CA2331589C - Compressor unit for refrigeration - Google Patents

Compressor unit for refrigeration Download PDF

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Publication number
CA2331589C
CA2331589C CA002331589A CA2331589A CA2331589C CA 2331589 C CA2331589 C CA 2331589C CA 002331589 A CA002331589 A CA 002331589A CA 2331589 A CA2331589 A CA 2331589A CA 2331589 C CA2331589 C CA 2331589C
Authority
CA
Canada
Prior art keywords
rotor
refrigerant gas
eccentric
orbiting
chamber
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CA002331589A
Other languages
French (fr)
Other versions
CA2331589A1 (en
Inventor
Peter P. M. Randolphi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
RANDELL TECHNOLOGIES Inc
Original Assignee
RANDELL TECHNOLOGIES Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by RANDELL TECHNOLOGIES Inc filed Critical RANDELL TECHNOLOGIES Inc
Priority to CA002331589A priority Critical patent/CA2331589C/en
Priority to US09/782,486 priority patent/US6520754B2/en
Priority to ES02709932T priority patent/ES2265490T3/en
Priority to PCT/CA2002/000058 priority patent/WO2002057634A1/en
Priority to DE60211654T priority patent/DE60211654T2/en
Priority to AT02709932T priority patent/ATE327437T1/en
Priority to EP02709932A priority patent/EP1354136B1/en
Publication of CA2331589A1 publication Critical patent/CA2331589A1/en
Application granted granted Critical
Publication of CA2331589C publication Critical patent/CA2331589C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/0042Driving elements, brakes, couplings, transmissions specially adapted for pumps
    • F04C29/005Means for transmitting movement from the prime mover to driven parts of the pump, e.g. clutches, couplings, transmissions
    • F04C29/0064Magnetic couplings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/22Rotary-piston pumps specially adapted for elastic fluids of internal-axis type with equidirectional movement of co-operating members at the points of engagement, or with one of the co-operating members being stationary, the inner member having more teeth or tooth equivalents than the outer member
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04CROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C23/00Combinations of two or more pumps, each being of rotary-piston or oscillating-piston type, specially adapted for elastic fluids; Pumping installations specially adapted for elastic fluids; Multi-stage pumps specially adapted for elastic fluids
    • F04C23/008Hermetic pumps

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
  • Compressor (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

A compressor for a refrigeration unit having a stator, a rotor orbiting in engagement with the stator to cyclically open, fill with refrigerant gas from at least one inlet port, compress and discharge compressed refrigerant gas through at least one discharge port, a rotary drive for orbiting the rotor, a driven element of a magnetic coupling in driving connection with the rotary drive, a casing sealed save for the ports and enclosing all of the foregoing components, a driving element of the magnetic coupling outside of the casing in close proximity to the driven element, and a motor to rotate the driving element.
Preferably the rotor is a multilobed rotor orbiting within a trochoidal chamber defined by the stator. Most preferably, a three lobed rotor is journalled on an eccentric carried by a shaft of the rotary drive and has a ring gear driven by a gear of the rotary drive having the same eccentricity as the eccentric and rotated in synchronism therewith, the gear ratio of the ring gear to the eccentric being three to one.

Description

COMPRESSOR UNIT FOR REFRIGERATION
FIELD OF THE INVENTION
This invention relates to refrigeration compressor units especially but not exclusively units for small refrigeration units such are suitable for use in domestic ice cream makers, small refrigerators and similar appliances. Such units must be compact, quiet, reliable and economical to manufacture and operate.
BACKGROUND OF THE INVENTION
Compressor units for domestic refrigerators are commonly of the sealed unit type in which both the compressor and a motor permanently coupled to the compressor are located within an enclosure which is completely and permanently sealed except for refrigerant connections to the remainder of the refrigeration unit. Such a unit has the disadvantages that failure of either the motor or the compressor requires both to be discarded, different sealed units are required for electrical supplies requiring different motors, even though the compressor is identical, and two devices, both of which generate unwanted heat. are thermally coupled within the same enclosure.
It is known in compressor units for automotive air conditioning systems, which are engine driven, and thus require a clutch mechanism, to utilize an electromagnetic clutch between a belt driven pulley and the compressor.
It is also known to use magnetic couplings in drives for pumps so as to avoid the necessity of sealing a drive shaft entering the pump chamber. Examples of such arrangements are to be found in U.S. Patents Nos. 3,584,975 (Frohbieter);
3,680,984 (Young et al.); 4,065,234 (Yoshiyuki et al.); and 5,334,004 (Lefevre et al), and in ISOCHEM (Trademark) pumps from Pulsafeeder. Although the first of the patents relates to a circulation pump for an absorption type air conditioning system, the use of a permanent magnet coupling in the drive to the compressor of a compressor type refrigeration unit has not to the best of my knowledge previously been proposed.
Reasons may include the sharply fluctuating torque required by piston type compressors normally used in such systems.
In the interests of smoother and more silent compression, there has been some adoption of scroll type compressors in compression type refrigeration units, available for example from Lennox, Copeland and EDPAC International.
An alternative form of piston compressor which has been proposed, although not to the best of my knowledge for refrigeration applications, is the rotary piston compressor using a lobed rotor in a trochoidal chamber and having some superficial resemblance to rotary piston engines such as the Wankel engine although the operating cycle is substantially different and the shaft is driven by an external power source rather than being driven by the rotary piston. Such compressors are exemplified in U.S.
Patents Nos. 3,656,875 (Luck); 4,018,548 (Berkowitz); and 4,487,561 (Eiermann).
U.S. Patent 5,310,325 (Gulyash) discloses a rotary engine using a symmetrical lobed piston moving in a trochoidal chamber on an eccentric mounted on a rotary shaft and driven through a ring gear by a similarly eccentric planet gear rotated at the same rate as the eccentric, the gear ratio of the ring gear to the planet gear being equal to the number of lobes on the rotor, typically three. The apices of the lobes trace trochoidal paths tangent to the trochoidal chamber wall thus simplifying sealing. There is no suggestion that similar principles of construction could be used in a compressor.
SUMMARY OF THE INVENTION
In its broadest aspect, the invention provides a compressor for a refrigeration unit having a stator, a rotor orbiting in engagement with the stator to cyclically open, fill with refrigerant gas from at least one inlet port, compress and discharge compressed refrigerant gas through at least one discharge port, a rotary drive for orbiting the rotor, a driven element of a magnetic coupling in driving connection with the rotary drive, a casing sealed save for the ports and enclosing all of the foregoing components, a driving element of the magnetic coupling outside of the casing in close proximity to the driven element, and means to rotate the driving element.
Preferably the rotor is a multilobed rotor orbiting within a trochoidal chamber defined by the stator, although a scroll type compressor with stationary and orbiting scrolls may also be utilized. Most preferably, a three lobed rotor is journalled on an eccentric carried by a shaft of the rotary drive and has a ring gear driven by a gear of the rotary drive having the same eccentricity as the eccentric and rotated in synchronism therewith, the gear ratio of the ring gear to the eccentric being three to one.
Further features of the invention will be apparent from the following description of a presently preferred embodiment thereof.
SHORT DESCRIPTION OF THE DRAWINGS
Figures 1 - 4 are cross-sectional views through a compressor in accordance with the invention, showing different phases of its operation, Figure 1 being a section on the line 1 - 1 in Figure 5; and Figure 5 is a longitudinal section of the unit on the line 5 - 5 in Figure 1, with the compressor and drive separated for clarity.
DESCRIPTION OF THE PREFERRED EMBODIMENT
Referring to Figure 5, a compressor 2 comprises a casing 4 which is completely sealed apart from input and output pipes 6 and 8 which connect the compressor 2 respectively to the evaporator and the condenser (not shown) of a refrigeration unit. A
third pipe 10 is used only to charge the unit with refrigerant and is then permanently sealed.
Internally the pipes 6 and 8 are connected to chambers 12 and 14 respectively (see Figs. 1 - 4) formed between the casing 4 and a stator 16 of the compressor, the chambers being separated by walls 38. A compressor drive shaft 18 is journalled in bearings 20 in end walls 22, 24 of the stator, and carries at one end a driven element 26 of a magnetic coupling which may for example consist of concentric rings of ceramic S
equipped with spring valves such as reed valves 58 to prevent unwanted reverse flow.
Figure 1 shows the position of the rotor 40 when the maximum eccentricities of the eccentric 40 and gear 46 are directed upwardly (as seen in the drawing). The direction of rotation in this example is clockwise, and the apices of the lobes of the rotor are labeled A, B and C for convenient reference. The geometry of the rotor and stator and of the drive are such that the apices remain in contact with the wall of trochoidal chamber 44. Apex B contacts the wall between the lower ports 54 and 56, while the surface of the rotor between apices A and C lies against the chamber wall, obturating the upper ports 54 and 56. As the rotor moves clockwise, gas is drawn through the lower port 56 into the chamber labeled D, while gas in chamber E is compressed and forced out of the chamber through lower port 54 past valve 58 if its pressure exceeds that in chamber 14.
As the rotor reaches the position shown in Figure 2, apex B moves past lower port 56 cutting off the induction of gas into chamber D and then apex A moves past upper port 54 so that gas compressed in chamber D on further motion of the rotor can pass through that port once its pressure exceeds that in chamber 14. At the same time, that portion of the rotor between apices A and C moves away from the stator forming chamber F into which gas is induced through upper port 56, and pressurized gas continues to be expelled through lower port 54 from chamber E.
In Figure 3, the position is analogous to that in Figure 1, except that apex A
lies between upper ports 54 and 56, and lower ports 54 and 56 are obturated by the surface of the rotor between apices B and C. In Figure 4 the position is analogous to that in Figure 2, with chamber F filled, chamber E refilling, and compressed gas being expelled from chamber D. When the eccentric again reaches the position shown in Figure 1, the rotor has turned through 120 degrees and a similar sequence is then repeated.
After three sequences, the rotor has turned through 360 degrees. In effect, three compression cycles are occurring simultaneously, 120 degrees out of phase, providing high volumetric efficiency and a very smooth action.
Particularly if at least one of the rotor and the stator is molded from synthetic plastic, it may be possible to dispense with apex seals, thus further simplifying construction. The use of an external motor means that the latter may also power other functions of S apparatus including a refrigeration unit incorporating the compressor, for example mixing paddles in an icecream maker. The compactness of the equipment suits it for use in portable applications such as refrigerated protective clothing.
Although a particularly preferred embodiment of compressor has been described, other forms of compressor using rotors orbiting in trochoidal chambers may be utilized, as may scroll compressors.

Claims (6)

1. A compressor for a refrigeration unit comprising:
a sealed casing having at least one inlet port for receiving refrigerant gas and at least one discharge port for discharging compressed refrigerant gas, a stator enclosed by the staled casing and defining a chamber in communication with the at least one inlet port and in communication with the at least one discharge port, a rotor enclosed by the sealed casing, the rotor orbiting in said chamber defined within the stator and being in engagement with the at least one inlet port for receiving refrigerant gas and at least one discharge port to cyclically receive refrigerant gas through the at least one inlet port into said chamber, compress the refrigerant gas within the stator, and discharge the compressed refrigerant gas through the at least one discharge port, a rotary drive enclosed by the sealed casing and orbiting the rotor, a driven element of a magnetic coupling in driving connection with the rotary drive and orbiting the rotor, the driven element enclosed by the sealed casing and including at least one magnet, a driving element of the magnetic coupling outside of the casing in close proximity to the driven element, and an arrangement for rotating the driving element.
2. A compressor according to claim 1, wherein the rotor is a multilobed rotor and said chamber in which the rotor is orbiting is a trochoidal chamber.
3. A compressor according to claim 2, wherein the rotor is a three lobed rotor journalled on an eccentric carried by a shaft of the rotary drive and has a ring gear driven by an eccentric gear, the eccentric gear having the same eccentricity as the eccentric and being constrained to rotate in synchronism therewith, the gear ratio of the ring gear to the eccentric gear being three to one.
4. A compressor according to claim 1, wherein the arrangement for rotating the driving element includes an electric motor.
5. A compressor according to claim 1, wherein the magnet includes a plurality of permanent magnets.
6. A compressor according to claim 5, wherein the driving element includes a plurality of permanent magnets.
CA002331589A 2001-01-22 2001-01-22 Compressor unit for refrigeration Expired - Fee Related CA2331589C (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
CA002331589A CA2331589C (en) 2001-01-22 2001-01-22 Compressor unit for refrigeration
US09/782,486 US6520754B2 (en) 2001-01-22 2001-02-13 Compressor unit for refrigeration
PCT/CA2002/000058 WO2002057634A1 (en) 2001-01-22 2002-01-17 Refrigeration compressor with magnetic coupling
DE60211654T DE60211654T2 (en) 2001-01-22 2002-01-17 COOLING COMPRESSOR WITH MAGNETIC COUPLING
ES02709932T ES2265490T3 (en) 2001-01-22 2002-01-17 COOLING COMPRESSOR WITH MAGNETIC COUPLING.
AT02709932T ATE327437T1 (en) 2001-01-22 2002-01-17 REFRIGERANT COMPRESSOR WITH MAGNETIC COUPLING
EP02709932A EP1354136B1 (en) 2001-01-22 2002-01-17 Refrigeration compressor with magnetic coupling

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA002331589A CA2331589C (en) 2001-01-22 2001-01-22 Compressor unit for refrigeration

Publications (2)

Publication Number Publication Date
CA2331589A1 CA2331589A1 (en) 2002-07-22
CA2331589C true CA2331589C (en) 2005-05-24

Family

ID=4168132

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002331589A Expired - Fee Related CA2331589C (en) 2001-01-22 2001-01-22 Compressor unit for refrigeration

Country Status (5)

Country Link
EP (1) EP1354136B1 (en)
AT (1) ATE327437T1 (en)
CA (1) CA2331589C (en)
DE (1) DE60211654T2 (en)
ES (1) ES2265490T3 (en)

Also Published As

Publication number Publication date
DE60211654D1 (en) 2006-06-29
DE60211654T2 (en) 2007-05-03
EP1354136A1 (en) 2003-10-22
EP1354136B1 (en) 2006-05-24
ES2265490T3 (en) 2007-02-16
CA2331589A1 (en) 2002-07-22
ATE327437T1 (en) 2006-06-15

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Effective date: 20200122