FR1052475A - Combustion chambers particularly suitable for gas turbines - Google Patents

Combustion chambers particularly suitable for gas turbines

Info

Publication number
FR1052475A
FR1052475A FR1052475DA FR1052475A FR 1052475 A FR1052475 A FR 1052475A FR 1052475D A FR1052475D A FR 1052475DA FR 1052475 A FR1052475 A FR 1052475A
Authority
FR
France
Prior art keywords
particularly suitable
combustion chambers
gas turbines
chambers particularly
turbines
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)
Inventor
Michel Garnier
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1052475A publication Critical patent/FR1052475A/en
Expired legal-status Critical Current

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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • 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
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1052475D 1952-03-15 1952-03-15 Combustion chambers particularly suitable for gas turbines Expired FR1052475A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1052475T 1952-03-15

Publications (1)

Publication Number Publication Date
FR1052475A true FR1052475A (en) 1954-01-25

Family

ID=9595317

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1052475D Expired FR1052475A (en) 1952-03-15 1952-03-15 Combustion chambers particularly suitable for gas turbines

Country Status (1)

Country Link
FR (1) FR1052475A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE961672C (en) * 1953-01-19 1957-04-11 Lucas Industries Ltd Annular combustion chamber for jet engines, gas turbines or the like.
DE1108516B (en) * 1956-04-03 1961-06-08 Bristol Siddeley Engines Ltd Burning device
EP1840466A1 (en) * 2006-03-30 2007-10-03 Snecma Configuration of dilution openings in a wall of a turbomachine combustion chamber
RU2626876C2 (en) * 2012-05-25 2017-08-02 Снекма Turbomachine combustion chamber shell

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE961672C (en) * 1953-01-19 1957-04-11 Lucas Industries Ltd Annular combustion chamber for jet engines, gas turbines or the like.
DE1108516B (en) * 1956-04-03 1961-06-08 Bristol Siddeley Engines Ltd Burning device
EP1840466A1 (en) * 2006-03-30 2007-10-03 Snecma Configuration of dilution openings in a wall of a turbomachine combustion chamber
FR2899315A1 (en) * 2006-03-30 2007-10-05 Snecma Sa CONFIGURING DILUTION OPENINGS IN A TURBOMACHINE COMBUSTION CHAMBER WALL
US7891194B2 (en) 2006-03-30 2011-02-22 Snecma Configuration of dilution openings in a turbomachine combustion chamber wall
RU2626876C2 (en) * 2012-05-25 2017-08-02 Снекма Turbomachine combustion chamber shell

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