US3619078A - Centrifugal gas compressor - Google Patents

Centrifugal gas compressor Download PDF

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Publication number
US3619078A
US3619078A US48358A US3619078DA US3619078A US 3619078 A US3619078 A US 3619078A US 48358 A US48358 A US 48358A US 3619078D A US3619078D A US 3619078DA US 3619078 A US3619078 A US 3619078A
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valve
links
casing
pair
diffuser passage
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US48358A
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Gordon L Mount
James W Endress
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Carrier Corp
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Carrier Corp
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44Fluid-guiding means, e.g. diffusers
    • F04D29/46Fluid-guiding means, e.g. diffusers adjustable
    • F04D29/462Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps
    • F04D29/464Fluid-guiding means, e.g. diffusers adjustable especially adapted for elastic fluid pumps adjusting flow cross-section, otherwise than by using adjustable stator blades

Definitions

  • One pair is disposed normal to the other pairs
  • Like ends of the links are pivotally connected to the machine casing
  • the opposite ends of the links of each pair are pivotally connected to the valve at diametrically opposite sides thereof, whereby the valve is held concentric with the impeller for free linear movement across the diffuser passage.
  • Power means is provided for imparting such linear movement to the valve.
  • centrifugal gas compressors may be controlled by varying the flow of gas through the diffuser passage of the compressor as by movement of an annular diffuser valve transversely across the diffuser passage.
  • annular valve is slidably mounted on a series of guide pins fixed in the casing of the machine.
  • valve is slidably mounted in a circular recess formed in a sidewall of the diffuser passage.
  • the valve is mounted in such manner that upon relative rotation between the valve and a circular cam member, linear movement is imparted to the valve.
  • Our invention has as an object a diffuser valve supporting and operating mechanism involving only a few parts of a simple form which are manufactured at an exceptionally low cost and which serve to support the valve for free movement without canting or binding and requiring only nominal power to effect such movement.
  • FIG. 1 is an end elevational view of the diffuser valve and the supporting mechanism, the view being indicated as by the line 1-1 ofFIG. 2;
  • FIG. 2 is a sectional view taken diametrically through the disclosure in FIG. 1, as indicated by the line 2-2 and including contiguous portions of the compressor;
  • FIG. 3 is a partial sectional view taken as indicated by line 33 of FIG. 1;
  • FIG. 4 is an enlarged view taken on line 4-4 of FIG. 1;
  • FIG. 5 is a view similar to FIG. 4 taken on line 55 of FIG. 1.
  • the general arrangement of the compressor is of conventional form including a housing in which there is joumaled a shaft 11 to which is affixed an impeller 12.
  • the housing 10 forms one wall 13 of the diffuser passage 14.
  • the opposite wall 15 of the diffuser passage is formed by an annular member 16 seated in a circular recess formed in the housing 10 and having a radial flange 17 against a shoulder formed in the housing.
  • the machine further includes an outer housing section 20 fixedly secured to the housing 10 as by screws 21.
  • the outer section 20 is formed with a cylindrical flange 23 which abuts against the flange 17 of the member 16 to fixedly secure the same to the housing 10.
  • An outer intake manifold section 25 is fixedly mounted to the section 20 as by screws 27.
  • An inner manifold section is also fixed within the section 20 as by screws 31.
  • the annular diffuser valve is formed with a cylindrical flange portion 37 positioned between the bore of the member 16 and the periphery of the inner end of the inner manifold section 30 (FIG. 2).
  • the valve 35 is supported by two pairs of links.
  • 40, d1 designates one pair of these links.
  • the links are disposed in spaced-apart parallel relation; and like ends of these links 40, 41 are pivotally connected to the machine casing, specifically to the annular diffuser wall member 16.
  • This connection is established by blocks 43 fixed to the member 16 as by screws 45.
  • the blocks 43 are apertured to receive a shaft 47 having end portions extending beyond the blocks and to which the links 40, 41 are connected. REtaining members 50 applied to the ends of the shaft 47 restrain displacement of the links 40, 41 therefrom.
  • the supporting structure for the valve includes a second pair of links 60, 61.
  • the second pair of links are pivotally connected to the member 16 and to the valve 35 in like fashion to the connection for the links 40, 41.
  • the links 60, 61 are also disposed in spaced parallel relationship with like ends pivotally connected to the member 16 by shaft 67 mounted in blocks 68 fixed to the member 16 by screws 69.
  • the second pair of links 60, 61 are disposed normal to the links 40, 41; and the pivotal connection between the inner ends of these links and the valve 35 is by way of screws 70.
  • the screws 51, 70 are mounted in the valve 35 at diametrically opposite sides thereof, the screws 70 being displaced circumferentially on the valve 35 90 from the screws 51.
  • Retaining members 73 are employed to prevent displacement of the inner ends of the links 60, 61 from the screws 70.
  • the links 40, 41 and 60, 61 are curved at their ends whereby the main connecting portion of the links is offset from the mounting pivots 47, 67, 51, 70. It will be observed, referring to FIGS. 2 and 3, the links 40, 41 are formed with a greater offset than the links 60, 61 inasmuch as one of the links 40, 41 has to be disposed above the links 60 or 61 of the other pair.
  • the diffuser valve 35 hangs perfectly normal to the axis of the impeller concentrically thereto and for free movement in an axial direction of the impeller transversely of the diffuser passage 14. With this arrangement, there is no possibility of a diffuser valve canting or binding.
  • a small motor is fixedly mounted on the member 16 as by screws 81 extending through elongated apertures 82 formed in the motor base and threading into the member 16.
  • the motor includes a suitable gear reduction and has an output shaft 83 to which there is affixed a cam 85.
  • the cam is positioned in an elongated aperture 87 formed in a block 88 fixed to the valve 35 as by screws 90.
  • the motor 80 is of the reversible type; and upon energization of the motor, effecting rotation of the cam 85, it will be apparent that the valve member 35 is moved transversely across the diffuser passage 14.
  • a centrifugal gas compressor including a casing, an impeller joumaled in said casing, said casing being formed with a diffuser passage encircling said impeller and extending outwardly therefrom, an annular diffuser valve disposed for movement transversely of said diffuser passage to control the flow of gas through said passage, mechanism for reciprocating said valve for movement transversely across said diffuser passage, said mechanism comprising a first pair of links extending in spaced-apart parallel relation, said links being pivotally connected at like ends to said casing outwardly from said valve, said links being pivotally connected at their opposite ends to said valve at diametrically opposite sides thereof, a second pair of like links pivotally connected in like manner to said casing and said valve, the links of said second pair extending in a direction normal to the links of said first pair, the pivotal connection between the links of said second wall of said diffuser passage, said like ends of said links being pivotally connected to said annular member.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The annular diffuser valve of the centrifugal compressor is supported on two pairs of links or bars. One pair is disposed normal to the other pair. Like ends of the links are pivotally connected to the machine casing. The opposite ends of the links of each pair are pivotally connected to the valve at diametrically opposite sides thereof, whereby the valve is held concentric with the impeller for free linear movement across the diffuser passage. Power means is provided for imparting such linear movement to the valve.

Description

United States Patent Gordon L. Mount West Monroe; James W. Endress, Syracuse. both of N.Y.
Inventors Appl No. 48,358
Filed June 22, 1970 Patented Nov. 9, 1971 Assignee Carrler Corporation Syracuse. N.Y.
CENTRIFUGAL GAS COMPRESSOR 3 Claims, 5 Drawing Figs.
U.S.Cl 415/150 Int. Cl ..F04d 27/00. F04d 15/00 Field of Search 415/148,
[56] References Cited UNITED STATES PATENTS 565,848 8/1896 Elmer .4 415/158 2,682,826 7/1954 Wahlborg 415/157 2,861,774 11/1953 Buchi 60/13 3,032,259 5/1962 Jassniker... 415/148 3,079,127 2/1963 Rowlett et al 415/150 Primary Examiner-Henry F Raduazo Allorneys-Harry G. Martin. 11'. and 1. Raymond Curtin ABSTRACT: The annular diffuser valve of the centrifugal compressor is supported on two pairs of links or bars. One pair is disposed normal to the other pairs Like ends of the links are pivotally connected to the machine casing The opposite ends of the links of each pair are pivotally connected to the valve at diametrically opposite sides thereof, whereby the valve is held concentric with the impeller for free linear movement across the diffuser passage. Power means is provided for imparting such linear movement to the valve.
PATENTEUN V 9 SHEET 1 OF 2 ATTORNEY PATENTEUunv 9197i SHEET 2 BF 2 INVENTOR. G DON L. MOUNT ES ENDRESS ATTZZNEY CENTRIFUGAL GAS COMPRESSOR BACKGROUND OF THE INVENTION The output or capacity of centrifugal gas compressors may be controlled by varying the flow of gas through the diffuser passage of the compressor as by movement of an annular diffuser valve transversely across the diffuser passage. Various arrangements have been employed for supporting such a valve and for moving the same for regulation of the compressor capacity. In one arrangement, the annular valve is slidably mounted on a series of guide pins fixed in the casing of the machine. In another construction, the valve is slidably mounted in a circular recess formed in a sidewall of the diffuser passage. In still another arrangement, the valve is mounted in such manner that upon relative rotation between the valve and a circular cam member, linear movement is imparted to the valve.
All of these constructions are complicated and costly to build and assemble in the compressor. A further disadvantage resides in the fact that the valves so mounted tend to cant and stick and become inoperable, requiring disassembly of a major I portion of the machine to correct the difficulty.
Our invention has as an object a diffuser valve supporting and operating mechanism involving only a few parts of a simple form which are manufactured at an exceptionally low cost and which serve to support the valve for free movement without canting or binding and requiring only nominal power to effect such movement.
SUMMARY OF THE INVENTION BRIEF DESCRIPTION OF THE DRAWINGS In the drawings, FIG. 1 is an end elevational view of the diffuser valve and the supporting mechanism, the view being indicated as by the line 1-1 ofFIG. 2;
FIG. 2 is a sectional view taken diametrically through the disclosure in FIG. 1, as indicated by the line 2-2 and including contiguous portions of the compressor;
FIG. 3 is a partial sectional view taken as indicated by line 33 of FIG. 1;
FIG. 4 is an enlarged view taken on line 4-4 of FIG. 1; and
FIG. 5 is a view similar to FIG. 4 taken on line 55 of FIG. 1.
DESCRIPTION OF THE PREFERRED EMBODIMENT The general arrangement of the compressor is of conventional form including a housing in which there is joumaled a shaft 11 to which is affixed an impeller 12. The housing 10 forms one wall 13 of the diffuser passage 14. The opposite wall 15 of the diffuser passage is formed by an annular member 16 seated in a circular recess formed in the housing 10 and having a radial flange 17 against a shoulder formed in the housing. The machine further includes an outer housing section 20 fixedly secured to the housing 10 as by screws 21. The outer section 20 is formed with a cylindrical flange 23 which abuts against the flange 17 of the member 16 to fixedly secure the same to the housing 10. An outer intake manifold section 25 is fixedly mounted to the section 20 as by screws 27. An inner manifold section is also fixed within the section 20 as by screws 31.
The annular diffuser valve is formed with a cylindrical flange portion 37 positioned between the bore of the member 16 and the periphery of the inner end of the inner manifold section 30 (FIG. 2).
The valve 35 is supported by two pairs of links. Referring to FIG. 1, 40, d1 designates one pair of these links. It will be seen that the links are disposed in spaced-apart parallel relation; and like ends of these links 40, 41 are pivotally connected to the machine casing, specifically to the annular diffuser wall member 16. This connection is established by blocks 43 fixed to the member 16 as by screws 45. The blocks 43 are apertured to receive a shaft 47 having end portions extending beyond the blocks and to which the links 40, 41 are connected. REtaining members 50 applied to the ends of the shaft 47 restrain displacement of the links 40, 41 therefrom.
The opposite ends of these links are pivotally connected to the difiuser valve 35 as by screws 51 extending through the valve to receive the opposite ends of the links, which are retained against displacement by retaining rings 53 applied to the inner ends of the screws.
The supporting structure for the valve includes a second pair of links 60, 61. The second pair of links are pivotally connected to the member 16 and to the valve 35 in like fashion to the connection for the links 40, 41. Referring again to FIG. I, it will be seen the links 60, 61 are also disposed in spaced parallel relationship with like ends pivotally connected to the member 16 by shaft 67 mounted in blocks 68 fixed to the member 16 by screws 69. The second pair of links 60, 61 are disposed normal to the links 40, 41; and the pivotal connection between the inner ends of these links and the valve 35 is by way of screws 70. The screws 51, 70 are mounted in the valve 35 at diametrically opposite sides thereof, the screws 70 being displaced circumferentially on the valve 35 90 from the screws 51. Retaining members 73 are employed to prevent displacement of the inner ends of the links 60, 61 from the screws 70.
The links 40, 41 and 60, 61 are curved at their ends whereby the main connecting portion of the links is offset from the mounting pivots 47, 67, 51, 70. It will be observed, referring to FIGS. 2 and 3, the links 40, 41 are formed with a greater offset than the links 60, 61 inasmuch as one of the links 40, 41 has to be disposed above the links 60 or 61 of the other pair.
With this arrangement, it will be apparent that the diffuser valve 35 hangs perfectly normal to the axis of the impeller concentrically thereto and for free movement in an axial direction of the impeller transversely of the diffuser passage 14. With this arrangement, there is no possibility of a diffuser valve canting or binding.
To effect movement of the valve transversely of the diffuser passage, a small motor is fixedly mounted on the member 16 as by screws 81 extending through elongated apertures 82 formed in the motor base and threading into the member 16. (See FIG. 1) The motor includes a suitable gear reduction and has an output shaft 83 to which there is affixed a cam 85. (See FIG. 5.) The cam is positioned in an elongated aperture 87 formed in a block 88 fixed to the valve 35 as by screws 90. The motor 80 is of the reversible type; and upon energization of the motor, effecting rotation of the cam 85, it will be apparent that the valve member 35 is moved transversely across the diffuser passage 14.
We claim:
1. A centrifugal gas compressor including a casing, an impeller joumaled in said casing, said casing being formed with a diffuser passage encircling said impeller and extending outwardly therefrom, an annular diffuser valve disposed for movement transversely of said diffuser passage to control the flow of gas through said passage, mechanism for reciprocating said valve for movement transversely across said diffuser passage, said mechanism comprising a first pair of links extending in spaced-apart parallel relation, said links being pivotally connected at like ends to said casing outwardly from said valve, said links being pivotally connected at their opposite ends to said valve at diametrically opposite sides thereof, a second pair of like links pivotally connected in like manner to said casing and said valve, the links of said second pair extending in a direction normal to the links of said first pair, the pivotal connection between the links of said second wall of said diffuser passage, said like ends of said links being pivotally connected to said annular member.
3. A centrifugal gas compressor as set forth in claim 1 wherein said casing includes an annular mcmber'forming a wall of said diffuser passage, and said power valve operating means includes a prime mover fixedly mounted on said annular member and motion transmitting means operatively connecting said prime mover to said valve.
w a a 1- s UNITED PATENT OFF ICE 7 CERTIFICAFFE OF CORRECTION Patent No. 3,619,078 Dated November 9, 1971 Inventor(s) GORDON L. MOUNT 80 JAMES W. ENDRESS It is certified that error appears in the above-identified patent and that said Letters Patent are hereby corrected as shown below:
Column 1, line 39, after impeller insert --for free movement in a direction axially of the impeller-- Signed and sealed this 30th day of May 1972.
(SEAL Attest:
EDWARD M.FLETCHER, JR. ROBERT GOTTSGHALK V Attesting Officer Commissioner of Patents USCOMM'DC 0081 l-POD RM PO-1050 (10-69] a us. aovunuim Pnmflnu umc: nu o-au-au

Claims (3)

1. A centrifugal gas compressor including a casing, an impeller journaled in said casing, said casing being formed with a diffuser passage encircling said impeller and extending outwardly therefrom, an annular diffuser valve disposed for movement transversely of said diffuser passage to control the flow of gas through said passage, mechanism for reciprocating said valve for movement transversely across said diffuser passage, said mechanism comprising a first pair of links extending in spacedapart parallel relation, said links being pivotally connected at like ends to said casing outwardly from said valve, said links being pivotally connected at their opposite ends to said valve at diametrically opposite sides thereof, a second pair of like links pivotally connected in like manner to said casing and said valve, the links of said second pair extending in a direction normal to the links of said first pair, the pivotal connection between the links of said second pair and said valve being spaced circumferentially of said valve 90* from such connections of the links in said first pair, whereby said valve is supported and maintained in concentric relation to said impeller by said links for axial movement in a linear path transversely of said diffuser passage, and power valve operating means connected to said casing and operable to effect such movement of said valve.
2. A centrifugal gas compressor as set forth in claim 1 wherein said casing includes an annular member forming a wall of said diffuser passage, said like ends of said links being pivotally connected to said annular member.
3. A centrifugal gas compressor as set forth in claim 1 wherein said casing includes an annular member forming a wall of said diffuser passage, and said power valve operating means includes a prime mover fixedly mounted on said annular member and motion transmitting means operatively connecting said prime mover to said valve.
US48358A 1970-06-22 1970-06-22 Centrifugal gas compressor Expired - Lifetime US3619078A (en)

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Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4219305A (en) * 1978-12-26 1980-08-26 Carrier Corporation Diffuser control
US4257733A (en) * 1978-12-26 1981-03-24 Carrier Corporation Diffuser control
US4416583A (en) * 1980-04-04 1983-11-22 Carrier Corporation Centrifugal vapor compressor
US4460310A (en) * 1982-06-28 1984-07-17 Carrier Corporation Diffuser throttle ring control
WO2014074448A1 (en) * 2012-11-09 2014-05-15 Johnson Controls Technology Company Variable geometry diffuser having extended travel and control method thereof
US20150275917A1 (en) * 2014-03-26 2015-10-01 Kabushiki Kaisha Toyota Jidoshokki Centrifugal Compressor
US20160208808A1 (en) * 2013-08-26 2016-07-21 Gree Electric Appliances, Inc. Of Zhuhai Regulator assembly and centrifugal compressor
EP4177476A1 (en) * 2021-11-03 2023-05-10 Trane International Inc. Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors
EP4177477A1 (en) * 2021-11-03 2023-05-10 Trane International Inc. Compressor interstage throttle, and method of operating therof
US11661949B2 (en) 2020-04-30 2023-05-30 Trane International Inc. Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors
US11859621B2 (en) 2020-04-30 2024-01-02 Trane International Inc. Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US565848A (en) * 1896-08-11 Turbine
US2682826A (en) * 1944-07-12 1954-07-06 Hjorth & Co Ab Electrically driven fan
US2861774A (en) * 1950-02-16 1958-11-25 Alfred J Buchi Inlet control for radial flow turbines
US3032259A (en) * 1957-12-23 1962-05-01 Sulzer Ag Turbocompressor having a radial diffuser
US3079127A (en) * 1956-11-23 1963-02-26 Garrett Corp Temperature responsive variable means for controlling flow in turbomachines

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US565848A (en) * 1896-08-11 Turbine
US2682826A (en) * 1944-07-12 1954-07-06 Hjorth & Co Ab Electrically driven fan
US2861774A (en) * 1950-02-16 1958-11-25 Alfred J Buchi Inlet control for radial flow turbines
US3079127A (en) * 1956-11-23 1963-02-26 Garrett Corp Temperature responsive variable means for controlling flow in turbomachines
US3032259A (en) * 1957-12-23 1962-05-01 Sulzer Ag Turbocompressor having a radial diffuser

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4219305A (en) * 1978-12-26 1980-08-26 Carrier Corporation Diffuser control
US4257733A (en) * 1978-12-26 1981-03-24 Carrier Corporation Diffuser control
US4416583A (en) * 1980-04-04 1983-11-22 Carrier Corporation Centrifugal vapor compressor
US4460310A (en) * 1982-06-28 1984-07-17 Carrier Corporation Diffuser throttle ring control
CN107255083B (en) * 2012-11-09 2019-11-29 江森自控科技公司 With the geometry-variable diffuser and its control method for extending stroke
US11092166B2 (en) 2012-11-09 2021-08-17 Johnson Controls Technology Company Variable geometry diffuser having extended travel and control method thereof
CN107313986B (en) * 2012-11-09 2020-01-17 江森自控科技公司 Variable geometry diffuser, compressor having the same, and control method thereof
EP3171034A1 (en) * 2012-11-09 2017-05-24 Johnson Controls Technology Company Variable geometry diffuser having extended travel
EP3171035A1 (en) * 2012-11-09 2017-05-24 Johnson Controls Technology Company Variable geometry diffuser having extended travel
CN104854351B (en) * 2012-11-09 2017-09-01 江森自控科技公司 Geometry-variable diffuser and its control method with extension stroke
CN107255083A (en) * 2012-11-09 2017-10-17 江森自控科技公司 Geometry-variable diffuser and its control method with extension stroke
CN107313986A (en) * 2012-11-09 2017-11-03 江森自控科技公司 Geometry-variable diffuser and its control method with extension stroke
WO2014074448A1 (en) * 2012-11-09 2014-05-15 Johnson Controls Technology Company Variable geometry diffuser having extended travel and control method thereof
US10378553B2 (en) 2012-11-09 2019-08-13 Johnson Controls Technology Company Variable geometry diffuser having extended travel and control method thereof
US10082147B2 (en) * 2013-08-26 2018-09-25 Gree Electric Appliances, Inc. Of Zhuhai Regulator assembly and centrifugal compressor
US20160208808A1 (en) * 2013-08-26 2016-07-21 Gree Electric Appliances, Inc. Of Zhuhai Regulator assembly and centrifugal compressor
US9874226B2 (en) * 2014-03-26 2018-01-23 Kabushiki Kaisha Toyota Jidoshokki Centrifugal compressor
US20150275917A1 (en) * 2014-03-26 2015-10-01 Kabushiki Kaisha Toyota Jidoshokki Centrifugal Compressor
US11661949B2 (en) 2020-04-30 2023-05-30 Trane International Inc. Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors
US11859621B2 (en) 2020-04-30 2024-01-02 Trane International Inc. Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors
EP4177476A1 (en) * 2021-11-03 2023-05-10 Trane International Inc. Interstage capacity control valve with side stream flow distribution and flow regulation for multi-stage centrifugal compressors
EP4177477A1 (en) * 2021-11-03 2023-05-10 Trane International Inc. Compressor interstage throttle, and method of operating therof
US11841026B2 (en) 2021-11-03 2023-12-12 Trane International Inc. Compressor interstage throttle, and method of operating therof

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