FR2446384B1 - - Google Patents

Info

Publication number
FR2446384B1
FR2446384B1 FR7900836A FR7900836A FR2446384B1 FR 2446384 B1 FR2446384 B1 FR 2446384B1 FR 7900836 A FR7900836 A FR 7900836A FR 7900836 A FR7900836 A FR 7900836A FR 2446384 B1 FR2446384 B1 FR 2446384B1
Authority
FR
France
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
FR7900836A
Other languages
French (fr)
Other versions
FR2446384A1 (en
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 to FR7900836A priority Critical patent/FR2446384A1/en
Priority to GB8000515A priority patent/GB2040359B/en
Priority to DE19803000614 priority patent/DE3000614A1/en
Priority to JP300080A priority patent/JPS55117035A/en
Publication of FR2446384A1 publication Critical patent/FR2446384A1/en
Application granted granted Critical
Publication of FR2446384B1 publication Critical patent/FR2446384B1/fr
Granted legal-status Critical Current

Links

Classifications

    • 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
    • F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors
    • 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
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
    • F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
    • 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
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • 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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
FR7900836A 1979-01-15 1979-01-15 TURBOMACHINE Granted FR2446384A1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7900836A FR2446384A1 (en) 1979-01-15 1979-01-15 TURBOMACHINE
GB8000515A GB2040359B (en) 1979-01-15 1980-01-08 Turbo machine
DE19803000614 DE3000614A1 (en) 1979-01-15 1980-01-09 TURBO MACHINE
JP300080A JPS55117035A (en) 1979-01-15 1980-01-14 Turboomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7900836A FR2446384A1 (en) 1979-01-15 1979-01-15 TURBOMACHINE

Publications (2)

Publication Number Publication Date
FR2446384A1 FR2446384A1 (en) 1980-08-08
FR2446384B1 true FR2446384B1 (en) 1982-06-25

Family

ID=9220728

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7900836A Granted FR2446384A1 (en) 1979-01-15 1979-01-15 TURBOMACHINE

Country Status (4)

Country Link
JP (1) JPS55117035A (en)
DE (1) DE3000614A1 (en)
FR (1) FR2446384A1 (en)
GB (1) GB2040359B (en)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0383862A1 (en) * 1988-08-01 1990-08-29 TOBLER, Max Rotary combustion chamber with water injection and water cooling for a turbine
DE4232383A1 (en) * 1992-09-26 1994-03-31 Asea Brown Boveri Gas turbine group
GB2349671A (en) * 1999-04-26 2000-11-08 Andrew David James Sampson Gas turbine having rotating mixing chambers and helical flow
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.
CN113279857B (en) * 2021-05-27 2022-03-15 中国科学院工程热物理研究所 High thrust-weight ratio gas turbine generator suitable for unmanned aerial vehicle

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2704645A (en) * 1955-03-22 colvin
GB598774A (en) * 1945-09-10 1948-02-26 Wolfgang Bial Improvements in or relating to internal combustion jet and power units
FR383966A (en) * 1907-09-26 1908-03-25 Armand Ferrier Internal combustion turbine
FR980201A (en) * 1949-02-07 1951-05-09 Combustion engine
DE821736C (en) * 1950-02-04 1951-11-19 Hardy Radermacher Jet engine
US2748563A (en) * 1953-08-21 1956-06-05 Wiktor Dominik Single burner turbojet engine
US3015524A (en) * 1958-11-19 1962-01-02 Owens Corning Fiberglass Corp Inverted turbine
FR1466403A (en) * 1965-11-24 1967-01-20 Device and method for increasing the efficiency of the reactor
FR1594147A (en) * 1968-12-05 1970-06-01
DE2116654A1 (en) * 1971-04-06 1972-11-02 Kuske, Albrecht, Prof. Dr.-Ing., 3392 Clausthal-Zellerfeld Gas turbine
DE2122782A1 (en) * 1971-05-08 1972-11-16 Unbehaun, Dieter, 8500 Nürnberg Gas turbine with rotating combustion chamber
DE2419972A1 (en) * 1974-04-25 1975-11-06 Lothar Strach Gas turbine blade arrangement achieving high input temperature - blades fitted on idler wheel and inside runner

Also Published As

Publication number Publication date
FR2446384A1 (en) 1980-08-08
JPS55117035A (en) 1980-09-09
GB2040359A (en) 1980-08-28
GB2040359B (en) 1982-12-08
DE3000614A1 (en) 1980-07-17

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Legal Events

Date Code Title Description
ST Notification of lapse