FR1044704A - Turbine à écoulement axial - Google Patents

Turbine à écoulement axial

Info

Publication number
FR1044704A
FR1044704A FR1044704DA FR1044704A FR 1044704 A FR1044704 A FR 1044704A FR 1044704D A FR1044704D A FR 1044704DA FR 1044704 A FR1044704 A FR 1044704A
Authority
FR
France
Prior art keywords
axial flow
flow turbine
turbine
axial
flow
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)
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.)
MAN AG
Original Assignee
MAN Maschinenfabrik Augsburg Nuernberg AG
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 MAN Maschinenfabrik Augsburg Nuernberg AG filed Critical MAN Maschinenfabrik Augsburg Nuernberg AG
Application granted granted Critical
Publication of FR1044704A publication Critical patent/FR1044704A/fr
Expired 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
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1044704D 1950-05-09 1951-05-08 Turbine à écoulement axial Expired FR1044704A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE304143X 1950-05-09

Publications (1)

Publication Number Publication Date
FR1044704A true FR1044704A (fr) 1953-11-20

Family

ID=6115870

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1044704D Expired FR1044704A (fr) 1950-05-09 1951-05-08 Turbine à écoulement axial

Country Status (3)

Country Link
US (1) US2806355A (fr)
CH (1) CH304143A (fr)
FR (1) FR1044704A (fr)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3135496A (en) * 1962-03-02 1964-06-02 Gen Electric Axial flow turbine with radial temperature gradient
DE1269418B (de) * 1964-08-21 1968-05-30 Gen Motors Corp Gasturbine
US3490747A (en) * 1967-11-29 1970-01-20 Westinghouse Electric Corp Temperature profiling means for turbine inlet
US3652181A (en) * 1970-11-23 1972-03-28 Carl F Wilhelm Jr Cooling sleeve for gas turbine combustor transition member
GB1519590A (en) * 1974-11-11 1978-08-02 Rolls Royce Gas turbine engine
US4083649A (en) * 1976-05-05 1978-04-11 Carrier Corporation Cooling system for turbomachinery
US4195474A (en) * 1977-10-17 1980-04-01 General Electric Company Liquid-cooled transition member to turbine inlet
US4321006A (en) * 1980-03-05 1982-03-23 Von Ohain Hans J P Gas compression cycle and apparatus therefor

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1368751A (en) * 1918-11-29 1921-02-15 Auguste C E Rateau Means for cooling turbine-rotors
US1708402A (en) * 1926-09-04 1929-04-09 Holzwarth Gas Turbine Co Turbine blade
FR781057A (fr) * 1934-01-29 1935-05-08 Cem Comp Electro Mec Procédé et dispositif pour protéger contre les hautes températures les organes de turbo-machines plongés dans un fluide chaud en mouvement, en particulier les aubes de turbines à gaz ou à vapeur
CH210655A (de) * 1938-09-16 1940-07-31 Sulzer Ag Axial arbeitende Brennkraftturbine.
US2326072A (en) * 1939-06-28 1943-08-03 Bbc Brown Boveri & Cie Gas turbine plant
BE461929A (fr) * 1939-12-19
USRE23172E (en) * 1940-09-21 1949-11-29 Bochi
GB589541A (en) * 1941-09-22 1947-06-24 Hayne Constant Improvements in axial flow turbines, compressors and the like
FR973663A (fr) * 1941-10-30 1951-02-13 Rateau Soc Dispositif de refroidissement des enveloppes de moteurs thermiques à turbines à gaz
US2435042A (en) * 1942-11-09 1948-01-27 Goetaverken Ab Plural fluid turbine combining impulse and reaction blading
US2563269A (en) * 1943-05-22 1951-08-07 Lockheed Aircraft Corp Gas turbine
US2501633A (en) * 1943-06-28 1950-03-21 Lockheed Aircraft Corp Gas turbine aircraft power plant having ducted propulsive compressor means
FR957575A (fr) * 1946-10-02 1950-02-23
US2628066A (en) * 1946-10-02 1953-02-10 Rolls Royce Turbine disk
US2483616A (en) * 1947-05-22 1949-10-04 Svenska Flygmotor Aktiebolaget Rotor for multistage turbines or similar machines

Also Published As

Publication number Publication date
US2806355A (en) 1957-09-17
CH304143A (de) 1954-12-31

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