US2325477A - Pump - Google Patents

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US2325477A
US2325477A US315983A US31598340A US2325477A US 2325477 A US2325477 A US 2325477A US 315983 A US315983 A US 315983A US 31598340 A US31598340 A US 31598340A US 2325477 A US2325477 A US 2325477A
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impeller
pump
suction
case
fluid
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US315983A
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Collins Arthur Lee
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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
    • F04D7/00Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts
    • F04D7/02Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts of centrifugal type
    • F04D7/04Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts of centrifugal type the fluids being viscous or non-homogenous
    • F04D7/045Pumps adapted for handling specific fluids, e.g. by selection of specific materials for pumps or pump parts of centrifugal type the fluids being viscous or non-homogenous with means for comminuting, mixing stirring or otherwise treating
    • 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

  • My invention has to do with a centrifugal pump and particularly the type used for hydraulic dredging and a means for increasing the pressure at the intake of the pump impeller.
  • the pump must develop not only a suction liftwhich causes fluid to flow to the pump through the suction pipe, but also must maintain a pressure and rate of flow at the pump discharge outlet.
  • the total suction lift developed by the impeller can never be greater than the atmospheric pressure or less than about 15 pounds per square inch due to the vaporization of the fluid. This limited head then is required to overcome the entrance head, velocity head and friction head in the suction pipe and also the vertical lift of the fluid mixture ii the pump impeller is above the intake water surface.
  • the pump When the sum of the losses mentioned above exceeds the suction lift capacity of the impeller the pump will fail to operate satisfactorily due to the development of the water vapor at the impeller.
  • the impeller will accumulate a mixture of air and water vapor and will stop pumping with a sudden decrease in pressure at the pump discharge pipe. As a matter of fact the water in the discharge pipe will probably reverse its direction momentarily and even build up a positive pressure in the suction pipe when the suction head reaches its limit.
  • the object of my invention is to relieve the impeller of part of its responsibility for overcoming all of the various suction head losses. 0bviously to do this energy must be added to the suction stream from a source other than that developed by the impeller at the impeller intake. This is accomplished by introducing a relatively small stream of water at high velocity which will dissipate its energy in the slower moving suction stream entering the impeller.
  • Another object of the invention is to clear the impeller blades of sticw material, which may have adhered to vane surfaces, by the impact of the high velocity stream.
  • water vapor has a tendency to accumulate at various parts of the impeller and particularly at the tips of the vanes. at the impeller intake.
  • the deterioration of the pump metals at various surfaces due to the negative pressure condition is known as cavitation.
  • the jet will eliminate to a certain extent this efiect by breaking up the air pockets.
  • Fig. a. and Fig. B are elevation views of a centrifugal pump of which Fig. A is the side view of the pump looking at the suction.
  • Fig. C is a section. of a modified form of an inlet to the pump.
  • Numeral i designates the case in which the impeller .2 revolves.
  • the impeller vanes 2a and 2b may consist of a greater number than two. Impellers are also made with but one vane.
  • the pump case is supported on the blocksB and 9.
  • the impeller is supported by the shaft 3 and bearings 3a and 3b, and receives its power to rotate through the shall; by means of a motor or other power unit.
  • the shaft supporting the impeller enters the back of the case and the suction pipe is attached to the front of the case.
  • the suction pipe is l, of which 5 is a part.
  • the extended pump case is it. zles t and l are for operating and directing the fluid jets.
  • One or more jets can be used effectively.
  • Water from a suitable water source is supplied to the nozzles 6 and I as a means for developing a high velocity jet.
  • the jet is directed toward the impeller as well as to impinge upon the impeller surfaces.
  • Part 5 can be constructed with an annular
  • the discharge pipe is ill in Fig. A.
  • the noz- I chamber; Fig. 0. which can be attached to the pump ca e in place of 5 in Fig. B, and by means of a fluid s urce W, direct the Jet to the impeller.
  • the wall r in Fig. C corresponds to the wall s in Fig. 13..
  • the exterior wall of the annular section is e.
  • the inlet passages u and v are the equivalent oi nozzle 8 and I which direct the high velocity fluid at W to the impeller inlet 9.
  • the high velocity Jet will dissipate its energy in the zone indicated at the impeller inlet 1) and thereby facilitate the passing of the fluid mixture through the impeller and improve the pump operations materially by enabling the pump to maintain a more satisfactory suction lift. It is evident that the jets entering at an angle give an additional swirl and help the water enter the impeller thereby.
  • a centrifugal pump having a pump case and an impeller in said case, said case having an intake opening in axial alignment with said impeller, and a discharge opening z-in combination a plurality of nozzles on the intake side of said impeller to provide sources of added energy in conveying and directing liquid through the pump, said nozzles being disposed with respect to said impeller and each other to direct crossing but separated Jets in the general direction of the suction flow, and each nozzle being disposed to direct'its jet along a path leading from one side of the intake opening and through the impeller ports toward the discharge zone of said impeller opposite to said one side, said-path being spaced from the region of the axis of said impeller in the direction of the rotation of the said impeller.

Description

July 27, 1943- A. L COLLINS PUMP Filed Jan. 27, 1940 llll ll Yam INVENTOR.
WITNESSES Patented July 27, 1943 afar ' Arthur Lee Outline, Berkeley, Calif.
Application January 27, 1940, Serial No. 315,983
(Cl. Ills-) 1 Olalm.
My invention has to do with a centrifugal pump and particularly the type used for hydraulic dredging and a means for increasing the pressure at the intake of the pump impeller. The
pump when operated will have attached to it several feet of suction pipe and a discharge pipe.
The pump must develop not only a suction liftwhich causes fluid to flow to the pump through the suction pipe, but also must maintain a pressure and rate of flow at the pump discharge outlet.
As the fluid actually passes through the impeller it is first subjected to a negative pressure at the impeller inlet and then a positive pressure as it leaves the impeller. Obviously there is a zone in the impeller which is neither positive nor negative and is equal to the atmospheric pressure.
The total suction lift developed by the impeller can never be greater than the atmospheric pressure or less than about 15 pounds per square inch due to the vaporization of the fluid. This limited head then is required to overcome the entrance head, velocity head and friction head in the suction pipe and also the vertical lift of the fluid mixture ii the pump impeller is above the intake water surface.
Another loss of head in the suction system is the sharp angle which the fluid must follow as it enters the pump case and passes radially through the impeller. This loss is particularly important when the fluid becomes heavy by the addition'of solids.
When the sum of the losses mentioned above exceeds the suction lift capacity of the impeller the pump will fail to operate satisfactorily due to the development of the water vapor at the impeller. The impeller will accumulate a mixture of air and water vapor and will stop pumping with a sudden decrease in pressure at the pump discharge pipe. As a matter of fact the water in the discharge pipe will probably reverse its direction momentarily and even build up a positive pressure in the suction pipe when the suction head reaches its limit.
The object of my invention is to relieve the impeller of part of its responsibility for overcoming all of the various suction head losses. 0bviously to do this energy must be added to the suction stream from a source other than that developed by the impeller at the impeller intake. This is accomplished by introducing a relatively small stream of water at high velocity which will dissipate its energy in the slower moving suction stream entering the impeller.
Another object of the invention is to clear the impeller blades of sticw material, which may have adhered to vane surfaces, by the impact of the high velocity stream.
Also water vapor has a tendency to accumulate at various parts of the impeller and particularly at the tips of the vanes. at the impeller intake. The deterioration of the pump metals at various surfaces due to the negative pressure condition is known as cavitation. The jet will eliminate to a certain extent this efiect by breaking up the air pockets. W
My invention is now described. Fig. a. and Fig. B are elevation views of a centrifugal pump of which Fig. A is the side view of the pump looking at the suction. Fig. C is a section. of a modified form of an inlet to the pump. Numeral i designates the case in which the impeller .2 revolves. The impeller vanes 2a and 2b may consist of a greater number than two. Impellers are also made with but one vane. The pump case is supported on the blocksB and 9. The impeller is supported by the shaft 3 and bearings 3a and 3b, and receives its power to rotate through the shall; by means of a motor or other power unit. The shaft supporting the impeller enters the back of the case and the suction pipe is attached to the front of the case. The suction pipe is l, of which 5 is a part. The extended pump case is it. zles t and l are for operating and directing the fluid jets. The independent source of water W pump case at an angle m to the radius O-R, Fig.
A, and at an angle n to the direction of the stream in the suction pipe. One or more jets can be used effectively.
When the pump is in operation the impeller is revolving in the direction indicated by 7:, Fig. A, and fluid is'flowing into the pump unit through the suction pipe 4 and 5, suction inlet H, impeller inlet 11 and impeller passages or so-called ports, to the case and case outlet.
Water from a suitable water source is supplied to the nozzles 6 and I as a means for developing a high velocity jet. The jet is directed toward the impeller as well as to impinge upon the impeller surfaces.
Obviously it is possible to xtend the pump case inlet ll of the pump case proper so as to incorporate the pipe section 5 and make it unnecessary to provide this detachable part in order to accommodate the jet.
Part 5 can be constructed with an annular The discharge pipe is ill in Fig. A. The noz- I chamber; Fig. 0. which can be attached to the pump ca e in place of 5 in Fig. B, and by means of a fluid s urce W, direct the Jet to the impeller. The wall r in Fig. C corresponds to the wall s in Fig. 13.. The exterior wall of the annular section is e. The inlet passages u and v are the equivalent oi nozzle 8 and I which direct the high velocity fluid at W to the impeller inlet 9.
When the improvement to the pump is in operation the high velocity Jet will dissipate its energy in the zone indicated at the impeller inlet 1) and thereby facilitate the passing of the fluid mixture through the impeller and improve the pump operations materially by enabling the pump to maintain a more satisfactory suction lift. It is evident that the jets entering at an angle give an additional swirl and help the water enter the impeller thereby.
Iclaim: In a centrifugal pump having a pump case and an impeller in said case, said case having an intake opening in axial alignment with said impeller, and a discharge opening z-in combination a plurality of nozzles on the intake side of said impeller to provide sources of added energy in conveying and directing liquid through the pump, said nozzles being disposed with respect to said impeller and each other to direct crossing but separated Jets in the general direction of the suction flow, and each nozzle being disposed to direct'its jet along a path leading from one side of the intake opening and through the impeller ports toward the discharge zone of said impeller opposite to said one side, said-path being spaced from the region of the axis of said impeller in the direction of the rotation of the said impeller. ARTHUR L. COLLINS;
US315983A 1940-01-27 1940-01-27 Pump Expired - Lifetime US2325477A (en)

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2933045A (en) * 1954-01-27 1960-04-19 Morris D Isserlis Centrifugal pumps
US2986327A (en) * 1957-11-04 1961-05-30 Fairchild Engine & Airplane Axial flow centrifugal compressor and surge control system therefor
US5385443A (en) * 1993-10-12 1995-01-31 Les Traitements Des Eaux Poseidon Inc. Centrifugal liquid pump with internal gas injection assembly

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2933045A (en) * 1954-01-27 1960-04-19 Morris D Isserlis Centrifugal pumps
US2986327A (en) * 1957-11-04 1961-05-30 Fairchild Engine & Airplane Axial flow centrifugal compressor and surge control system therefor
US5385443A (en) * 1993-10-12 1995-01-31 Les Traitements Des Eaux Poseidon Inc. Centrifugal liquid pump with internal gas injection assembly

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