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AU2003281869A1 - Vortex turbine engine - Google Patents

Vortex turbine engine

Info

Publication number
AU2003281869A1
AU2003281869A1 AU2003281869A AU2003281869A AU2003281869A1 AU 2003281869 A1 AU2003281869 A1 AU 2003281869A1 AU 2003281869 A AU2003281869 A AU 2003281869A AU 2003281869 A AU2003281869 A AU 2003281869A AU 2003281869 A1 AU2003281869 A1 AU 2003281869A1
Authority
AU
Australia
Prior art keywords
turbine engine
vortex turbine
vortex
engine
turbine
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.)
Abandoned
Application number
AU2003281869A
Other versions
AU2003281869A8 (en
Inventor
David A. Platts
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.)
University of California San Diego UCSD
Original Assignee
University of California Berkeley
University of California San Diego UCSD
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 University of California Berkeley, University of California San Diego UCSD filed Critical University of California Berkeley
Publication of AU2003281869A1 publication Critical patent/AU2003281869A1/en
Publication of AU2003281869A8 publication Critical patent/AU2003281869A8/en
Abandoned legal-status Critical Current

Links

Classifications

    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • F02C3/05Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes
    • F05D2240/127Vortex generators, turbulators, or the like, for mixing
    • 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
AU2003281869A 2002-07-23 2003-07-14 Vortex turbine engine Abandoned AU2003281869A1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US20242102A 2002-07-23 2002-07-23
US10/202,421 2002-07-23
PCT/US2003/021732 WO2004013473A2 (en) 2002-07-23 2003-07-14 Vortex turbine engine

Publications (2)

Publication Number Publication Date
AU2003281869A1 true AU2003281869A1 (en) 2004-02-23
AU2003281869A8 AU2003281869A8 (en) 2004-02-23

Family

ID=31494244

Family Applications (1)

Application Number Title Priority Date Filing Date
AU2003281869A Abandoned AU2003281869A1 (en) 2002-07-23 2003-07-14 Vortex turbine engine

Country Status (2)

Country Link
AU (1) AU2003281869A1 (en)
WO (1) WO2004013473A2 (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3126703A (en) * 1959-12-24 1964-03-31 Gas turbine power plant with rotary fuel atomization

Also Published As

Publication number Publication date
WO2004013473A2 (en) 2004-02-12
WO2004013473A3 (en) 2004-07-08
AU2003281869A8 (en) 2004-02-23

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Legal Events

Date Code Title Description
MK6 Application lapsed section 142(2)(f)/reg. 8.3(3) - pct applic. not entering national phase