GB2452379A - Scroll compressor back pressure chamber defined between seals on spaced planes - Google Patents

Scroll compressor back pressure chamber defined between seals on spaced planes Download PDF

Info

Publication number
GB2452379A
GB2452379A GB0814752A GB0814752A GB2452379A GB 2452379 A GB2452379 A GB 2452379A GB 0814752 A GB0814752 A GB 0814752A GB 0814752 A GB0814752 A GB 0814752A GB 2452379 A GB2452379 A GB 2452379A
Authority
GB
United Kingdom
Prior art keywords
base
scroll member
scroll
back pressure
pressure 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.)
Withdrawn
Application number
GB0814752A
Other versions
GB0814752D0 (en
Inventor
Carlos A Zamudio
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.)
Danfoss Scroll Technologies LLC
Original Assignee
Scroll Technologies LLC
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 Scroll Technologies LLC filed Critical Scroll Technologies LLC
Publication of GB0814752D0 publication Critical patent/GB0814752D0/en
Publication of GB2452379A publication Critical patent/GB2452379A/en
Withdrawn legal-status Critical Current

Links

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
    • F04C18/00Rotary-piston pumps specially adapted for elastic fluids
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0215Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form where only one member is moving
    • 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
    • F04C18/02Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents
    • F04C18/0207Rotary-piston pumps specially adapted for elastic fluids of arcuate-engagement type, i.e. with circular translatory movement of co-operating members, each member having the same number of teeth or tooth-equivalents both members having co-operating elements in spiral form
    • F04C18/0246Details concerning the involute wraps or their base, e.g. geometry
    • F04C18/0253Details concerning the base
    • 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
    • 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
    • F04C27/00Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
    • 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
    • F04C27/00Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
    • F04C27/005Axial sealings for working fluid
    • 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
    • F04C27/00Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids
    • F04C27/008Sealing arrangements in rotary-piston pumps specially adapted for elastic fluids for other than working fluid, i.e. the sealing arrangements are not between working chambers of the machine

Abstract

A scroll compressor has a back pressure chamber 56 defined by two seals 58, 64 on different planes. Locating the seals on two distinct planes allows a more direct connection for a tap 66 from a compression chamber to the back pressure chamber and the volume of the back pressure chamber can be made significantly larger, reducing resistance at startup of the scroll compressor. The radially inner seal 58 may be formed between a radially extending flange 54 on the foot of an orbiting scroll drive boss 52 and a crank case lower surface 60. The radially outer seal 64 may be at a portion of the crank case adjacent the orbiting scroll base 51. The seals may be held in either or both of the orbiting scroll components or the crank case.

Description

AXIAL COMPLIANCE
BACKGROUND OF THE INVENTION
This application relates to a scroll compressor wherein a back pressure chamber is defined by inner and outer seals, with the seals on different planes. The formation of a tap for the back pressure chamber is simplified, and there is also less resistance at startup.
Scroll compressors are becoming widely utilized in refrigerant compression applications. In a scroll compressor, a first scroll member has a base and a generally spiral wrap extending from the base. A second scroll member has a base and a generally spiral wrap extending from its base. The wraps interfit to define compression chambers, and one of the two scroll members is caused to orbit relative to the other. As the scroll member orbits, the size of the compression chambers decreases and an entrapped refrigerant is compressed.
Generally, at least one of the two scroll members is allowed to move axially away from the other. As compression occurs a separating force is created which tends to drive the two scroll members apart. To address the separating force, scroll compressor designers have typically provided a "back pressure chamber." A back pressure chamber typically includes a sealed chamber into which compressed refrigerant is tapped. This compressed refrigerant works in opposition to the previously mentioned separating force, causing the two scroll members to be held in contact with each other.
In the prior art, the back pressure chamber has typically been formed by two radially spaced seals which are mounted in seal recesses in a face of a crankcase.
The prior art back pressure chamber has required that a tap from an intermediate compression chamber to the back pressure chamber go through a plurality of drilled holes. This has resulted in some difficulty in machining the tap.
In addition, due to seal location in a crankcase seal face, and the part geometry (crankcase and orbiting scroll), the prior art back chamber pressure volume is limited to a relatively small volume. Thus, at startup of the compressor, the back pressure chamber fills quickly driving the scroll members into contact, and causing resistance to the orbiting movement from a point relatively soon after startup. This raises challenges under differential pressures for an electric motor that drives the scroll member to orbit.
SUMMARY OF TIlE INVENTION
In the disclosed embodiment of this invention, one of the two seals for defining the back pressure chamber is at a surface which is spaced away from the plane which receives the other seal. In this manner, the seals may be spaced radially further from each other such that a more direct path from the compression chamber to the back pressure chamber can be utilized, and a simple drilled hole can provide the tap.
Further, the radially innermost of the seals can be spaced axially from the radially outermost of the seals to define a relatively large volume back pressure chamber. Thus, it will take a relatively longer time for the back pressure chamber to fill, and for the scroll members to be brought in contact with each other at startup.
In this manner, resistance to movement of the scroll member at startup is significantly reduced. This new arrangement also provides greater flexibility to tailor back chamber volume for optimized starting versus compression ramp-up.
The seals may be in the crankcase or in the orbital scroll.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief
description.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 shows a prior art scroll compressor.
Figure lB shows a detail of the prior art.
Figure 2 shows the inventive scroll compressor.
Figure 3 shows a second embodiment.
Figure 4 shows a third embodiment.
Figure 5 shows a fourth embodiment.
DETAILED DESCRiPTION OF THE PREFERRED EMBODIMENT
A prior art scroll compressor 20 is illustrated in Figure 1. As known, a crankcase 22 is fixed to a non-orbiting scroll member 24. Non-orbiting scroll member 24 has a base 26 and a generally spiral wrap 28 extending from its base. An orbiting scroll member 29 has a base 30 and a generally spiral wrap 32 extending from its base. The orbiting scroll member 29 is supported on the crankcase 22. The wraps of the orbiting scroll and non-orbiting scroll interfit to define compression chambers such as 42. A boss 44 extends rearwardly away from the base 30 and receives a driveshaft 46 through an intermediate slider block 48. As known, the orbiting scroll member is caused to orbit relative to the non-orbiting scroll member.
As this occurs, the size of the compression chambers 42 is decreased to compress an entrapped refrigerant.
A separating force is created in the compression chambers as the refrigerant is compressed. To address this separating force, a back pressure chamber 34 is provided. A radially outer seal 36 and a radially inner seal 38 are mounted within recesses in a face of the crankcase 22. Refrigerant is tapped through a tap 40 from an intermediate pressure compression chamber 42. As shown in Figure 1 B, the tap typically includes three sub portions 40A, 40B and 40C. This is necessary since a compression chamber of significantly high pressure tends to be more radially centered, and the crankcase face which receives the innermost seal is not sufficiently centered. Typically, the crossing path 40B must be drilled from an outer surface of the orbiting scroll and then plugged. The creation of this three-part path is somewhat complex.
In addition, as can be appreciated, the back pressure chamber 34 is very small in volume. At startup, refrigerant sufficient to fill the back pressure chamber 34 is quickly directed through the tap 40 increasing the back chamber pressure and pushing the orbiting scroll member 29 into contact with the non-orbiting scroll 24.
At this point, the motor 100 rotating the driveshaft 46 is still starting up, and it is somewhat difficult for it to overcome the compressive resistance. Therefore, a relatively high torque exists to begin compressing refrigerant. This situation is worst when discharge pressure is significantly higher than suction pressure.
Figure 2 shows a scroll compressor 50 which is modified to address the concerns mentioned above. Scroll compressor 50 modifies the boss 52 such that it has an outwardly extending flange 54. Flange 54 defines an enlarged chamber 56 between a lower surface 60 of the crankcase 22 and an upper surface 62. Lower surface 60 receives a seal 58, while upper surface 62 receives a seal 64. In this manner, the radially inner seal 58 may be positioned more radially inwardly than in the prior art. Thus, the tap 66 can extend directly through the base of the orbiting scroll member. Forming the tap 66 is much simpler than forming the tap 40. In addition, the volume of the chamber 56 is much larger than the volume of the prior art back pressure chamber 34. A longer period of time is required after startup for the back pressure chamber 56 to pressurize and push the orbiting scroll member 51 into contact with the non-orbiting scroll member 24. The volume that controls this start-up torque can be adjusted by several methods, including, as an example, thickening of flange 54 or boss 52 or adding additional boss to upper surface 62.
Thus, the start-up torque resistance on the motor is reduced until the motor is rotating at a significantly higher speed.
An embodiment 150 is shown in Figure 3, wherein the radially inner seal 156 is in the hub 154 of the orbiting scroll 152. The radially outer seal 64 remains in the crankcase. Of course, the two seal locations could be reversed, with the radially outer seal in the orbiting scroll and the radially inner seal in the crankcase.
Figure 4 shows another embodiment 250 wherein the orbiting scroll 252 has the hub 254 receiving the radially inner seal 258. The base of the orbiting scroll 252 receives the radially outer seal 256.
Figure 5 shows another embodiment 300 wherein the orbiting scroll 302 includes a hub 305 with a separate member 308 that contacts the radially inner seal 306. The radially outer seal 304 sits in the crankcase in this embodiment. In this embodiment, the formation of the orbiting scroll is simplified in that the hub need not have the radially outwardly extending lowermost portion, but can instead receive a separate component to provide that function.
Although a preferred embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.

Claims (10)

  1. I. A scroll compressor comprising: a first scroll member having a base and a generally spiral wrap extending fromitsbase; a second scroll member having a base and a generally spiral wrap extending from its base, said second scroll member having a boss extending in an opposed direction from said base relative to said wrap, and a driveshafi causing orbiting motion of the scroll members relative to each other; a housing supporting said second scroll member, said housing having a first surface adjacent to said base of said second scroll member, and a radially outer seal sealing at said first surface, said second scroll member being adjacent to a second surface of said housing on a plane spaced from said first surface and said base of said second scroll member, a radially inner seal at said second surthce, and said inner and outer seals defining a back pressure chamber; and a tap extending from a compression chamber through said base of said second scroll member and into said back pressure chamber.
  2. 2. The scroll compressor as recited in Claim 1, wherein said tap extends directly through said base along a single direction.
  3. 3. The scroll compressor as recited in Claim I or 2, wherein said boss extends axially away from said base and then has a surface which is adjacent to said second surface.
  4. 4. The scroll compressor as recited in Claim 3, wherein said surface is formed integrally with said boss.
  5. 5. The scroll compressor as recited in Claim 3, wherein said surface is formed as a separate part from said boss.
  6. 6. The scroll compressor as recited in any of Claims I to 5, wherein said radially inner and said radially outer seals are both received in recesses in said housing.
  7. 7. The scroll compressor as recited in any of Claims 1 to 5, wherein said radially inner and said radially outer seals are both received in said recesses in said second scroll member.
  8. 8. The scroll compressor as recited in any of Claims Ito 5, wherein one of said radially inner seal and said radially outer seal is received in a recess in said housing, and the other of said radially inner seal and said radially outer seal is received in a recess in said second scroll member.
  9. 9. A scroll compressor comprising: a first scroll member having a base and a generally spiral wrap extending from its base; a second scroll member having a base and a generally spiral wrap extending from its base, said second scroll member having a boss extending in an opposed direction from said base relative to said wrap, said second scroll member receiving a driveshaft within said boss, and said driveshaft causing said second scroll member to orbit relative to said first scroll member; a crankcase supporting said second scroll member, said crankcase having a first surface in contact with said base of said second scroll member, and receiving a radially outer seal, said second scroll member contacting a second surface of said crankcase on a plane spaced from a contact plane between said first surface and said base of said second scroll member, said second surface receiving a radially inner seal, and said inner and outer seals defining a back pressure chamber, said boss extends axially away from said base and then has a radially outwardly extending lip which contacts said second surface; and a tap extending from said one of said compression chambers along a single direction through said base of said second scroll member and into said back pressure chamber.
  10. 10. A scroll compressor substantially as described herein and as illustrated in the accompanying drawings.
GB0814752A 2007-08-30 2008-08-13 Scroll compressor back pressure chamber defined between seals on spaced planes Withdrawn GB2452379A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/847,464 US20090060767A1 (en) 2007-08-30 2007-08-30 Axial compliance

Publications (2)

Publication Number Publication Date
GB0814752D0 GB0814752D0 (en) 2008-09-17
GB2452379A true GB2452379A (en) 2009-03-04

Family

ID=39790677

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0814752A Withdrawn GB2452379A (en) 2007-08-30 2008-08-13 Scroll compressor back pressure chamber defined between seals on spaced planes

Country Status (3)

Country Link
US (1) US20090060767A1 (en)
CN (1) CN101377197A (en)
GB (1) GB2452379A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112204259A (en) * 2018-07-05 2021-01-08 大金工业株式会社 Scroll compressor having a discharge port

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107476970B (en) * 2016-06-07 2020-01-31 艾默生环境优化技术(苏州)有限公司 Scroll compressor having a plurality of scroll members
US10975868B2 (en) 2017-07-07 2021-04-13 Emerson Climate Technologies, Inc. Compressor with floating seal
US11692548B2 (en) 2020-05-01 2023-07-04 Emerson Climate Technologies, Inc. Compressor having floating seal assembly
US11578725B2 (en) 2020-05-13 2023-02-14 Emerson Climate Technologies, Inc. Compressor having muffler plate
US11655818B2 (en) 2020-05-26 2023-05-23 Emerson Climate Technologies, Inc. Compressor with compliant seal
US11767846B2 (en) 2021-01-21 2023-09-26 Copeland Lp Compressor having seal assembly
CN114215750B (en) * 2021-11-24 2024-01-23 苏州为山之环境技术有限公司 Axial sealing mechanism and scroll compressor comprising same

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01187388A (en) * 1988-01-19 1989-07-26 Hitachi Ltd Scroll compressor
US6139294A (en) * 1998-06-22 2000-10-31 Tecumseh Products Company Stepped annular intermediate pressure chamber for axial compliance in a scroll compressor
US20050226755A1 (en) * 2004-04-12 2005-10-13 Takeshi Tsuchiya Scroll compressor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH01187388A (en) * 1988-01-19 1989-07-26 Hitachi Ltd Scroll compressor
US6139294A (en) * 1998-06-22 2000-10-31 Tecumseh Products Company Stepped annular intermediate pressure chamber for axial compliance in a scroll compressor
US20050226755A1 (en) * 2004-04-12 2005-10-13 Takeshi Tsuchiya Scroll compressor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112204259A (en) * 2018-07-05 2021-01-08 大金工业株式会社 Scroll compressor having a discharge port
CN112204259B (en) * 2018-07-05 2021-09-07 大金工业株式会社 Scroll compressor having a discharge port

Also Published As

Publication number Publication date
CN101377197A (en) 2009-03-04
GB0814752D0 (en) 2008-09-17
US20090060767A1 (en) 2009-03-05

Similar Documents

Publication Publication Date Title
GB2452379A (en) Scroll compressor back pressure chamber defined between seals on spaced planes
US9316225B2 (en) Scroll compressor with thrust sliding surface oiling groove
WO2012127795A1 (en) Scroll-type compressor
AU780605B2 (en) Scroll compressor having a clearance for the oldham coupling
US9541083B2 (en) Scroll compressor including communication hole with improved back pressure chamber and back pressure hole locations
JP4903826B2 (en) Scroll fluid machinery
KR20070093638A (en) Oil separation apparatus for scroll compressor
JP2012097646A (en) Scroll compressor
CN102985696A (en) Scroll compressor
US20150322947A1 (en) Scroll-Type Fluid Machine
CN109844318B (en) Scroll compressor having a plurality of scroll members
JP4882643B2 (en) Scroll type expander
JP4930022B2 (en) Fluid machinery
JP6906887B2 (en) Scroll fluid machine
JP2008121481A (en) Scroll fluid machine
US5848883A (en) Scroll compressor having a back pressure partitioning member
US9695823B2 (en) Compressor with unloader counterweight assembly
US7641456B2 (en) Scroll compressor with back pressure chamber cavity for assisting in start-up
JP2016156297A (en) Scroll compressor
JP2006009614A (en) Scroll compressor
JP4385917B2 (en) Scroll compressor
KR20070120849A (en) Back pressure sealing apparatus for scroll compressor
KR100524789B1 (en) Thrust bearing for scroll compressor
JP2743877B2 (en) Scroll compressor
JPH09158857A (en) Hermetic type motor-driven scroll compressor

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)