US1440000A - Refrigeration - Google Patents

Refrigeration Download PDF

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Publication number
US1440000A
US1440000A US378467A US37846720A US1440000A US 1440000 A US1440000 A US 1440000A US 378467 A US378467 A US 378467A US 37846720 A US37846720 A US 37846720A US 1440000 A US1440000 A US 1440000A
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medium
compressor
motor
refrigerating
expansion
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US378467A
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Charles E Bonine
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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
    • F25B27/00Machines, plants or systems, using particular sources of energy
    • 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
    • F25B11/00Compression machines, plants or systems, using turbines, e.g. gas turbines
    • F25B11/02Compression machines, plants or systems, using turbines, e.g. gas turbines as expanders
    • 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
    • F25B9/00Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point
    • F25B9/002Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant
    • F25B9/004Compression machines, plants or systems, in which the refrigerant is air or other gas of low boiling point characterised by the refrigerant the refrigerant being air

Description

3 SHEETS-SHEET 1 C E BONINE REFRIGERATION Fl LED MAY 3' 1920 FIGi I I/lVE/VTOR:
(lizarwslifianine,
ATTORNEYS.
WIT/75%5:
Dec. 26, 1922. 1,440,000
v C. E. BONINE.
REFRIGERATION.
FILED MAY 3, 1920. 3 SHEETS-SHEET 2 Melrose Park, in
tivity,the same Patented Dec. 26, 1922.
ICE.
GIEIAIREILIES E. BONINE,- OF MELROSE PARK, PENNSYLVANIA.
REFRIGERATION.
Application filed May 3,
T o allwhom it may concern,
Be it known that I, CHARLES E. BONINE, a ,bitizLen of the United States, residing in the township of Cheltenham, in the county of @State of Pennsylvania, *haveinvented certain new and useful Improvements in Refrigeration, whereof the following is a specification, reference being had to the accompanying drawings.
y invention relates to refrigeration, and especially to systems and processes in which a refrigerating or working medium (preferably air or other elastic fluid) is given the capacity for absorbing heat (which constitutes refrigerating power) by compressing it,
abstracting heat from it,-as by cooling with some extrinsic medium or agency,--and expanding it and thereby reducing its temperature below whatever temperature is to be brought about or maintained in the object or region to be refrigerated. Such refrigerating systems are advantageously operated by circulation of a bodyof working medium or fluid in a closed circuit and cycle of successive stages of compression, extrinsic cooling, expansion and refrigerating acbody ofmedium thus traversing the entire circuit of the apparatus and repeating the complete cycle of stages or operations over and overagain.
he aim of my inventionupon such oration in such wise as to permit the extrinsic cooling operation to be effected at relatively wide ranges of temperature (even when it is desired to attain very low temperatures of refrigeration), to allow the compression and expansion to be effected with great economy and convenlence, and I to simplify the apparatus and e uipme'nt required as much as possible. y invention, furthermore, enables the apparatus to be made compact, simple, rugged, and inexpensive in construction and arrangement; convenient and easy to operate and repair; and free from derangement. Hence it is especially applicable to household plants or equipments, where only slight and unskilled attention to operation and upkeep will ordinarily be given. I ['How these and other advantages can be realized inconnection with be apparent from the description hereinafter-of the best methods, operations and apparatus for the purpose at present known- Montgomery and is to improve processes and systems. of refr1gmy invention will understood from my claims. It will be seen that while I some of its broader aspects it can be carried out with many other types and forms of apparatus.
In the drawings, Fig. I is a somewhat diagrammatlc general view of a refrigerating system suitable for the purposes of my ventlon, one of shown in mid-sectlon.
Fig. II is an F 1g. I, certain portions being shown in 1ongitudinal mid-section. 7
Figs. III and IV show transverse sections through the compressor and expander portions of the apparatus illustrated in Fig. II, taken as indicated by the lines III-III and IV-IV on Fig. II, and looking in the direction of the arrows.
The closed circulatory system illustrated in Fig. I includes a compression and expansion operating unit comprehensively indi--' cated by the numeral 1, a cooling device 6,
room. or refrigerating apparatus conventionally represented in dotted lines,.and comprehensively indicated by the numeral 18. The operating unit'l shown consists of a unitary structure comprising a motor 2" re.- ceiving power from an external source, a
compressor 3 for compressing the working med1um,.and a motor 4 which serves for and is operated by expansion of the compressed medium to restore its refrigerating power.
have disclosed compressing and enlarged elevation of a com-'. pression and expansion unit appearing in The compressor 3 is driven by the motors i 2 and 4 n co-operation, through a drive element common to all three of these machines. The cooling device 6 is shown as an upright cylindrical storage tank receiving the compressed medium at its top through piping 5 from the compressor 3, and delivering to the, heat interchanger 9 through piping 8 that enters the tank a suitable distance above its bottom. The comparative arrest of the medium in the tank'fi permits precipitation and separation oii of any moisture suspended therein or condensing therefrom, and a drain cock 7 in the bottom .of'tlie tank allows the accumulated water to be drawn off from time a yp 16 to the chamber 12,
ating activity to time.
The heat interchanger 9 consists of a cylindrical casing 10 having in its opposite ends inlet and discharge chambers 11 and 12 formed by tube-sheets 13 and 14, and connected by a number of tubes 15. In the central compartment 16, between the tubesheets, are alternating, staggered, upper and lower transverse baflies 17. The compressed medium delivered from the pipe 8 enters the chamber 11 passes through the tubes and is thence delivered to the motor 4 through the piping 20. The expanding medium that has been exhausted and delivered from themotor 4 through the piping 21 tothe cooling coil 22 or the like of the refrigerating apparatus 18 returns from its refrigerating activity therein through the piping 23 and 24 to the compressor 3. On its way, this, returning medium passes through the compartment 16 of the interchanger 9, traversing a serpentine course through this compartment back and forth around and amongst the tubes 16, and in a general direction counter to the flow of compressed medium through the tubes 15; Thus an interchange of heat is effected between the medium intermediate the cooling and expansion stages of its cycle and the medium returning from its refrigerto the compression stage.
Referring, now, to Figs. 11,111, and IV,
it will be seen thatthe three machines com posing the operating unit 1 are of rotary with a common rotary shaft 25 as their drive element, and a unitary casing and frame structure The base of this structure is that of the frame of the centrally arranged-motor 2 (here'shown as an electric one), which carries the shaft bearings 26, 26. The casing of the compressor 3 and the fluid motor 4 are secured" to the motor frame at opposite sides, as by means of' bolts taking into openwork bracket ex- The open air spaces intervening between the electric motor 2 and the compressor 3 and the fluid motor 4 at opposite sides thereof prevent or minimize the interchange of heat between said electric motor 2 and either of said other devices 3 and 4, or between said devices 3 and 4 themselves.
The rotary compressor 3 is of multi-stage centrifugal type, with centrifugal rotor elements 27 and 28 spaced apart on the reduced end of the shaft 25 by means of a sleeve 29, and secured by a nut 30. From the compressor inlet channel 31,- the working medium enters the first compression stage, passing inward through stationary passages 32 and sidewiseinto the moving vane-channels or passage The medium or fluid discharged peripherally at high velocity 33 of the rotor section 27 from the rotor 27' passes through the stationary vane or noz- 34 inithe' casing, which are so shaped as to utilize the velocity of the fluid in compressing it. The partially compressed fluid now enters the second compression stage, traverses stationary and moving passages 35, 36, and 37 in the casing (see Fig. III) and 28 (all'simil'ar 'to the. sages in the first stage), and is in like man- .ner further compressed. The fluid is finally collected in an annular outlet chamber zle assages 38 of gradually increasing cross-section that surrounds the nozzle-passages 37 (and is similar to the inlet channel 31), and is discharged into the piping 5' at the desired pressure, and at a temperature corresponding to that at the in the rotor section corresponding pasinlet 11 and to the work of compression done upon it. The nozzle passages 34 and 37 are preferably designed to effect the compression in a practically adiabatic manner, so as to minimize the temperature increase and the work of compression. 9
When air is used as refrigerating medium and the system is operated at comparatively low pressure, the make up supply of medium required in starting and to compensate for leakage losses may be admitted "and drawn into the system, during operation, through one or more openings 39 in the casing wall at the inlet or suctionside of the compressor. Makeup air may also be obtained through the clearance around the shaft 25, by omitting the packing ring 40 ordinarily employed at the suction side of the machine.
' The rotary expansion motor 4 is shown as of multi-stage axial flow turbine type. The working medium entering through the inlet 45 is discharged through inclined stationary expansion nozzles 46 against the first row of moving blades or buckets 47 car'- ried by the rotor disk The'fluid issuing from the buckets 47 passes through a row of stationary reguidebuckets 49 mounted on the turbine casing, and then enters and traverses the second row of moving buckets 50, carried by said. rotor disk 4:5. The nozzle and bucket passages 46, 47, 49 and 50 may be of such progressively increasing size as to develop and utilize the velocity of the fuel obtainable'by expansion fractionally, as shown, impact or reaction types. The fluid is next discharged through the inclined stationary expansion nozzles 51 in the interstage diaphragm v the rotor disk of sure being thus further converted into velocity and utilized to assist in driving the compressor 3. Thefluid finally issues from the turbine outlet 53, and enters the piping 21 in an expanded condition, and at a low temperature corresponding to that when it and maybe of either entered the turbine and to the expansion it has undergone, so that its former refrigerating power when it enters the refrigerating apparatus 18 is restored. Preferably, the turbine is designed (as indicated) so as to effect the expansion as nearly adiabatically asp'o'ssible, in order that the maximum power output may be obtained and that the final temperature may be as low as possible.
It will be seen'that the system as a Whole is as simple as possible, and that the operating unit, likewise, has a minimum of parts, and has only two hearings to be lubricated. Owing to the utilization of the energy obtainable from the expansion of the working fluid to assist in driving the compressor 3,
the net power consumption of the system is reduced to a minimum. The interchange of heat between the relatively warm compressed medium on its way from the cooler 6 tothe expander 4 and the relatively cold medium returning to the compressor 3 is doubly advantageous. It results in a low minimum temperature for the medium after expansion, and hence in maximum refrigerating power; and it results in a relatively high temperature for the medium in the cooler 6, so as to permit cooling at a relatively high temperature range and. thus promotes maximum abstraction of heat from it by the agency employed, such as the surroundin atmosphere. Thus the high heat level 0' the refrigerating cycle is, as it were, jacked up, by forcing down the low heat level, and vice versa.
am aware that it proposed, in U. S. patent to Allen, No. 231,886, Sept. 1, 1880, touse an engine driven by the expanding refrigerating me dium to assist in the work of compression. The system shown in that patent is, however, so complicated and subject to such other dishas been previously advantages as to be of quite limited utility, and under inany conditions quite impracticable. 1
Having thus described my invention, I claim:
1. A refrigeration compressing and expanding unit comprising, on a common shaft, and in a unitary casing and frame structure, a rotary compressor device for compressing the Working medium; a rotary fluid motor device for expanding the medium thus compressed to restore its refrigere ating power; and additional motor device receiving power from an external source and cooperating with the first-mentioned motor to drive said compressor; and a base for said unit with one of said devices mounted directly thereon and carrying the others through their attachment to that so mounted.
2. A refrigeration compressing and expanding unit comprising a base for the unit and a motor receiving power from an external source mounted directly thereon; a rotary compressor for compressing the working-medium attached to said motor by openwork, with an intervening air space, and thereby carried from said base; a rdtary fluid motor for expanding the medium thus compressed to restore its refrigerating power cooperating with the aforesaid motor to drive said compressor, and attached to the aforesaid motor by openwork, with an intervening air space, and thereby carried from said base; and a common shaft for said compressor and said motors.
In testimony whereof, I have hereunto signed my name at Philadelphia, Pennsylvania, this 29th day of April 1920.
CHARLES E. BONINE.
Witnesses:
JAMES H. BELL, E. L. FULLERTON.
US378467A 1920-05-03 1920-05-03 Refrigeration Expired - Lifetime US1440000A (en)

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Cited By (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2486034A (en) * 1945-06-05 1949-10-25 Katzow Abram Heat operated compression refrigeration
US2491314A (en) * 1946-10-14 1949-12-13 Gen Electric Turbogenerator cooling system
US2637984A (en) * 1950-07-26 1953-05-12 Gen Electric Turbine
US2767560A (en) * 1951-10-29 1956-10-23 Power Jets Res & Dev Ltd Fluid cooling plant for mines
US2893204A (en) * 1956-09-11 1959-07-07 Thompson Ramo Wooldridge Inc Self-cooled turbine drive
US2928254A (en) * 1954-09-20 1960-03-15 Garrett Corp Storage tank for low temperature liquids
DE1092938B (en) * 1957-12-31 1960-11-17 Ianemaia Veb Maschf Gas chiller
US2970437A (en) * 1956-02-28 1961-02-07 Thompson Ramo Wooldridge Inc High temperature pumping system with variable speed pump and refrigeration by-product
US3194026A (en) * 1963-10-24 1965-07-13 Fleur Corp Power-refrigeration system
US3214938A (en) * 1963-01-02 1965-11-02 Martin Marietta Corp Thermally powered cryogenic system
US3225538A (en) * 1960-03-25 1965-12-28 Catacycle Company Inc Conversion of heats of chemical reactions to sensible energy
US3285001A (en) * 1965-03-04 1966-11-15 Conductron Corp Thermal fluid moving apparatus
US3400555A (en) * 1966-05-02 1968-09-10 American Gas Ass Refrigeration system employing heat actuated compressor
US3477239A (en) * 1967-05-16 1969-11-11 Messer Griesheim Gmbh Multistage compression drive in gas separation
US3495402A (en) * 1968-01-18 1970-02-17 John W Yates Power system
US3508399A (en) * 1968-01-18 1970-04-28 Babcock Atlantique Sa Generation of energy in a closed gas cycle
US4138848A (en) * 1976-12-27 1979-02-13 Bates Kenneth C Compressor-expander apparatus
EP0004609A2 (en) * 1978-04-10 1979-10-17 Hughes Aircraft Company Screw compressor-expander cryogenic system
EP0589425A2 (en) * 1992-09-25 1994-03-30 STN Systemtechnik Nord GmbH Cooling device, particularly for air conditioning of rooms
EP0667499A1 (en) * 1992-10-30 1995-08-16 Kajima Corporation Pneumatic ice making device
EP0676600A2 (en) * 1994-04-05 1995-10-11 Carrier Corporation Two phase flow turbine
EP0728996A2 (en) * 1995-01-30 1996-08-28 Carrier Corporation Subcooler level control for a turbine expansion refrigeration cycle
US5586440A (en) * 1994-12-06 1996-12-24 Vincent; David M. Pneumatic refrigeration system and method
EP1762793A2 (en) * 2005-09-09 2007-03-14 Mitsubishi Heavy Industries, Ltd. Closed type air cycle refrigerator and cooling method using the same

Cited By (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2486034A (en) * 1945-06-05 1949-10-25 Katzow Abram Heat operated compression refrigeration
US2491314A (en) * 1946-10-14 1949-12-13 Gen Electric Turbogenerator cooling system
US2637984A (en) * 1950-07-26 1953-05-12 Gen Electric Turbine
US2767560A (en) * 1951-10-29 1956-10-23 Power Jets Res & Dev Ltd Fluid cooling plant for mines
US2928254A (en) * 1954-09-20 1960-03-15 Garrett Corp Storage tank for low temperature liquids
US2970437A (en) * 1956-02-28 1961-02-07 Thompson Ramo Wooldridge Inc High temperature pumping system with variable speed pump and refrigeration by-product
US2893204A (en) * 1956-09-11 1959-07-07 Thompson Ramo Wooldridge Inc Self-cooled turbine drive
DE1092938B (en) * 1957-12-31 1960-11-17 Ianemaia Veb Maschf Gas chiller
US3225538A (en) * 1960-03-25 1965-12-28 Catacycle Company Inc Conversion of heats of chemical reactions to sensible energy
US3214938A (en) * 1963-01-02 1965-11-02 Martin Marietta Corp Thermally powered cryogenic system
US3194026A (en) * 1963-10-24 1965-07-13 Fleur Corp Power-refrigeration system
US3285001A (en) * 1965-03-04 1966-11-15 Conductron Corp Thermal fluid moving apparatus
US3400555A (en) * 1966-05-02 1968-09-10 American Gas Ass Refrigeration system employing heat actuated compressor
US3477239A (en) * 1967-05-16 1969-11-11 Messer Griesheim Gmbh Multistage compression drive in gas separation
US3495402A (en) * 1968-01-18 1970-02-17 John W Yates Power system
US3508399A (en) * 1968-01-18 1970-04-28 Babcock Atlantique Sa Generation of energy in a closed gas cycle
US4138848A (en) * 1976-12-27 1979-02-13 Bates Kenneth C Compressor-expander apparatus
EP0004609A2 (en) * 1978-04-10 1979-10-17 Hughes Aircraft Company Screw compressor-expander cryogenic system
EP0004609A3 (en) * 1978-04-10 1979-10-31 Hughes Aircraft Company Screw compressor-expander cryogenic system
EP0589425A2 (en) * 1992-09-25 1994-03-30 STN Systemtechnik Nord GmbH Cooling device, particularly for air conditioning of rooms
EP0589425A3 (en) * 1992-09-25 1994-11-17 Nord Systemtechnik Cooling device, particularly for air conditioning of rooms.
EP0667499A1 (en) * 1992-10-30 1995-08-16 Kajima Corporation Pneumatic ice making device
EP0667499A4 (en) * 1992-10-30 1995-11-15 Kajima Corp Pneumatic ice making device.
EP0676600A2 (en) * 1994-04-05 1995-10-11 Carrier Corporation Two phase flow turbine
EP0676600A3 (en) * 1994-04-05 1996-12-18 Carrier Corp Two phase flow turbine.
US5586440A (en) * 1994-12-06 1996-12-24 Vincent; David M. Pneumatic refrigeration system and method
EP0728996A2 (en) * 1995-01-30 1996-08-28 Carrier Corporation Subcooler level control for a turbine expansion refrigeration cycle
EP0728996A3 (en) * 1995-01-30 1998-01-21 Carrier Corporation Subcooler level control for a turbine expansion refrigeration cycle
EP1762793A2 (en) * 2005-09-09 2007-03-14 Mitsubishi Heavy Industries, Ltd. Closed type air cycle refrigerator and cooling method using the same
EP1762793A3 (en) * 2005-09-09 2013-12-25 Mitsubishi Heavy Industries, Ltd. Closed type air cycle refrigerator and cooling method using the same

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