GB1267023A - - Google Patents

Info

Publication number
GB1267023A
GB1267023A GB1267023DA GB1267023A GB 1267023 A GB1267023 A GB 1267023A GB 1267023D A GB1267023D A GB 1267023DA GB 1267023 A GB1267023 A GB 1267023A
Authority
GB
United Kingdom
Prior art keywords
liquid
inducer
chamber
pressure
zone
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
Application number
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 filed Critical
Publication of GB1267023A publication Critical patent/GB1267023A/en
Expired legal-status Critical Current

Links

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
    • F04D29/66Combating cavitation, whirls, noise, vibration or the like; Balancing
    • F04D29/669Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for liquid pumps
    • 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
    • F04D29/04Shafts or bearings, or assemblies thereof
    • F04D29/041Axial thrust balancing
    • F04D29/0416Axial thrust balancing balancing pistons
    • 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
    • F04D29/00Details, component parts, or accessories
    • F04D29/40Casings; Connections of working fluid
    • F04D29/42Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/426Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for liquid pumps
    • F04D29/4273Casings; Connections of working fluid for radial or helico-centrifugal pumps especially adapted for liquid pumps suction eyes

Landscapes

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

Abstract

1,267,023. Centrifugal and axial-flow pumps. WORTHINGTON CORP. July 28, 1970 [July 31, 1969], No.36457/70. Heading F1C. A centrifugal or axial-flow pump comprises an inducer 24 coaxial with and preceding the impeller 13, means being provided to exert a fluid-dynamic action in at least one peripheral zone of the pump casing coincident with or adjacent the suction side of the inducer so as to act on the main flow and on the return flow pre-set in the zone in such manner as to stabilize the position of the return flow under substantially all operation conditions. The means comprises a slot 25 through which liquid is injected at an angle so as to overcome the tendency for the return flow zone to extend upstream of the leading edges of the inducer blades at low delivery rates. The liquid comes from a collecting chamber 26 which is kept at a pressure substantially equal to the pump suction pressure by means of ports 29, 30 and is supplied with liquid from the delivery side 19 leaking past wear rings 17 into at least one channel 28 opening into the collecting chamber and also with liquid from the discharge zone 21 of the inducer leaking past a clearance 22 into the channel. In order to balance end thrust, a chamber 23 receiving liquid leaking from the delivery side 19 past wear rings 18 is kept at the suction pressure, e.g., by being connected via a pipe 31 with the chamber 26. If the suction pressure is materially higher than the atmospheric pressure, a regulating valve may be provided in the pipe 31 to afford a compensatory increase in the pressure in the chamber 23.
GB1267023D 1969-07-31 1970-07-28 Expired GB1267023A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT2037969 1969-07-31

Publications (1)

Publication Number Publication Date
GB1267023A true GB1267023A (en) 1972-03-15

Family

ID=11166199

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1267023D Expired GB1267023A (en) 1969-07-31 1970-07-28

Country Status (8)

Country Link
AT (1) AT313066B (en)
BE (1) BE753794A (en)
DE (1) DE2037785A1 (en)
FR (1) FR2053339B1 (en)
GB (1) GB1267023A (en)
NL (1) NL7011212A (en)
NO (1) NO126637B (en)
SE (1) SE362931B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113775533A (en) * 2021-09-15 2021-12-10 浙江理工大学 Turbo pump device for rocket engine

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2621201C3 (en) * 1976-05-13 1979-09-27 Maschinenfabrik Augsburg-Nuernberg Ag, 8900 Augsburg Impeller for a turbomachine
DE2622155C2 (en) * 1976-05-19 1984-04-05 Robert Bosch Gmbh, 7000 Stuttgart Fuel pump
SU1023138A1 (en) * 1979-03-19 1983-06-15 Предприятие П/Я В-8534 Impeller pump
US4708584A (en) * 1986-10-09 1987-11-24 Rockwell International Corporation Shrouded inducer pump
CN111911446A (en) * 2020-09-23 2020-11-10 江西艾斯欧匹精密智造科技有限公司 Low-cost fan shock attenuation bearing structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113775533A (en) * 2021-09-15 2021-12-10 浙江理工大学 Turbo pump device for rocket engine
CN113775533B (en) * 2021-09-15 2024-02-20 浙江理工大学 Turbopump device for rocket engine

Also Published As

Publication number Publication date
SE362931B (en) 1973-12-27
FR2053339A1 (en) 1971-04-16
NL7011212A (en) 1971-02-02
DE2037785A1 (en) 1971-02-11
NO126637B (en) 1973-03-05
FR2053339B1 (en) 1973-03-16
BE753794A (en) 1970-12-31
AT313066B (en) 1974-01-25

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee