CH269601A - Device for starting a gas turbine plant. - Google Patents

Device for starting a gas turbine plant.

Info

Publication number
CH269601A
CH269601A CH269601DA CH269601A CH 269601 A CH269601 A CH 269601A CH 269601D A CH269601D A CH 269601DA CH 269601 A CH269601 A CH 269601A
Authority
CH
Switzerland
Prior art keywords
starting
gas turbine
turbine plant
plant
gas
Prior art date
Application number
Other languages
German (de)
Inventor
Limited Rolls-Royce
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of CH269601A publication Critical patent/CH269601A/en

Links

Classifications

    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27—Fluid drives
    • F02C7/272—Fluid drives generated by cartridges
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • F02C7/277—Mechanical drives the starter being a separate turbine

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
CH269601D 1947-07-04 1948-07-02 Device for starting a gas turbine plant. CH269601A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB269601X 1947-07-04

Publications (1)

Publication Number Publication Date
CH269601A true CH269601A (en) 1950-07-15

Family

ID=10251889

Family Applications (1)

Application Number Title Priority Date Filing Date
CH269601D CH269601A (en) 1947-07-04 1948-07-02 Device for starting a gas turbine plant.

Country Status (3)

Country Link
CH (1) CH269601A (en)
FR (1) FR968718A (en)
GB (1) GB624345A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1374813A (en) * 1971-02-15 1974-11-20 Lucas Industries Ltd Fuel supply systems for gas turbine engines
FR2501290B1 (en) * 1981-03-06 1985-11-08 Snecma ACCELERATION LIMITER FOR TURBOMACHINE

Also Published As

Publication number Publication date
FR968718A (en) 1950-12-04
GB624345A (en) 1949-06-02

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