FR63025E - Improved combustion apparatus, burners or similar apparatus, in particular for supplying gas turbines - Google Patents

Improved combustion apparatus, burners or similar apparatus, in particular for supplying gas turbines

Info

Publication number
FR63025E
FR63025E FR63025DA FR63025E FR 63025 E FR63025 E FR 63025E FR 63025D A FR63025D A FR 63025DA FR 63025 E FR63025 E FR 63025E
Authority
FR
France
Prior art keywords
burners
supplying gas
gas turbines
improved combustion
similar
Prior art date
Legal status (The legal status 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 status listed.)
Expired
Application number
Other languages
French (fr)
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Compagnie Francaise Thomson Houston SA
Original Assignee
Compagnie Francaise Thomson Houston SA
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 Compagnie Francaise Thomson Houston SA filed Critical Compagnie Francaise Thomson Houston SA
Application granted granted Critical
Publication of FR63025E publication Critical patent/FR63025E/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • F23R3/08Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR63025D 1951-09-28 1951-09-28 Improved combustion apparatus, burners or similar apparatus, in particular for supplying gas turbines Expired FR63025E (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR63025T 1951-09-28

Publications (1)

Publication Number Publication Date
FR63025E true FR63025E (en) 1955-07-13

Family

ID=8696344

Family Applications (1)

Application Number Title Priority Date Filing Date
FR63025D Expired FR63025E (en) 1951-09-28 1951-09-28 Improved combustion apparatus, burners or similar apparatus, in particular for supplying gas turbines

Country Status (1)

Country Link
FR (1) FR63025E (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0049190A1 (en) * 1980-09-25 1982-04-07 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Air film cooling device for the flame tube of a gas turbine engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0049190A1 (en) * 1980-09-25 1982-04-07 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Air film cooling device for the flame tube of a gas turbine engine

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