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FR2081220A1 - - Google Patents

Info

Publication number
FR2081220A1
FR2081220A1 FR7009794A FR7009794A FR2081220A1 FR 2081220 A1 FR2081220 A1 FR 2081220A1 FR 7009794 A FR7009794 A FR 7009794A FR 7009794 A FR7009794 A FR 7009794A FR 2081220 A1 FR2081220 A1 FR 2081220A1
Authority
FR
France
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.)
Withdrawn
Application number
FR7009794A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to FR7009794A priority Critical patent/FR2081220A1/fr
Publication of FR2081220A1 publication Critical patent/FR2081220A1/fr
Withdrawn legal-status Critical Current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
    • F23R3/02—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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR7009794A 1970-03-19 1970-03-19 Withdrawn FR2081220A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7009794A FR2081220A1 (en) 1970-03-19 1970-03-19

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7009794A FR2081220A1 (en) 1970-03-19 1970-03-19

Publications (1)

Publication Number Publication Date
FR2081220A1 true FR2081220A1 (en) 1971-12-03

Family

ID=9052502

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7009794A Withdrawn FR2081220A1 (en) 1970-03-19 1970-03-19

Country Status (1)

Country Link
FR (1) FR2081220A1 (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0584661A1 (en) * 1992-08-28 1994-03-02 Asea Brown Boveri Ag Process for producing a combustible gas flow in a heat generator and generator for carrying out the process
EP1840466A1 (en) * 2006-03-30 2007-10-03 Snecma Configuration of dilution openings in a wall of a turbomachine combustion chamber
FR2948987A1 (en) * 2009-08-04 2011-02-11 Snecma Combustion chamber for e.g. jet engine, of airplane, has inlet openings with oblong shape, so that maximum space between two points of edge of projections is greater than maximum space between two other points of edge of projections
FR2958012A1 (en) * 2010-03-23 2011-09-30 Snecma Annular combustion chamber for use between upstream high pressure compressor and downstream high pressure turbine of airplane, has rotary walls comprising orifices whose axis is inclined with respect to axis of chamber at specific angle

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0584661A1 (en) * 1992-08-28 1994-03-02 Asea Brown Boveri Ag Process for producing a combustible gas flow in a heat generator and generator for carrying out the process
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
FR2948987A1 (en) * 2009-08-04 2011-02-11 Snecma Combustion chamber for e.g. jet engine, of airplane, has inlet openings with oblong shape, so that maximum space between two points of edge of projections is greater than maximum space between two other points of edge of projections
FR2958012A1 (en) * 2010-03-23 2011-09-30 Snecma Annular combustion chamber for use between upstream high pressure compressor and downstream high pressure turbine of airplane, has rotary walls comprising orifices whose axis is inclined with respect to axis of chamber at specific angle

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Legal Events

Date Code Title Description
ST Notification of lapse