EP1204818A4 - Moteur turbine efficacit am lior e - Google Patents

Moteur turbine efficacit am lior e

Info

Publication number
EP1204818A4
EP1204818A4 EP99956476A EP99956476A EP1204818A4 EP 1204818 A4 EP1204818 A4 EP 1204818A4 EP 99956476 A EP99956476 A EP 99956476A EP 99956476 A EP99956476 A EP 99956476A EP 1204818 A4 EP1204818 A4 EP 1204818A4
Authority
EP
European Patent Office
Prior art keywords
turbine engine
efficiency enhanced
enhanced turbine
efficiency
engine
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Withdrawn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
EP99956476A
Other languages
German (de)
English (en)
Other versions
EP1204818A1 (fr
Inventor
Michael A Wilson
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 claimed from PCT/US1999/016305 external-priority patent/WO2001006102A1/fr
Publication of EP1204818A1 publication Critical patent/EP1204818A1/fr
Publication of EP1204818A4 publication Critical patent/EP1204818A4/fr
Withdrawn legal-status Critical Current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
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • 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
    • F01D5/022Blade-carrying members, e.g. rotors with concentric rows of axial blades
    • 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
    • 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
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant
    • F02C5/04Gas-turbine plants characterised by the working fluid being generated by intermittent combustion characterised by the arrangement of the combustion chamber in the chamber in the plant the combustion chambers being formed at least partly in the turbine rotor
    • 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
    • F02C7/125Cooling of plants by partial arc admission of the working fluid or by intermittent admission of working and cooling fluid
    • 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)
EP99956476A 1999-07-19 1999-07-19 Moteur turbine efficacit am lior e Withdrawn EP1204818A4 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1999/016305 WO2001006102A1 (fr) 1997-03-31 1999-07-19 Moteur à turbine à efficacité améliorée

Publications (2)

Publication Number Publication Date
EP1204818A1 EP1204818A1 (fr) 2002-05-15
EP1204818A4 true EP1204818A4 (fr) 2005-04-27

Family

ID=22273239

Family Applications (1)

Application Number Title Priority Date Filing Date
EP99956476A Withdrawn EP1204818A4 (fr) 1999-07-19 1999-07-19 Moteur turbine efficacit am lior e

Country Status (5)

Country Link
EP (1) EP1204818A4 (fr)
JP (1) JP2003505636A (fr)
AU (1) AU1307800A (fr)
CA (1) CA2376163C (fr)
MX (1) MXPA01013226A (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10876407B2 (en) * 2017-02-16 2020-12-29 General Electric Company Thermal structure for outer diameter mounted turbine blades
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB473714A (en) * 1937-01-18 1937-10-19 Patrick William Burke Improvements in or relating to turbines
US2370217A (en) * 1941-09-22 1945-02-27 Elwood H Wright Turbine type engine
US2524549A (en) * 1945-07-11 1950-10-03 Theimer Oscar Turbine
FR1010935A (fr) * 1950-02-07 1952-06-17 Turbine à combustion
US3685287A (en) * 1970-12-08 1972-08-22 Mcculloch Corp Re-entry type integrated gas turbine engine and method of operation
US3811796A (en) * 1971-10-21 1974-05-21 Gen Power Corp Integral turbo-compressor wave engine
US4503669A (en) * 1983-02-25 1985-03-12 Henri Geoffroy Gas turbine thrust system
GB2253657A (en) * 1990-12-08 1992-09-16 Colin Andrew Millar Tayler Improvements in or relating to gas turbines
US5960625A (en) * 1998-08-21 1999-10-05 Zdvorak, Sr.; Edward H. Constant volume combustion turbine with plurality flow turbine wheels

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB473714A (en) * 1937-01-18 1937-10-19 Patrick William Burke Improvements in or relating to turbines
US2370217A (en) * 1941-09-22 1945-02-27 Elwood H Wright Turbine type engine
US2524549A (en) * 1945-07-11 1950-10-03 Theimer Oscar Turbine
FR1010935A (fr) * 1950-02-07 1952-06-17 Turbine à combustion
US3685287A (en) * 1970-12-08 1972-08-22 Mcculloch Corp Re-entry type integrated gas turbine engine and method of operation
US3811796A (en) * 1971-10-21 1974-05-21 Gen Power Corp Integral turbo-compressor wave engine
US4503669A (en) * 1983-02-25 1985-03-12 Henri Geoffroy Gas turbine thrust system
GB2253657A (en) * 1990-12-08 1992-09-16 Colin Andrew Millar Tayler Improvements in or relating to gas turbines
US5960625A (en) * 1998-08-21 1999-10-05 Zdvorak, Sr.; Edward H. Constant volume combustion turbine with plurality flow turbine wheels

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of WO0106102A1 *

Also Published As

Publication number Publication date
CA2376163A1 (fr) 2001-01-25
JP2003505636A (ja) 2003-02-12
CA2376163C (fr) 2005-04-26
AU1307800A (en) 2001-02-05
MXPA01013226A (es) 2003-08-20
EP1204818A1 (fr) 2002-05-15

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