CH304143A - Method for operating a gas turbine plant and device for carrying out the method. - Google Patents

Method for operating a gas turbine plant and device for carrying out the method.

Info

Publication number
CH304143A
CH304143A CH304143DA CH304143A CH 304143 A CH304143 A CH 304143A CH 304143D A CH304143D A CH 304143DA CH 304143 A CH304143 A CH 304143A
Authority
CH
Switzerland
Prior art keywords
carrying
operating
gas turbine
turbine plant
plant
Prior art date
Application number
Other languages
German (de)
Inventor
Ag Maschine Augsburg-Nuernberg
Original Assignee
Maschf 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 Maschf Augsburg Nuernberg Ag filed Critical Maschf Augsburg Nuernberg Ag
Publication of CH304143A publication Critical patent/CH304143A/en

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)
CH304143D 1950-05-09 1951-04-02 Method for operating a gas turbine plant and device for carrying out the method. CH304143A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
CH304143A true CH304143A (en) 1954-12-31

Family

ID=6115870

Family Applications (1)

Application Number Title Priority Date Filing Date
CH304143D CH304143A (en) 1950-05-09 1951-04-02 Method for operating a gas turbine plant and device for carrying out the method.

Country Status (3)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1269418B (en) * 1964-08-21 1968-05-30 Gen Motors Corp Gas turbine

Families Citing this family (7)

* 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
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 (en) * 1934-01-29 1935-05-08 Cem Comp Electro Mec Method and device for protecting against high temperatures the parts of turbo-machines immersed in a hot moving fluid, in particular the blades of gas or steam turbines
CH210655A (en) * 1938-09-16 1940-07-31 Sulzer Ag Axial internal combustion turbine.
US2326072A (en) * 1939-06-28 1943-08-03 Bbc Brown Boveri & Cie Gas turbine plant
BE461929A (en) * 1939-12-19
BE442789A (en) * 1940-09-21
GB589541A (en) * 1941-09-22 1947-06-24 Hayne Constant Improvements in axial flow turbines, compressors and the like
FR973663A (en) * 1941-10-30 1951-02-13 Rateau Soc Cooling device for thermal gas turbine engine casings
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 (en) * 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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1269418B (en) * 1964-08-21 1968-05-30 Gen Motors Corp Gas turbine

Also Published As

Publication number Publication date
US2806355A (en) 1957-09-17
FR1044704A (en) 1953-11-20

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