FR1135017A - Perfectionnement aux chambres de combustion de machines à combustion interne à flux continu - Google Patents

Perfectionnement aux chambres de combustion de machines à combustion interne à flux continu

Info

Publication number
FR1135017A
FR1135017A FR1135017DA FR1135017A FR 1135017 A FR1135017 A FR 1135017A FR 1135017D A FR1135017D A FR 1135017DA FR 1135017 A FR1135017 A FR 1135017A
Authority
FR
France
Prior art keywords
improvement
continuous flow
machines
internal combustion
flow internal
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
English (en)
Inventor
Hans Hering
Lothar Menz
Edouard Caffier
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 FR1135017A publication Critical patent/FR1135017A/fr
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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Measuring Fluid Pressure (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1135017D 1955-10-28 1955-10-28 Perfectionnement aux chambres de combustion de machines à combustion interne à flux continu Expired FR1135017A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1135017T 1955-10-28

Publications (1)

Publication Number Publication Date
FR1135017A true FR1135017A (fr) 1957-04-23

Family

ID=9639615

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1135017D Expired FR1135017A (fr) 1955-10-28 1955-10-28 Perfectionnement aux chambres de combustion de machines à combustion interne à flux continu

Country Status (4)

Country Link
US (1) US3082603A (fr)
BE (1) BE551418A (fr)
FR (1) FR1135017A (fr)
GB (1) GB812201A (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2406075A1 (fr) * 1977-10-11 1979-05-11 Snecma Appareil de combustion et son procede de realisation
EP2500655A1 (fr) * 2009-11-10 2012-09-19 Mitsubishi Heavy Industries, Ltd. Chambre de combustion de turbine à gaz et turbine à gaz

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS548890B1 (fr) * 1971-04-01 1979-04-19
US4265615A (en) * 1978-12-11 1981-05-05 United Technologies Corporation Fuel injection system for low emission burners
US5323605A (en) * 1990-10-01 1994-06-28 General Electric Company Double dome arched combustor
JPH094825A (ja) * 1995-06-21 1997-01-10 Mitsubishi Heavy Ind Ltd 燃焼器
DE19649486A1 (de) * 1996-11-29 1998-06-04 Abb Research Ltd Brennkammer
US6021570A (en) * 1997-11-20 2000-02-08 Caterpillar Inc. Annular one piece combustor liner
US6729141B2 (en) * 2002-07-03 2004-05-04 Elliot Energy Systems, Inc. Microturbine with auxiliary air tubes for NOx emission reduction
GB2441342B (en) * 2006-09-01 2009-03-18 Rolls Royce Plc Wall elements with apertures for gas turbine engine components
US8707708B2 (en) 2010-02-22 2014-04-29 United Technologies Corporation 3D non-axisymmetric combustor liner
EP2420730B1 (fr) * 2010-08-16 2018-03-07 Ansaldo Energia IP UK Limited Brûleur de post-combustion
US11747019B1 (en) * 2022-09-02 2023-09-05 General Electric Company Aerodynamic combustor liner design for emissions reductions

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR962581A (fr) * 1950-06-16
US945967A (en) * 1909-07-14 1910-01-11 Julius A Mahr Oil-burner.
US2546432A (en) * 1944-03-20 1951-03-27 Power Jets Res & Dev Ltd Apparatus for deflecting a fuel jet towards a region of turbulence in a propulsive gaseous stream
BE466639A (fr) * 1944-12-13
BE485523A (fr) * 1947-11-03
US2644512A (en) * 1949-06-13 1953-07-07 Heizmotoren Ges Uberlingen Am Burner device having heat exchange and gas flow control means for maintaining pyrophoric ignition therein
GB687667A (en) * 1950-04-03 1953-02-18 Bristol Aeroplane Co Ltd Improvements in or relating to combustion systems
US2828609A (en) * 1950-04-03 1958-04-01 Bristol Aero Engines Ltd Combustion chambers including suddenly enlarged chamber portions
US2825202A (en) * 1950-06-19 1958-03-04 Snecma Pipes traversed by pulsating flow gases
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
GB726491A (en) * 1952-07-16 1955-03-16 Onera (Off Nat Aerospatiale) Improvements in internal combustion engines through which a continuous gaseous stream is flowing and in particular in turbo-jet and turbo-prop engines
US2907171A (en) * 1954-02-15 1959-10-06 Lysholm Alf Combustion chamber inlet for thermal power plants
FR998079A (fr) * 1958-08-22 1952-01-14 Snecma Dispositif pour l'entrée de l'air dans la zone primaire d'une chambre de combustion de turbo-machine

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2406075A1 (fr) * 1977-10-11 1979-05-11 Snecma Appareil de combustion et son procede de realisation
EP2500655A1 (fr) * 2009-11-10 2012-09-19 Mitsubishi Heavy Industries, Ltd. Chambre de combustion de turbine à gaz et turbine à gaz
EP2500655A4 (fr) * 2009-11-10 2014-12-03 Mitsubishi Heavy Ind Ltd Chambre de combustion de turbine à gaz et turbine à gaz
US8950190B2 (en) 2009-11-10 2015-02-10 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor having contraction member on inner wall surface

Also Published As

Publication number Publication date
GB812201A (en) 1959-04-22
US3082603A (en) 1963-03-26
BE551418A (fr)

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