FR1002314A - Turbo-engine - Google Patents

Turbo-engine

Info

Publication number
FR1002314A
FR1002314A FR1002314DA FR1002314A FR 1002314 A FR1002314 A FR 1002314A FR 1002314D A FR1002314D A FR 1002314DA FR 1002314 A FR1002314 A FR 1002314A
Authority
FR
France
Prior art keywords
turbo
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.)
Expired
Application number
Other languages
French (fr)
Inventor
Rene Leduc
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 filed Critical
Application granted granted Critical
Publication of FR1002314A publication Critical patent/FR1002314A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/52—Toroidal combustion chambers
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
    • F04D25/045—Units comprising pumps and their driving means the pump being fluid-driven the pump wheel carrying the fluid driving means, e.g. turbine blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/42—Casings; Connections of working fluid for radial or helico-centrifugal pumps
    • F04D29/44—Fluid-guiding means, e.g. diffusers
    • F04D29/441—Fluid-guiding means, e.g. diffusers especially adapted for elastic fluid pumps

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)
  • Supercharger (AREA)
FR1002314D 1946-09-06 1946-09-06 Turbo-engine Expired FR1002314A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1002314T 1946-09-06

Publications (1)

Publication Number Publication Date
FR1002314A true FR1002314A (en) 1952-03-05

Family

ID=9562046

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1002314D Expired FR1002314A (en) 1946-09-06 1946-09-06 Turbo-engine

Country Status (3)

Country Link
US (1) US2658338A (en)
FR (1) FR1002314A (en)
GB (1) GB629819A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5094069A (en) * 1989-06-10 1992-03-10 Mtu Motoren Und Turbinen Union Muenchen Gmbh Gas turbine engine having a mixed flow compressor
US7127897B2 (en) 2003-01-31 2006-10-31 Alstom Technology Ltd. Combustion chamber
CN105508081A (en) * 2015-12-29 2016-04-20 西北工业大学 Coaxial turbo-shaft engine

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2759662A (en) * 1950-04-26 1956-08-21 Carrier Corp Centrifugal compressors
US2801519A (en) * 1951-02-17 1957-08-06 Garrett Corp Gas turbine motor scroll structure
US2855754A (en) * 1953-12-31 1958-10-14 Hugo V Giannottl Gas turbine with combustion chamber of the toroidal flow type and integral regenerator
US3150823A (en) * 1962-02-12 1964-09-29 Ass Elect Ind Diffusers
US3365892A (en) * 1965-08-10 1968-01-30 Derderian George Turbomachine
US3604818A (en) * 1969-12-10 1971-09-14 Avco Corp Centrifugal compressor diffuser
US3709629A (en) * 1970-05-26 1973-01-09 E Traut Integrated flow gas turbine
US4151709A (en) * 1975-09-19 1979-05-01 Avco Corporation Gas turbine engines with toroidal combustors
US4375937A (en) * 1981-01-28 1983-03-08 Ingersoll-Rand Company Roto-dynamic pump with a backflow recirculator
US4375938A (en) * 1981-03-16 1983-03-08 Ingersoll-Rand Company Roto-dynamic pump with a diffusion back flow recirculator
US4502837A (en) * 1982-09-30 1985-03-05 General Electric Company Multi stage centrifugal impeller
US4487548A (en) * 1983-05-19 1984-12-11 Chandler Evans Inc. Centrifugal main fuel pump having starting element
FR2588612B1 (en) * 1985-10-16 1989-09-08 Onera (Off Nat Aerospatiale) IMPROVEMENTS TO TURBOCHARGERS.
US5101620A (en) * 1988-12-28 1992-04-07 Sundstrand Corporation Annular combustor for a turbine engine without film cooling
JP4295611B2 (en) 2001-06-15 2009-07-15 コンセプツ・イーティーアイ・インコーポレーテッド Flow stabilizer
US6796130B2 (en) * 2002-11-07 2004-09-28 Siemens Westinghouse Power Corporation Integrated combustor and nozzle for a gas turbine combustion system
US7025557B2 (en) * 2004-01-14 2006-04-11 Concepts Eti, Inc. Secondary flow control system
EP1828683B1 (en) * 2004-12-01 2013-04-10 United Technologies Corporation Combustor for turbine engine
US9970452B2 (en) * 2015-02-17 2018-05-15 Honeywell International Inc. Forward-swept impellers and gas turbine engines employing the same
US10465907B2 (en) * 2015-09-09 2019-11-05 General Electric Company System and method having annular flow path architecture
EP4015830A1 (en) * 2020-12-18 2022-06-22 Siemens Energy Global GmbH & Co. KG Radial turbomachine

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE441683C (en) * 1922-01-14 1927-03-08 Lorenzen G M B H C Method for operating gas turbines
US1926225A (en) * 1930-09-12 1933-09-12 Birmann Rudolph Turbo compressor
US1959703A (en) * 1932-01-26 1934-05-22 Birmann Rudolph Blading for centrifugal impellers or turbines
US2080425A (en) * 1933-02-10 1937-05-18 Milo Ab Turbine
US2114285A (en) * 1936-11-28 1938-04-19 Adolph L Berger Diffuser for centrifugal compressors
US2151002A (en) * 1937-08-14 1939-03-21 Lewis Gompers Pipe for smoking tobacco
US2256198A (en) * 1938-05-27 1941-09-16 Ernst Heinkel Aircraft power plant
US2272676A (en) * 1938-12-23 1942-02-10 Leduc Rene Continuous flow gas turbine
US2489692A (en) * 1942-04-07 1949-11-29 Power Jets Res Dev Ltd Compressor
US2408743A (en) * 1942-05-18 1946-10-08 Elliott Albert George Jet-propulsion apparatus for aircraft
US2556161A (en) * 1944-03-21 1951-06-12 Power Jets Res & Dev Ltd Gas diffusers for air supplied to combustion chambers
CH243902A (en) * 1944-10-02 1946-08-15 Sulzer Ag Centrifugal compressor with conical-helical flow course.
US2595505A (en) * 1946-04-20 1952-05-06 Continental Aviat & Engineerin Coaxial combustion products generator, turbine, and compressor

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5094069A (en) * 1989-06-10 1992-03-10 Mtu Motoren Und Turbinen Union Muenchen Gmbh Gas turbine engine having a mixed flow compressor
US7127897B2 (en) 2003-01-31 2006-10-31 Alstom Technology Ltd. Combustion chamber
US7237385B2 (en) 2003-01-31 2007-07-03 Alstom Technology Ltd. Method of using a combustion chamber for a gas turbine
US7318317B2 (en) 2003-01-31 2008-01-15 Alstom Technology Ltd. Combustion chamber for a gas turbine
DE102004003816B4 (en) * 2003-01-31 2015-07-02 Alstom Technology Ltd. Combustion chamber for a gas turbine
CN105508081A (en) * 2015-12-29 2016-04-20 西北工业大学 Coaxial turbo-shaft engine

Also Published As

Publication number Publication date
GB629819A (en) 1949-09-28
US2658338A (en) 1953-11-10

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