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US3644054A - Compressor base and intercoolers - Google Patents

Compressor base and intercoolers
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Publication number
US3644054A
US3644054AUS44034AUS3644054DAUS3644054AUS 3644054 AUS3644054 AUS 3644054AUS 44034 AUS44034 AUS 44034AUS 3644054D AUS3644054D AUS 3644054DAUS 3644054 AUS3644054 AUS 3644054A
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fluid
compressor
stage
intercooler
heat exchangers
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US44034A
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Karol Pilarczyk
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Carrier Corp
Elliott Turbomachinery Co Inc
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Carrier Corp
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Assigned to ELLIOTT TURBOMACHINERY CO., INC.reassignmentELLIOTT TURBOMACHINERY CO., INC.ASSIGNMENT OF ASSIGNORS INTEREST.Assignors: CARRIER CORPORATION, A CORP OF DEL.
Assigned to FIRST NATIONAL BANK OF CHICAGO, THEreassignmentFIRST NATIONAL BANK OF CHICAGO, THELICENSE (SEE DOCUMENT FOR DETAILS).Assignors: ELLIOT TURBOMACHINERY CO., INC.
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Abstract

A base containing a pair of identical heat exchangers, demisters and separators has rigidly mounted thereon a cast multistage compressor casing provided with integral air inlet and discharge passages in direct communication with corresponding passages in the top wall of the base for providing the intercooling between stages. Fluid passes through the intercoolers by moving downwardly through the heat exchangers, downwardly through restricted nozzles and reversely upwardly for separating condensation, upwardly through the demisters and through central partition walls forming central manifold chambers. The liquid connections for the intercoolers may be uncoupled at one end for sliding the intercoolers off shelves from the opposite end. A telescopic resilient coupling between the casing inlet to the rotor and an inlet housing rigidly coupled to a fluid supply will prevent transmission of forces therebetween. The base further mounts the drive structure for the compressor and carries an oil sump below the drive structure.

Description

[ Feb. 22, 1972 United States Patent Pilarczyk [54] COMPRESSOR BASE AND Primary Examiner-Henry F. Raduazo Attorney-Harry G. Martin, Jr. and J Raymond Curtin INTERCOOLERS [72] Inventor: Karo1Pi1arczyk,Loudonvi1le,N.Y.
ABSTRACT [73] Assignee: Carrier Corporation, Syracuse, NY.
.c t r-ll mp m nOdV icne ewm. h 2. .m w d w ".w fmo. HOD. fetu m i s hd u i nS.1. u e n ia now 0.0 t e umhw 0 t1 mm w P uo Ufi C 0 t. c Y nwmm uv i mnhl b fi y un 35 m W mmmh uht 66mm 415/122 .415/199 v....4l5/179 .....415/199 ....415/l75 FOREIGN PATENTS OR APPLICATIONS transmission of forces therebetween. The base further mounts 1/1968 Medgyesy.... 485 11/1969 1 sump the drive structure for the compressor and carries an oi below the drive structure.
Kunderman M S m c E mn T La A mmm i S wo D SSH m 57 N M66 U 999 111 WW 1 226 959 630 mm% 333 12 Claims, 5 Drawing Figures 563,532 8/1944 GreatBritain........................415/199 COMPRESSOR BASE AND INTERCOOLERS BACKGROUND OF THE INVENTION intercooler structure has heretofore been one of the largest components of a multistage compressor, which not only increases the cost of the compressor but of more importance increases the space required for mounting the compressor unit. The intercooler structure of the patent to Schierl, U.S. Pat. No. 3,001,692, issued Sept. 26, 1961, overcomes some of the problems in the prior art but still employs a rather large base in comparison to the size of the heat exchangers used and employs a considerable amount of piping between stages and waste space within the base.
The air connections for the Olmstead et al. patent, US. Pat. No. 2,849,960, issued Sept. 2, 1958, have advantages with respect to force transmittal, but present a rather complicated structure that must be assembled at the use location and does not provide any rigid support for the adjacent piping extending away from the pump.
CROSS-REFERENCE TO RELATED APPLICATIONS The features of the invention of this application may be used in combination with the features of the inventions in applicants following related applications of the same filing date and assignee as the present application, the disclosures of which are incorporated herein in their entirety by reference: Compressor Barrel Assembly," Ser. No 44,446; Compressor Power Recovery," Ser. No. 44,463; Interchangeable Compressor Drive, Ser. No. 44,403; Variable Capacity Compressor," Ser. No. 44,263.
BRIEF DESCRIPTION OF THE DRAWING Further objects, features and advantages in the present invention will become more clear from the following detailed description of a preferred embodiment as shown in the attached drawing, in which:
FIG. 1 is a perspective view of a multistage centrifugal compressor;
FIG. 2 is a schematic flow diagram showing the relationship of the compressor stages and intercoolers;
FIG. 3 is a partial cross section side elevation view, with the cross sections being taken in a vertical plane passing through the axes of rotation of the compressor rotor and drive assembly;
FIG. 4 is a partial cross section and exploded view of a portion ofthe structure as shown in FIG. 1; and
FIG. 5 is a cross-sectional view taken on line 5-5 in FIG. 3 showing the air discharge manifold of the intercoolers.
DETAILED DESCRIPTION OF THE DRAWING The base 1 as shown in FIG. I has mounted rigidly thereon anfluid inlet housing 2 by means of a plurality of bolts (not shown) passing throughbolt holes 3, a one-piececast compressor casing 4 by means of a plurality of bolts 5, a gear housing 6 by means ofa plurality ofbolts 7, anelectric drive motor 8 by means of resilient pads 9, and acontrol panel 10 by any conventional means.
Theinlet housing 2 is provided with an annular flange 11 provided with a plurality of peripherally arrangedholes 12 for rigidly securing thereto an inlet fluid pipe when assembling the compressor at the use location. An upwardly extendingintegral mounting arm 13 is provided on the flange 11 for mounting thereto by means of bolts, or the like, asupport bracket 14 that carries thediaphragm control mechanism 15 of aninlet valve member 16, with the interposition of asuitable linkage 17. Theinlet valve mechanism 15, 16, 17 is conventional per se for throttling the inlet fluid on partial load and for density control in a known manner. The diaphragm control is provided with apressure feedback tube 18 for this purpose. The multistage impeller rotor and fluid guide structure is contained within the one-piece cast casing 4, which casing is providcd with an axially throughcylindrical bore 19, a
downwardly facingplanar surface 20 engaging the correspondingly planar upper surface of thetop wall 21 of the base I, and with an upwardly extendingboss 22 that is bored for fluid communication with the outlet ofthe last compressor The drive assembly for the compressor may be of any type.
but preferably employs theelectric motor 8 that drives a gearset within the gear housing 6. Particularly, the drive structure may be of the type mentioned in one of applicant's previously identified applications wherein the structure is set forth in detail.
Welded steel fabrication is used for constructing the base 1, preferably from stock sheet and plate steel. Thefront wall 23 is provided with oppositely openingdoors 24, which lead to a control and auxiliary component compartment having therein the inlet and outlet water couplings for the intercoolers. Thesupply 25 andoutlet 26 water pipes for the intercoolers extend permanently through thesidewall 27 and are provided at their outer ends with suitable couplings to be connected during installation at the site of use.
The basic fluid flow for the compressor is shown in FIG. 2 wherein the impeller of afirst stage 28 passes fluid downwardly through afirst intercooler 29. Thereafter, the fluid passes through thesecond stage impeller 30, which directs it downwardly through thesecond intercooler 31. Finally, the fluid passes upwardly and through thethird stage impeller 32 for discharge to the point of use. Theimpellers 28, 32, 30 form an integral rotor drivingly connected with a spurhelical pinion gear 33 that is driven by means ofa drivehelical gear 34 mounted on a parallel axis geardrive input shaft 35.
The inlet connection is shown in more detail in FIG. 3. A cylindrical mounting portion 36 of theinlet housing 2 is telescopically received over acylindrical mounting portion 37 with the interposition of an O-ring 38. From the drawing, it is seen that the adjacent cylindrical surfaces of mountingportions 36, 37 are radially spaced from each other so that the O-ring 38 provides the only engaging connection between theinlet housing 2 and thecompressor casing 4, while sealing these structures. Thus, theinlet housing 2 is independently supported on the base 1 to prevent transmittal of inlet housing vibration, canting, axial movement, radial movement and rotational movement to thecompressor casing 4. Thus. the complete compressor may be supplied to a user and the user may rigidly couple his inlet fluid pipes directly to theinlet housing 2, without fear that forces relating to the coupling and inlet pipes will be transmitted to the compressor casing. Further, the stresses due to tightening of the connections between the inlet casing and fluid supply pipes will not be transferred to the compressor casing.
The removable barrel structure of the compressor includes separate shrouds, diffusers, and annular fluid guide elements all received in a stacked relationship within thecylindrical bore 19 of the one-piece compressor casing 4. Thecompressor casing 4 is provided with integrally cast passages extending between the barrel assembly and the base 1. Particularly, afirst passage 39 extends between thebore 19 and theplanar surface 20 to conduct fluid from the discharge of the first stage,second passage 40 extends from thebore 19 to theplanar surface 20 to conduct the fluid into the third-stage inlet,third passage 41 extends from thebore 19 to theplanar surface 20 to conduct fluid discharged from the second stage andfourth passage 42 extends from thebore 19 to theplanar surface 20 to conduct fluid to the inlet of the second stage. The base 1 is provided with atop wall 21, opposedsidewalls 27 and 43, opposed front andback walls 23 and 44, and abottom wall 45, which together form a substantially closed main chamber containing the intercooler structure. Thetop wall 21 is provided with a plurality of passages, also shown in FIG. 4, extending between the passages 39-42 and the intercooler main chamber. Particularly, thetop plate 21 is provided withholes 46 that align withpassages 39,holes 47 that align withpassage 42,hole 48 that aligns withpassage 40 andhole 49 that aligns withpassage 41.
Twoparallel partition walls 50, which are parallel to thewalls 27, 43, extend completely from thetop wall 21 to thebottom wall 45 and extend from thefront wall 23 to thebackwall 44 to form acentral manifold chamber 51.Additional partition walls 52 subdivide the manifold chamber into three aligned subchambers, with theoutside subchambers 53 being in fluid communication between theholes 47 in the top wall and correspondingly aligned holes in the left-hand partition wall 50, and with theinside subchamber 54 being in fluid communication between thehole 48 and ahole 55 in the right-hand partition wall 50 as shown in FIG. 3. In this manner, the main intercooler chamber is further divided into afirst intercooler chamber 55 to the left of thepartition walls 50 and asecond intercooler chamber 56 to the right of thepartition walls 50, as seen in H6. 3. identical and interchangeable parallel tubefluid heat exchangers 57 are mounted onshelves 58 within theirrespective intercooler chambers 55, 56 so that they may be horizontally slid into and out of the base 1 after the releasablysecure back wall 44 is removed. For this purpose, thepipes 25, 26 are provided withreleasable couplings 59 for uncoupling the heat exchangers, without affecting the location of thepipes 25, 26.
It is seen from FIG. 3, that fluid discharged respectively from the first stage and the second stage will pass throughpassages 39, 41 andholes 46, 49 downwardly intointercooler chambers 55, 56 to pass through theircorresponding heat exchangers 57. Thereafter, the thus cooled fluid will be directed bybaffle plates 60 through vertically extending restricted nozzle-type passages 61 where the flow of fluid will approach sonic velocity. The high-speed fluid then passes through a sharp acute angle and upwardly throughdemisters 62. Thus, it is seen that thebaffles 60 formed in thenozzletype passages 61 constitute separators that will take the cooled fluid from the heat exchangers having condensed droplets therein, accelerate this cooled fluid and substantially reverse the flow of the accelerated cooled fluid to separate the condensate. Further, moisture will be removed from this separated fluid by means ofdemister 62. Thereafter, the relatively dry fluid will pass through respective holes in thepartition walls 50 so that the fluid from theintercooler chamber 55 will pass into thesubmanifold chambers 53 and fluid from theintercooler 56 will pass into thesubmanifold chamber 54. It is noted that the left-hand passage 61 is substantially larger than the right-hand passage 61 as shown in FIG. 3, which difference is proportional to the difference in volume offluid handled by the two intercoolers due to compression. For this same reason, twosubmanifold chambers 53 are provided for returning fluid to the second stage, while only one submanifold chamber is provided for returning fluid to the third stage.
Beneath thedrive assembly 8, 6, the base 1 is provided with anoil sump 63, which is in direct communication with the interior of the gear housing 6.
From the above, it is seen that the compressor base of the present invention separately and rigidly mounts a rigid comprcssor casing and a rigid fluid inlet casing, and provides a telescopic coupling therebetween having only a flexible interengagement by means of the O-ring 38. With this coupling, the users rigid fluid inlet pipes may be rigidly connected directly to thefluid inlet casing 2 for support thereof, without fear that the stresses produced by the rigid supply Coupling will be transmitted to thecompressor casing 4. Also, any vibrations, thermal expansion, settling, misalignment, etc. associated with the user's fluid supply pipes 'will be transmitted only to the heavy rigid base and not transmitted directly to the compressor casing. Further, this O-ring seal 38 and flexible coupling will accommodate misalignment and tolerances as between thecasings 2 and 4, as well as preventing force transmittal therebetween because of the considerable radial spacing between the telescopingcylindrical portions 36, 37. Further, the inlet casing may be advantageously used for a conventional type of inlet valve, without fear that forces associated with the inlet valve will be transmitted to the compressor casing.
The compressor casing is of a one-piece cast construction with integral fluid passages between stages communicating between each stage and intercoolers within the base, respectively, so that no bulky, costly and cumbersome external piping connections are required. For this purpose, the base has a top compressor supporting wall that is provided with integral passages aligned respectively in fluid communication with the compressor casing integral passages so that fluid is conducted from the first and second stages downwardly into the intercooler chambers and upwardly from the intercooler chambers into the second and third stages.
The base is further of a compact construction in that it requires very little extra room over that of the plan view dimensions associated with the compressor casing and inlet fluid casing, with respect to its enclosure for housing intercoolers, centrifugal separators, and demisters. The intercoolers are identical and the demisters are identical to provide for interchangeability and inexpensive manufacture. Also, the separators are formed by baffles that are identical although assembled in mirror image fashion. The fluid flows downwardly through the intercoolers through a restricted passage formed by the separator baffles so that the cooled fluid approaches or reaches sonic velocity before it is sharply and reversely guided upwardly through the demisters, so that during this reversal, droplets of condensate will be discharged downwardly where they will be collected and removed if desired. The fluid moving upwardly through demisters is further directed upwardly through submanifold chambers located centrally between the two intercooler chambers for discharge through the top wall of the base. Construction of the base is rigid and relatively inexpensive in that it is of welded steel fabrication employing only planar sheets and plates, with the partition walls forming the submanifold chambers considerably contributing to the rigidity of the entire structure by providing cross bracing.
The portion of the base under the drive mechanism, particularly an electric motor and gear train, is of relatively shallow construction due to the greater height of these components and forms a sump for the oil lubrication system. Preferably this sump is in direct communication with the gear housing.
The intercoolers are mounted within their respective intercooler chambers by means of shelves so that they may be slid horizontally in one direction out of the base, after the removal of the adjacent releasably mounted wall. The wall opposite from the releasably mounted wall is provided with access means so that rigid cooling liquid supply and exhaust pipes may be quickly coupled and uncoupled from the intercoolers. In a like manner, the demisters are mounted on respective shelves to be horizontally slid out of their respective intercooler chambers in the same direction'as the heat exchangers, for purposes of repair, replacement or the like.
While a preferred embodiment of the present invention has been specifically described with respect to specific advantageous features, it is to be realized that the invention, in its broader aspects, includes further modifications, embodiments and variations.
What is claimed is:
1. A multistage compressor, comprising: a base; a compressor rotor having at least two impellers; casing means rigidly secured on said base and rotatably supporting said compressor rotor for providing at least two compression stages, said casing means having an integral fluid outlet for the first stage and an integral fluid inlet for the second stage; said base including an upper wall, sidewalls, and a lower wall forming therebetween a substantially closed intercooler chamber, and said upper wall having an integral chamber inlet in fluid communication directly with said first stage fluid outlet, and an integral chamber outlet in direct fluid communication with said second-stage fluid inlet.
2. The compressor of claim 1, wherein said casing means includes a one-piece cast casing having an axially through cylinder bore receiving concentrically therein said compressor rotor and a downwardly facing horizontally planar surface; said casing means inlets and outlets extending between said bore and said planar surface, with their respective ends opening upwardly and downwardly; said base upper wall having an upwardly facing substantially horizontally planar surface engaging the entire casing planar surface.
3. The compressor of claim L including liquid gas heat exchanger means mounted in said intercooler chamber in fluid communication between said chamber fluid inlet and said chamber fluid outlet; and chamber partition means forming a constricted passage for the fluid downstream of said heat exchanger means for passing the fluid downwardly and sharply reversing the fluid upwardly to discharge condensed liquid therefrom.
4. The compressor ofclaim 3, including demister means mounted in said intercooler chamber downstream of said separator.
5. The compressor of claim 1. wherein said compressor rotor has three impellers and said casing means provides three compression stages; said casing means further has an integral fluid outlet for the second stage and an integral fluid inlet for the third stage; said upper wall further has an integral chamber fluid inlet in direct fluid communication with said third-stage fluid inlet; and including two separate heat exchangers in said intercooler chamber, means mounting one of said heat exchangers fluid interposed between said first-stage fluid outlet and said second-stage fluid inlet, and the other of said heat exchangers fluid interposed between said second-stage fluid outlet and said third-stage fluid inlet.
6. The compressor of claim 5, including partition wall means in said base forming three aligned manifold subchambers, with the two outside manifold subchambers being in fluid communication with said second-stage fluid inlet and the middle manifold subchamber being in fluid communication with said third stage inlet.
7. The compressor of claim 5, including generally vertical partition wall means in said base forming at least two manifolds extending vertically for substantially the entire height of said intercooler chamber and being respectively in direct fluid communication through said upper wall with said second-stage fluid inlet and said third-stage fluid inlet.
8. The compressor ofclaim 7, including said partition wall means further dividing said intercooler chamber into a separate first intercooler subchamber on one side of said manifolds and a separate second intercooler subchamber on the other side of said manifolds, with said first-stage fluid outlet discharging downwardly directly into said first intercooler subchamber and said second-stage fluid outlet discharging downwardly directly into said second intercooler subchamber; and passage means interconnecting respective intercooler subchambers and manifolds.
9. The compressor ofclaim 8, wherein said heat exchangers are identical; said base having shelf means mounting each of said heat exchangers for relative horizontal sliding in the same direction for removal and assembly; said base having one sidewall being perpendicular to said direction and being removable to provide access for assembly and withdrawal of said heat exchangers; rigid inlet and outlet liquid conduits on the other side of said heat exchangers opposite from said one sidewall having releasable coupling means fluid connecting them respectively to said heat exchangers; and said base having removable wall means on said other side for providing access to said releasable couplings.
10. The compressor of claim 9, including demister means operatively mounted in each of said intercooler subchambers respectively downstream from said heat exchangers; and fluid guide means for respectively directing fluid from said heat exchangers downwardly and then reversely upwardly through said demister means.
11. The compressor ofclaim 10, wherein said fluid guide means each have a narrow vertically extending nozzle passage for accelerating and directing the fluid downwardly closely adjacent the bottom of each intercooler subchamber and then upwardly through said demister means to constitute condensate separators.
12. The compressor ofclaim 10. wherein each of said heat exchangers is mounted above the corresponding interconnecting passage means and each of said demister means is mounted below the corresponding interconnecting passage means.

Claims (12)

US44034A1970-06-081970-06-08Compressor base and intercoolersExpired - LifetimeUS3644054A (en)

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CH (1)CH520875A (en)
DE (1)DE2128232B2 (en)
FR (1)FR2096062A5 (en)
GB (1)GB1357184A (en)
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Cited By (18)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3912000A (en)*1972-04-191975-10-14Worthington CeiMulti-cooling housing for a multi-stage compressing system
US4288204A (en)*1978-03-021981-09-08Klein, Schanzlin & Becker AgSupport for multi-stage compressors
US4830580A (en)*1985-03-041989-05-16Nippon Air Brake Co., Ltd.Two-stage air compressor unit
US5362207A (en)*1993-06-091994-11-08Ingersoll-Rand CompanyPortable diesel-driven centrifugal air compressor
US5613843A (en)*1992-09-111997-03-25Hitachi, Ltd.Package-type screw compressor
US6018962A (en)*1998-12-162000-02-01American Standard Inc.Centrifugal compressor oil sump demister apparatus
US6572350B2 (en)*2000-06-302003-06-03Hitachi, Ltd.Screw compressor
US6692235B2 (en)*2001-07-302004-02-17Cooper Cameron CorporationAir cooled packaged multi-stage centrifugal compressor system
US20040031286A1 (en)*2002-08-062004-02-19York International CorporationSuction connection for dual centrifugal compressor refrigeration systems
US20130251555A1 (en)*2012-03-262013-09-26Pedro Ismael DePAZPower system arrangement
US20140086733A1 (en)*2012-09-242014-03-27Samsung Techwin Co., Ltd.Compressing system
US20150330409A1 (en)*2014-05-142015-11-19Ingersoll-Rand CompanyAir compressor system
US20150337861A1 (en)*2014-05-232015-11-26Howden Roots LlcApparatus to support components of a fluid handling system and implementation thereof
US9677551B2 (en)2015-08-212017-06-13Ingersoll-Rand CompanyCompressor and oil drain system
DE102016113067A1 (en)*2016-07-152018-01-18Man Diesel & Turbo Se Geared turbine machine
US10087797B2 (en)2015-08-212018-10-02Ingersoll-Rand CompanyCompressor and oil drain system
US20210048034A1 (en)*2016-09-272021-02-18Atlas Copco Comptec LlcIntegrated oil system manifold
US11067081B2 (en)*2015-12-222021-07-20Kobe Steel, Ltd.Screw compressor

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US6564839B1 (en)2000-11-012003-05-20The Goodyear Tire & Rubber CompanyPneumatic tire having a load dependent adaptive footprint shape

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GB563532A (en)*1941-12-201944-08-18Sulzer AgImprovements in or relating to centrifugal pumps
US3001692A (en)*1949-07-261961-09-26Schierl OttoMultistage compressors
US3203352A (en)*1962-05-241965-08-31Schafranek GustavMultiple pump assembly
US3355096A (en)*1966-02-151967-11-28Ingersoll Rand CoMulti-stage intercooled compressor
US3361073A (en)*1964-10-301968-01-02Sulzer AgCasing for multi-stage centrifugal pump
US3476485A (en)*1967-09-181969-11-04Dresser IndMultistage centrifugal compressor

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GB563532A (en)*1941-12-201944-08-18Sulzer AgImprovements in or relating to centrifugal pumps
US3001692A (en)*1949-07-261961-09-26Schierl OttoMultistage compressors
US3203352A (en)*1962-05-241965-08-31Schafranek GustavMultiple pump assembly
US3361073A (en)*1964-10-301968-01-02Sulzer AgCasing for multi-stage centrifugal pump
US3355096A (en)*1966-02-151967-11-28Ingersoll Rand CoMulti-stage intercooled compressor
US3476485A (en)*1967-09-181969-11-04Dresser IndMultistage centrifugal compressor

Cited By (27)

* Cited by examiner, † Cited by third party
Publication numberPriority datePublication dateAssigneeTitle
US3912000A (en)*1972-04-191975-10-14Worthington CeiMulti-cooling housing for a multi-stage compressing system
US4288204A (en)*1978-03-021981-09-08Klein, Schanzlin & Becker AgSupport for multi-stage compressors
US4830580A (en)*1985-03-041989-05-16Nippon Air Brake Co., Ltd.Two-stage air compressor unit
US5613843A (en)*1992-09-111997-03-25Hitachi, Ltd.Package-type screw compressor
US5362207A (en)*1993-06-091994-11-08Ingersoll-Rand CompanyPortable diesel-driven centrifugal air compressor
US6018962A (en)*1998-12-162000-02-01American Standard Inc.Centrifugal compressor oil sump demister apparatus
US6572350B2 (en)*2000-06-302003-06-03Hitachi, Ltd.Screw compressor
US6679689B2 (en)*2000-06-302004-01-20Hitachi, Ltd.Screw compressor
US20080273991A1 (en)*2001-07-302008-11-06Cameron International CorporationAir cooled packaged multi-stage centrifugal compressor method
US20040184927A1 (en)*2001-07-302004-09-23Kolodziej Robert M.Air cooled packaged multi-stage centrifugal compressor system
US6692235B2 (en)*2001-07-302004-02-17Cooper Cameron CorporationAir cooled packaged multi-stage centrifugal compressor system
US7819634B2 (en)2001-07-302010-10-26Cameron International CorporationAir cooled packaged multi-stage centrifugal compressor method
US7832992B2 (en)2001-07-302010-11-16Cameron International CorporationAir cooled packaged multi-stage centrifugal compressor system
US6910349B2 (en)2002-08-062005-06-28York International CorporationSuction connection for dual centrifugal compressor refrigeration systems
US20040031286A1 (en)*2002-08-062004-02-19York International CorporationSuction connection for dual centrifugal compressor refrigeration systems
US20130251555A1 (en)*2012-03-262013-09-26Pedro Ismael DePAZPower system arrangement
CN103671179B (en)*2012-09-242017-11-03韩华泰科株式会社Compressibility
US20140086733A1 (en)*2012-09-242014-03-27Samsung Techwin Co., Ltd.Compressing system
US20150330409A1 (en)*2014-05-142015-11-19Ingersoll-Rand CompanyAir compressor system
US10047766B2 (en)*2014-05-142018-08-14Ingersoll-Rand CompanyAir compressor system
US20150337861A1 (en)*2014-05-232015-11-26Howden Roots LlcApparatus to support components of a fluid handling system and implementation thereof
US9677551B2 (en)2015-08-212017-06-13Ingersoll-Rand CompanyCompressor and oil drain system
US10087797B2 (en)2015-08-212018-10-02Ingersoll-Rand CompanyCompressor and oil drain system
US11067081B2 (en)*2015-12-222021-07-20Kobe Steel, Ltd.Screw compressor
DE102016113067A1 (en)*2016-07-152018-01-18Man Diesel & Turbo Se Geared turbine machine
US20210048034A1 (en)*2016-09-272021-02-18Atlas Copco Comptec LlcIntegrated oil system manifold
US12098727B2 (en)*2016-09-272024-09-24Atlas Copco Comptec LlcIntegrated oil system manifold

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SE371474B (en)1974-11-18
GB1357184A (en)1974-06-19
DE2128232B2 (en)1975-07-31
DE2128232A1 (en)1971-12-16
CH520875A (en)1972-03-31
FR2096062A5 (en)1972-02-11
CA936504A (en)1973-11-06
NL7107687A (en)1971-12-10

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Owner name:ELLIOTT TURBOMACHINERY CO., INC., A CORP OF DELAWA

Free format text:ASSIGNMENT OF ASSIGNORS INTEREST. SUBJECT TO LICENSE RECITED.;ASSIGNOR:CARRIER CORPORATION, A CORP OF DEL.;REEL/FRAME:004499/0922

Effective date:19851220

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Owner name:FIRST NATIONAL BANK OF CHICAGO, THE,ILLINOIS

Free format text:LICENSE;ASSIGNOR:ELLIOT TURBOMACHINERY CO., INC.;REEL/FRAME:004940/0562

Effective date:19871109

Owner name:FIRST NATIONAL BANK OF CHICAGO, THE, ONE FIRST NAT

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