CH307864A - Gas turbine plant. - Google Patents

Gas turbine plant.

Info

Publication number
CH307864A
CH307864A CH307864DA CH307864A CH 307864 A CH307864 A CH 307864A CH 307864D A CH307864D A CH 307864DA CH 307864 A CH307864 A CH 307864A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine plant
plant
gas
turbine
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 CH307864A publication Critical patent/CH307864A/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
CH307864D 1951-04-25 1952-08-26 Gas turbine plant. CH307864A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB970951A GB719301A (en) 1951-04-25 1951-04-25 Improvements relating to gas turbine engines

Publications (1)

Publication Number Publication Date
CH307864A true CH307864A (en) 1955-06-15

Family

ID=9877266

Family Applications (1)

Application Number Title Priority Date Filing Date
CH307864D CH307864A (en) 1951-04-25 1952-08-26 Gas turbine plant.

Country Status (2)

Country Link
CH (1) CH307864A (en)
GB (1) GB719301A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1074920B (en) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Method and device for regulating gas turbine combustion chambers with subdivided combustion and several pressure levels
DE1078816B (en) * 1956-01-23 1960-03-31 Snecma Fuel supply device
DE1123163B (en) * 1958-05-23 1962-02-01 Gen Electric Recoil engine with afterburners
DE1127152B (en) * 1959-09-18 1962-04-05 Bristol Siddeley Engines Ltd Air jet engine with an afterburner device in the jet pipe
DE1133185B (en) * 1959-04-21 1962-07-12 Snecma Combustion device on recoil engines, especially for post-combustion
DE1297941B (en) * 1964-07-06 1969-06-19 Nord Aviat Soc Nationale De Co Combustion chamber for turbo jet engines

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1051071B (en) * 1955-07-13 1959-02-19 Sud Aviation Combustion device for supersonic ramjet engines

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1074920B (en) * 1955-07-07 1960-02-04 Ing habil Fritz A F Schmidt Murnau Dr (Obb) Method and device for regulating gas turbine combustion chambers with subdivided combustion and several pressure levels
DE1078816B (en) * 1956-01-23 1960-03-31 Snecma Fuel supply device
DE1123163B (en) * 1958-05-23 1962-02-01 Gen Electric Recoil engine with afterburners
DE1133185B (en) * 1959-04-21 1962-07-12 Snecma Combustion device on recoil engines, especially for post-combustion
DE1127152B (en) * 1959-09-18 1962-04-05 Bristol Siddeley Engines Ltd Air jet engine with an afterburner device in the jet pipe
DE1297941B (en) * 1964-07-06 1969-06-19 Nord Aviat Soc Nationale De Co Combustion chamber for turbo jet engines

Also Published As

Publication number Publication date
GB719301A (en) 1954-12-01

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