US2000741A - Fluid jet pump - Google Patents

Fluid jet pump Download PDF

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Publication number
US2000741A
US2000741A US695249A US69524933A US2000741A US 2000741 A US2000741 A US 2000741A US 695249 A US695249 A US 695249A US 69524933 A US69524933 A US 69524933A US 2000741 A US2000741 A US 2000741A
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United States
Prior art keywords
boundary layer
jet pump
conduit
iluid
nozzle
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Expired - Lifetime
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US695249A
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Bruce O Buckland
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General Electric Co
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General Electric Co
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Priority to US695249A priority Critical patent/US2000741A/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04FPUMPING OF FLUID BY DIRECT CONTACT OF ANOTHER FLUID OR BY USING INERTIA OF FLUID TO BE PUMPED; SIPHONS
    • F04F5/00Jet pumps, i.e. devices in which flow is induced by pressure drop caused by velocity of another fluid flow
    • F04F5/44Component parts, details, or accessories not provided for in, or of interest apart from, groups F04F5/02 - F04F5/42
    • F04F5/46Arrangements of nozzles
    • F04F5/467Arrangements of nozzles with a plurality of nozzles arranged in series
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S415/00Rotary kinetic fluid motors or pumps
    • Y10S415/914Device to control boundary layer

Definitions

  • the present invention relates to uid iet pumps or injectors for conveying a uid by means oi a fast-moving stream of the same or another iluid and converting the velocity en- '5 ergy of the mixture into pressure energy in a the formation of a boundary layer of slowly moving iluid within the diiluser.
  • One object of the present invention is to provide an improved construction for pumps of the type above referred to in which the boundary layer is readily removed or substantially minimized in thickness.
  • the pump comprises a casing defining a suction chamber III having an inlet II for receiving uid to be conveyed and a diifuser or discharge conduit I2 having a diverging or diiluser portion in which the diilusion takes place.
  • a nozzle Il fastened to the casing by means o! bolts Il opens into the chamber in the direction o! the axis of the diffuser.
  • a iiuid under pressure is discharged through the nozzle I3 into the suction chamber III, where the jet or jets from the nozzle I3 entrain and increase the velocity of the fluid entering the inlet II.
  • the resulting mixture suilers a reduction in velocity and an increase in pressure in its passage through the diffuser I2.
  • a typical application oi pumps oi this kind is their use for conveying feed-water to a boiler y by means oi elastic fluid received from the boiler and discharged through the nozzle I3 into the suction chamber.
  • steam discharged from the nozzle I3 mixes with the water supplied through the inlet II whereby the steam condenses and creates a vacuum.
  • the mixture of iluid in the diffuser forms a boundary layer which moves very slowly or not at all and thereby renders the pump unstable and reduces its efllciency.
  • this boundary layer is eilectively removed by the provision of recesses or slots in the wall surface ofthe difiuser or discharge conduit and connecting these recesses to a point or points of lower pressure.
  • I have shown two annular slots or recesses I5 axially spaced apart 5 and provided in the wall oi the diffuser.
  • the diil'user wall deilning these slots has bulges I6.
  • the slots are connected to the suction chamber Il by means oi' conduits I1.
  • the slowly moving boundary4 layer being under l0 a pressure higher than the pressure existing in the suction chamber I0, is discharged through the conduits Il into the suction chamber.
  • the slots or recesses I5 are provided in the diverging or diiluser portion oi the conl5 duit I2 where the diiiusion takes place.
  • vfor removing the boundary layer I may provide an 25 auxiliary nozzle arrangement for injecting impelling fluid in tangential direction along the walls of the diiiuser.
  • anged portions Il uniting the suction chamber with the diiiuser are recessed to dene an annular chan- 30 nel I 9 connected to a conduit 20 for receiving impelling iiuid and discharging through one or a plurality oi nozzles 22 into the diffuser.
  • the impelling iluid discharged from the annular channel I9 accelerates the slowly moving bound- 35 ary layer and thus aids in removing the boundary layer.
  • the arrangement of the auxiliary slots-forms a part o! and is more fully disclosed in the application of Hans Krait, Serial No. 695,299, namelyd on the same date with the present 40 application.
  • my invention which comprises the provision of a plurality of grooves or slots in the diiluser wall and means for discharging the boundary layer 45 through the slot or slots to a point or points of lower pressure may be used singly or together with the auxiliary nozzle arrangement.
  • a casing defining a. suction chamber with an inlet ioriluid to be conveyed and a dischargeconduit having a daring diffuser portion, a nozzle for discharging a iet of impelling iluid into the chamber in the direction of the axis of the conduit, and conduit means connected to the flaring portion for removing a slowly moving boundary layer of fluid in said flaring portion to maintain stability during operation.
  • a casing denning' a suction chamber with an inlet for iluid-to be conveyed and a discharge conduit having a flaring diifuser portion, a nozzle for discharging a jet of impelling fluid into the chamber in the direction oi the axis of the conduit, and means for removing a slowly moving boundary layer oi' iluid in the conduit comprising at least one circumierentlally extending slot in the flaring portion of the discharge conduit connected to a point o! lower pressure.
  • a casing defining a suction chamber with an inlet for iluid to be conveyed and a discharge conduit having a naringdiiiuscr portion, a nozzle for discharging a iet of impelling iluid into the chamber in the direction o! the axis of the conduit, and means for removing a slowly moving boundary layer of iluid in the ilaring portion oi.' the conduit comprising a plurality of axially spaced apart circumferentially extending recesses in the flaring portion of the discharge conduit and conduits connecting the recesses to points of lower pressure.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)

Description

May 7, li935- 0 B. o. BUCKLAND 2,000,741
FLUID JET PUMP Filed Oct. 26, 1933 Inventor: Bruc vOrBuc Iad, by
HIS ttorney.
Patented May 1935 UNITED STATES PATENTA OFFICE FLUID JET PUMP Bruce 0. Buckland, Schenectady, N. Y., alsignor to General Electric Company, a corporation o! New York The present invention relates to uid iet pumps or injectors for conveying a uid by means oi a fast-moving stream of the same or another iluid and converting the velocity en- '5 ergy of the mixture into pressure energy in a the formation of a boundary layer of slowly moving iluid within the diiluser.
One object of the present invention is to provide an improved construction for pumps of the type above referred to in which the boundary layer is readily removed or substantially minimized in thickness.
For a consideration of what I believe to be novel and my invention, attention is directed to the following description and the claims appended thereto in connection with the accom-v drawing.
In the single ligure of the drawing I -have shown a sectional view of a iet pump embodying my invention. The pump comprises a casing defining a suction chamber III having an inlet II for receiving uid to be conveyed and a diifuser or discharge conduit I2 having a diverging or diiluser portion in which the diilusion takes place. A nozzle Il fastened to the casing by means o! bolts Il opens into the chamber in the direction o! the axis of the diffuser. The arrangement so far described is generally known in the art. During operation a iiuid under pressure is discharged through the nozzle I3 into the suction chamber III, where the jet or jets from the nozzle I3 entrain and increase the velocity of the fluid entering the inlet II. The resulting mixture suilers a reduction in velocity and an increase in pressure in its passage through the diffuser I2.
A typical application oi pumps oi this kind is their use for conveying feed-water to a boiler y by means oi elastic fluid received from the boiler and discharged through the nozzle I3 into the suction chamber. In this particular case steam discharged from the nozzle I3 mixes with the water supplied through the inlet II whereby the steam condenses and creates a vacuum. As pointed out above, the mixture of iluid in the diffuser forms a boundary layer which moves very slowly or not at all and thereby renders the pump unstable and reduces its efllciency. In accordance with my invention this boundary layer is eilectively removed by the provision of recesses or slots in the wall surface ofthe difiuser or discharge conduit and connecting these recesses to a point or points of lower pressure.
In the present instance I have shown two annular slots or recesses I5 axially spaced apart 5 and provided in the wall oi the diffuser. The diil'user wall deilning these slots has bulges I6. The slots are connected to the suction chamber Il by means oi' conduits I1. During operation the slowly moving boundary4 layer, being under l0 a pressure higher than the pressure existing in the suction chamber I0, is discharged through the conduits Il into the suction chamber. It is noted that the slots or recesses I5 are provided in the diverging or diiluser portion oi the conl5 duit I2 where the diiiusion takes place. The withdrawal of the boundary layer in the diiiuser renders the operation of the jet pump more stable in that itreduces the tendency of backilow of the boundary layer at certain points oi 20l the diiluser. Backiiow oi the boundary layer leads to whirling which reduces the eiliciency of a Jet pump.
In addition to the means just described vfor removing the boundary layer I may provide an 25 auxiliary nozzle arrangement for injecting impelling fluid in tangential direction along the walls of the diiiuser. To this end anged portions Il uniting the suction chamber with the diiiuser are recessed to dene an annular chan- 30 nel I 9 connected to a conduit 20 for receiving impelling iiuid and discharging through one or a plurality oi nozzles 22 into the diffuser. The impelling iluid discharged from the annular channel I9 accelerates the slowly moving bound- 35 ary layer and thus aids in removing the boundary layer. The arrangement of the auxiliary slots-forms a part o! and is more fully disclosed in the application of Hans Krait, Serial No. 695,299, iiled on the same date with the present 40 application.
It will be readily understood that my invention which comprises the provision of a plurality of grooves or slots in the diiluser wall and means for discharging the boundary layer 45 through the slot or slots to a point or points of lower pressure may be used singly or together with the auxiliary nozzle arrangement.
With my invention I have accomplished an improved construction oi fluid jet pumps or 50 injectors which are stable during operation and in addition have a higher eiliciency than ordinary jet pumps.
Having described the method of operation oi my invention, together with -the apparatus 55.
which I now consider to reprent the best embodiment thereof, I desire to have it understood that the apparatus shown is only illustrative and that the invention may be carried out by other means.
WhatIclaimasnew anddesiretosecureby Letters Patent of the United States is:
1. In a l1et pump, a casing defining a. suction chamber with an inlet ioriluid to be conveyed and a dischargeconduit having a daring diffuser portion, a nozzle for discharging a iet of impelling iluid into the chamber in the direction of the axis of the conduit, and conduit means connected to the flaring portion for removing a slowly moving boundary layer of fluid in said flaring portion to maintain stability during operation.
2. In a jet pump, a casing denning' a suction chamber with an inlet for iluid-to be conveyed and a discharge conduit having a flaring diifuser portion, a nozzle for discharging a jet of impelling fluid into the chamber in the direction oi the axis of the conduit, and means for removing a slowly moving boundary layer oi' iluid in the conduit comprising at least one circumierentlally extending slot in the flaring portion of the discharge conduit connected to a point o! lower pressure.
3. In a jet pump. a casing defining a suction chamber with an inlet for iluid to be conveyed and a discharge conduit having a naringdiiiuscr portion, a nozzle for discharging a iet of impelling iluid into the chamber in the direction o! the axis of the conduit, and means for removing a slowly moving boundary layer of iluid in the ilaring portion oi.' the conduit comprising a plurality of axially spaced apart circumferentially extending recesses in the flaring portion of the discharge conduit and conduits connecting the recesses to points of lower pressure.
4. In a jet pump, a casing deilning a suction chamber with an inlet for iluid to be conveyed and a discharge conduit having a ilaring dinuser portion, a nozzle for discharging a jet oi impeiling uid into the chamber in the direction ot the axis of the conduit, and means for removing a boundary layer of iluidin the flaring portion of the conduit comprising a plurality oi concentric axially spaced apart annular slots in the flaring portion of the discharge conduit and conduits connecting chamber. r
said slots to the suctionV BRUCE O. BUCKLAND. 25
US695249A 1933-10-26 1933-10-26 Fluid jet pump Expired - Lifetime US2000741A (en)

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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2892582A (en) * 1956-08-17 1959-06-30 O'rourke Neil Simplified boundary layer control for a jet
US2978169A (en) * 1957-10-03 1961-04-04 Bristol Siddeley Engines Ltd Means for preventing the accumulation of ice or other solids in ducts
US3045897A (en) * 1961-06-28 1962-07-24 Ethyl Corp Vacuum generation
US3047208A (en) * 1956-09-13 1962-07-31 Sebac Nouvelle Sa Device for imparting movement to gases
US3194056A (en) * 1962-01-26 1965-07-13 Hopkins Mfg Corp Inc Permeability testing method and apparatus
US3363545A (en) * 1966-07-08 1968-01-16 Owens Illinois Inc Electrical printing apparatus with means to control boundary layer effect
US3456456A (en) * 1966-07-01 1969-07-22 Philips Corp Cryogenic apparatus for producing cold
US3464230A (en) * 1966-07-01 1969-09-02 Philips Corp Systems for producing cold and ejectors in such systems
US3496735A (en) * 1967-07-27 1970-02-24 Philips Corp Ejector in refrigerating device
US3507294A (en) * 1966-12-14 1970-04-21 Philco Ford Corp Fluid flow control apparatus
US4029430A (en) * 1975-09-02 1977-06-14 Fonda Bonardi Giusto Short subsonic diffuser for large pressure ratios
US4493185A (en) * 1980-02-09 1985-01-15 Rolls-Royce Limited Gas turbine engine air intake
US4519899A (en) * 1982-12-13 1985-05-28 Sulzer-Escher Wyss Ltd. Purification of oil using a jet pump mixer
US4838307A (en) * 1985-09-18 1989-06-13 Nissan Motor Company, Limited Fuel tank arrangement
WO1993006340A1 (en) * 1991-09-23 1993-04-01 Benton Christopher E Method and apparatus for cooling an object
US5931643A (en) * 1993-02-12 1999-08-03 Skaggs; Bill D. Fluid jet ejector with primary fluid recirculation means
US6017195A (en) * 1993-02-12 2000-01-25 Skaggs; Bill D. Fluid jet ejector and ejection method
US6312229B1 (en) * 1998-04-27 2001-11-06 Evgueni D. Petroukhine Method for operating a pumping-ejection apparatus and apparatus for realising said method
EP1870146A3 (en) * 2006-01-04 2008-01-02 General Electric Company Reduced boundary layer separation steam jet air ejector assembly and method

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2892582A (en) * 1956-08-17 1959-06-30 O'rourke Neil Simplified boundary layer control for a jet
US3047208A (en) * 1956-09-13 1962-07-31 Sebac Nouvelle Sa Device for imparting movement to gases
US2978169A (en) * 1957-10-03 1961-04-04 Bristol Siddeley Engines Ltd Means for preventing the accumulation of ice or other solids in ducts
US3045897A (en) * 1961-06-28 1962-07-24 Ethyl Corp Vacuum generation
US3194056A (en) * 1962-01-26 1965-07-13 Hopkins Mfg Corp Inc Permeability testing method and apparatus
US3456456A (en) * 1966-07-01 1969-07-22 Philips Corp Cryogenic apparatus for producing cold
US3464230A (en) * 1966-07-01 1969-09-02 Philips Corp Systems for producing cold and ejectors in such systems
US3363545A (en) * 1966-07-08 1968-01-16 Owens Illinois Inc Electrical printing apparatus with means to control boundary layer effect
US3507294A (en) * 1966-12-14 1970-04-21 Philco Ford Corp Fluid flow control apparatus
US3496735A (en) * 1967-07-27 1970-02-24 Philips Corp Ejector in refrigerating device
US4029430A (en) * 1975-09-02 1977-06-14 Fonda Bonardi Giusto Short subsonic diffuser for large pressure ratios
US4493185A (en) * 1980-02-09 1985-01-15 Rolls-Royce Limited Gas turbine engine air intake
US4519899A (en) * 1982-12-13 1985-05-28 Sulzer-Escher Wyss Ltd. Purification of oil using a jet pump mixer
US4838307A (en) * 1985-09-18 1989-06-13 Nissan Motor Company, Limited Fuel tank arrangement
WO1993006340A1 (en) * 1991-09-23 1993-04-01 Benton Christopher E Method and apparatus for cooling an object
US5931643A (en) * 1993-02-12 1999-08-03 Skaggs; Bill D. Fluid jet ejector with primary fluid recirculation means
US6017195A (en) * 1993-02-12 2000-01-25 Skaggs; Bill D. Fluid jet ejector and ejection method
US6312229B1 (en) * 1998-04-27 2001-11-06 Evgueni D. Petroukhine Method for operating a pumping-ejection apparatus and apparatus for realising said method
EP1870146A3 (en) * 2006-01-04 2008-01-02 General Electric Company Reduced boundary layer separation steam jet air ejector assembly and method
US20090320478A1 (en) * 2006-01-04 2009-12-31 General Electric Company Reduced boundary layer separation steam jet air ejector assembly and method

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