FR1165074A - Gas turbine - Google Patents

Gas turbine

Info

Publication number
FR1165074A
FR1165074A FR1165074DA FR1165074A FR 1165074 A FR1165074 A FR 1165074A FR 1165074D A FR1165074D A FR 1165074DA FR 1165074 A FR1165074 A FR 1165074A
Authority
FR
France
Prior art keywords
gas turbine
turbine
gas
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.)
Anstalt fuer Stroemungsmaschinen GmbH
Original Assignee
Anstalt fuer Stroemungsmaschinen GmbH
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 Anstalt fuer Stroemungsmaschinen GmbH filed Critical Anstalt fuer Stroemungsmaschinen GmbH
Application granted granted Critical
Publication of FR1165074A publication Critical patent/FR1165074A/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
    • F23R3/02—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
    • F23R3/42—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)
FR1165074D 1956-10-11 1956-10-15 Gas turbine Expired FR1165074A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEA0025845 1956-10-11

Publications (1)

Publication Number Publication Date
FR1165074A true FR1165074A (en) 1958-10-17

Family

ID=6926002

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1165074D Expired FR1165074A (en) 1956-10-11 1956-10-15 Gas turbine

Country Status (1)

Country Link
FR (1) FR1165074A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008180496A (en) * 2007-01-23 2008-08-07 Snecma Gas turbine engine diffuser, combustion chamber, and gas turbine engine comprising them
EP2700879A3 (en) * 2012-08-24 2014-03-12 Alstom Technology Ltd Method for mixing a dilution air in a sequential combustion system of a gas turbine
US20150338102A1 (en) * 2013-03-12 2015-11-26 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
EP2966356A1 (en) * 2014-07-10 2016-01-13 Alstom Technology Ltd Sequential combustor arrangement with a mixer
US10208956B2 (en) 2013-03-12 2019-02-19 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US10955140B2 (en) 2013-03-12 2021-03-23 Pratt & Whitney Canada Corp. Combustor for gas turbine engine

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008180496A (en) * 2007-01-23 2008-08-07 Snecma Gas turbine engine diffuser, combustion chamber, and gas turbine engine comprising them
EP2700879A3 (en) * 2012-08-24 2014-03-12 Alstom Technology Ltd Method for mixing a dilution air in a sequential combustion system of a gas turbine
US20150338102A1 (en) * 2013-03-12 2015-11-26 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US10208956B2 (en) 2013-03-12 2019-02-19 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US10788209B2 (en) * 2013-03-12 2020-09-29 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US10955140B2 (en) 2013-03-12 2021-03-23 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
EP2966356A1 (en) * 2014-07-10 2016-01-13 Alstom Technology Ltd Sequential combustor arrangement with a mixer
US10215417B2 (en) 2014-07-10 2019-02-26 Ansaldo Energia Switzerland AG Sequential combustor arrangement with a mixer

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