US3504986A - Wide range inducer - Google Patents

Wide range inducer Download PDF

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Publication number
US3504986A
US3504986A US712427A US3504986DA US3504986A US 3504986 A US3504986 A US 3504986A US 712427 A US712427 A US 712427A US 3504986D A US3504986D A US 3504986DA US 3504986 A US3504986 A US 3504986A
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inducer
passage
fluid
impeller
pressure
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US712427A
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Clive Jackson
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Bendix Corp
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Bendix Corp
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    • 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
    • F04D29/2277Rotors specially for centrifugal pumps with special measures for increasing NPSH or dealing with liquids near boiling-point
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D15/00Control, e.g. regulation, of pumps, pumping installations or systems
    • F04D15/0005Control, e.g. regulation, of pumps, pumping installations or systems by using valves
    • F04D15/0011Control, e.g. regulation, of pumps, pumping installations or systems by using valves by-pass valves

Definitions

  • a pressure gradient can be determined and when pressure downstream becomes high, indicating reduced flow from the pump, this high pressure can operate to open a fluid return passage so that fluid may be'recirculated from the downstream side of the inducer to the upstream side of the inducer.
  • An inducer which is required to function over a wide flow range at high speed can develop a condition of cyclic flow instability at low flow rates. This is caused by prerotation of the fluidupstream of the inducer entry plane which may cause a cylindrical core of vaporto appear in the inducer entry passage. This cavity can go into forced radial oscillation at frequency dependent upon the system configuration.
  • the pressure pulses produced at the pump discharge can be violent enough to destroy the system, unless the pump speed is reduced or the flow raate is increased to regain a stable operating condition.
  • inducer rotational speed is proportional to or equal to main pump rotational speed as is the case in aircraft after burner applications where independent rotation of the inducer would cause an increase in weight and/or a decrease in available power. It is, therefore, an object of this invention to provide an inducer capable of stable operation over a wide range of flow rates and which does not require an independent driving source.
  • This invention discloses a method of automatically varying flow rate through the inducer in such a way that pump output is not affected. It, therefore, is an object of this invention to provide an inducer capable of stable operation over a wide range of pump output flow conditions. It is also an object of this invention to provide a novel means of recirculating pump flow. It is a further object of this invention to provide an automatic means for a high-speed fluid pump of by-passing fluid back to the upstream side of the inducer, whenever the downstream pressure conditions indicate approaching instability in the operating conditions of the pump.
  • the drawing shows a high speed centrifugal pump indicated generally by 10.
  • the inducer section indicated generally by 11, consists of a helical inducerblade or blades 12 formed on a shaft 14 which is a part of the main pump shaft 16.
  • Centrifugal impeller blades 18 and 20 radiate from the main pump shaft 16.
  • Surrounding the blade 12 is slidable valve or sleeve 22 which moves to open or close the port 24 of by-pass or recirculating passage 26. Passage 26 communicates with the main fluid passage 34 upstream of the inducer blade 12.
  • the sleeve 22 includes a flange 28 and seal 30 received in annular recess 32.
  • Fluid passage 36 extends from the recess 32 and communicates with the main fluid passage 34.
  • Fluid passage 38 extends from the recess 32 and communicates with the main fluid passage 34 downstream of the inducer blade 12.
  • Spring 40 is shown biasing the sleeve 22 to close the opening 24.
  • the flow characteristic of inducers is such that the pressure of fluid at the downstream side of the inducer is greater than the pressure at the upstream side of the inducer and the pressure at the downstream side is also inversely proportional to the flow through the inducer.
  • the passages 36 and 38 serve to establish the pressure rise across the impeller blade 12 and the spring 40 provides suflicient bias pressure against the flange 28 to keep the sleeve valve 22 closed until the downstream pressure rises to a sufllcient degree to indicate that the flow has approached the desired minimum for the inducer. At this point, the pressure in passage 38 will begin to move the flange 28 and sleeve 22 against the bias of the spring 40 and the port 24 will begin to open.
  • the improvement in the inducer comprising:
  • a main fluid passage operative to communicate a fluid to be pumped to the inlet of the downstream high speed pump;
  • said inducer comprising a helically bladed axial flow impeller rotatably located in said main fluid passage;
  • recirculatory passage means having an inlet port downstream from said impeller and an outlet port upstream from said impeller, operative to increase total flow through said impeller;
  • sensing means communicating with said main fluid passage downstream of said impeller and upstream of said high speed pump operative to sense fluid flow through said impeller;
  • valve means in co-operative association with said recirculatory passage means and operatively coupled to said sensing means to control fluid flow through said recirculatory passage means.
  • sensing means sense fluid flow by comparing fluid pressure upstream and downstream from said impeller.
  • valve means comprise a normally-closed valve means located in proximity to the inlet ports of said passage means.
  • sensing means comprise mechanical positioning means connected to said valve means, means for sensing and comparing fluid pressure upstream and downstream of said impeller and means for applying the resultant pressure to said mechanical positioning means.
  • An inducer for a high speed pump having a main fluid passage comprising: a helical axial flow impeller located in said passage; fluid by-pass means connected to said passage and operable when open to circulate fluid from the downstream side of the impeller to the upstream side of the impeller; and flow control means in cooperative association with said fluid by-pass to control flow therethrough operative to increase flow therethrough, as the fluid output from said pump decreases below a predetermined minimum wherein said flow control means comprise in combination:
  • each of said pressure sensing passages connected to opposed portions of said chamber, the other end of said first pressure sensing passage connected to said main fluid passage upstream of said impeller, the other end of said second pressure passage connected to said main fluid passage downstream of said impeller;
  • said pressure comparison chamber divided by a slidable partition to isolate each of said pressure sensing passages from the other;
  • valve control means connected to said partition to control valve position in response to partition position.
  • An inducer for a fluid pump having a main fluid passage comprising:
  • a slidable sleeve having a flange surrounding said impeller and in frictional contact with the wall defining said fluid input passage
  • said sleeve slidable from a first position to a second position and yieldably biased toward said first position by said spring
  • At least one recirculating passage having inlet and outlet passages in said main fluid passage, said inlet being downstream of said impeller and said outlet being upstream of said impeller;
  • said inlet being defined by the first and second positions of the downstream edge of said sleeve such that when said sleeve is in said first position, said inlet is closed;
  • said second passage operative to apply fluid pressure to said flange in opposition to said spring to position said flange insaid passage and control said inlet.
  • a device comprising in combination:
  • a high speed centrifugal pump having a fluid inlet passage
  • an axial flow inducer located in said inlet passage
  • said inducer including a helically bladed rotatable impeller
  • recirculatory passages means having inlet and outlet ports in said inlet passage and forming a by-pass around said inducer;
  • sensing means in communication with said inlet passage operative to sense fluid flow through said inducer
  • valve means in cooperative association with said recirculatory passage means and operatively coupled to said sensing means to control fluid flow through said recirculatory passage means to maintain flow through the inlet passage above a predetermined minimum.
  • valve means comprise normally closed sleeve valve means.

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

Description

April 7, 1 970 C/JACKSON I I 3,504,986
WIDE RANGE INDUCER Filgd March 12, 1968 CLIVE JACKSON INVENTOR.
United States Patent Office 3,504,986 WIDE RANGE INDUCER Clive Jackson, 'Clayville, N.Y., assignor to The Bendix Corporation, a corporation of Delaware Filed Mar. 12, 1968, Ser. No. 712,427 Int. Cl. F04tl 15/00 U.S. Cl. 415-11 Claims ABSTRACT OF THE DISCLOSURE An inducer for use in conjunction with high speed fluid pumps required to operate over a'wide flow range at high suction specific speeds. By placing pressure sensing passages upstream and downstream of the inducer, a pressure gradient can be determined and when pressure downstream becomes high, indicating reduced flow from the pump, this high pressure can operate to open a fluid return passage so that fluid may be'recirculated from the downstream side of the inducer to the upstream side of the inducer.
BRIEF SUMMARY OF THE INVENTION In high speed pumps which employ rote-dynamic effects to accomplish pumping and which are required to operate over a wide range of flows at low inlet pressures and/or high temperatures, it is often necessary to employ inducers to provide fluid to the impeller ofthe pump at suflicient pressure to overcome the vapor pressure of the fluid.
An inducer which is required to function over a wide flow range at high speed can develop a condition of cyclic flow instability at low flow rates. This is caused by prerotation of the fluidupstream of the inducer entry plane which may cause a cylindrical core of vaporto appear in the inducer entry passage. This cavity can go into forced radial oscillation at frequency dependent upon the system configuration. The pressure pulses produced at the pump discharge can be violent enough to destroy the system, unless the pump speed is reduced or the flow raate is increased to regain a stable operating condition.
This is especially true in applications where inducer rotational speed is proportional to or equal to main pump rotational speed as is the case in aircraft after burner applications where independent rotation of the inducer would cause an increase in weight and/or a decrease in available power. It is, therefore, an object of this invention to provide an inducer capable of stable operation over a wide range of flow rates and which does not require an independent driving source.
This invention discloses a method of automatically varying flow rate through the inducer in such a way that pump output is not affected. It, therefore, is an object of this invention to provide an inducer capable of stable operation over a wide range of pump output flow conditions. It is also an object of this invention to provide a novel means of recirculating pump flow. It is a further object of this invention to provide an automatic means for a high-speed fluid pump of by-passing fluid back to the upstream side of the inducer, whenever the downstream pressure conditions indicate approaching instability in the operating conditions of the pump. Other and further objects and advantages of the present invention will be obvious to the man skilled in the art from the included drawing and the appended claims.
BRIEF DESCRIPTION OF THE DRAWING The drawing shows, in schematic section, a preferred embodiment of an inducer and pump made according to the present invention with the control valve in a partiallyopen condition.
3,504,986 Patented Apr. 7, 1970 DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT The drawing shows a high speed centrifugal pump indicated generally by 10. The inducer section, indicated generally by 11, consists of a helical inducerblade or blades 12 formed on a shaft 14 which is a part of the main pump shaft 16. Centrifugal impeller blades 18 and 20 radiate from the main pump shaft 16. Surrounding the blade 12 is slidable valve or sleeve 22 which moves to open or close the port 24 of by-pass or recirculating passage 26. Passage 26 communicates with the main fluid passage 34 upstream of the inducer blade 12.
The sleeve 22 includes a flange 28 and seal 30 received in annular recess 32. Fluid passage 36 extends from the recess 32 and communicates with the main fluid passage 34. Fluid passage 38 extends from the recess 32 and communicates with the main fluid passage 34 downstream of the inducer blade 12. Spring 40 is shown biasing the sleeve 22 to close the opening 24.
OPERATION The flow characteristic of inducers is such that the pressure of fluid at the downstream side of the inducer is greater than the pressure at the upstream side of the inducer and the pressure at the downstream side is also inversely proportional to the flow through the inducer.
The passages 36 and 38 serve to establish the pressure rise across the impeller blade 12 and the spring 40 provides suflicient bias pressure against the flange 28 to keep the sleeve valve 22 closed until the downstream pressure rises to a sufllcient degree to indicate that the flow has approached the desired minimum for the inducer. At this point, the pressure in passage 38 will begin to move the flange 28 and sleeve 22 against the bias of the spring 40 and the port 24 will begin to open.
As the port 24 begins to open, static pressure on the downstream side of the inducer blade 12 will cause fluid to enter the port 24 and flow through the passage 26 to be discharged back into the main fluid stream 34 upstream of the inducer 11. Once the valve 22 begins to open, flow through the inducer 11 will remain substantially constant as pump output continues to decrease. For a given inducer and pump combination, the point at which the recirculating begins can be selected to give the best compromise between inducer power consumption and fluid temperature rise due to recirculation.
The persent invention accomplishes its stated objectives, but the description of the preferred embodiment should not be taken as limiting the scope of the invention, inasmuch as the man skilled in the art could alter the preferred embodiment without departing from the spirit of the invention as contained in the claims which follow.
I claim:
1. In the combination comprising an inducer and a high speed downstream pump wherein said combination is required to pump a fluid capable of becoming a twophase fluid, the improvement in the inducer comprising:
a main fluid passage operative to communicate a fluid to be pumped to the inlet of the downstream high speed pump; said inducer comprising a helically bladed axial flow impeller rotatably located in said main fluid passage;
recirculatory passage means having an inlet port downstream from said impeller and an outlet port upstream from said impeller, operative to increase total flow through said impeller;
sensing means communicating with said main fluid passage downstream of said impeller and upstream of said high speed pump operative to sense fluid flow through said impeller; and
valve means in co-operative association with said recirculatory passage means and operatively coupled to said sensing means to control fluid flow through said recirculatory passage means.
2. The device claimed in claim 1 wherein said sensing means sense fluid flow by comparing fluid pressure upstream and downstream from said impeller.
3. The device claimed in claim 1 wherein said valving means comprise a normally-closed valve means located in proximity to the inlet ports of said passage means.
4. The device as claimed in claim 1 where said sensing means comprise mechanical positioning means connected to said valve means, means for sensing and comparing fluid pressure upstream and downstream of said impeller and means for applying the resultant pressure to said mechanical positioning means.
5. An inducer for a high speed pump having a main fluid passage comprising: a helical axial flow impeller located in said passage; fluid by-pass means connected to said passage and operable when open to circulate fluid from the downstream side of the impeller to the upstream side of the impeller; and flow control means in cooperative association with said fluid by-pass to control flow therethrough operative to increase flow therethrough, as the fluid output from said pump decreases below a predetermined minimum wherein said flow control means comprise in combination:
first and second pressure sensing passages;
a pressure comparison chamber;
one end of each of said pressure sensing passages connected to opposed portions of said chamber, the other end of said first pressure sensing passage connected to said main fluid passage upstream of said impeller, the other end of said second pressure passage connected to said main fluid passage downstream of said impeller;
said pressure comparison chamber divided by a slidable partition to isolate each of said pressure sensing passages from the other;
said partition positionable in response to diflerential pressure in said pressure sensing passages; and
valve control means connected to said partition to control valve position in response to partition position.
6. An inducer for a fluid pump having a main fluid passage comprising:
an impeller rotatably mounted in said passage;
a slidable sleeve having a flange surrounding said impeller and in frictional contact with the wall defining said fluid input passage;
a spring retained within said passage;
said sleeve slidable from a first position to a second position and yieldably biased toward said first position by said spring;
said flange slidable in a recess in said wall and said spring contained in said recess acting against said flange;
at least one recirculating passage having inlet and outlet passages in said main fluid passage, said inlet being downstream of said impeller and said outlet being upstream of said impeller;
said inlet being defined by the first and second positions of the downstream edge of said sleeve such that when said sleeve is in said first position, said inlet is closed;
a first passage communicating said fluid input passage upstream of said impeller and said recess;
a second passage communicating said fluid input passage downstream of said impeller and said recess; and
said second passage operative to apply fluid pressure to said flange in opposition to said spring to position said flange insaid passage and control said inlet.
7. A device comprising in combination:
a high speed centrifugal pump having a fluid inlet passage;
an axial flow inducer located in said inlet passage;
said inducer including a helically bladed rotatable impeller;
recirculatory passages means having inlet and outlet ports in said inlet passage and forming a by-pass around said inducer;
sensing means in communication with said inlet passage operative to sense fluid flow through said inducer; and
valve means in cooperative association with said recirculatory passage means and operatively coupled to said sensing means to control fluid flow through said recirculatory passage means to maintain flow through the inlet passage above a predetermined minimum.
8. The device as claimed in claim 7 wherein said impeller has an operational speed proportional to the 0perational speed of said pump.
9. The device as claimed in claim 7 wherein said impeller is drivably connected to said pump.
10. The device as claimed in claim 7 wherein said valve means comprise normally closed sleeve valve means.
References Cited UNITED STATES PATENTS 2,786,420 3/1957 Kenney 103-97 2,865,297 12/1958 Cliborn et al. 103-97 2,874,642 2/ 1959 Forrest 103-97 3,070,025 12/1962 Cliborn 103-97 3,106,165 10/1963 Tyler 103-97 3,163,119 12/1964 Huppert et a1. 103-88 1,111,498 9/1914 Rotter 230- 2,398,619 4/1946 Clark et al. 230-115 FOREIGN PATENTS 611,447 10/ 1948 Great Britain. 605,032 7/ 1948 Great Britain.
HENRY F. RADUAZO, Primary Examiner US. Cl. X.R.
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US3994620A (en) * 1975-06-30 1976-11-30 Wallace-Murray Corporation Variable exducer turbine control
US4120603A (en) * 1977-03-28 1978-10-17 General Motors Corporation Jet flap controlled fuel pump
US4149825A (en) * 1977-11-08 1979-04-17 Chandler Evans Inc. Power conserving inducer
US4375938A (en) * 1981-03-16 1983-03-08 Ingersoll-Rand Company Roto-dynamic pump with a diffusion back flow recirculator
US4375937A (en) * 1981-01-28 1983-03-08 Ingersoll-Rand Company Roto-dynamic pump with a backflow recirculator
US4643635A (en) * 1984-07-02 1987-02-17 Chandler Evans Inc. Vapor core centrifugal pump having main and low flow impellers
DE3724299A1 (en) * 1986-10-09 1988-04-21 Rockwell International Corp PUMP WITH COVERED WHEEL
EP0297464A2 (en) * 1987-06-25 1989-01-04 A. Ahlstrom Corporation Method and apparatus for pumping high consistency fiber suspension
US4930978A (en) * 1988-07-01 1990-06-05 Household Manufacturing, Inc. Compressor stage with multiple vented inducer shroud
US4930979A (en) * 1985-12-24 1990-06-05 Cummins Engine Company, Inc. Compressors
WO1990014510A1 (en) * 1989-05-18 1990-11-29 Sundstrand Corporation Compressor shroud air bleed passages
US5059091A (en) * 1989-07-21 1991-10-22 Rolls-Royce Plc Gas turbine engine compressor assembly
US5156522A (en) * 1990-04-30 1992-10-20 Exxon Production Research Company Deflector means for centrifugal pumps
US5214920A (en) * 1990-11-27 1993-06-01 Leavesley Malcolm G Turbocharger apparatus
US5235803A (en) * 1992-03-27 1993-08-17 Sundstrand Corporation Auxiliary power unit for use in an aircraft
US5427501A (en) * 1994-05-03 1995-06-27 Parker-Hannifin Corporation Fuel pump impeller with pump down extension
US5505587A (en) * 1995-01-05 1996-04-09 Northrop Grumman Corporation RAM air turbine generating apparatus
WO2002103209A1 (en) * 2001-06-15 2002-12-27 Concepts Eti, Inc. Flow stabilizing device
US20050152775A1 (en) * 2004-01-14 2005-07-14 Concepts Eti, Inc. Secondary flow control system
WO2008141381A1 (en) * 2007-05-21 2008-11-27 Weir Minerals Australia Ltd Improvements in and relating to pumps
US20090060708A1 (en) * 2007-07-30 2009-03-05 Thomas Hale Radial flow compressor for a turbo-supercharger
US20090301082A1 (en) * 2005-11-16 2009-12-10 Alain Lombard Turbocharger having piston-type variable nozzle with integrated actuation system
EP2163769A2 (en) * 2008-09-11 2010-03-17 Honeywell International Compressor with variable-geometry ported shroud
US20140377051A1 (en) * 2013-06-25 2014-12-25 Ford Global Technologies, Llc Turbocharger
AU2013202763B2 (en) * 2007-05-21 2015-09-17 Weir Minerals Australia Ltd Improvements in and relating to pumps
US20160131145A1 (en) * 2014-11-10 2016-05-12 Honeywell International Inc. Adjustable-trim centrifugal compressor with ported shroud, and turbocharger having same
US20180045214A1 (en) * 2016-08-15 2018-02-15 Borgwarner, Inc. Compressor wheel, method of making the same, and turbocharger including the same
EP1473465B2 (en) 2003-04-30 2018-08-01 Holset Engineering Company Limited Compressor
US20180238236A1 (en) * 2015-07-24 2018-08-23 Nuovo Pignone Technologie Srl Charge gas compression train for ethylene
US20190368374A1 (en) * 2018-05-29 2019-12-05 Ford Global Technologies, Llc Systems and methods for a variable inlet compressor
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Cited By (66)

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Publication number Priority date Publication date Assignee Title
US3994620A (en) * 1975-06-30 1976-11-30 Wallace-Murray Corporation Variable exducer turbine control
US4120603A (en) * 1977-03-28 1978-10-17 General Motors Corporation Jet flap controlled fuel pump
US4149825A (en) * 1977-11-08 1979-04-17 Chandler Evans Inc. Power conserving inducer
DE2848514A1 (en) * 1977-11-08 1979-05-10 Chandler Evans Inc POWER-SAVING PUMP WHEEL
US4375937A (en) * 1981-01-28 1983-03-08 Ingersoll-Rand Company Roto-dynamic pump with a backflow recirculator
US4375938A (en) * 1981-03-16 1983-03-08 Ingersoll-Rand Company Roto-dynamic pump with a diffusion back flow recirculator
US4643635A (en) * 1984-07-02 1987-02-17 Chandler Evans Inc. Vapor core centrifugal pump having main and low flow impellers
US4930979A (en) * 1985-12-24 1990-06-05 Cummins Engine Company, Inc. Compressors
DE3724299A1 (en) * 1986-10-09 1988-04-21 Rockwell International Corp PUMP WITH COVERED WHEEL
EP0297464A2 (en) * 1987-06-25 1989-01-04 A. Ahlstrom Corporation Method and apparatus for pumping high consistency fiber suspension
EP0297464A3 (en) * 1987-06-25 1989-07-26 A. Ahlstrom Corporation Method and apparatus for pumping high consistency fiber suspension
US4884943A (en) * 1987-06-25 1989-12-05 A. Ahlstrom Corporation Method and apparatus for pumping high-consistency fiber suspension
US4930978A (en) * 1988-07-01 1990-06-05 Household Manufacturing, Inc. Compressor stage with multiple vented inducer shroud
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Also Published As

Publication number Publication date
GB1257567A (en) 1971-12-22
DE1912623A1 (en) 1969-10-09
FR2003743A1 (en) 1969-11-14

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