MXPA01013226A - Efficiency enhanced turbine engine. - Google Patents

Efficiency enhanced turbine engine.

Info

Publication number
MXPA01013226A
MXPA01013226A MXPA01013226A MXPA01013226A MXPA01013226A MX PA01013226 A MXPA01013226 A MX PA01013226A MX PA01013226 A MXPA01013226 A MX PA01013226A MX PA01013226 A MXPA01013226 A MX PA01013226A MX PA01013226 A MXPA01013226 A MX PA01013226A
Authority
MX
Mexico
Prior art keywords
turbine engine
efficiency enhanced
enhanced turbine
efficiency
engine
Prior art date
Application number
MXPA01013226A
Other languages
Spanish (es)
Inventor
Michael A Wilson
Original Assignee
Michael A Wilson
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 Michael A Wilson filed Critical Michael A Wilson
Priority claimed from PCT/US1999/016305 external-priority patent/WO2001006102A1/en
Publication of MXPA01013226A publication Critical patent/MXPA01013226A/en

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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02—Gas-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
    • 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
    • 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
    • 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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/02—Gas-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
    • F02C5/04—Gas-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
    • 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
    • F02C7/00—Features, 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
    • F02C7/12—Cooling of plants
    • F02C7/125—Cooling of plants by partial arc admission of the working fluid or by intermittent admission of working and cooling fluid
    • 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
MXPA01013226A 1999-07-19 1999-07-19 Efficiency enhanced turbine engine. MXPA01013226A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1999/016305 WO2001006102A1 (en) 1997-03-31 1999-07-19 Efficiency enhanced turbine engine

Publications (1)

Publication Number Publication Date
MXPA01013226A true MXPA01013226A (en) 2003-08-20

Family

ID=22273239

Family Applications (1)

Application Number Title Priority Date Filing Date
MXPA01013226A MXPA01013226A (en) 1999-07-19 1999-07-19 Efficiency enhanced turbine engine.

Country Status (5)

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

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

Family Cites Families (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 (en) * 1950-02-07 1952-06-17 Combustion turbine
US3685287A (en) * 1970-12-08 1972-08-22 Mcculloch Corp Re-entry type integrated gas turbine engine and method of operation
BE790403A (en) * 1971-10-21 1973-04-20 Gen Power Corp INTEGRAL WAVE TURBO-COMPRESSOR
US4503669A (en) * 1983-02-25 1985-03-12 Henri Geoffroy Gas turbine thrust system
GB9026748D0 (en) * 1990-12-08 1991-01-30 Tayler Colin A M 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

Also Published As

Publication number Publication date
EP1204818A4 (en) 2005-04-27
CA2376163A1 (en) 2001-01-25
JP2003505636A (en) 2003-02-12
EP1204818A1 (en) 2002-05-15
AU1307800A (en) 2001-02-05
CA2376163C (en) 2005-04-26

Similar Documents

Publication Publication Date Title
EP1196686A4 (en) High efficiency, air bottoming engine
GB2360551B (en) Turbines
EP1198669A4 (en) Low emission, diesel-cycle engine
GB2347221B (en) Gas turbine engine
GB2355784B (en) Gas turbine
GB0025244D0 (en) Turbine
DE50101990D1 (en) Turbine
GB9925856D0 (en) Turbine engines
ZA200110324B (en) High efficiency turbine.
GB2346177B (en) Gas turbine engine
PL373858A1 (en) Turbine engine
GB2348675B (en) Gas turbine engine
GB9904277D0 (en) Gas turbine engine
GB2356022B (en) Gas turbine engines
GB2366599B (en) Gas turbine engine system
GB2355302B (en) Gas turbine engines
GB9923809D0 (en) A gas turbine engine
MXPA01013226A (en) Efficiency enhanced turbine engine.
GB9929012D0 (en) Modified exhaust turbine
GB9918074D0 (en) Turbine inlet
GB9902502D0 (en) Turbine engine
ZA200001060B (en) Internal-combustion engine.
AU2001295007A1 (en) Gas turbine engine having improved efficiency
GB2356671B (en) Gas turbine engine
GB0027605D0 (en) Internal combustion turbine