US2641190A - Balanced impeller for centrifugal pumps - Google Patents

Balanced impeller for centrifugal pumps Download PDF

Info

Publication number
US2641190A
US2641190A US128813A US12881349A US2641190A US 2641190 A US2641190 A US 2641190A US 128813 A US128813 A US 128813A US 12881349 A US12881349 A US 12881349A US 2641190 A US2641190 A US 2641190A
Authority
US
United States
Prior art keywords
impeller
shroud
chamber
fluid
inlet
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
US128813A
Inventor
Thomas W Johnson
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.)
Bendix Aviation Corp
Original Assignee
Bendix Aviation Corp
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 Bendix Aviation Corp filed Critical Bendix Aviation Corp
Priority to US128813A priority Critical patent/US2641190A/en
Application granted granted Critical
Publication of US2641190A publication Critical patent/US2641190A/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
    • F04D29/18Rotors
    • F04D29/22Rotors specially for centrifugal pumps
    • F04D29/2261Rotors specially for centrifugal pumps with special measures
    • F04D29/2266Rotors specially for centrifugal pumps with special measures for sealing or thrust balance

Definitions

  • the present invention relates to centrifugal pumps and particularly to means and methods for balancing the axial reactive forces on the impellers thereof.
  • the casing It is, therefore, one of the objects of the presit contains an impeller chamber 18, having front ent invention to provide a novel method of baland rear walls It and 2
  • tary power 24 also contains an outlet
  • Another object of the invention is to provide chamber l8a peripherally disposed about impeller an impeller for a centrifugal pump whereby sevof chamber I8 and communicating therewith.
  • the eral of the power losses now present are elimseal 26 of the shaft 22 is considerably smaller in mated, diameter than inlet conduit 28, which difference
  • Another object of the invention is to provide contributes-to the unbalance of the axial loads on an impeller for a centrifugal pump whereby the impeller as hereinafter explained.
  • a seal shallow grooves of a specified size and number encompasses e aft 2 and prevents leakage on the rear of the shroud act as non-deliver- 3 from the chamber l8.
  • the impeller 20 includes ing centrifugal pumps so as to create a pressure a front shroud 32 and a rear shroud 34 held on the shroud to balance the other fluid forces together by pins 35.
  • Vanes 31 are provided thereon. in the'rear shroud 34 and open from the interior Still another object of the invention is to proof the impeller 20 to the chamber 18 and outlet vide a balanced impeller for a centrifugal pump 35 chamber 18a. 7 I thereby obviating the necessity for thrust bear- During normal operation of the pump, a clearings on the impeller.
  • ance space A between the front shroud 32 of the Another object of the invention is to balance impeller and the front wall IQ of impeller chamth fgrces on t impeller of a t if l pump ber l8, and a clearance space B between the rear in such a manner to permit a shorter overall 40 Shroud 34 0f e i p and the rear Wall 2
  • the rear shroud 34 of Still another object of the invention is to prothe impeller 20 contains a series of relatively vide means of the above-indicated character shallow slots 40 radially disposed about the which shall be simple and economical to manperiphery thereof and extending towards the ufacture and install, yet positive and reliable in shaft 22.
  • the length L of the slots 40 is adjusted operation. as hereinafter explained depending upon the The foregoing and other objects and adrelative unbalance of the impeller.
  • the pressure on the rear Shroud 34 would ordinarily be greater than the pres. sure on the front shroud 32 thereby causing an undesirable axial component in the direction of the inlet I4.
  • the slots 40 in the rear shroud 34 impart a turning swirling action to the fluid between the face 01 the rear shroud, 34 and the adjacent rear wall IQ of chamber I8, and in effect act as non-delivering centrifugal pumps, with the result that the total pressure on the rear shroud 34 is reduced tending to balance ra her than over ome the pr ssure on the front shroud, 32.
  • the invention permits extremely finite balancing of the impeller forces since the shallow grooves 40 may first be cut of insufficient length L to balance the impeller, and the operation tested and then gradually increased in length L after each test run, there. bygradually approaching and ultimately reaching the precise balance point.
  • the invention accomplishes the balancing of the impeller without the necessity of increasing the overall pump length since the fluid swirling means are contained within the impeller itself without protruding therefrom.
  • a centrifugal pump of the type including a casing, an impeller chamber in said casing having front and rear walls, an axial inlet said front wall, an outlet including an outlet chamber peripherally disposed about said im-, peller chamber, and an impeller mounted for rotation in said impeller chamber, said impeller having front and rear shrouds arranged in spaced relationship with the front and rear walls of said impeller chamber and pumping vanes interposed between said front and rear shrouds, said inlet opening into the interior of said im-.
  • the improvement comprising a plurality of shallow grooves formed in the outer radial surface of said rear shroud opposite said inlet, said grooves extending radially inwards from the periphery of said rear shroud and effective upon the retation of said impeller to rotate the fluid between said rear shroud and the wall of said impeller chamber adjacent said rear shroud whereby the rotational velocity of the rotating fluid is greatest adjacent the periphery of said rear shroud and the forces produced on the surface of said rear shroud by said rotating fluid are effective to balance the summation of all forces acting on the remaining surfaces of said impeller.
  • a centrifugal pump of the type including a casing, an impeller chamber in said casing having front and rear walls, an axial inlet in said front wall, an outlet including an outlet chamber peripherally disposed about said impeller chamber, and an impeller mounted forrotation in said impeller chamber, said impeller having front and rear shrouds arranged in spaced relationship with the front and rear walls of said impeller chamber and pumping vanes interposed between said front and rear shrouds, said inlet opening into the interior of said impeller whereby the rotation of said impeller pumps a fluid from said inlet to said outlet, said rear shroud having a greater outer surface than the outer surface of said front shroud whereby a greater force is produced on said rear shroud upon rotation of said impeller to pump a fluid from said inlet to said outlet;- the improvement comprising a plurality of radial grooves formed in the outer surface of said rear shroud, said radial grooves extending inwardly from the periphery of said rear shroud and

Description

June 9, 1953 1-. w. JOHNSON BALANCED IMPELLER FOR CENTRIFUGAL PUMPS Filed NOV. 22, 1949 2 Sheets-Sheet 1 INVENTOR.
m w H W M M w T,
June 9, 1953 Filed NOV. 22', 1949 T. W. JOHNSON BALANCED IMPELLER FOR CENTRIFUGAL PUMPS FIG. 3
2 Sheets-Sheet 2 v IN VEN TOR.
T HOMAS W OHNSON BY Patented June 9, 1953 BALANCED IMPELLER FOR c'ENTRIFUGAL PUMPS Thomas W. Johnson, Parsippany, N. J., assignor to Bendix Aviation Corporation, Teterboro, N. J a corporation of Delaware Application November 22, 1949, Serial-No. 128,813
The present invention relates to centrifugal pumps and particularly to means and methods for balancing the axial reactive forces on the impellers thereof.
r The action of the impeller during the opera- 5 of theinvention. tion of the pump is to hurl the fluid into the de- Referring to the drawin wherein like referlivery chamber from the impeller chamber thereenee characters designate l p r by causing a pressure gradient to exist about Fig. 1 iS an ele p y in section of a the impeller. The effect of this pumping action Centrifugal P p assemblyis to cause more fluid to flow into the pump cas- 8 2 is a perspective view of the impeller, rear ing, and as the action of the impeller is conce upw rdstinuous, the pressure gradient above-mentioned 3 is a View Showing the'lelative magnitude remains continuously across the impeller. Be- 0f the unbalanced areas of e peller. cause of the difference in area of the face of the Referring H W t th draw s d more p rear shroud and the face of the front shroud of ula y to F a Ce t fugal pump generally the impeller, the impeller and shaft are subdesig by he numeral 10 comprises a casjected to an undesirable axial thrust, illg l2 and inlet l4 and outlet is. The casing It is, therefore, one of the objects of the presit contains an impeller chamber 18, having front ent invention to provide a novel method of baland rear walls It and 2|, respectively, and where-' ancing the impeller means whereby the foregoing in the impeller 29 is free to rotate, driven y the disadvantage is eliminated, and to do so in a a t 22 which is coupled to the source of ronovel and effective manner. tary power 24. Casing l2 also contains an outlet Another object of the invention is to provide chamber l8a peripherally disposed about impeller an impeller for a centrifugal pump whereby sevof chamber I8 and communicating therewith. The eral of the power losses now present are elimseal 26 of the shaft 22 is considerably smaller in mated, diameter than inlet conduit 28, which difference Another object of the invention is to provide contributes-to the unbalance of the axial loads on an impeller for a centrifugal pump whereby the impeller as hereinafter explained. A seal shallow grooves of a specified size and number encompasses e aft 2 and prevents leakage on the rear of the shroud act as non-deliver- 3 from the chamber l8. The impeller 20 includes ing centrifugal pumps so as to create a pressure a front shroud 32 and a rear shroud 34 held on the shroud to balance the other fluid forces together by pins 35. Vanes 31 are provided thereon. in the'rear shroud 34 and open from the interior Still another object of the invention is to proof the impeller 20 to the chamber 18 and outlet vide a balanced impeller for a centrifugal pump 35 chamber 18a. 7 I thereby obviating the necessity for thrust bear- During normal operation of the pump, a clearings on the impeller. ance space A between the front shroud 32 of the Another object of the invention is to balance impeller and the front wall IQ of impeller chamth fgrces on t impeller of a t if l pump ber l8, and a clearance space B between the rear in such a manner to permit a shorter overall 40 Shroud 34 0f e i p and the rear Wall 2| pump length of chamber l8 are filled with fluid from the Still another object of the invention is to inoutlet chamber |8a and therefore, the shrouds crease the efficiency of a centrifugal pump by 32 and 34 are subjected to pressure therefrom eliminating the energy losses caused by the longiover the surfaces 36 and 38, respectively (Fig. 3). tudinal pull on the impeller. Referring now to Fig. 2, the rear shroud 34 of Still another object of the invention is to prothe impeller 20 contains a series of relatively vide means of the above-indicated character shallow slots 40 radially disposed about the which shall be simple and economical to manperiphery thereof and extending towards the ufacture and install, yet positive and reliable in shaft 22. The length L of the slots 40 is adjusted operation. as hereinafter explained depending upon the The foregoing and other objects and adrelative unbalance of the impeller. vantages will appear more fully hereinafter from Having thus explained the invention, it will a consideration of the detailed description which now be apparent to those skilled in the art that follows, taken together with the accompanying when a fluid from the inlet I4 is drawn into the drawings, wherein one embodiment of the invenimpeller 20 and hurled against the walls of the 2 Claims. (01. 103-103) tion is illustrated by way of example. It is to be expressly understood, however, that the drawings are for the purpose of illustration only, and are not to be construed as defining the limits outlet chamber [8a for ejection through the outlet It, all of the clearance space between the front shroud 32 and on the surface 38 of rear shroud 34. the rear shroud 34 and rear wall 2! of chamber [8 will become filled with fluid which will exercise a pressure on the surface 36 of the front shroud 32 and on the surface 32 of rear shroud 34.
Since the surface 38 is greater than the surface 36, partly because of the greater diameter of the inlet conduit 28 compared to the seal 24 of the shaft 22, the pressure on the rear Shroud 34 would ordinarily be greater than the pres. sure on the front shroud 32 thereby causing an undesirable axial component in the direction of the inlet I4. However, the slots 40 in the rear shroud 34 impart a turning swirling action to the fluid between the face 01 the rear shroud, 34 and the adjacent rear wall IQ of chamber I8, and in effect act as non-delivering centrifugal pumps, with the result that the total pressure on the rear shroud 34 is reduced tending to balance ra her than over ome the pr ssure on the front shroud, 32.
It is to be noted that the invention permits extremely finite balancing of the impeller forces since the shallow grooves 40 may first be cut of insufficient length L to balance the impeller, and the operation tested and then gradually increased in length L after each test run, there. bygradually approaching and ultimately reaching the precise balance point.
There are thus provided means for balancing the forces on the impeller of a centrifugal pump which are simple and economical to manufacture and yet positive and reliable in operation and which obviate the necessity for expensive thrust bearings.
It is further to be noted that the invention accomplishes the balancing of the impeller without the necessity of increasing the overall pump length since the fluid swirling means are contained within the impeller itself without protruding therefrom.
Although only one embodiment and one ap-s plication of the invention has been illustrated and described, other changes in form and relative arrangements of the parts may be made to suit requirements.
What is claimed is:
1. In a centrifugal pump of the type including a casing, an impeller chamber in said casing having front and rear walls, an axial inlet said front wall, an outlet including an outlet chamber peripherally disposed about said im-, peller chamber, and an impeller mounted for rotation in said impeller chamber, said impeller having front and rear shrouds arranged in spaced relationship with the front and rear walls of said impeller chamber and pumping vanes interposed between said front and rear shrouds, said inlet opening into the interior of said im-. peller whereby the rotation of said impeller pumps a fluid from said inlet to said outlet, and said impeller being effected by an unbalanced pressure distribution over the inner and outer surfaces of the front and rear shrouds upon Cal the pumping of a fluid as aforesaid, the improvement comprising a plurality of shallow grooves formed in the outer radial surface of said rear shroud opposite said inlet, said grooves extending radially inwards from the periphery of said rear shroud and effective upon the retation of said impeller to rotate the fluid between said rear shroud and the wall of said impeller chamber adjacent said rear shroud whereby the rotational velocity of the rotating fluid is greatest adjacent the periphery of said rear shroud and the forces produced on the surface of said rear shroud by said rotating fluid are effective to balance the summation of all forces acting on the remaining surfaces of said impeller.
2', In a centrifugal pump of the type including a casing, an impeller chamber in said casing having front and rear walls, an axial inlet in said front wall, an outlet including an outlet chamber peripherally disposed about said impeller chamber, and an impeller mounted forrotation in said impeller chamber, said impeller having front and rear shrouds arranged in spaced relationship with the front and rear walls of said impeller chamber and pumping vanes interposed between said front and rear shrouds, said inlet opening into the interior of said impeller whereby the rotation of said impeller pumps a fluid from said inlet to said outlet, said rear shroud having a greater outer surface than the outer surface of said front shroud whereby a greater force is produced on said rear shroud upon rotation of said impeller to pump a fluid from said inlet to said outlet;- the improvement comprising a plurality of radial grooves formed in the outer surface of said rear shroud, said radial grooves extending inwardly from the periphery of said rear shroud and terminating short of the center thereof, said radial grooves being effective upon the rotation of said impeller to produce a whirling of the fluid between said rear shroud and said rear wall to thereby produce a pressure distribution on the outer SUI. face of said rear shroud decreasing proportionately from a high value adjacent the periphery of said radial grooves toward a lower value adjacent the inner ends thereof whereby the forces on the front and rear shrouds are equalized.
THOMAS W. JOHNSON.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 633,732 Price Sept. 26, 1899 2,228,207 Forssell Jan. 7, 1941 2,247,813 Huitson July 1, 1941 2,361,521 Yates Oct. 31, 1944 FOREIGN PATENTS Number Country Date 443,332 Germany Apr. 26, 1927 698,291 France s Nov. 17, 1930
US128813A 1949-11-22 1949-11-22 Balanced impeller for centrifugal pumps Expired - Lifetime US2641190A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US128813A US2641190A (en) 1949-11-22 1949-11-22 Balanced impeller for centrifugal pumps

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US128813A US2641190A (en) 1949-11-22 1949-11-22 Balanced impeller for centrifugal pumps

Publications (1)

Publication Number Publication Date
US2641190A true US2641190A (en) 1953-06-09

Family

ID=22437094

Family Applications (1)

Application Number Title Priority Date Filing Date
US128813A Expired - Lifetime US2641190A (en) 1949-11-22 1949-11-22 Balanced impeller for centrifugal pumps

Country Status (1)

Country Link
US (1) US2641190A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2977042A (en) * 1957-12-13 1961-03-28 Sulzer Ag One-stage radial compressor
US3535051A (en) * 1968-12-03 1970-10-20 Ellicott Machine Corp Recessed expeller vanes
US5713719A (en) * 1995-12-08 1998-02-03 Caterpillar Inc. Self flushing centrifugal pump
US20030029393A1 (en) * 2001-02-15 2003-02-13 Litens Automotive Internal combustion engine combination with direct camshaft driven coolant pump
WO2004015274A2 (en) * 2002-08-13 2004-02-19 Litens Automotive Internal combustion engine combination with direct camshaft drive coolant pump
US20040136826A1 (en) * 2002-11-14 2004-07-15 Britt Timothy D. Centrifugal pump with self cooling and flushing features
US20150139828A1 (en) * 2013-11-19 2015-05-21 Charles Wayne Zimmerman Two piece impeller centrifugal pump
CZ305908B6 (en) * 2014-12-18 2016-04-27 Vysoké Učení Technické V Brně Modification of hydraulic machine rotor wheel for reducing axial force and hydraulic losses

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US633732A (en) * 1898-03-26 1899-09-26 Gomer W Price Centrifugal pump.
DE443332C (en) * 1927-04-26 Fritz Kugel Impeller for centrifugal pumps and centrifugal fans
FR698291A (en) * 1930-07-02 1931-01-29 Improvements to centrifugal pumps
US2228207A (en) * 1939-12-02 1941-01-07 Morris Machine Works Centrifugal pump
US2247813A (en) * 1939-08-11 1941-07-01 Gen Electric Centrifugal impeller
US2361521A (en) * 1943-11-01 1944-10-31 W S Darley & Company Centrifugal pump

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE443332C (en) * 1927-04-26 Fritz Kugel Impeller for centrifugal pumps and centrifugal fans
US633732A (en) * 1898-03-26 1899-09-26 Gomer W Price Centrifugal pump.
FR698291A (en) * 1930-07-02 1931-01-29 Improvements to centrifugal pumps
US2247813A (en) * 1939-08-11 1941-07-01 Gen Electric Centrifugal impeller
US2228207A (en) * 1939-12-02 1941-01-07 Morris Machine Works Centrifugal pump
US2361521A (en) * 1943-11-01 1944-10-31 W S Darley & Company Centrifugal pump

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2977042A (en) * 1957-12-13 1961-03-28 Sulzer Ag One-stage radial compressor
US3535051A (en) * 1968-12-03 1970-10-20 Ellicott Machine Corp Recessed expeller vanes
US5713719A (en) * 1995-12-08 1998-02-03 Caterpillar Inc. Self flushing centrifugal pump
US7047914B2 (en) * 2001-02-15 2006-05-23 Litens Automotive Internal combustion engine combination with direct camshaft driven coolant pump
US20030029393A1 (en) * 2001-02-15 2003-02-13 Litens Automotive Internal combustion engine combination with direct camshaft driven coolant pump
WO2004015274A2 (en) * 2002-08-13 2004-02-19 Litens Automotive Internal combustion engine combination with direct camshaft drive coolant pump
WO2004015274A3 (en) * 2002-08-13 2004-07-01 Litens Automotive Internal combustion engine combination with direct camshaft drive coolant pump
US20040136826A1 (en) * 2002-11-14 2004-07-15 Britt Timothy D. Centrifugal pump with self cooling and flushing features
US7008177B2 (en) 2002-11-14 2006-03-07 Cummins Inc. Centrifugal pump with self cooling and flushing features
US20150139828A1 (en) * 2013-11-19 2015-05-21 Charles Wayne Zimmerman Two piece impeller centrifugal pump
US9739284B2 (en) * 2013-11-19 2017-08-22 Charles Wayne Zimmerman Two piece impeller centrifugal pump
US20170314565A1 (en) * 2013-11-19 2017-11-02 Charles Wayne Zimmerman Two piece impeller centrifugal pump
US10100802B2 (en) * 2013-11-19 2018-10-16 Charles Wayne Zimmerman Two piece impeller centrifugal pump
CZ305908B6 (en) * 2014-12-18 2016-04-27 Vysoké Učení Technické V Brně Modification of hydraulic machine rotor wheel for reducing axial force and hydraulic losses

Similar Documents

Publication Publication Date Title
US9951786B2 (en) Centrifugal pump impellor with novel balancing holes that improve pump efficiency
US2349731A (en) Centrifugal pump
US2618433A (en) Means for bleeding air from compressors
US4164845A (en) Rotary compressors
US2641191A (en) Guide means on impeller for centrifugal pumps or blowers
US2233825A (en) Pump
US2641190A (en) Balanced impeller for centrifugal pumps
US2678537A (en) Axial flow turbine type hydraulic torque converter
US1334461A (en) Centrifugal pump
US2681760A (en) Centrifugal compressor
US3493169A (en) Bleed for compressor
US2741992A (en) Bladeless impeller balance means
US3541607A (en) Centrifugal pump
US1871747A (en) Impeller for centrifugal pumps
US3620021A (en) Gas turbine engines
US4315714A (en) Rotary compressors
US2362514A (en) Centrifugal compressor
US2546034A (en) Multiple pump and motor unit for aircraft fuel systems
US2399072A (en) Centrifugal compressor
US2395704A (en) Rotor
US2441239A (en) Blower apparatus
US2527971A (en) Axial-flow compressor
US2737897A (en) High altitude fuel system
US2397060A (en) Compressor
US2306951A (en) Pump