GB9602118D0 - Multi stage concentric compressor for turbine engines - Google Patents

Multi stage concentric compressor for turbine engines

Info

Publication number
GB9602118D0
GB9602118D0 GBGB9602118.3A GB9602118A GB9602118D0 GB 9602118 D0 GB9602118 D0 GB 9602118D0 GB 9602118 A GB9602118 A GB 9602118A GB 9602118 D0 GB9602118 D0 GB 9602118D0
Authority
GB
United Kingdom
Prior art keywords
turbine engines
multi stage
stage concentric
compressor
concentric compressor
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Withdrawn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
GBGB9602118.3A
Other versions
GB2309745A (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 GB9602118A priority Critical patent/GB2309745A/en
Publication of GB9602118D0 publication Critical patent/GB9602118D0/en
Publication of GB2309745A publication Critical patent/GB2309745A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/064—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor having concentric stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/022—Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/022—Multi-stage pumps with concentric rows of vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB9602118A 1996-02-02 1996-02-02 Multi-stage compressor Withdrawn GB2309745A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9602118A GB2309745A (en) 1996-02-02 1996-02-02 Multi-stage compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9602118A GB2309745A (en) 1996-02-02 1996-02-02 Multi-stage compressor

Publications (2)

Publication Number Publication Date
GB9602118D0 true GB9602118D0 (en) 1996-04-03
GB2309745A GB2309745A (en) 1997-08-06

Family

ID=10788007

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9602118A Withdrawn GB2309745A (en) 1996-02-02 1996-02-02 Multi-stage compressor

Country Status (1)

Country Link
GB (1) GB2309745A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023103398A1 (en) * 2021-12-06 2023-06-15 李云峰 Air compression acting device and double-pressure jet engine having same
US11802507B2 (en) 2021-12-06 2023-10-31 Yunfeng Li Dual-pressure jet engine and device for work done by compressed air thereof

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3015589B1 (en) * 2013-12-23 2019-05-17 Safran Aircraft Engines AXIAL DOUBLE COMPRESSOR TURBOMACHINE

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB594522A (en) * 1944-01-31 1947-11-13 Power Jets Res & Dev Ltd Improvements in or relating to internal combustion turbine power plants
GB586554A (en) * 1941-11-22 1947-03-24 Karl Baumann Improvements in or relating to turbines
US2458037A (en) * 1946-08-01 1949-01-04 Continental Aviat & Engineerin Fluid energy machine
FR971613A (en) * 1948-09-14 1951-01-19 Axial flow generator or receiver turbomachine
GB698783A (en) * 1951-12-20 1953-10-21 Inconex Handelsgesellschaft M Compressor apparatus
GB838602A (en) * 1957-03-06 1960-06-22 Power Jets Res & Dev Ltd Improvements in or relating to gas turbine plant
GB9117859D0 (en) * 1991-08-19 1991-10-09 Framo Dev Ltd Pump or compressor unit

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023103398A1 (en) * 2021-12-06 2023-06-15 李云峰 Air compression acting device and double-pressure jet engine having same
US11802507B2 (en) 2021-12-06 2023-10-31 Yunfeng Li Dual-pressure jet engine and device for work done by compressed air thereof

Also Published As

Publication number Publication date
GB2309745A (en) 1997-08-06

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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)