GB9919886D0 - Radial in flow gas turbine improvement - Google Patents

Radial in flow gas turbine improvement

Info

Publication number
GB9919886D0
GB9919886D0 GBGB9919886.3A GB9919886A GB9919886D0 GB 9919886 D0 GB9919886 D0 GB 9919886D0 GB 9919886 A GB9919886 A GB 9919886A GB 9919886 D0 GB9919886 D0 GB 9919886D0
Authority
GB
United Kingdom
Prior art keywords
radial
gas turbine
flow gas
improvement
turbine improvement
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.)
Withdrawn
Application number
GBGB9919886.3A
Other versions
GB2354043A (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
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 by Individual filed Critical Individual
Priority to GB9919886A priority Critical patent/GB2354043A/en
Publication of GB9919886D0 publication Critical patent/GB9919886D0/en
Publication of GB2354043A publication Critical patent/GB2354043A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/04Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • F01D5/046Heating, heat insulation or cooling means
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/04Blade-carrying members, e.g. rotors for radial-flow machines or engines
    • F01D5/043Blade-carrying members, e.g. rotors for radial-flow machines or engines of the axial inlet- radial outlet, or vice versa, type
    • F01D5/048Form or construction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/08Heating, heat-insulating or cooling means
    • F01D5/085Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor
    • F01D5/088Heating, heat-insulating or cooling means cooling fluid circulating inside the rotor in a closed cavity
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
GB9919886A 1999-08-24 1999-08-24 Cooling radial flow turbine Withdrawn GB2354043A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9919886A GB2354043A (en) 1999-08-24 1999-08-24 Cooling radial flow turbine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9919886A GB2354043A (en) 1999-08-24 1999-08-24 Cooling radial flow turbine

Publications (2)

Publication Number Publication Date
GB9919886D0 true GB9919886D0 (en) 1999-10-27
GB2354043A GB2354043A (en) 2001-03-14

Family

ID=10859614

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9919886A Withdrawn GB2354043A (en) 1999-08-24 1999-08-24 Cooling radial flow turbine

Country Status (1)

Country Link
GB (1) GB2354043A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9033670B2 (en) 2012-04-11 2015-05-19 Honeywell International Inc. Axially-split radial turbines and methods for the manufacture thereof
US9115586B2 (en) 2012-04-19 2015-08-25 Honeywell International Inc. Axially-split radial turbine
US9476305B2 (en) 2013-05-13 2016-10-25 Honeywell International Inc. Impingement-cooled turbine rotor

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB673393A (en) * 1950-02-14 1952-06-04 Burmeister & Wains Mot Mask Improvements in or relating to gas turbine rotors
GB711985A (en) * 1951-01-18 1954-07-14 Helmut Philipp Georg Alexander Improvements in gas turbines
GB705387A (en) * 1951-02-15 1954-03-10 Power Jets Res & Dev Ltd Improvements relating to radial-flow turbine or centrifugal compressors
GB741054A (en) * 1952-10-02 1955-11-23 Power Jets Res & Dev Ltd Improvements in or relating to radial flow turbines and centrifugal compressors
US4312625A (en) * 1969-06-11 1982-01-26 The United States Of America As Represented By The Secretary Of The Air Force Hydrogen cooled turbine
US4136516A (en) * 1977-06-03 1979-01-30 General Electric Company Gas turbine with secondary cooling means
GB2030656B (en) * 1978-09-26 1982-06-30 Savonuzzi G Bladed rotor for a centripetal turbine
GB2252368B (en) * 1981-03-20 1993-02-17 Rolls Royce Liquid cooled aerofoil blade
FR2769341B1 (en) * 1997-10-02 1999-11-19 Snecma FLUID COOLED TURBINE MONOBLOCK BLADE DISC

Also Published As

Publication number Publication date
GB2354043A (en) 2001-03-14

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)