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CH291319A - Gas turbine installation. - Google Patents

Gas turbine installation.

Info

Publication number
CH291319A
CH291319A CH291319DA CH291319A CH 291319 A CH291319 A CH 291319A CH 291319D A CH291319D A CH 291319DA CH 291319 A CH291319 A CH 291319A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine installation
installation
gas
turbine
Prior art date
Application number
Other languages
French (fr)
Inventor
Limited The Austin Mot Company
Original Assignee
Austin Motor Company Limited
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 Austin Motor Company Limited filed Critical Austin Motor Company Limited
Publication of CH291319A publication Critical patent/CH291319A/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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
CH291319D 1949-07-23 1950-07-22 Gas turbine installation. CH291319A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB291319X 1949-07-23

Publications (1)

Publication Number Publication Date
CH291319A true CH291319A (en) 1953-06-15

Family

ID=10286667

Family Applications (1)

Application Number Title Priority Date Filing Date
CH291319D CH291319A (en) 1949-07-23 1950-07-22 Gas turbine installation.

Country Status (2)

Country Link
CH (1) CH291319A (en)
DE (1) DE893594C (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE972972C (en) * 1951-09-09 1959-11-12 Brown Ag Gas turbine system for generating hot compressed air

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE337315C (en) * 1918-12-31 1921-05-28 Bbc Brown Boveri & Cie Process to prevent oscillation (pumping) of the delivery rate in centrifugal compressors

Also Published As

Publication number Publication date
DE893594C (en) 1953-10-19

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