FR980201A - Combustion engine - Google Patents

Combustion engine

Info

Publication number
FR980201A
FR980201A FR980201DA FR980201A FR 980201 A FR980201 A FR 980201A FR 980201D A FR980201D A FR 980201DA FR 980201 A FR980201 A FR 980201A
Authority
FR
France
Prior art keywords
combustion engine
combustion
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
Marcel-Francois Guillon
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
Priority to FR980201T priority Critical
Application granted granted Critical
Publication of FR980201A publication Critical patent/FR980201A/en
Application status is Expired legal-status Critical

Links

Classifications

    • 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
    • F01D5/34Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • 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
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16Gas-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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/56Combustion chambers having rotary flame tubes
    • 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
    • Y02T50/67Relevant aircraft propulsion technologies
    • Y02T50/671Measures to reduce the propulsor weight
FR980201D 1949-02-07 1949-02-07 Combustion engine Expired FR980201A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR980201T 1949-02-07

Publications (1)

Publication Number Publication Date
FR980201A true FR980201A (en) 1951-05-09

Family

ID=9523139

Family Applications (1)

Application Number Title Priority Date Filing Date
FR980201D Expired FR980201A (en) 1949-02-07 1949-02-07 Combustion engine

Country Status (1)

Country Link
FR (1) FR980201A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1286331B (en) * 1964-10-23 1969-01-02 Rolls Royce Gas turbine engine
DE1291555B (en) * 1964-03-06 1969-03-27 Rolls Royce LPG producers
FR2389772A1 (en) * 1977-05-05 1978-12-01 Mordellet Roger Jet engine for subsonic aircraft - has hollow rotor with internal blades to produce secondary stream of air within annular primary stream
FR2446384A1 (en) * 1979-01-15 1980-08-08 Simon Jean Turbomachinery
EP1285714A1 (en) * 2001-08-23 2003-02-26 Snecma Moteurs Turbine rotor disc and manufacturing method thereof
FR2842246A1 (en) * 2002-07-15 2004-01-16 Remy Eric Patrick Mercier Centrifugal heat engine has chamber divided by concentric separator into two compartments that are sub-divided into sectors
NL1030744C2 (en) * 2005-12-22 2007-06-25 Micro Turbine Technology B V Reaction Turbine.

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1291555B (en) * 1964-03-06 1969-03-27 Rolls Royce LPG producers
DE1286331B (en) * 1964-10-23 1969-01-02 Rolls Royce Gas turbine engine
FR2389772A1 (en) * 1977-05-05 1978-12-01 Mordellet Roger Jet engine for subsonic aircraft - has hollow rotor with internal blades to produce secondary stream of air within annular primary stream
FR2446384A1 (en) * 1979-01-15 1980-08-08 Simon Jean Turbomachinery
EP1285714A1 (en) * 2001-08-23 2003-02-26 Snecma Moteurs Turbine rotor disc and manufacturing method thereof
FR2828824A1 (en) * 2001-08-23 2003-02-28 Snecma Moteurs Method for manufacturing a rotor block block disk and corresponding disc
US6905312B2 (en) 2001-08-23 2005-06-14 Snecma-Moteurs Method of manufacturing an integral rotor blade disk and corresponding disk
FR2842246A1 (en) * 2002-07-15 2004-01-16 Remy Eric Patrick Mercier Centrifugal heat engine has chamber divided by concentric separator into two compartments that are sub-divided into sectors
NL1030744C2 (en) * 2005-12-22 2007-06-25 Micro Turbine Technology B V Reaction Turbine.

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