CH310034A - Dispositif de combustion pour installation de turbine à gaz. - Google Patents

Dispositif de combustion pour installation de turbine à gaz.

Info

Publication number
CH310034A
CH310034A CH310034DA CH310034A CH 310034 A CH310034 A CH 310034A CH 310034D A CH310034D A CH 310034DA CH 310034 A CH310034 A CH 310034A
Authority
CH
Switzerland
Prior art keywords
gas turbine
combustion device
turbine installation
installation
combustion
Prior art date
Application number
Other languages
English (en)
Inventor
Guerin Meschino Ronald
Original Assignee
Canadian Patents Dev
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 Canadian Patents Dev filed Critical Canadian Patents Dev
Publication of CH310034A publication Critical patent/CH310034A/fr

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
    • F23R3/42—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
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
    • 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
    • F02C7/264—Ignition
    • F02C7/266—Electric

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH310034D 1950-03-06 1951-03-06 Dispositif de combustion pour installation de turbine à gaz. CH310034A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB310034X 1950-03-06

Publications (1)

Publication Number Publication Date
CH310034A true CH310034A (fr) 1955-09-30

Family

ID=10316462

Family Applications (1)

Application Number Title Priority Date Filing Date
CH310034D CH310034A (fr) 1950-03-06 1951-03-06 Dispositif de combustion pour installation de turbine à gaz.

Country Status (4)

Country Link
CH (1) CH310034A (fr)
DE (1) DE882775C (fr)
FR (1) FR1033404A (fr)
GB (1) GB691366A (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2952126A (en) * 1955-05-10 1960-09-13 Midland Ross Corp Combustion unit for supplying hot gas for jet aircraft

Also Published As

Publication number Publication date
GB691366A (en) 1953-05-13
DE882775C (de) 1953-07-13
FR1033404A (fr) 1953-07-10

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