separator 10 by means of conduit 11 which contains expansion valve 12 into the evaporator 13, and out ofthe evaporator by means of conduit 14 to the jet pump 15.
  • the motive fluid moving into the jet pump 15 draws the refrigerant into the jet pump where it is compressed and mixed with the motive fluid at an elevated temperature.
  • conduit 16 the refrigerant and mo'-' tive fluid are led into heat exchanger 17, where the sensible heat of the motive fluid is transferred by out-of-contact heat exchange means to the compressed motive fluid just prior to the latters entering boiler 31.
  • the mixtures of refrigerant and motive fluid is led out by line 18 to be drawn into jet pump 19.
  • additional compression is achieved and additional heat transfer takes place between the motive.
  • fluid and refrigerant both in the fluid mixture and in heat exchanger 21 which is comparable to heat exchanger 17.
  • Conduit 22 leads the fluid mixture into condenser 23 where the fluids are liquefied and subsequently returned by means of line 24 to separator 10.
  • the motive fluid is drawn as by line 25 to pump 26 where it is compressed and simultaneously heated.
  • conduit 27 the compressed and heated motive fluid is passed through distributor valve 28 which directs a portion of the motive fluid into ledby, conduit 30 toboiler 31where it isvaporizedby;
  • Pig. 2 illustrates one possible scheme in which one boilerand-one heat exchanger may be used to serve the two'jet pumps.
  • the motive fluid andrefrigerant goingi to jet pump :15 in the same manner.
  • the vaporized. motive fluid enters-jet pump 15, and with the refrigerant is compressed, led out by line 115 and passed through heat exchanger 41 where it gives up part of its; sensible heat to the motive fluid before the latter enters boiler 43..
  • the mixture of motive fluid and refrigerant passes to the second jet pump 19 by way of line 18; An.
  • auxiliary cooler 0-rnay be placed in line 18 to cool the mixture before it enters jet pump 19 to reduce the work of compression. Cooling fluid, such as water, may be introduced into auxiliary cooler 50 by means of line 51. The compressed fluid. mixture from jet pump 19 leaves by line 20, passes throughheat exchanger 41, and then enters coudenser 23 .as in .Fig, 1..
  • The. motive fluid. leaving heat exchanger. 41 is led by line.v 42 into boiler. 43. Heat is supplied to boiler 43 by means of burner 44 fed by fuel line 45. After being vaporizedin boiler 43, the motive fluid goes. by line 46 to a distributingvalve 47 where the stream is split, half going by line 48 into jet pump 15, and half going by line 49 to jet pump 19.
  • Figs.- 1 audit illustrate the separation of the motivefluid and refrigerant by gravitational means
  • other ways of physically separating them may be used, such ascentrifuging, etc.
  • the two fluids should possess difle'rent densities for ease of separation.
  • Thejet pumps 15 and. 19 are of any suitable. type known in the art.
  • Pump 26 may be a conventional posifive-displacement type, or may be a liquid jet injector type.
  • Thexefrigerantfluid being water, had a lesser density than the; motive fluid. andiformed the top layer in sepalrator; Water, drawn from separator 10 at about 100 F? and-1.0 p.s.i.a-.-, was expanded in valvelz to 40 F;
  • the motive fluid was simultaneously drawn off the bottom portion of separator 10, raised to 150 p.s.i.a. by pump 26, and directed into boilers 31 and by way of heat exchangers 17 and 21.
  • vaporized motive fluid passed into and through jet pumps 15 and 19, it drew water vapor from conduit 14 and water vaporc F O mixture from conduit 18-into the The fluid mixtures were compressed in the jet pumps.
  • the 100 F. and a pressure of 0.3 p.s.i;a. in conduit 185 The mixture then passed through condenser 23 and, after leaving condenser 23, was a liquid mixture having a temperature of 100 F. and 1.0 p.s.i.a. Thereafter, the mixture returned to a separator at essentially the same temperature and pressure.
  • the coeflicient of performance in the example given was about 0.7, which compares favorablywith an average of about 0.3 for steam jet pump refrigeration systems.
  • the latent heat per. unit of weight is relatively low.
  • the sensible heat. is high and affords recoverable heat for heating the mo tivefluid entering the boiler. Thus, where the amount.
  • Fig. 3 there'is illustrated a thermodynamic chart of a typical motive fluid of this invention, such a cyclic.
  • ABCDEF represents the output of the cycle
  • area HABCDEGK represents the energy input to the. cycle.
  • the motive fluid employed additionally possessedv the desirable characteristics of being nontoxic, noninfl'ammable, and noncorrosive to metallic equipment.
  • Other motive fluids possessing analogous characteristics can be employed satisfactorily, such as compounds related to the particular motive fluid employed here.
  • Such compounds may have the empirical formula 0 (CFz) mCE(CFa) nCFS where m is an integer of 3-4 and n is an integer such that the total number of carbon atoms is in the range 6-10;
  • the refrigerant fluid which, in the example given, was wa:- ter.
  • Water is considered desirable as a refrigerant fluid, since it is nonreactive and immiscible with the motive fluid and possesses a substantially different density to make the separation therebetween expeditious. I have-found it further desirable that the two fluids have approximately identical-boiling pressuresat the condensing. (ambient) fluid mixture had a temperature'of" In the case of most temperature, and that they both may be vaporized at temperatures and pressures within the range of conditions readily permissible in present-day equipment.
  • Water and other low molecular weight, low-boiling liquids such as methanol, ethanol, and ammonia, are considered highly desirable for use as refrigerant fluids.
  • Use of a low molecular weight refrigerant fluid such as water aids in obtaining of the high and desirable COPs characteristic of the system of my invention.
  • a method of furnishing refrigeration comprising separating a liquified refrigerant and a liquified motive fluid, the motive fluid being a cyclic fluorocarbon ether having the formula 0 (CFr) mCF(CF1)nCF;
  • n is an integer such that the total number of carbon atoms is from 6 to 10, evaporating said refrigerant to provide refrigeration, reuniting said refrigerant and said motive fluid in a jet pump, previous to said reunion passing said motive fluid through heat exchange means and boiler means, passing said united refrigerant and motive fluid through's'aid heat exchange means and through condenser means, and returning said united refrigerant and motive fluid to means for separating the same.
  • a method of furnishing refrigeration from a binary jet fluid system employing water as the refrigerant and a cyclic fluoroether' of the formula C F O as the motive fluid comprising compressing the said water in a jet pump in conjunction with the expansion of said cyclic fluoroether, condensing the mixture of said water and said fluoroether, separating the said mixture, evaporating the said water at sub-atmospheric pressure to provide refrigeration, heating the said cyclic ether, and reuniting said cyclic ether and said evaporated water for the compressing of said water.
  • a motive fluid into heat exchange relation with a source of heat
  • said motive fluid being a cyclic fluorocarbon ether having the formula 0 (CFa) n F(CF2)nCFI wherein m is an integer of from 3 to 4, and n is an integer such that the total number of carbon atoms is from 6 to 10
  • flowing said motive fluid from said source to a jet pump combining a refrigerant fluid with said motive fluid in said jet pump, and passing said combined fluids in heat exchange relation with said motive fluid prior to the flowing thereof into heat exchange relation with said source of heat.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Sorption Type Refrigeration Machines (AREA)

Description

April 5, 1960 M. DUBITZKY 2,931,190
JET REFRIGERATION SYSTEM Filed May 29, 1957 2 Sheets-Sheet l A TTORNEVS.
April 5, 1960 M. DUBITZKY JET REFRIGERATION SYSTEM 2 Sheets-Sheet 2 Filed May 29, 1957 I R m M E V Z W w w r w E m M R E i T T qv N M W m C m G K v, B Y w m m m m ME A H BM E wmDbxmwmiwk JET REFRIGERATION SYSTEM Michael Dubitzky, Stoneham, Mass., assignor, by mesne assignments, to The Coleman Company, Inc., Wichita, Kaus., a corporation of Kansas Application May 29, 1957, Serial No. 662,360 7 Claims. (Cl. 62-114) This invention relates to an improvement in refrigeration, and more particularly to an improvement in a fluid jet refrigeration system employing heat as a source of energy.
A refrigeration system employing jet pumps in a heatoperated cycle possesses a distinct advantage over conventional refrigeration systems in being able to operate without the need for electrical power. Further, such refrigeration systems operate noiselessly and can be provided through the use of relatively simple equipment and at low cost.
These advantages, particularly the freedom from the need for using electrical power, recommend the fluid jet refrigeration system for use in railway cars, trucks, small craft, and home air conditioning where gaseous or liquid fuel is relatively inexpensive.
' The jet, heat-operated refrigeration systems heretofore available have been characterized by an unacceptably low efliciency, or, more precisely, coeflicient of performance. The coeflicient of performance of a refrigeration system (hereinafter designated COP) is defined as the ratio of effective refrigeration to the total heat energy input. A much investigated fluid jet refrigeration system employed the use of steam as the fluid. The factor of low efliciency referred to above is particularly applicable to steam jet refrigeration which, at normal air conditioning temperatures, has a COP of about 0.25 to about 0.35. Even advances in the design of ejectors (jet pumps) have not contributed significantly to the achievement of higher COPs.
The fact that a good refrigerant does not make the good motive fluid needed in a fluid jet system and that a good motive fluid does not make up a good refrigerant, led workers in this field to suggest that the use of two fluids might improve the performance of a fluid jet refrigeration system. However, no two-fluid system has been advanced that meets the requirements of efliciency of many refrigeration systems, particularly those intended to be used for heat-operated air conditioning devices.
It is a general object of this invention to provide an improved fluid jet refrigeration system that overcomes the disadvantages and problems set forth above. Another object is to provide a heat-operated refrigeration cycle which has an efficiency superior to known heatoperated cycles. Yet another object is to provide a heat-operated refrigeration cycle which is competitive with conventional electricallywperated cycles. Still another object is to provide a heat-operated, fluid jet refrigeration cycle Which employs two different fluids. A still further object is to provide a refrigeration system capable of operating on gaseous or liquid fuels. Another object is to provide a heat-operated refrigeration system that is particularly useful in air conditioning applications. Other objects and advantages of my invention can be seen as this specification proceeds.
The binary jet refrigeration cycle employing this invention has two fluids to accomplish the cooling efiect atent by means of heat. The primary or motive fluid acts very much like steam in a power plant: emerges from a boiler as a vapor at high temperature and pressure, expands in an ejector to a lower pressure and temperature, and after it is condensed by external means, it is pumped and fed back to the boiler. The refrigeration or secondary fluid goes through a conventional vapor refrigeration cycle of expansion, evaporation, compression, and condensationexcept that it is compressed in the ejector by the expanding motive fluid.
Such a fluid jet refrigeration system employing two fluids operates between three temperatures: the boiler temperature, the condensing temperature, and the refrigerant evaporating temperature. The two latter temperatures are defined by the application. The refrigerant evaporating temperature depends upon the level at which refrigeration is desired. In air conditioning, for example, this level normally is between 35 and 45 F. The condensing temperature depends upon the external cooling means available, and is generally between and F. for water-cooled units, and between and F. for air-cooled units. The boiler temperature is somewhat more flexible, but is subject to the practical limitations of materials used and boiler efliciency desired. A temperature of about 500 F. is usually found reasonable.
My invention will be explained, in an illustrative embodiment, in conjunction with the accompanying drawings, in which- Figure 1 is a flow diagram showing a fluid jet refrigeration cycle having two boilers and two heat-exchangers; Fig. 2 is a flow diagram showing a fluid jet refrigeration cycle having one boiler and one heat-exchanger; and Fig. 3 is a representation of the thermodynamic cycle for a typical motive fluid of this invention.
The cycles illustrated in Figs. 1 and 2 are typical of cycles which may be used to embody the process of this invention. Figs. 1 and 2 differ in the number of boilers and heat exchangers used. Fig. 1 shows a boiler and a. heat exchanger for each jetpump, while Fig. 2 shows one boiler and one heat exchanger serving both jet pumpsl In Fig. 1 there is provided a separator 10 in which the motive fluid and refrigerant are physically separated by gravity or other means as indicated hereinafter. From this separator 10, each of the fluids is drawn off to enter its own part of the cycle. The following description will trace first the refrigerant and then the motive fluid, for the sake of simplicity. The refrigerant is taken from separator 10 by means of conduit 11 which contains expansion valve 12 into the evaporator 13, and out ofthe evaporator by means of conduit 14 to the jet pump 15. The motive fluid moving into the jet pump 15 draws the refrigerant into the jet pump where it is compressed and mixed with the motive fluid at an elevated temperature. By means of conduit 16 the refrigerant and mo'-' tive fluid are led into heat exchanger 17, where the sensible heat of the motive fluid is transferred by out-of-contact heat exchange means to the compressed motive fluid just prior to the latters entering boiler 31. 7 From heat exchanger 17 the mixtures of refrigerant and motive fluid is led out by line 18 to be drawn into jet pump 19. In jet pump 19, additional compression is achieved and additional heat transfer takes place between the motive. fluid and refrigerant both in the fluid mixture and in heat exchanger 21 which is comparable to heat exchanger 17. Conduit 22 leads the fluid mixture into condenser 23 where the fluids are liquefied and subsequently returned by means of line 24 to separator 10.
From separator 10 the motive fluid is drawn as by line 25 to pump 26 where it is compressed and simultaneously heated. By means of conduit 27 the compressed and heated motive fluid is passed through distributor valve 28 which directs a portion of the motive fluid into ledby, conduit 30 toboiler 31where it isvaporizedby;
heatrfurnishedit to'theboilerfrorn burner 37 feduby fuel-dine: 39, and passed by means of line '32to jet pump 15: The: remaining portionof the compressed motive fluid is directed by distributor valve 28-through line 33.-
toheat exchanger 21, and then by line 34- to boiler 35 (whereit is:vaporized by heat from burner'Sfl fed by fuel line 40), and conduit 36 to jet pump 19. Thus, the second portion. of motive fluid is subjected to treatment duplicating that through which the first portion passes; In jet pump .19 the remaining motive fluid enterst-the fluid mixture stream.
Pig. 2 illustrates one possible scheme in which one boilerand-one heat exchanger may be used to serve the two'jet pumps. As in'the case of the cycle shown in Big; 1, and described above, the motive fluid andrefrigerant goingi to jet pump :15 in the same manner. Likewise, the vaporized. motive fluid enters-jet pump 15, and with the refrigerant is compressed, led out by line 115 and passed through heat exchanger 41 where it gives up part of its; sensible heat to the motive fluid before the latter enters boiler 43.. After leaving heat exchanger 41, the mixture of motive fluid and refrigerant passes to the second jet pump 19 by way of line 18; An. auxiliary cooler 0-rnay be placed in line 18 to cool the mixture before it enters jet pump 19 to reduce the work of compression. Cooling fluid, such as water, may be introduced into auxiliary cooler 50 by means of line 51. The compressed fluid. mixture from jet pump 19 leaves by line 20, passes throughheat exchanger 41, and then enters coudenser 23 .as in .Fig, 1..
The. motive fluid. leaving heat exchanger. 41 is led by line.v 42 into boiler. 43. Heat is supplied to boiler 43 by means of burner 44 fed by fuel line 45. After being vaporizedin boiler 43, the motive fluid goes. by line 46 to a distributingvalve 47 where the stream is split, half going by line 48 into jet pump 15, and half going by line 49 to jet pump 19.
Although Figs.- 1 audit illustrate the separation of the motivefluid and refrigerant by gravitational means, other ways of physically separating them may be used, such ascentrifuging, etc. Preferably, the two fluids should possess difle'rent densities for ease of separation.
Thejet pumps 15 and. 19 are of any suitable. type known in the art. Pump 26 may be a conventional posifive-displacement type, or may be a liquid jet injector type.
Optimum results have been achieved when systems of the. character shown in Figs. 1 and 2 have been employed usingwater as the refrigerant fluid and a cyclic fluorocarbon ether havingthe formula C F O as the motive fliiidi This compound is described in U.S. Patent No.
2,644,823 issued July 7, 1953, and is commercially available under the trade name Fluorochernical 0-75 from the Minnesota Mining & Manufacturing Company, of St. Paul, Minnesota. An example of the operation of a fluid jet refrigeration system. using this binary mixture is set forth below.
Example "Ihemotive-fluid, as indicatedfabove, had the empirical formula C3F15O and. at room temperature was a colorless liquid. Its boiling-point was 101 (2., its density at 2'5f C. was 1.760. grams per cubic centimeter. The specific heat ratio of-this compound was slightly over 1.0, i.e., below 1.1.
Thexefrigerantfluid, being water, had a lesser density than the; motive fluid. andiformed the top layer in sepalrator; Water, drawn from separator 10 at about 100 F? and-1.0 p.s.i.a-.-, was expanded in valvelz to 40 F;
stream of the jet pumps.
and 0.12 p.s.i.a. The motive fluid was simultaneously drawn off the bottom portion of separator 10, raised to 150 p.s.i.a. by pump 26, and directed into boilers 31 and by way of heat exchangers 17 and 21. As vaporized motive fluid passed into and through jet pumps 15 and 19, it drew water vapor from conduit 14 and water vaporc F O mixture from conduit 18-into the The fluid mixtures were compressed in the jet pumps.
For example, the 100 F. and a pressure of 0.3 p.s.i;a. in conduit 185 The mixture then passed through condenser 23 and, after leaving condenser 23, was a liquid mixture having a temperature of 100 F. and 1.0 p.s.i.a. Thereafter, the mixture returned to a separator at essentially the same temperature and pressure. The coeflicient of performance in the example given was about 0.7, which compares favorablywith an average of about 0.3 for steam jet pump refrigeration systems.
I. have found that an important contribution to the: successful operation of a fluid jet refrigeration system.
is madeby the thermodynamic. characteristics of the motive. fluid C F O. Of particular importancein this.
connection is the above mentioned ratio of-specific heats which results in appreciable sensible heat in the vapor as well as in the liquid phase. fluids, the sensible heat is negligible compared to the latent heat. The sensible heat, in the example given, 15.
the product of the specific heat taken atconstant pressure and the temperature difference existingbetween the boiler temperature and the condenser temperature. How-- ever, thtis is not the case for the motive fluid described.
' above. Because of the relatively high molecular weight.
of thismotive fluid, the latent heat per. unit of weight is relatively low. On the other hand, the sensible heat. is high and affords recoverable heat for heating the mo tivefluid entering the boiler. Thus, where the amount.
of heat thus recovered is appreciable, a-very significant improvement in COP can be obtained with little orno,
increase in heat transfer surface. The heat requiredto be put into the boiler is decreased by the use of heat exchange surface, thereby improving the COP.
The effect of the considerable. amount of sensible heat displaced by this motive fluid is shown in Fig. 3. In Fig. 3, there'is illustrated a thermodynamic chart of a typical motive fluid of this invention, such a cyclic.
fluoroether of the formula C F O. In Fig. 3, the area.
ABCDEF represents the output of the cycle, while the area HABCDEGK represents the energy input to the. cycle. When the saturated vapor is expanded isentropically, there is created a highly superheated vapor having an appreciable amount of sensible heat represented by area JFDGK in Fig. 3.
The motive fluid employed additionally possessedv the desirable characteristics of being nontoxic, noninfl'ammable, and noncorrosive to metallic equipment. Other motive fluids possessing analogous characteristics can be employed satisfactorily, such as compounds related to the particular motive fluid employed here. Such compounds may have the empirical formula 0 (CFz) mCE(CFa) nCFS where m is an integer of 3-4 and n is an integer such that the total number of carbon atoms is in the range 6-10;
A significant contribution toward the achievement of the excellent results discussed. above was made by the refrigerant fluid, which, in the example given, was wa:- ter. Water is considered desirable as a refrigerant fluid, since it is nonreactive and immiscible with the motive fluid and possesses a substantially different density to make the separation therebetween expeditious. I have-found it further desirable that the two fluids have approximately identical-boiling pressuresat the condensing. (ambient) fluid mixture had a temperature'of" In the case of most temperature, and that they both may be vaporized at temperatures and pressures within the range of conditions readily permissible in present-day equipment. Water and other low molecular weight, low-boiling liquids such as methanol, ethanol, and ammonia, are considered highly desirable for use as refrigerant fluids. Use of a low molecular weight refrigerant fluid such as water aids in obtaining of the high and desirable COPs characteristic of the system of my invention.
I also have found that the achievement of excellent results is brought about by having the saturation pressure of the motive fluid at evaporating temperature much lower than the saturation pressure of the refrigerant fluid. This is achieved where the motive fluid possesses a high rate of change of vapor pressure with temperature.
While, in the foregoing specification, I have described at considerable length and in considerable detail certain specific embodiments of my invention, it will be understood that these embodiments are illustrative only and that many variations therein may be made by persons skilled in the art without departing from the spirit of my invention.
I claim:
1. A method of furnishing refrigeration, comprising separating a liquified refrigerant and a liquified motive fluid, the motive fluid being a cyclic fluorocarbon ether having the formula 0 (CFr) mCF(CF1)nCF;
wherein m is an integer of from about 3 to 4, and n is an integer such that the total number of carbon atoms is from 6 to 10, evaporating said refrigerant to provide refrigeration, reuniting said refrigerant and said motive fluid in a jet pump, previous to said reunion passing said motive fluid through heat exchange means and boiler means, passing said united refrigerant and motive fluid through's'aid heat exchange means and through condenser means, and returning said united refrigerant and motive fluid to means for separating the same.
2. A method according to claim 1, in which the said motive fluid is a' cyclic fluoroether of the formula CaFmO. a
3. A method of furnishing refrigeration from a binary jet fluid system employing water as the refrigerant and a cyclic fluoroether' of the formula C F O as the motive fluid, comprising compressing the said water in a jet pump in conjunction with the expansion of said cyclic fluoroether, condensing the mixture of said water and said fluoroether, separating the said mixture, evaporating the said water at sub-atmospheric pressure to provide refrigeration, heating the said cyclic ether, and reuniting said cyclic ether and said evaporated water for the compressing of said water.
4. A method according to claim 3, in which the temperature during condensing is less than about F., and the temperature during the step of evaporating is in the range of about 35-45 F.
5. A method of furnishing refrigeration from a binary jet fluid system employing a cyclic fluorocarbon ether having the formula wherein m is an integer of from about 3 to 4, and n is an integer such that the total number of carbon atoms is from 6 to 10, as the motive fluid and water as the refrigerant fluid, comprising compressing the refrigerant fluid in a jet pump in conjunction with the expansion of said cyclic fluorocarbon ether, condensing the mixture of said refrigerant fluid and said fluorocarbon ether, separating the said mixture, evaporating the said refrigerant fluid at sub-atmospheric pressure to provide refrigeration, heating the said cyclic fluorocarbon ether, and reuniting said cyclic fluorocarbon ether and said evaporated refrigerant fluid for compressing the said refrigerant fluid.
6. In a method of furnishing refrigeration employing a jet pump, the steps of flowing a motive fluid into heat exchange relation with a source of heat, said motive fluid being a cyclic fluorocarbon ether having the formula 0 (CFa) n F(CF2)nCFI wherein m is an integer of from 3 to 4, and n is an integer such that the total number of carbon atoms is from 6 to 10, flowing said motive fluid from said source to a jet pump, combining a refrigerant fluid with said motive fluid in said jet pump, and passing said combined fluids in heat exchange relation with said motive fluid prior to the flowing thereof into heat exchange relation with said source of heat.
7. A method according to claim 6 wherein the motive fluid 1 5 caFmo- References Cited in the file of this patent UNITED STATES PATENTS 1,014,120 Coleman Jan. 9, 1912 1,906,414 Randel May 2, 1933 2,014,701 Seligmann Sept. 17. 1935 2,658,356 Neumann Nov. 10, 1953

Claims (1)

1. A METHOD OF FURNISHING REFRIGERATION, COMPRISING SEPARATING A LIQUIFIED REFRIGERANT AND A LIQUIFIED MOTIVE FLUID, THE MOTIVE FLUID BEING A CYCLIC FLUOROCARBON ETHER HAVING THE FORMULA
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Cited By (18)

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US3199310A (en) * 1963-01-24 1965-08-10 Ralph C Schiichtig Ejector type refrigeration system
US3203194A (en) * 1962-12-01 1965-08-31 Hoechst Ag Compression process for refrigeration
US3242679A (en) * 1964-04-07 1966-03-29 Edward G Fisher Solar refrigeration unit
US3246505A (en) * 1963-09-09 1966-04-19 Boeing Co Leak detection method and apparatus
US3276226A (en) * 1964-10-08 1966-10-04 Carrier Corp Refrigeration system with turbine drive for compressor
US3277659A (en) * 1964-07-17 1966-10-11 American Air Filter Co Refrigeration
US3298196A (en) * 1965-05-03 1967-01-17 Ralph C Schlichtig Dynamic pump type refrigeration system
US3309897A (en) * 1965-10-21 1967-03-21 Russell Jacob Bruce Constant pressure refrigeration cycle
US3427817A (en) * 1964-12-19 1969-02-18 Philips Corp Device for producing cold and/or liquefying gases
US3456456A (en) * 1966-07-01 1969-07-22 Philips Corp Cryogenic apparatus for producing cold
EP0149413A2 (en) * 1984-01-12 1985-07-24 Dori Hershgal Method and apparatus for refrigeration
EP0152308A2 (en) * 1984-02-16 1985-08-21 George Ernest Carpenter (deceased), legally represented by Carpenter, Mary Isobel and Martin, Alice Improved vapour cycle system
DE3431240A1 (en) * 1984-08-24 1986-03-06 Michael 4150 Krefeld Laumen REFRIGERATION MACHINE OR HEAT PUMP AND JET PUMP HERE
US4625522A (en) * 1985-01-09 1986-12-02 Institut Francais Du Petrole Process for producing cold and/or heat by using a non-azeotropic mixture of fluids in a cycle with ejector
EP2227662A1 (en) * 2007-11-27 2010-09-15 The Curators Of The University Of Missouri Thermally driven heat pump for heating and cooling
US20110079022A1 (en) * 2009-10-01 2011-04-07 Hongbin Ma Hybrid thermoelectric-ejector cooling system
US20130111944A1 (en) * 2010-07-23 2013-05-09 Carrier Corporation High Efficiency Ejector Cycle
US20130125569A1 (en) * 2010-07-23 2013-05-23 Carrier Corporation Ejector Cycle

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US1906414A (en) * 1930-01-22 1933-05-02 Randel Bo Folke Method of refrigeration
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US1014120A (en) * 1901-06-19 1912-01-09 Clyde J Coleman Refrigerating apparatus.
US2014701A (en) * 1928-08-18 1935-09-17 Seligmann Arthur Refrigerating plant
US1906414A (en) * 1930-01-22 1933-05-02 Randel Bo Folke Method of refrigeration
US2658356A (en) * 1951-07-05 1953-11-10 Ultra Mechanisms Inc Jet pump refrigeration system

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3203194A (en) * 1962-12-01 1965-08-31 Hoechst Ag Compression process for refrigeration
US3199310A (en) * 1963-01-24 1965-08-10 Ralph C Schiichtig Ejector type refrigeration system
US3246505A (en) * 1963-09-09 1966-04-19 Boeing Co Leak detection method and apparatus
US3242679A (en) * 1964-04-07 1966-03-29 Edward G Fisher Solar refrigeration unit
US3277659A (en) * 1964-07-17 1966-10-11 American Air Filter Co Refrigeration
US3276226A (en) * 1964-10-08 1966-10-04 Carrier Corp Refrigeration system with turbine drive for compressor
US3427817A (en) * 1964-12-19 1969-02-18 Philips Corp Device for producing cold and/or liquefying gases
US3298196A (en) * 1965-05-03 1967-01-17 Ralph C Schlichtig Dynamic pump type refrigeration system
US3309897A (en) * 1965-10-21 1967-03-21 Russell Jacob Bruce Constant pressure refrigeration cycle
US3456456A (en) * 1966-07-01 1969-07-22 Philips Corp Cryogenic apparatus for producing cold
EP0149413A3 (en) * 1984-01-12 1986-02-19 Dori Hershgal Method and apparatus for refrigeration
EP0149413A2 (en) * 1984-01-12 1985-07-24 Dori Hershgal Method and apparatus for refrigeration
EP0152308A3 (en) * 1984-02-16 1986-02-26 George Ernest Carpenter (deceased), legally represented by Carpenter, Mary Isobel and Martin, Alice Improved vapour cycle system
EP0152308A2 (en) * 1984-02-16 1985-08-21 George Ernest Carpenter (deceased), legally represented by Carpenter, Mary Isobel and Martin, Alice Improved vapour cycle system
DE3431240A1 (en) * 1984-08-24 1986-03-06 Michael 4150 Krefeld Laumen REFRIGERATION MACHINE OR HEAT PUMP AND JET PUMP HERE
WO1986001582A1 (en) * 1984-08-24 1986-03-13 Michael Laumen Refrigerator or heat pump and jet pump therefor
US4748826A (en) * 1984-08-24 1988-06-07 Michael Laumen Thermotechnik Ohg. Refrigerating or heat pump and jet pump for use therein
US4625522A (en) * 1985-01-09 1986-12-02 Institut Francais Du Petrole Process for producing cold and/or heat by using a non-azeotropic mixture of fluids in a cycle with ejector
EP2227662A4 (en) * 2007-11-27 2014-01-22 Univ Missouri Thermally driven heat pump for heating and cooling
EP2227662A1 (en) * 2007-11-27 2010-09-15 The Curators Of The University Of Missouri Thermally driven heat pump for heating and cooling
US10101059B2 (en) 2007-11-27 2018-10-16 The Curators Of The University Of Missouri Thermally driven heat pump for heating and cooling
US20110079022A1 (en) * 2009-10-01 2011-04-07 Hongbin Ma Hybrid thermoelectric-ejector cooling system
US8763408B2 (en) 2009-10-01 2014-07-01 The Curators Of The University Of Missouri Hybrid thermoelectric-ejector cooling system
US20130125569A1 (en) * 2010-07-23 2013-05-23 Carrier Corporation Ejector Cycle
US9752801B2 (en) * 2010-07-23 2017-09-05 Carrier Corporation Ejector cycle
US20130111944A1 (en) * 2010-07-23 2013-05-09 Carrier Corporation High Efficiency Ejector Cycle
US11149989B2 (en) * 2010-07-23 2021-10-19 Carrier Corporation High efficiency ejector cycle

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