FR383966A - Turbine à combustion interne - Google Patents

Turbine à combustion interne

Info

Publication number
FR383966A
FR383966A FR383966DA FR383966A FR 383966 A FR383966 A FR 383966A FR 383966D A FR383966D A FR 383966DA FR 383966 A FR383966 A FR 383966A
Authority
FR
France
Prior art keywords
internal combustion
combustion turbine
turbine
internal
combustion
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.)
Expired
Application number
Other languages
English (en)
Inventor
Armand Ferrier
Pierre-Max-Raoul Salles
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.)
ARMAND FERRIER
Original Assignee
ARMAND FERRIER
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 ARMAND FERRIER filed Critical ARMAND FERRIER
Application granted granted Critical
Publication of FR383966A publication Critical patent/FR383966A/fr
Expired 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
    • 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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • 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
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • F02C7/141—Cooling of plants of fluids in the plant, e.g. lubricant or fuel of working fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR383966D 1907-09-26 1907-09-26 Turbine à combustion interne Expired FR383966A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR383966T 1907-09-26

Publications (1)

Publication Number Publication Date
FR383966A true FR383966A (fr) 1908-03-25

Family

ID=1429944

Family Applications (1)

Application Number Title Priority Date Filing Date
FR383966D Expired FR383966A (fr) 1907-09-26 1907-09-26 Turbine à combustion interne

Country Status (1)

Country Link
FR (1) FR383966A (fr)

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2424610A (en) * 1943-04-12 1947-07-29 Daniel And Florence Guggenheim Rotating combustion apparatus
US2425904A (en) * 1941-11-29 1947-08-19 James B Vernon Turbine
US2448972A (en) * 1944-10-20 1948-09-07 Edward W Gizara Internal-combusstion engine
US2490064A (en) * 1945-01-12 1949-12-06 Kollsman Paul Thermodynamic machine
US2584805A (en) * 1945-07-18 1952-02-05 Robert F Leftwich Method and apparatus for producing an emulsion, including water, fuel oil, and finely divided solids for combustion
US2631429A (en) * 1948-06-08 1953-03-17 Jr Harold M Jacklin Cooling arrangement for radial flow gas turbines having coaxial combustors
US2659196A (en) * 1949-08-09 1953-11-17 United Aircraft Corp Centrifugal fuel supply means for jet engine afterburners
US2671315A (en) * 1948-11-12 1954-03-09 Rocheville Engineering Inc Internal-combustion geared turbine
US2945619A (en) * 1954-09-21 1960-07-19 Mclure Carl Ballard Stage expansion reaction turbines
DE1190734B (de) * 1963-09-12 1965-04-08 Sergio Simioni Verbrennungsturbine
FR2446384A1 (fr) * 1979-01-15 1980-08-08 Simon Jean Turbomachine
EP0071419A1 (fr) * 1981-07-30 1983-02-09 Solar Turbines Incorporated Appareil de combustion à émission réduite d'oxydes d'azote
EP2102471A4 (fr) * 2006-12-28 2017-04-26 Rotoboost AS Dispositif rotatif

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2425904A (en) * 1941-11-29 1947-08-19 James B Vernon Turbine
US2424610A (en) * 1943-04-12 1947-07-29 Daniel And Florence Guggenheim Rotating combustion apparatus
US2448972A (en) * 1944-10-20 1948-09-07 Edward W Gizara Internal-combusstion engine
US2490064A (en) * 1945-01-12 1949-12-06 Kollsman Paul Thermodynamic machine
US2584805A (en) * 1945-07-18 1952-02-05 Robert F Leftwich Method and apparatus for producing an emulsion, including water, fuel oil, and finely divided solids for combustion
US2631429A (en) * 1948-06-08 1953-03-17 Jr Harold M Jacklin Cooling arrangement for radial flow gas turbines having coaxial combustors
US2671315A (en) * 1948-11-12 1954-03-09 Rocheville Engineering Inc Internal-combustion geared turbine
US2659196A (en) * 1949-08-09 1953-11-17 United Aircraft Corp Centrifugal fuel supply means for jet engine afterburners
US2945619A (en) * 1954-09-21 1960-07-19 Mclure Carl Ballard Stage expansion reaction turbines
DE1190734B (de) * 1963-09-12 1965-04-08 Sergio Simioni Verbrennungsturbine
FR2446384A1 (fr) * 1979-01-15 1980-08-08 Simon Jean Turbomachine
EP0071419A1 (fr) * 1981-07-30 1983-02-09 Solar Turbines Incorporated Appareil de combustion à émission réduite d'oxydes d'azote
EP2102471A4 (fr) * 2006-12-28 2017-04-26 Rotoboost AS Dispositif rotatif

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