AU2635897A - Gas-turbine unit - Google Patents

Gas-turbine unit

Info

Publication number
AU2635897A
AU2635897A AU26358/97A AU2635897A AU2635897A AU 2635897 A AU2635897 A AU 2635897A AU 26358/97 A AU26358/97 A AU 26358/97A AU 2635897 A AU2635897 A AU 2635897A AU 2635897 A AU2635897 A AU 2635897A
Authority
AU
Australia
Prior art keywords
gas
compressor
turbine unit
turbine
plate
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
AU26358/97A
Inventor
Nadine Jung
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
Priority claimed from DE19630792A external-priority patent/DE19630792A1/en
Application filed by Individual filed Critical Individual
Publication of AU2635897A publication Critical patent/AU2635897A/en
Abandoned 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
    • F02C3/045—Gas-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
    • F02C3/05—Gas-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
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/12—Combinations with mechanical gearing
    • 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/045—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector for radial flow machines or engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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)
  • Separation By Low-Temperature Treatments (AREA)
  • Gas Separation By Absorption (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

The invention includes a gas-turbine unit with a compressor. In order to design a compact, single-shaft gas turbine so that it can easily and rapidly coupled as a module to various machines, the invention proposes that the rotor of the compressor and a turbine wheel (12) are located next to each other on the same shaft (14), diffusor blades at the radial extreme of the compressor rotor being located at one side of a plate (54) and guide vanes on the other side of the plate which has openings connecting with cooling channels or cavities in the guide vanes.
AU26358/97A 1996-04-04 1997-04-02 Gas-turbine unit Abandoned AU2635897A (en)

Applications Claiming Priority (5)

Application Number Priority Date Filing Date Title
DE19613781 1996-04-04
DE19613781 1996-04-04
DE19630792A DE19630792A1 (en) 1996-04-04 1996-07-31 Gas turbine unit
DE19630792 1996-07-31
PCT/EP1997/001659 WO1997038218A2 (en) 1996-04-04 1997-04-02 Gas-turbine unit

Publications (1)

Publication Number Publication Date
AU2635897A true AU2635897A (en) 1997-10-29

Family

ID=26024549

Family Applications (1)

Application Number Title Priority Date Filing Date
AU26358/97A Abandoned AU2635897A (en) 1996-04-04 1997-04-02 Gas-turbine unit

Country Status (5)

Country Link
EP (1) EP0891482B1 (en)
AT (1) ATE244820T1 (en)
AU (1) AU2635897A (en)
DE (1) DE19780258D2 (en)
WO (1) WO1997038218A2 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6897578B1 (en) * 2003-12-08 2005-05-24 Ingersoll-Rand Energy Systems Corporation Integrated microturbine gearbox generator assembly
US10907640B2 (en) 2016-02-16 2021-02-02 Apgn Inc. Gas turbine blower/pump
US11008938B2 (en) 2016-02-16 2021-05-18 Apgn Inc. Gas turbine blower/pump
WO2017139863A1 (en) * 2016-02-16 2017-08-24 Greentech Gas Turbine Inc. / Turbine A Gaz Greentech Inc. Gas turbine blower/pump

Family Cites Families (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE718650C (en) * 1940-09-10 1942-03-17 Turbinenfabrik Brueckner Kanis Internal combustion turbine
US2409159A (en) * 1944-08-26 1946-10-08 Allis Chalmers Mfg Co Elastic fluid conditioning apparatus
GB774415A (en) * 1954-08-20 1957-05-08 Power Jets Res & Dev Ltd An improved air conditioning plant
DE1079389B (en) * 1954-10-08 1960-04-07 David Dutton Budworth Combustion turbine with fuel evaporator
GB838332A (en) * 1955-12-20 1960-06-22 David Dutton Budworth Improvements in gas turbines
FR1304701A (en) * 1961-08-16 1962-09-28 Turboshaft Current Generating Machine
GB970189A (en) * 1963-01-31 1964-09-16 Rolls Royce Combustion equipment for a gas turbine engine
US3739572A (en) * 1972-07-19 1973-06-19 Gen Motors Corp Engine turbocharger drive system
US3955360A (en) * 1974-07-08 1976-05-11 Traut Earl W Integrated flow washboard turbine
US3994630A (en) * 1974-08-21 1976-11-30 International Harvester Company Monorotor turbine and method of cooling
US4312191A (en) * 1980-02-15 1982-01-26 Sundstrand Corporation Environmental control system for aircraft with improved efficiency
DE3302318A1 (en) * 1983-01-25 1983-08-04 Franz-Josef 3500 Kassel Weber Gas turbine
DE3402618A1 (en) * 1984-01-26 1985-08-08 Krupp Mak Maschinenbau Gmbh, 2300 Kiel DEVICE FOR AIR CONDITIONING
US4930306A (en) * 1988-05-26 1990-06-05 Sundstrand Corporation Reducing carbon buildup in a turbine engine
US5101620A (en) * 1988-12-28 1992-04-07 Sundstrand Corporation Annular combustor for a turbine engine without film cooling
GB2237372B (en) * 1989-10-10 1993-12-15 Aisin Seiki Exhaust driven air cycle air conditioner
US5105616A (en) * 1989-12-07 1992-04-21 Sundstrand Corporation Gas turbine with split flow radial compressor
US5174108A (en) * 1989-12-11 1992-12-29 Sundstrand Corporation Turbine engine combustor without air film cooling
DE4212984C2 (en) * 1992-02-07 1995-07-06 Man Nutzfahrzeuge Ag Motor vehicle with an internal combustion engine which can be charged by means of an exhaust gas turbocharger and a hydrostatic-mechanical drive for the auxiliary units
US5572862A (en) * 1993-07-07 1996-11-12 Mowill Rolf Jan Convectively cooled, single stage, fully premixed fuel/air combustor for gas turbine engine modules
GB9508043D0 (en) * 1995-04-20 1995-06-07 British Aerospace Environmental control system

Also Published As

Publication number Publication date
EP0891482B1 (en) 2003-07-09
DE19780258D2 (en) 1999-09-23
ATE244820T1 (en) 2003-07-15
EP0891482A2 (en) 1999-01-20
WO1997038218A2 (en) 1997-10-16
WO1997038218A3 (en) 1997-12-11

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