US2300766A - Multistage centrifugal compressor - Google Patents

Multistage centrifugal compressor Download PDF

Info

Publication number
US2300766A
US2300766A US391581A US39158141A US2300766A US 2300766 A US2300766 A US 2300766A US 391581 A US391581 A US 391581A US 39158141 A US39158141 A US 39158141A US 2300766 A US2300766 A US 2300766A
Authority
US
United States
Prior art keywords
vanes
guide vanes
shaft
casing
impellers
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 - Lifetime
Application number
US391581A
Inventor
Baumann Adolf
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.)
BBC Brown Boveri AG Germany
BBC Brown Boveri France SA
Original Assignee
BBC Brown Boveri France SA
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 BBC Brown Boveri France SA filed Critical BBC Brown Boveri France SA
Application granted granted Critical
Publication of US2300766A publication Critical patent/US2300766A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D17/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D17/08Centrifugal pumps
    • F04D17/10Centrifugal pumps for compressing or evacuating
    • F04D17/12Multi-stage pumps
    • F04D17/122Multi-stage pumps the individual rotor discs being, one for each stage, on a common shaft and axially spaced, e.g. conventional centrifugal multi- stage compressors
    • 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
    • F04D29/4206Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps
    • F04D29/4213Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for elastic fluid pumps suction ports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00Geometry
    • F05D2250/50Inlet or outlet
    • F05D2250/51Inlet

Definitions

  • the present invention relates to multistage centrifugal compressors and in particularto regulating means therefor.
  • FIG. 1 is an axial section through a multistage compressor embodying the invention
  • Fig. 2 is a section on the line 2-2 of Fig-1;'
  • FIG. 3 is an enlarged fragmentary detail view on the same section as Fig. 1;
  • Figs. 4 and 5 are axial and transverse sections, respectively, illustrating a modied drive arrangement for the adjustable guide vanes
  • Figs. 6 and 'l are axial and transverse sections, respectively, illustrating another modified drive arrangement for the adjustable guide vanes; and Figs. 8 and 9 are axial and transverse sections respectively, illustrating still another modified drive, arrangement for the adjustable guide vanes.
  • I, 2, 3 and 4 indicate the successive impellers which are retained in spaced rela-- tion ⁇ on thecompressor shaft Ii by means of spacing bushings 5.
  • the impellers are keyed or otherwise rigidly fastened on the shaft 6 which is driven by a suitable prime mover, not shown.
  • the first impeller I discharges circumferentlally into a diffuser 1 in which the velocity of the gas is converted into a pressure head.
  • the diffuser leads into a reversing passage 8 into which the iiuid is turned to flow radially inwardly to the intake ofthe next impeller wheel 2 where the cycle is repeated.
  • Adjustable guide vanes 9 are mounted adjacent the inner portion of the reversing passage 8 on pivots I0 journalled respectively in spaced disk members II and I2.
  • the disk Il is provided with a central aperture, receiving the shaft 6 and with suitable packing I3 which seals the same against the bushing 5.
  • the disk I2 is provided with a ange overlapping the adjacent rotor Wheel and carries a suitable packing I4 for sealing the joint.
  • the disk II adjacent its periphery carries fixed guide vanes I5 through which it is connected to a counter-ring I6 which is secured peripherally on the disk I2 by screws or bolts I1.
  • the disk I I and the disk I2 and the peripheral ring I6 form an annular cage or housing with denitely spacedrside walls between' which theV adjustable guide vanes are mounted, y
  • the passage provided by thecompressor casing which is aligned with the' passage provided by the disks Il and i2 when the casing is assembled in position, is provided with fixed reversing vanes 22 which, as seen more clearly in Fig. 2, align with the fixed guide vanes I5 so that each of the latter constitutes thetail end or tip of one of the vanes 22.
  • the fixed guide vanes 22 and the adjustable guide vanes4 9 are so shaped and mounted relative to each other that in all positions of adjustment ofV the vanes 9 the fluid pumped is guided in the Adesired path to the impellers with the least possible loss.
  • the fixed vanes 22 and I5 are curved in the direction of fluid flow from the diii'users 1 and are set to provide guideways in which the uid is turned toward the axis and its circumferential component of movement reduced.
  • the adjustable vanes S are streamlined and curved in cross-section from leading to trailing edge and the pivotal axis I0 thereof is positioned at the leading edge in spaced relation to the tip of the rigid vane sections Il so that the vanes 9 define guideways leading from the guideways between the vanes 22--I6 and adjustable as to direction of discharge with respect to the axis of rotation of the impellers.
  • the shaft 26 carries a bevel gear 21 at its outer end which is driven from control shaft 26 by a gear '21 mounted thereonzie
  • the control shaft .26 is disposed in a recess formed by a bulge in the mating halves il and 34 of the casing and in its pasage from one stage to the next is ⁇ provided with packing 29.
  • Pins 22 are for the purpose of closing drilled In the position of adjustment of the vanes 2 shown in Fig.
  • the uid is fed substantially radially into the eye of the succeeding impeller without any appreciable tangential component, whereas, with the vanes 9 in the position shown in Fig. 2a. the fluid isgiven a fore-rotation or tangential component in the direction of rotation of the impellers.
  • the relation and shape of the adjustable vanes 9 with respect to the fixed vanes 22-Ii5 is such that the guideways formed by the vanes effect the desired directional feed to the impellers without production of eddy currents and with a minimum of loss of ediciency.
  • the vanes 2 are interconnected for simultaneous adjustment through the medium of 'suitable drive connections which, as shown, may consist of cable connections.
  • the pivot shaft I0 of each vane extends at one end through the disk i2 and has a pulley i! mounted on the projecting end thereof.
  • V 'I'he pulleys I3 are driven by a cable or rope 2li which makes a turn around each pulley in succession and has its ends joined by connectors which can be tightened to keep the cable tensioned.
  • shaft 2B and other driving parts of the vane adjusting mechanism lie in the plane of separation 33--32 of the casing halves SI-M and that the shaft mountings are carried half by each of the casing sectionsso that the same are exposed for removal upon lifting of the top casing half 3l.
  • the adjusting shaft 26 rotated by suitable means externally of the casing, drives the shaft 26 when adjustment of the guide vanes to a diiferent' setting is desired and the cable and pulley connections eifect the same adjustment of all of the vanes to effect the desired directional iiow through the reversing guideways to the eye of the respective succeeding impellers.
  • the shaft 26 is replaced by a belt, chain or cable 2l which drives one of the pulleys Il from la pulley on the shaft 26.
  • a link and lever connection is employed for transmitting motion from the shaft 26 to the pivot shafts lo of the vanes 2, theconnectinglink 26 being connected at its ends to crank levers 26a and 2Gb on the shaft 26 and one of the pivot shafts Il, respectively.
  • segmental spur gear 31 carried by the shaft 26 drives a larger intermediate spur gear 21a journalied in the casing and the latter drives a spur gear segment 2lb mounted on one of the pivot shafts I0. While preferred embodiments of the invention have been shown and described by. way of illustration, it will be understood that other modificai tions in the details of construction may be made without departing from the spirit of the invention within the scope of the appended claims.
  • a multistage centrifugal' compressor oomprising a casing, a rotor shaft extending longitudinally within said casing, impellers mounted in spaced relation on said rotor shaft, means carried by said casing providing a diifusenfor eachl of said impellers and said casing including spaced wall portions defining the outervportion of a reand defining the inner portion of the reversing fluid passage leading to a next succeeding impeller, means rigidly connecting said disk members in spaced relation including rigid guide vanes extending between the same adjacent Vthe circumferential portions thereof, adjustable guidel vanes pivotally mounted on pivot shafts between said disk members inwardly of said rigid guide vanes and drive connections between the pivot shafts of said adjustable guide vanes; a control shaft extending longitudinally'within said casing and driving means effective to establish a drive between said control shaft and the drive connections of said pivoted vanes when said cage unit Ywall portions defining the outer portion of a reversing fiuid passage to convey fluid from a diffuser
  • adjustable guide vanes for effecting simultaneous adjustmentthereof; a longitudinally split casing comprising two halves formed with seating portions for each cage unit and with wall portions defining a diffuser chamber for the impeller in advance of each cage unit and a fluid passage leading from said diffuserchamber to the circumfere'nce of each cage unit when said casing halves are joined, with said rotor shaft, impellers and cage vunits enclosed therein, a control shaft mounted in said casing adjacent the circumferential wall thereof, and drive connections between said control shaft and the interconnections between said adjustable vanes.
  • a centrifugal compressor according to claim 3 in which the casing members are formed to provide a longitudinally extending recess within lthe Acasing for mounting said control shaft and said control shaft extends parallel to the axis of said rotor shaft.
  • a rotor shaft In a multistage centrifugal compressor, a rotor shaft; a plurality of impellers 'mounted in spaced relation on said rotor shaft; av cage unit disposed between adjacent impellers, said cage units comprising spaced disk members each having an axial opening for passage of said rotor shaft therethrough, means rigidly connecting said disk members in spaced relation including rigid guide vanes extending between the same adjustable vanes.
  • said interconnecting means comprise a cable and pulley connection between the pivot shafts of said adiustable vanes and said drive connections comprise a pulley and cable drive between said control shaft and one of said pivot shafts.

Landscapes

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

Description

Nov. 3, 1942. I A. `BAUMANN 2,300,766
MULM'TI STAGE CENTRIFUGAL COMPRESSOR NOV 3, 1942- A. BAUMANN MULTISTAGE CENTRIFUGAL COMPRESSOR 3 Sheets-Sheet 2 Filed May 2, 1941 Nov. 3, 1,942. A. BAUMANN MULTISTAGE CENTRIFUGAL COMPRESSOR Filed May 2, 1941 '5 Sheets-Sheet 3 -intentes Nov. s, v1942 2,300,766 v MULTISTAGE CENTBIFUGAL COMPRESSOR Adolf Baumann, Wettingen,
to Aktiengesellschaft Brown,
Switzerland, assignor l Boveri & Cie,
Baden, Switzerland, a joint stock company oi' Switzerland Application May 2, 1941, serial No. 391,581
1n switzerland May 1o, 1940 9 claims. (ci. 23o-114) The present invention relates to multistage centrifugal compressors and in particularto regulating means therefor.
It has previously been proposed to provide adjustable guide vanes in the gas passages between successive impellers of multistage centrifugal compressors in order to divert the duid stream more or less from a helical path into a radial path as it enters the intake of each succeeding impeller.- guide vanes in one direction or another determines the pressure output of the compressor, depending upon whether the adjustment of the guide vanes results in fore-rotation or counterrotation of the air stream.
In the prior proposals the means for adjusting the movable guide vanes, usually arranged behind the impellers, are not' adaptable to the adjustment of guide vanes immediately in advance of the axial intake of the impellers but are confined to use with guide vanes adjacent the circumference of the passages between the diffuser of one impeller and the entrance of the intake passage of the next. Heretofore it has not been considered practical to build a multistage centrifugal compressor with adjustable guidevanes immediately adjacent the axially located intake ports of the impellers because of the resultant undue lengthening of the compressor to provide sufficient space between adjacent impellers to accommodate the vane mounting and adjusting mechanism.
It is an object of the present invention to pro- The amount of adjustment of thesev vide a multistage centrifugal compressor with i adjustable guide vanes immediately in advance of the axially disposed intakes of the'respective impellers and to just-ing mechanism for the guide vanes which does not result in increase in the over-al1 length of the compressor.
More specifically, it is an object of the invention to provide a compressor of any desired number of stages with adjustable guide vanes in advance of the intake of the impellers in which the adjustable guide vanes are built or mounted in a cage or unit separate from the housing of the compressor, suchcages being mounted on the rotor shaft between the impellers and assembled therewith in the housing and forming with portions of the housing the continuation of the uid reversing passages between the rotors, whereby the vanes mounted in said cages form, in effect, continuations of the guide vanes mounted vin the housing itself.
provide novel mounting and ad novel transmission connectionsv the adjustable guide vanes.
Other objects and advantages of the invention will become apparent during the course of the following detailed description of the same and reference to the accompanying drawings referred to therein. y
In the drawings Fig. 1 is an axial section through a multistage compressor embodying the invention; Fig. 2 is a section on the line 2-2 of Fig-1;'
Fig. 3 is an enlarged fragmentary detail view on the same section as Fig. 1;
Figs. 4 and 5 are axial and transverse sections, respectively, illustrating a modied drive arrangement for the adjustable guide vanes;
Figs. 6 and 'l are axial and transverse sections, respectively, illustrating another modified drive arrangement for the adjustable guide vanes; and Figs. 8 and 9 are axial and transverse sections respectively, illustrating still another modified drive, arrangement for the adjustable guide vanes. Y
Referring more particularly to the drawings, in which a four-stage compressor isshown by way of illustration, I, 2, 3 and 4 indicate the successive impellers which are retained in spaced rela-- tion` on thecompressor shaft Ii by means of spacing bushings 5. It will, of course, be understood that the impellers are keyed or otherwise rigidly fastened on the shaft 6 which is driven by a suitable prime mover, not shown. The first impeller I discharges circumferentlally into a diffuser 1 in which the velocity of the gas is converted into a pressure head. The diffuser leads into a reversing passage 8 into which the iiuid is turned to flow radially inwardly to the intake ofthe next impeller wheel 2 where the cycle is repeated. Adjustable guide vanes 9 are mounted adjacent the inner portion of the reversing passage 8 on pivots I0 journalled respectively in spaced disk members II and I2. The disk Il is provided with a central aperture, receiving the shaft 6 and with suitable packing I3 which seals the same against the bushing 5. The disk I2 is provided with a ange overlapping the adjacent rotor Wheel and carries a suitable packing I4 for sealing the joint. The disk II adjacent its periphery carries fixed guide vanes I5 through which it is connected to a counter-ring I6 which is secured peripherally on the disk I2 by screws or bolts I1. It will thus be It is also an object of the invention to-` provide seen that the disk I I and the disk I2 and the peripheral ring I6 form an annular cage or housing with denitely spacedrside walls between' which theV adjustable guide vanes are mounted, y
for regulating A on the shaft 6 by` means of screws i8, 4as seen v clearly in Fig. 3. `The two-part construction of the cages made up of the split disks il and l2 permits the assembling thereof between the rotor. wheels after the latter have been fixed in position on the shaft and also facilitates the insertion of the packings I3 and I4 into position. The cage formed by the disks H and |21 is centered in position with respect to the main casing and is held in proper registry with the same by means of mating shoulder portions between which the packing 2| is inserted. The passage provided by thecompressor casing, which is aligned with the' passage provided by the disks Il and i2 when the casing is assembled in position, is provided with fixed reversing vanes 22 which, as seen more clearly in Fig. 2, align with the fixed guide vanes I5 so that each of the latter constitutes thetail end or tip of one of the vanes 22.
The fixed guide vanes 22 and the adjustable guide vanes4 9 are so shaped and mounted relative to each other that in all positions of adjustment ofV the vanes 9 the fluid pumped is guided in the Adesired path to the impellers with the least possible loss. The fixed vanes 22 and I5 are curved in the direction of fluid flow from the diii'users 1 and are set to provide guideways in which the uid is turned toward the axis and its circumferential component of movement reduced.
The adjustable vanes S are streamlined and curved in cross-section from leading to trailing edge and the pivotal axis I0 thereof is positioned at the leading edge in spaced relation to the tip of the rigid vane sections Il so that the vanes 9 define guideways leading from the guideways between the vanes 22--I6 and adjustable as to direction of discharge with respect to the axis of rotation of the impellers.
ing shaft 2l mounted in suitable bearings in the casing between the wall defining oneeside of the passage 8 beyond the disk I2 and the adjacent wall of the next diffuser 1. The shaft 26 carries a bevel gear 21 at its outer end which is driven from control shaft 26 by a gear '21 mounted thereonzie The control shaft .26 is disposed in a recess formed by a bulge in the mating halves il and 34 of the casing and in its pasage from one stage to the next is` provided with packing 29. Pins 22 are for the purpose of closing drilled In the position of adjustment of the vanes 2 shown in Fig. 2, the uid is fed substantially radially into the eye of the succeeding impeller without any appreciable tangential component, whereas, with the vanes 9 in the position shown in Fig. 2a. the fluid isgiven a fore-rotation or tangential component in the direction of rotation of the impellers. In these, as well as in all other positions of adjustment, it will be observed that the relation and shape of the adjustable vanes 9 with respect to the fixed vanes 22-Ii5 is such that the guideways formed by the vanes effect the desired directional feed to the impellers without production of eddy currents and with a minimum of loss of ediciency.
The vanes 2 are interconnected for simultaneous adjustment through the medium of 'suitable drive connections which, as shown, may consist of cable connections. The pivot shaft I0 of each vane extends at one end through the disk i2 and has a pulley i! mounted on the projecting end thereof.V 'I'he pulleys I3 are driven by a cable or rope 2li which makes a turn around each pulley in succession and has its ends joined by connectors which can be tightened to keep the cable tensioned. A'gear segment 22, which may constitute part of one of the pulleys i9, is mounted on one of the pivot shafts il) and meshes with a bevel gear 2l carried by a radially extendopenings in the casing opposite the ends of the shafts 25.
It will be noted that the shaft 2B and other driving parts of the vane adjusting mechanism lie in the plane of separation 33--32 of the casing halves SI-M and that the shaft mountings are carried half by each of the casing sectionsso that the same are exposed for removal upon lifting of the top casing half 3l.
It will be noted that with this construction the normal distance between impellers is Vnot increased as compared with pumps without adJustable guide vanes, since there is necessarily a space between the wallof the reversing passage leading to an impeller and the wall of the diffuser leading therefrom due to the'hub shape of the impellers and the sealing at Il.
The operation will be obvious from the above. The adjusting shaft 26, rotated by suitable means externally of the casing, drives the shaft 26 when adjustment of the guide vanes to a diiferent' setting is desired and the cable and pulley connections eifect the same adjustment of all of the vanes to effect the desired directional iiow through the reversing guideways to the eye of the respective succeeding impellers.
In the embodiment shown in Figs. 4 .and 5, the shaft 26 is replaced by a belt, chain or cable 2l which drives one of the pulleys Il from la pulley on the shaft 26.
In the embodiment shown in Figs. 6 and 7, a link and lever connection is employed for transmitting motion from the shaft 26 to the pivot shafts lo of the vanes 2, theconnectinglink 26 being connected at its ends to crank levers 26a and 2Gb on the shaft 26 and one of the pivot shafts Il, respectively.
In the embodiment shown in Figs. B and 9.a
segmental spur gear 31 carried by the shaft 26 drives a larger intermediate spur gear 21a journalied in the casing and the latter drives a spur gear segment 2lb mounted on one of the pivot shafts I0. While preferred embodiments of the invention have been shown and described by. way of illustration, it will be understood that other modificai tions in the details of construction may be made without departing from the spirit of the invention within the scope of the appended claims.
I claim:
1. A multistage centrifugal' compressor oomprising a casing, a rotor shaft extending longitudinally within said casing, impellers mounted in spaced relation on said rotor shaft, means carried by said casing providing a diifusenfor eachl of said impellers and said casing including spaced wall portions defining the outervportion of a reand defining the inner portion of the reversing fluid passage leading to a next succeeding impeller, means rigidly connecting said disk members in spaced relation including rigid guide vanes extending between the same adjacent Vthe circumferential portions thereof, adjustable guidel vanes pivotally mounted on pivot shafts between said disk members inwardly of said rigid guide vanes and drive connections between the pivot shafts of said adjustable guide vanes; a control shaft extending longitudinally'within said casing and driving means effective to establish a drive between said control shaft and the drive connections of said pivoted vanes when said cage unit Ywall portions defining the outer portion of a reversing fiuid passage to convey fluid from a diffuser chamber to a next succeeding impeller, rigid guide vanes mounted between said spaced wall portions, a cage unit mounted between adjacent impellers and assembled with said rotor shaft and impellers in said casing, said cage unit comprising spaced disk members each having an axial opening for passage of said rotor shaft therethrough and defining the inner portion of the reversing nuid passage leading to a next succeeding impeller, means rigidly connecting said disk members in spaced relation including rigid guide vanes extending between the same adjacent the circumferential portions thereof, ad- ,instable guide vanes pivotally mounted on pivot adjacent the circumferential portion thereof, adjustable guide vanes pivotally mounted` between said disk members radially inwardly of said rigid guide vanes and means interconnecting said. adjustable guide vanes for effecting simultaneous adjustmentthereof; a longitudinally split casing comprising two halves formed with seating portions for each cage unit and with wall portions defining a diffuser chamber for the impeller in advance of each cage unit and a fluid passage leading from said diffuserchamber to the circumfere'nce of each cage unit when said casing halves are joined, with said rotor shaft, impellers and cage vunits enclosed therein, a control shaft mounted in said casing adjacent the circumferential wall thereof, and drive connections between said control shaft and the interconnections between said adjustable vanes.
4. A centrifugal compressor according to claim 3 in which the casing members are formed to provide a longitudinally extending recess within lthe Acasing for mounting said control shaft and said control shaft extends parallel to the axis of said rotor shaft.`
5. In a compressor as defined in claim 3, said drive connections being'disposed in the plane of Y control shaft and to the pivot shaft of one of said shafts between said disk members inwardly of` said rigid guide vanes, drive connections between the pivot shafts of said adjustable guide vanes; a control shaft extending longitudinally within said casing, driving means effective to establish a drive between said control shaft and the drive connections of said pivoted vanes when said cage unit is assembled in said casing and means for positioning said cage unit in said casing so that the rigid guide vanes of said cage unit form continuations of the rigid guide vanes mounted between said w'all portions of the casing.
3. In a multistage centrifugal compressor, a rotor shaft; a plurality of impellers 'mounted in spaced relation on said rotor shaft; av cage unit disposed between adjacent impellers, said cage units comprising spaced disk members each having an axial opening for passage of said rotor shaft therethrough, means rigidly connecting said disk members in spaced relation including rigid guide vanes extending between the same adjustable vanes.
7. A compressor according to claim 3 in which said interconnecting means comprise a cable and pulley connection between the pivot shafts of said adjustable vanes and said drive connections comprise a link and the crank connection between said control shaft and pivot shaft; of one of said adjustable vanes.
8. A compressor according to claim 3 in which said interconnecting means comprise a cable and pulley connection between the pivot shafts of said adiustable vanes and said drive connections comprise a pulley and cable drive between said control shaft and one of said pivot shafts.
9. A compressor according to claim 3 in which said interconnecting means comprise a cable and pulley connection between the pivot shafts of said adjustable vanes and said drive connections coml prise a gear drive between said control shaft and one of said pivot shafts. l
ADOLF BAUMANN.
US391581A 1940-05-10 1941-05-02 Multistage centrifugal compressor Expired - Lifetime US2300766A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH2300766X 1940-05-10

Publications (1)

Publication Number Publication Date
US2300766A true US2300766A (en) 1942-11-03

Family

ID=4568455

Family Applications (1)

Application Number Title Priority Date Filing Date
US391581A Expired - Lifetime US2300766A (en) 1940-05-10 1941-05-02 Multistage centrifugal compressor

Country Status (1)

Country Link
US (1) US2300766A (en)

Cited By (40)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2427136A (en) * 1944-04-08 1947-09-09 Westinghouse Electric Corp Supercharger
US2438133A (en) * 1944-08-10 1948-03-23 Birtman Electric Co Split cylindrical housing for suction cleaners
US2443263A (en) * 1944-09-18 1948-06-15 American Blower Corp Fluid flow control apparatus
US2671604A (en) * 1950-12-29 1954-03-09 Westinghouse Electric Corp Multiple-stage, centrifugal, refrigerant compressor
US2850227A (en) * 1954-12-03 1958-09-02 Gen Motors Corp Compressor air bleed-off valve
US2862687A (en) * 1953-10-09 1958-12-02 Sulzer Ag Axial flow turbomachine
US2930579A (en) * 1955-09-19 1960-03-29 Dominion Eng Works Ltd Turbine guide vane locking and vibration preventing arrangement
US2950084A (en) * 1953-10-15 1960-08-23 Power Jets Res & Dev Ltd Mounting of swivelling guide vane elements in elastic fluid machines
US3011322A (en) * 1958-08-12 1961-12-05 Dresser Operations Inc Stabilization of refrigeration centrifugal compressor
US20060222515A1 (en) * 2005-03-29 2006-10-05 Dresser-Rand Company Drainage system for compressor separators
WO2009111616A2 (en) * 2008-03-05 2009-09-11 Dresser-Rand Company Compressor assembly including separator and ejector pump
US20090321343A1 (en) * 2008-06-25 2009-12-31 Dresser-Rand Company Dual body drum for rotary separators
US20090324391A1 (en) * 2008-06-25 2009-12-31 Dresser-Rand Company Rotary separator and shaft coupler for compressors
US20100007133A1 (en) * 2006-09-25 2010-01-14 Dresser-Rand Company Axially moveable spool connector
US20100021292A1 (en) * 2006-09-25 2010-01-28 Dresser-Rand Company Fluid deflector for fluid separator devices
US20100038309A1 (en) * 2006-09-21 2010-02-18 Dresser-Rand Company Separator drum and compressor impeller assembly
US20100044966A1 (en) * 2006-09-25 2010-02-25 Dresser-Rand Company Coupling guard system
US20100074768A1 (en) * 2006-09-25 2010-03-25 Dresser-Rand Company Access cover for pressurized connector spool
US20100072121A1 (en) * 2006-09-26 2010-03-25 Dresser-Rand Company Improved static fluid separator device
US20100090087A1 (en) * 2006-09-25 2010-04-15 Dresser-Rand Company Compressor mounting system
US20100239437A1 (en) * 2009-03-20 2010-09-23 Dresser-Rand Co. Fluid channeling device for back-to-back compressors
US20100239419A1 (en) * 2009-03-20 2010-09-23 Dresser-Rand Co. Slidable cover for casing access port
US20100247299A1 (en) * 2009-03-24 2010-09-30 Dresser-Rand Co. High pressure casing access cover
US20110061536A1 (en) * 2009-09-15 2011-03-17 Dresser-Rand Company Density-based compact separator
US20110158802A1 (en) * 2008-06-25 2011-06-30 Dresser-Rand Company Shear ring casing coupler device
US20120134784A1 (en) * 2010-11-25 2012-05-31 Industrial Technology Research Institute Mechanism for modulating diffuser vane of diffuser
US20130034425A1 (en) * 2010-04-14 2013-02-07 Turbomeca Method for adapting the air flow of a turbine engine having a centrifugal compressor and diffuser for implementing same
US20130051977A1 (en) * 2011-08-26 2013-02-28 Baker Hughes Incorporated Adjustable vane diffuser insert for electrical submersible pump
US8434998B2 (en) 2006-09-19 2013-05-07 Dresser-Rand Company Rotary separator drum seal
US20130259644A1 (en) * 2010-10-18 2013-10-03 Hiromi Kobayashi Multi-stage centrifugal compressor and return channels therefor
US8596292B2 (en) 2010-09-09 2013-12-03 Dresser-Rand Company Flush-enabled controlled flow drain
US8657935B2 (en) 2010-07-20 2014-02-25 Dresser-Rand Company Combination of expansion and cooling to enhance separation
US8663483B2 (en) 2010-07-15 2014-03-04 Dresser-Rand Company Radial vane pack for rotary separators
US8673159B2 (en) 2010-07-15 2014-03-18 Dresser-Rand Company Enhanced in-line rotary separator
US8821362B2 (en) 2010-07-21 2014-09-02 Dresser-Rand Company Multiple modular in-line rotary separator bundle
US9095856B2 (en) 2010-02-10 2015-08-04 Dresser-Rand Company Separator fluid collector and method
US20150354599A1 (en) * 2013-01-14 2015-12-10 Thermodyn Sas Compressor unit with a variable aerodynamic profile
EP3376041A1 (en) * 2017-03-15 2018-09-19 Siemens Aktiengesellschaft Return stage and radial turbo fluid energy machine
US20190055947A1 (en) * 2016-02-29 2019-02-21 Mitsubishi Heavy Industries Compressor Corporation Centrifugal rotary machine
EP3521628A1 (en) 2018-02-06 2019-08-07 Honeywell International Inc. Vapor cycle centrifugal compressor with variable return channel vanes

Cited By (69)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2427136A (en) * 1944-04-08 1947-09-09 Westinghouse Electric Corp Supercharger
US2438133A (en) * 1944-08-10 1948-03-23 Birtman Electric Co Split cylindrical housing for suction cleaners
US2443263A (en) * 1944-09-18 1948-06-15 American Blower Corp Fluid flow control apparatus
US2671604A (en) * 1950-12-29 1954-03-09 Westinghouse Electric Corp Multiple-stage, centrifugal, refrigerant compressor
US2862687A (en) * 1953-10-09 1958-12-02 Sulzer Ag Axial flow turbomachine
US2950084A (en) * 1953-10-15 1960-08-23 Power Jets Res & Dev Ltd Mounting of swivelling guide vane elements in elastic fluid machines
US2850227A (en) * 1954-12-03 1958-09-02 Gen Motors Corp Compressor air bleed-off valve
US2930579A (en) * 1955-09-19 1960-03-29 Dominion Eng Works Ltd Turbine guide vane locking and vibration preventing arrangement
US3011322A (en) * 1958-08-12 1961-12-05 Dresser Operations Inc Stabilization of refrigeration centrifugal compressor
US20060222515A1 (en) * 2005-03-29 2006-10-05 Dresser-Rand Company Drainage system for compressor separators
US8075668B2 (en) 2005-03-29 2011-12-13 Dresser-Rand Company Drainage system for compressor separators
US8434998B2 (en) 2006-09-19 2013-05-07 Dresser-Rand Company Rotary separator drum seal
US8302779B2 (en) 2006-09-21 2012-11-06 Dresser-Rand Company Separator drum and compressor impeller assembly
US20100038309A1 (en) * 2006-09-21 2010-02-18 Dresser-Rand Company Separator drum and compressor impeller assembly
US8267437B2 (en) 2006-09-25 2012-09-18 Dresser-Rand Company Access cover for pressurized connector spool
US20100074768A1 (en) * 2006-09-25 2010-03-25 Dresser-Rand Company Access cover for pressurized connector spool
US20100090087A1 (en) * 2006-09-25 2010-04-15 Dresser-Rand Company Compressor mounting system
US8231336B2 (en) 2006-09-25 2012-07-31 Dresser-Rand Company Fluid deflector for fluid separator devices
US20100044966A1 (en) * 2006-09-25 2010-02-25 Dresser-Rand Company Coupling guard system
US20100021292A1 (en) * 2006-09-25 2010-01-28 Dresser-Rand Company Fluid deflector for fluid separator devices
US8079622B2 (en) 2006-09-25 2011-12-20 Dresser-Rand Company Axially moveable spool connector
US8733726B2 (en) 2006-09-25 2014-05-27 Dresser-Rand Company Compressor mounting system
US20100007133A1 (en) * 2006-09-25 2010-01-14 Dresser-Rand Company Axially moveable spool connector
US8061737B2 (en) 2006-09-25 2011-11-22 Dresser-Rand Company Coupling guard system
US20100072121A1 (en) * 2006-09-26 2010-03-25 Dresser-Rand Company Improved static fluid separator device
US8746464B2 (en) 2006-09-26 2014-06-10 Dresser-Rand Company Static fluid separator device
WO2009111616A3 (en) * 2008-03-05 2010-01-07 Dresser-Rand Company Compressor assembly including separator and ejector pump
US20110017307A1 (en) * 2008-03-05 2011-01-27 Dresser-Rand Company Compressor assembly including separator and ejector pump
GB2470151A (en) * 2008-03-05 2010-11-10 Dresser Rand Co Compressor assembly including separator and ejector pump
NO340185B1 (en) * 2008-03-05 2017-03-20 Dresser Rand Co Compressor assembly including separator and ejector pump
US8408879B2 (en) 2008-03-05 2013-04-02 Dresser-Rand Company Compressor assembly including separator and ejector pump
GB2470151B (en) * 2008-03-05 2012-10-03 Dresser Rand Co Compressor assembly including separator and ejector pump
WO2009111616A2 (en) * 2008-03-05 2009-09-11 Dresser-Rand Company Compressor assembly including separator and ejector pump
US20110158802A1 (en) * 2008-06-25 2011-06-30 Dresser-Rand Company Shear ring casing coupler device
US8062400B2 (en) 2008-06-25 2011-11-22 Dresser-Rand Company Dual body drum for rotary separators
US8430433B2 (en) 2008-06-25 2013-04-30 Dresser-Rand Company Shear ring casing coupler device
US8079805B2 (en) 2008-06-25 2011-12-20 Dresser-Rand Company Rotary separator and shaft coupler for compressors
US20090324391A1 (en) * 2008-06-25 2009-12-31 Dresser-Rand Company Rotary separator and shaft coupler for compressors
US20090321343A1 (en) * 2008-06-25 2009-12-31 Dresser-Rand Company Dual body drum for rotary separators
US8087901B2 (en) 2009-03-20 2012-01-03 Dresser-Rand Company Fluid channeling device for back-to-back compressors
US8210804B2 (en) 2009-03-20 2012-07-03 Dresser-Rand Company Slidable cover for casing access port
US20100239437A1 (en) * 2009-03-20 2010-09-23 Dresser-Rand Co. Fluid channeling device for back-to-back compressors
US20100239419A1 (en) * 2009-03-20 2010-09-23 Dresser-Rand Co. Slidable cover for casing access port
US20100247299A1 (en) * 2009-03-24 2010-09-30 Dresser-Rand Co. High pressure casing access cover
US8061972B2 (en) 2009-03-24 2011-11-22 Dresser-Rand Company High pressure casing access cover
US8414692B2 (en) 2009-09-15 2013-04-09 Dresser-Rand Company Density-based compact separator
US20110061536A1 (en) * 2009-09-15 2011-03-17 Dresser-Rand Company Density-based compact separator
US9095856B2 (en) 2010-02-10 2015-08-04 Dresser-Rand Company Separator fluid collector and method
US20130034425A1 (en) * 2010-04-14 2013-02-07 Turbomeca Method for adapting the air flow of a turbine engine having a centrifugal compressor and diffuser for implementing same
US8663483B2 (en) 2010-07-15 2014-03-04 Dresser-Rand Company Radial vane pack for rotary separators
US8673159B2 (en) 2010-07-15 2014-03-18 Dresser-Rand Company Enhanced in-line rotary separator
US8657935B2 (en) 2010-07-20 2014-02-25 Dresser-Rand Company Combination of expansion and cooling to enhance separation
US8821362B2 (en) 2010-07-21 2014-09-02 Dresser-Rand Company Multiple modular in-line rotary separator bundle
US8596292B2 (en) 2010-09-09 2013-12-03 Dresser-Rand Company Flush-enabled controlled flow drain
US20130259644A1 (en) * 2010-10-18 2013-10-03 Hiromi Kobayashi Multi-stage centrifugal compressor and return channels therefor
US20120134784A1 (en) * 2010-11-25 2012-05-31 Industrial Technology Research Institute Mechanism for modulating diffuser vane of diffuser
US8734093B2 (en) * 2010-11-25 2014-05-27 Industrial Technology Research Institute Mechanism for modulating diffuser vane of diffuser
US20130051977A1 (en) * 2011-08-26 2013-02-28 Baker Hughes Incorporated Adjustable vane diffuser insert for electrical submersible pump
US9206677B2 (en) * 2011-08-26 2015-12-08 Baker Hughes Incorporated Adjustable vane diffuser insert for electrical submersible pump
US9970461B2 (en) * 2013-01-14 2018-05-15 Thermodyn Sas Compressor unit with a variable aerodynamic profile
JP2016503145A (en) * 2013-01-14 2016-02-01 サーモダイン・エスエイエス Compressor unit with variable aerodynamic profile
US20150354599A1 (en) * 2013-01-14 2015-12-10 Thermodyn Sas Compressor unit with a variable aerodynamic profile
US20190055947A1 (en) * 2016-02-29 2019-02-21 Mitsubishi Heavy Industries Compressor Corporation Centrifugal rotary machine
US10844863B2 (en) * 2016-02-29 2020-11-24 Mitsubishi Heavy Industries Compressor Corporation Centrifugal rotary machine
EP3376041A1 (en) * 2017-03-15 2018-09-19 Siemens Aktiengesellschaft Return stage and radial turbo fluid energy machine
WO2018166716A1 (en) * 2017-03-15 2018-09-20 Siemens Aktiengesellschaft Backfeed stage and radial turbo fluid energy machine
CN110418896A (en) * 2017-03-15 2019-11-05 西门子股份公司 It returns and draws grade and radial turbine fluid energy machine
US10989202B2 (en) 2017-03-15 2021-04-27 Siemens Energy Global GmbH & Co. KG Backfeed stage and radial turbo fluid energy machine
EP3521628A1 (en) 2018-02-06 2019-08-07 Honeywell International Inc. Vapor cycle centrifugal compressor with variable return channel vanes

Similar Documents

Publication Publication Date Title
US2300766A (en) Multistage centrifugal compressor
US4334821A (en) Regenerative rotodynamic machines
US5156522A (en) Deflector means for centrifugal pumps
CN1026255C (en) Power transmission
US2318990A (en) Radial flow elastic fluid turbine or compressor
US4355953A (en) Flow-adjusted hydraulic rotary machine
US3316848A (en) Pump casing
US2862687A (en) Axial flow turbomachine
CN110273858A (en) Refrigeration system mix-flow compressor
US10731651B2 (en) Apertures spaced around impeller bottom shroud of centrifugal pump
EP0478468A1 (en) Regenerative centrifugal compressor
US2429978A (en) Centripetal-centrifugal pump
US4917571A (en) Flow-stabilizing volute pump and liner
US3217976A (en) Fan equipment
US3788764A (en) Multi-stage centrifugal pump with means for pulse cancellation
US3044685A (en) Air compressor
EP3421815A1 (en) Centrifugal compressor
US2438357A (en) Double rotation turbodrjve
US4231702A (en) Two-stage turbo compressor
JP2016522357A (en) Centrifugal rotor
JP2017180237A (en) Centrifugal compressor
US2923246A (en) Vortex pump
US3131877A (en) Pump
GB2036178A (en) Regenerative rotodynamic pumps and compressors
USRE31259E (en) Two-stage turbo compressor