GB191111890A - - Google Patents

Info

Publication number
GB191111890A
GB191111890A GBL11890DA GB191111890A GB 191111890 A GB191111890 A GB 191111890A GB L11890D A GBL11890D A GB L11890DA GB 191111890 A GB191111890 A GB 191111890A
Authority
GB
United Kingdom
Prior art keywords
flow
suction
guide
parallel
impeller
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.)
Active
Application number
Other languages
English (en)
Publication of GB191111890A publication Critical patent/GB191111890A/en
Active legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04DNON-POSITIVE-DISPLACEMENT PUMPS
    • F04D3/00Axial-flow pumps
    • F04D3/005Axial-flow pumps with a conventional single stage rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Hydraulic Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GBL11890D Active GB191111890A (ja)

Publications (1)

Publication Number Publication Date
GB191111890A true GB191111890A (ja)

Family

ID=1653109

Family Applications (1)

Application Number Title Priority Date Filing Date
GBL11890D Active GB191111890A (ja)

Country Status (1)

Country Link
GB (1) GB191111890A (ja)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3169747A (en) * 1961-01-06 1965-02-16 Bristol Siddeley Engines Ltd Rotary bladed power conversion machines
US3209537A (en) * 1960-05-02 1965-10-05 Bendix Corp Motive fluid control for a re-expansion gas turbine engine
US3751180A (en) * 1970-12-08 1973-08-07 United Aircraft Canada Vane rings
EP2295732A1 (en) * 2009-09-14 2011-03-16 Alstom Technology Ltd Axial turbine and method for discharging a flow from an axial turbine

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3209537A (en) * 1960-05-02 1965-10-05 Bendix Corp Motive fluid control for a re-expansion gas turbine engine
US3169747A (en) * 1961-01-06 1965-02-16 Bristol Siddeley Engines Ltd Rotary bladed power conversion machines
US3751180A (en) * 1970-12-08 1973-08-07 United Aircraft Canada Vane rings
EP2295732A1 (en) * 2009-09-14 2011-03-16 Alstom Technology Ltd Axial turbine and method for discharging a flow from an axial turbine
US8506233B2 (en) 2009-09-14 2013-08-13 Alstom Technology Ltd. Axial turbine and method for discharging a flow from an axial turbine
DE102010044819B4 (de) 2009-09-14 2022-12-15 General Electric Technology Gmbh Axialturbine und ein Verfahren zum Abführen eines Stroms von einer Axialturbine

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