US3229642A - Multiple-stage pump - Google Patents

Multiple-stage pump Download PDF

Info

Publication number
US3229642A
US3229642A US348080A US34808064A US3229642A US 3229642 A US3229642 A US 3229642A US 348080 A US348080 A US 348080A US 34808064 A US34808064 A US 34808064A US 3229642 A US3229642 A US 3229642A
Authority
US
United States
Prior art keywords
casing
stages
stage
pump
machine
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
US348080A
Inventor
Val S Lobanoff
Harold A Stahl
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.)
Ingersoll Rand Co
Original Assignee
Ingersoll Rand Co
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 Ingersoll Rand Co filed Critical Ingersoll Rand Co
Priority to US348080A priority Critical patent/US3229642A/en
Application granted granted Critical
Publication of US3229642A publication Critical patent/US3229642A/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
    • F04D1/00Radial-flow pumps, e.g. centrifugal pumps; Helico-centrifugal pumps
    • F04D1/06Multi-stage pumps
    • F04D1/063Multi-stage pumps of the vertically split casing type

Definitions

  • One form of multiple-stage centrifugal pump includes a cylindrical outer casing containing a shaft carrying a plurality of impellers and a corresponding number of discharge rings surrounding the impellers for guiding and conducting fluid between the impellers and converting the kinetic energy or velocity of the fluid to potential energy or static pressure.
  • These discharge rings are relatively easy to manufacture since they are separate from the casing.
  • the casing is hollow throughout its length, it expands considerably under high internal pressures. Such expansion is undesirable for various reasons including the fact that it usually causes relatively high rates of leakage between stages which reduces the efficiency of the pump.
  • Another form of pump uses a casing having the walls of the discharge passages for the impellers formed integrally with the casing.
  • This form of pump casing is much stronger because it contains internal webs which act to prevent the outer walls of the casing from expanding substantially under high pressures.
  • this type of pump is very laborious to manufacture with three or more stages because it inherently contains undercut surfaces which must be bored or machined blind with out the machinist being able to see the work or to progressively check it.
  • the principal object of this invention is to provide a multiple-stage centrifugal pump providing the advantages of the foregoing pumps and eliminating the disadvantages.
  • Another important objects of this invention include the following: to provide a multiple-stage centrifugal pump or motor having a relatively strong casing which can be manufactured without the need of blind boring or machining; to provide a better, more efficient multiplestage centrifugal pump or motor which can be manufactured less expensively and with less labor; to provide a multiple-stage centrifugal pump or motor having internal passages which can be easily cleaned; to provide a multiple-stage centrifugal pump or motor having a split casing which can be accurately bored and machined without separating the two casing halves each time a surface is checked or a machining tool is changed; to provide a multiple-stage centrifugal pump or motor which is bolted together midway of its length at points substantially near its axis to provide additional strength; and to provide a multiple-stage centrifugal pump or motor which reduces the leakage between stages to a minimum.
  • these objects are provided by making the pump casing with no more than two stages located midway of its length and having integral walls forming the impeller discharge passages and with the remainder of the stages being formed by separate fluid discharge rings.
  • the integral discharge passage walls reinforce the casing midway of its length and prevent the casing from expanding substantially under internal pressure. Since there are no more than two stages having integral discharge passage walls, these stages can be machined or bored without the need of blind boring methods.
  • FIG. 1 is an axial section of a pump embodying this invention
  • FIG. 1A is a fragmentary section showing the left end of the pump of FIG. 1 which is broken away from FIG. 1 along the line 1A1A because of lack of space on a single sheet;
  • FIG. 2 is a section of FIG. 1 taken along line 2-2 and drawn on an enlarged scale.
  • the multiple-stage centrifugal pump shown in FIG. 1 has six stages designated by the reference numbers 1 to 6.
  • the pump includes an outer casing 7 which is formed from longitudinally split halves 8 and 9 which are bolted together by bolts or studs 10, as shown in FIG. 2.
  • the casing 7 includes a fluid inlet 11 at one end and a fluid outlet 12 located about midway of its length.
  • the pump further includes bearings 14 supported at each end of the casing 7 and rotatably carrying an impeller shaft 15 which extends axially through the casing 7 and carries six impellers 16, corresponding to the number of pump stages 1 to 6.
  • the shaft 15 is adapted to be driven by a suitable power means such as an electric motor (not shown) connected to the right end of the shaft, shown in FIG. 1, projecting beyond the bearing 14. All of the foregoing structure is conventional and well known in the pump art.
  • the two central stages 3 and 6, located about midway of the ends of the shaft 15, are of the volute type wherein an impeller 16 discharges into a volute chamber 18 surrounding each impeller.
  • Each volute chamber 18 is formed in the casing 7 by webs or walls which are integral with the casing.
  • the chamber 18 for the third stage 3 is formed and located between walls 19 and 20 which are integral with the casing.
  • the chamber 18 for the sixth stage 6 is formed by similar walls 21 and 22.
  • the walls 19 and 22 lie in transverse planes relative to the axis of the casing 7 and serve to reinforce the casing against internal forces which tend to expand or bulge the casing outward.
  • the two walls 20 and 21 are connected together along their inner peripheries by a tubular section 23 extending axially of and surrounding the shaft 15.
  • the interior of the tubular section 23 is bored or machined and contains a conventional seal ring known as a channel ring 24.
  • the channel ring 24 engages and cooperates with an adjacent wear ring 25 carried by'the shaft 15 to form a seal betwen the third and sixth stages 3 and 6.
  • Each interior periphery of the walls 19 and 22 also carries a channel ring 26 which is larger in diameter than the channel ring 24 and cooperates with an adjacent impeller to form a seal between stages. Since the channel rings 26 for the walls 19 and 22 are larger than the channel ring 24, the seats for each channel ring 24 and 26 can be bored or machined without resorting to an undercutting operation.
  • the remaining stages 1, 2, 4 and 5, located outwardly of the stages 3 and 6, are of the diffuser ring type, wherein an impeller discharges into a diffuser ring 28 which is separate from the casing 7 and slides axially into the casing during its assembly.
  • Each diffuser ring 28 is similar for each stage and contains a series of discharge vanes 29 for receiving the high velocity fluid from an impeller 16 and converting the velocity into static pressure which flows into an annular cavity 30 surrounding the ring 28 and located between it and the casing 7.
  • the diffuser ring 28 further contains a group of inlet vanes 31 which direct the fluid radially inwardly from the annular cavity 30 to the inlet of the next succeeding stage.
  • the inlet vanes for the first stage 1 guide fluid from the annular cavity 30 of the first stage 1 to the inlet of the impeller 16 for the second stage 2.
  • Each end of the casing 7 is closed by an annular closure or end piece 33 and 34 having an annular rib 35 circling its circumference and fitting into an annular internal groove 36 formed in the casing 7.
  • Each of the end pieces axial thrust developed on'the impellers 16 of the first three stages 1 to 3 will counterbalance the thrust of the impellers 16 of the last three stages 4 to 6.
  • the total axial thrust on the shaft will be relatively small as compared to the thrust which would be developed if all of the stages were sequentially or numerically aligned.
  • volute chamber '18 of the sixth stage 6 is connected to the pump outlet 12 for discharging fluid from the pump. This connection is formed in the lower half 9 of the casing 7 during its casting.
  • the walls and 21 of the third and sixth stages; 3 and *6, are axially spaced and interconnected by horizontal flanges 39 which form extensions of the bolting flanges of the upper and lower halves 8 and 9 of the casing 7.
  • the flanges 39 extend radially and horizontally inwardly to the tubular section 23, surrounding the impeller shaft 1-5, as seen in FIG. 2. Since the flanges 39 extend inwardly near the shaft 1'5, they are bolted together by additional bolts or studs 40 located near the shaft 15 to provide the casing 7 with greatly in creased strength to resist expanding or bulging under internal pressures.
  • a multiple-stage centrifugal fluid machine having at least. three stages comprising:
  • a casing including integral internal walls located midway of its length and containing a volute dis charge passage for receiving fluid from the periphery of an impeller for at least one stage of the machine;
  • said casing is bolted together by bolt means extending transversely through said casing midway of its length near said shaft and within a radial distance from the axis of the shaft which is less than the radius of said separate rings.
  • said casing is formed of two separate halves which join each other along longitudinal surfaces and said closures include annular end plates having tongue and groove engagement with said casing halves for preventing said annular end plates from being forced axially apart from the casing by high internal pressures.

Landscapes

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

Description

18, 1966 v. s. LOBANOFF ETAL 3,229,642
MULTIPLE-STAGE PUMP 2 Sheets-Sheet 1 Filed Feb. 28, 1964 INVENTORS F M NM T M m w .0 m LRB mm 9 ATTORNEY 1966 v. s. LOBANOFF ETAL 3,229,642
MULT I PLES TAGE PUMP 2 Sheets-Sheet 2 Filed Feb. 28, 1964 WWW] S R m; M A w L 3 m HAROLD A. STAHL ATTORNEY United States Patent M 3,229,642 MULTIPLE-STAGE PUMP Val S. Lobanotf, Washington, N.J., and Harold A. Stahl, Easton, Pa., assignors to Ingersoll-Rand Company, New York, N.Y., a corporation of New Jersey Filed Feb. 28, 1964, Ser. No. 348,080 7 Claims. (Cl. 103-109) This invention relates to the art of fluid handling machines such as fluid pumps and fluid motors and particularly to plural-stage centrifugal pumps and motors.
One form of multiple-stage centrifugal pump includes a cylindrical outer casing containing a shaft carrying a plurality of impellers and a corresponding number of discharge rings surrounding the impellers for guiding and conducting fluid between the impellers and converting the kinetic energy or velocity of the fluid to potential energy or static pressure. These discharge rings are relatively easy to manufacture since they are separate from the casing. However, since the casing is hollow throughout its length, it expands considerably under high internal pressures. Such expansion is undesirable for various reasons including the fact that it usually causes relatively high rates of leakage between stages which reduces the efficiency of the pump.
Another form of pump uses a casing having the walls of the discharge passages for the impellers formed integrally with the casing. This form of pump casing is much stronger because it contains internal webs which act to prevent the outer walls of the casing from expanding substantially under high pressures. However, this type of pump is very laborious to manufacture with three or more stages because it inherently contains undercut surfaces which must be bored or machined blind with out the machinist being able to see the work or to progressively check it.
The principal object of this invention is to provide a multiple-stage centrifugal pump providing the advantages of the foregoing pumps and eliminating the disadvantages.
Other important objects of this invention include the following: to provide a multiple-stage centrifugal pump or motor having a relatively strong casing which can be manufactured without the need of blind boring or machining; to provide a better, more efficient multiplestage centrifugal pump or motor which can be manufactured less expensively and with less labor; to provide a multiple-stage centrifugal pump or motor having internal passages which can be easily cleaned; to provide a multiple-stage centrifugal pump or motor having a split casing which can be accurately bored and machined without separating the two casing halves each time a surface is checked or a machining tool is changed; to provide a multiple-stage centrifugal pump or motor which is bolted together midway of its length at points substantially near its axis to provide additional strength; and to provide a multiple-stage centrifugal pump or motor which reduces the leakage between stages to a minimum.
In general, these objects are provided by making the pump casing with no more than two stages located midway of its length and having integral walls forming the impeller discharge passages and with the remainder of the stages being formed by separate fluid discharge rings. The integral discharge passage walls reinforce the casing midway of its length and prevent the casing from expanding substantially under internal pressure. Since there are no more than two stages having integral discharge passage walls, these stages can be machined or bored without the need of blind boring methods.
The invention is described in connection with the accompanying drawings wherein:
FIG. 1 is an axial section of a pump embodying this invention;
3 ,229,642 Patented Jan. 18, 1966 FIG. 1A is a fragmentary section showing the left end of the pump of FIG. 1 which is broken away from FIG. 1 along the line 1A1A because of lack of space on a single sheet; and
FIG. 2 is a section of FIG. 1 taken along line 2-2 and drawn on an enlarged scale.
The multiple-stage centrifugal pump shown in FIG. 1 has six stages designated by the reference numbers 1 to 6. The pump includes an outer casing 7 which is formed from longitudinally split halves 8 and 9 which are bolted together by bolts or studs 10, as shown in FIG. 2. The casing 7 includes a fluid inlet 11 at one end and a fluid outlet 12 located about midway of its length. The pump further includes bearings 14 supported at each end of the casing 7 and rotatably carrying an impeller shaft 15 which extends axially through the casing 7 and carries six impellers 16, corresponding to the number of pump stages 1 to 6. The shaft 15 is adapted to be driven by a suitable power means such as an electric motor (not shown) connected to the right end of the shaft, shown in FIG. 1, projecting beyond the bearing 14. All of the foregoing structure is conventional and well known in the pump art.
The two central stages 3 and 6, located about midway of the ends of the shaft 15, are of the volute type wherein an impeller 16 discharges into a volute chamber 18 surrounding each impeller. Each volute chamber 18 is formed in the casing 7 by webs or walls which are integral with the casing. Thus, the chamber 18 for the third stage 3 is formed and located between walls 19 and 20 which are integral with the casing. The chamber 18 for the sixth stage 6 is formed by similar walls 21 and 22. The walls 19 and 22 lie in transverse planes relative to the axis of the casing 7 and serve to reinforce the casing against internal forces which tend to expand or bulge the casing outward.
The two walls 20 and 21 are connected together along their inner peripheries by a tubular section 23 extending axially of and surrounding the shaft 15. The interior of the tubular section 23 is bored or machined and contains a conventional seal ring known as a channel ring 24. The channel ring 24 engages and cooperates with an adjacent wear ring 25 carried by'the shaft 15 to form a seal betwen the third and sixth stages 3 and 6.
Each interior periphery of the walls 19 and 22 also carries a channel ring 26 which is larger in diameter than the channel ring 24 and cooperates with an adjacent impeller to form a seal between stages. Since the channel rings 26 for the walls 19 and 22 are larger than the channel ring 24, the seats for each channel ring 24 and 26 can be bored or machined without resorting to an undercutting operation.
The remaining stages 1, 2, 4 and 5, located outwardly of the stages 3 and 6, are of the diffuser ring type, wherein an impeller discharges into a diffuser ring 28 which is separate from the casing 7 and slides axially into the casing during its assembly. Each diffuser ring 28 is similar for each stage and contains a series of discharge vanes 29 for receiving the high velocity fluid from an impeller 16 and converting the velocity into static pressure which flows into an annular cavity 30 surrounding the ring 28 and located between it and the casing 7. The diffuser ring 28 further contains a group of inlet vanes 31 which direct the fluid radially inwardly from the annular cavity 30 to the inlet of the next succeeding stage. For example, the inlet vanes for the first stage 1 guide fluid from the annular cavity 30 of the first stage 1 to the inlet of the impeller 16 for the second stage 2.
Each end of the casing 7 is closed by an annular closure or end piece 33 and 34 having an annular rib 35 circling its circumference and fitting into an annular internal groove 36 formed in the casing 7. Each of the end pieces axial thrust developed on'the impellers 16 of the first three stages 1 to 3 will counterbalance the thrust of the impellers 16 of the last three stages 4 to 6. As a result, the total axial thrust on the shaft will be relatively small as compared to the thrust which would be developed if all of the stages were sequentially or numerically aligned.
The volute chamber '18 of the sixth stage 6 is connected to the pump outlet 12 for discharging fluid from the pump. This connection is formed in the lower half 9 of the casing 7 during its casting.
It will be noted that the walls and 21 of the third and sixth stages; 3 and *6, are axially spaced and interconnected by horizontal flanges 39 which form extensions of the bolting flanges of the upper and lower halves 8 and 9 of the casing 7. The flanges 39 extend radially and horizontally inwardly to the tubular section 23, surrounding the impeller shaft 1-5, as seen in FIG. 2. Since the flanges 39 extend inwardly near the shaft 1'5, they are bolted together by additional bolts or studs 40 located near the shaft 15 to provide the casing 7 with greatly in creased strength to resist expanding or bulging under internal pressures.
Although only one embodiment of the invention is illustrated and described in detail, it will be understood that the invention is not limited simply to this embodiment, but contemplates other embodiments and variations which utilize the concepts and teachings of this invention. For example, the invention may be useful with fluid motors as well as with the pump described.
Having described our invention, we claim:
'1. A multiple-stage centrifugal fluid machine having at least. three stages comprising:
(a) a casing including integral internal walls located midway of its length and containing a volute dis charge passage for receiving fluid from the periphery of an impeller for at least one stage of the machine;
(b) a plurality of separate rings mounted within said casing and containing discharge passages for. receiv ing fluid from the peripheries of impellers for other stages of the machine;
(c) a shaft extending axially through said casing and carrying multiple impellers corresponding with the stages of said machine; and
(d) removable closures at the opposite ends of said casing to close the interior of the casing.
2. The machine of claim 1 wherein:
(a) said casing is bolted together by bolt means extending transversely through said casing midway of its length near said shaft and within a radial distance from the axis of the shaft which is less than the radius of said separate rings.
3. The machine of claim 1 wherein:
(a) said casing is formed of two separate halves which join each other along longitudinal surfaces and said closures include annular end plates having tongue and groove engagement with said casing halves for preventing said annular end plates from being forced axially apart from the casing by high internal pressures.
4. The machine of claim 1 including:
(a) two center stages having discharge passages formed in integral internal walls in the casing; and
(b) at least one stage at each end of said casing having discharge passages formed in separate rings mounted in said casing.
5. The machine of claim 4 wherein: I
(a) said two center stages are spaced axially apart by walls containing bolts I extending transversely between said center stages and located radially near said shaft.
6. The machine of claim 5 including:
(a) at least two stages at each end of said center stages having discharge passages located in rings separ-ate from said casing.
7. The machine of claim 6 wherein:
(a) the third stage of said machine from one end discharges into a longitudinal passage conveying the fluid to a stage at the other end of said machine whereby the axial thrust developed in three stages of said machine acts in an opposite axial direction to the thrust developed in the other three stages of said machine.
References Cited by the Examiner FOREIGN PATENTS 3/1929 Germany. 12/ 1941 Switzerland.
SAMUEL LEVINE, Primary Examiner.
HENRY F. RADUAZO, Examiner.

Claims (1)

1. A MULTIPLE-STAGE CENTRIFUGAL FLUID MACHINE HAVING AT LEAST THREE STAGES COMPRISING: (A) A CASING INCLUDING INTEGRAL INTERNAL WALLS LOCATED MIDWAY OF ITS LENGTH AND CONTAINING A VOLUTE DISCHARGE PASSAGE FOR RECEIVING FLUID FROM THE PERIPHERY OF AN IMPELLER FOR AT LEAST ONE STAGE OF THE MACHINE; (B) A PLURALITY OF SEPARATE RINGS MOUNTED WITHIN SAID CASING AND CONTAINING DISCHARGE PASSAGES FOR RECEIVING FLUID FROM THE PERIPHERIES OF IMPELLERS FOR OTHER STAGES OF THE MACHINE;
US348080A 1964-02-28 1964-02-28 Multiple-stage pump Expired - Lifetime US3229642A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US348080A US3229642A (en) 1964-02-28 1964-02-28 Multiple-stage pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US348080A US3229642A (en) 1964-02-28 1964-02-28 Multiple-stage pump

Publications (1)

Publication Number Publication Date
US3229642A true US3229642A (en) 1966-01-18

Family

ID=23366559

Family Applications (1)

Application Number Title Priority Date Filing Date
US348080A Expired - Lifetime US3229642A (en) 1964-02-28 1964-02-28 Multiple-stage pump

Country Status (1)

Country Link
US (1) US3229642A (en)

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3861825A (en) * 1970-12-21 1975-01-21 Borg Warner Multistage pump and manufacturing method
DE3300505A1 (en) * 1983-01-08 1984-07-19 Klein, Schanzlin & Becker Ag, 6710 Frankenthal SEALING FOR LONG-SIDED HOUSINGS
US5246336A (en) * 1991-06-21 1993-09-21 Fuji Electric Co., Ltd. Motor driven complex pump apparatus
US20070110569A1 (en) * 2003-11-07 2007-05-17 Franco Sarri Multistage centrifugal compressor having a tank which can be opened horizontally
US20080213102A1 (en) * 2007-03-01 2008-09-04 Siemens Power Generation, Inc. Fluid pump having multiple outlets for exhausting fluids having different fluid flow characteristics
CN102606485A (en) * 2012-03-27 2012-07-25 上海阿波罗机械股份有限公司 Startup water feed pump for nuclear power station
US8985945B2 (en) 2009-08-19 2015-03-24 Mitsubishi Heavy Industries Compressor Corporation Radial gas expander
KR20150091515A (en) * 2012-12-05 2015-08-11 누보 피그노네 에스알엘 Back-to-back centrifugal pump
CN106030116A (en) * 2013-12-18 2016-10-12 诺沃皮尼奥内股份有限公司 Multi-section centrifugal compressor
CN106337821A (en) * 2016-09-29 2017-01-18 上海阿波罗机械股份有限公司 Startup feedwater pump set for nuclear power plant
US20180238332A1 (en) * 2015-08-10 2018-08-23 Nuovo Pignone Tecnologie Srl Centrifugal pump
US10364820B1 (en) * 2018-04-27 2019-07-30 Mitsubishi Heavy Industries Compressor Corporation Compressor and compressor-manufacturing method
US11326607B2 (en) * 2019-02-05 2022-05-10 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11359472B2 (en) 2019-02-05 2022-06-14 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11591899B2 (en) 2021-04-05 2023-02-28 Saudi Arabian Oil Company Wellbore density meter using a rotor and diffuser
US11788546B2 (en) * 2019-11-01 2023-10-17 Mitsubishi Heavy Industries Compressor Corporation Ammonia plant synthesis gas compressor train
US11994016B2 (en) 2021-12-09 2024-05-28 Saudi Arabian Oil Company Downhole phase separation in deviated wells

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE474126C (en) * 1927-04-30 1929-03-27 Michael Knoerlein Dipl Ing High-pressure centrifugal pump for relatively small delivery quantities (300 to about 1500 1 / min) against pressures of over 100 atue with several series-connected stage groups in a pressure-resistant housing
CH216495A (en) * 1940-04-05 1941-08-31 Escher Wyss Maschf Ag Multi-stage centrifugal pump with at least one inner bearing installed between two impellers.
US3160107A (en) * 1962-10-02 1964-12-08 Allis Chalmers Mfg Co Split casing pump

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE474126C (en) * 1927-04-30 1929-03-27 Michael Knoerlein Dipl Ing High-pressure centrifugal pump for relatively small delivery quantities (300 to about 1500 1 / min) against pressures of over 100 atue with several series-connected stage groups in a pressure-resistant housing
CH216495A (en) * 1940-04-05 1941-08-31 Escher Wyss Maschf Ag Multi-stage centrifugal pump with at least one inner bearing installed between two impellers.
US3160107A (en) * 1962-10-02 1964-12-08 Allis Chalmers Mfg Co Split casing pump

Cited By (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3861825A (en) * 1970-12-21 1975-01-21 Borg Warner Multistage pump and manufacturing method
DE3300505A1 (en) * 1983-01-08 1984-07-19 Klein, Schanzlin & Becker Ag, 6710 Frankenthal SEALING FOR LONG-SIDED HOUSINGS
US5246336A (en) * 1991-06-21 1993-09-21 Fuji Electric Co., Ltd. Motor driven complex pump apparatus
US7513735B2 (en) * 2003-11-07 2009-04-07 Nuovo Pignone Holding S.P.A. Multistage centrifugal compressor having a tank which can be opened horizontally
US20070110569A1 (en) * 2003-11-07 2007-05-17 Franco Sarri Multistage centrifugal compressor having a tank which can be opened horizontally
US7901177B2 (en) * 2007-03-01 2011-03-08 Siemens Energy, Inc. Fluid pump having multiple outlets for exhausting fluids having different fluid flow characteristics
US20080213102A1 (en) * 2007-03-01 2008-09-04 Siemens Power Generation, Inc. Fluid pump having multiple outlets for exhausting fluids having different fluid flow characteristics
US8985945B2 (en) 2009-08-19 2015-03-24 Mitsubishi Heavy Industries Compressor Corporation Radial gas expander
RU2548998C2 (en) * 2009-08-19 2015-04-20 Мицубиси Хэви Индастриз Компрессор Корпорейшн Radial expander
CN102606485A (en) * 2012-03-27 2012-07-25 上海阿波罗机械股份有限公司 Startup water feed pump for nuclear power station
US9803644B2 (en) * 2012-12-05 2017-10-31 Nuovo Pignone Srl Back-to-back centrifugal pump
KR20150091515A (en) * 2012-12-05 2015-08-11 누보 피그노네 에스알엘 Back-to-back centrifugal pump
US20150330391A1 (en) * 2012-12-05 2015-11-19 Nuovo Pignone Srl Back-to-back centrifugal pump
CN106030116A (en) * 2013-12-18 2016-10-12 诺沃皮尼奥内股份有限公司 Multi-section centrifugal compressor
US20160312786A1 (en) * 2013-12-18 2016-10-27 Nuovo Pignone Srl Multi-section centrifugal compressor
US10655627B2 (en) * 2013-12-18 2020-05-19 Nuovo Pignone Srl Multi-section centrifugal compressor
US11555496B2 (en) * 2015-08-10 2023-01-17 Nuovo Pignone Tecnologie Srl Centrifugal pump
US20180238332A1 (en) * 2015-08-10 2018-08-23 Nuovo Pignone Tecnologie Srl Centrifugal pump
CN106337821A (en) * 2016-09-29 2017-01-18 上海阿波罗机械股份有限公司 Startup feedwater pump set for nuclear power plant
US10364820B1 (en) * 2018-04-27 2019-07-30 Mitsubishi Heavy Industries Compressor Corporation Compressor and compressor-manufacturing method
JPWO2019207761A1 (en) * 2018-04-27 2021-04-22 三菱重工コンプレッサ株式会社 Compressor and method of manufacturing compressor
US11326607B2 (en) * 2019-02-05 2022-05-10 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11359472B2 (en) 2019-02-05 2022-06-14 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11686312B2 (en) 2019-02-05 2023-06-27 Saudi Arabian Oil Company Balancing axial thrust in submersible well pumps
US11788546B2 (en) * 2019-11-01 2023-10-17 Mitsubishi Heavy Industries Compressor Corporation Ammonia plant synthesis gas compressor train
US11591899B2 (en) 2021-04-05 2023-02-28 Saudi Arabian Oil Company Wellbore density meter using a rotor and diffuser
US11994016B2 (en) 2021-12-09 2024-05-28 Saudi Arabian Oil Company Downhole phase separation in deviated wells

Similar Documents

Publication Publication Date Title
US3229642A (en) Multiple-stage pump
US1973669A (en) Rotary pump
US2406947A (en) Centrifugal pump
US3043561A (en) Turbine rotor ventilation system
US2319730A (en) Pump
US3316848A (en) Pump casing
US3861825A (en) Multistage pump and manufacturing method
US2366964A (en) Centrifugal pump
US3051090A (en) Segmented casing for multistage centrifugal fluid machines
US3044684A (en) Centrifugal compressor construction
US2395704A (en) Rotor
US2365310A (en) Rotor unit
US1394959A (en) Shaft-packing
US2422763A (en) Centrifugal compressor
US2578617A (en) Multistage centrifugal compressor
US2543923A (en) Radial air compressor
US2496496A (en) Turbine pump
US3361073A (en) Casing for multi-stage centrifugal pump
US5527150A (en) Regenerative pumps
US9879690B2 (en) Compressor having hollow shaft
US2748713A (en) Multi-stage centrifugal pump or blower
US2430382A (en) Centrifugal machine casing
US1896809A (en) Multistage turbine
US1287367A (en) Centrifugal compressor.
US2306951A (en) Pump