FR2958372B1 - TURBOMACHINE COMBUSTION CHAMBER. - Google Patents

TURBOMACHINE COMBUSTION CHAMBER.

Info

Publication number
FR2958372B1
FR2958372B1 FR1001297A FR1001297A FR2958372B1 FR 2958372 B1 FR2958372 B1 FR 2958372B1 FR 1001297 A FR1001297 A FR 1001297A FR 1001297 A FR1001297 A FR 1001297A FR 2958372 B1 FR2958372 B1 FR 2958372B1
Authority
FR
France
Prior art keywords
combustion chamber
turbomachine combustion
turbomachine
chamber
combustion
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.)
Active
Application number
FR1001297A
Other languages
French (fr)
Other versions
FR2958372A1 (en
Inventor
Christophe Pieussergues
Denis Jean Maurice Sandelis
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
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR1001297A priority Critical patent/FR2958372B1/en
Publication of FR2958372A1 publication Critical patent/FR2958372A1/en
Application granted granted Critical
Publication of FR2958372B1 publication Critical patent/FR2958372B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
FR1001297A 2010-03-30 2010-03-30 TURBOMACHINE COMBUSTION CHAMBER. Active FR2958372B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1001297A FR2958372B1 (en) 2010-03-30 2010-03-30 TURBOMACHINE COMBUSTION CHAMBER.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1001297A FR2958372B1 (en) 2010-03-30 2010-03-30 TURBOMACHINE COMBUSTION CHAMBER.

Publications (2)

Publication Number Publication Date
FR2958372A1 FR2958372A1 (en) 2011-10-07
FR2958372B1 true FR2958372B1 (en) 2013-05-17

Family

ID=43244823

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1001297A Active FR2958372B1 (en) 2010-03-30 2010-03-30 TURBOMACHINE COMBUSTION CHAMBER.

Country Status (1)

Country Link
FR (1) FR2958372B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3080168B1 (en) * 2018-04-13 2020-03-20 Safran Aircraft Engines ASSEMBLY FOR A TURBOMACHINE COMBUSTION CHAMBER

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2089285C (en) * 1992-03-30 2002-06-25 Stephen Winthrop Falls Segmented centerbody for a double annular combustor
US6145319A (en) * 1998-07-16 2000-11-14 General Electric Company Transitional multihole combustion liner
US6266961B1 (en) * 1999-10-14 2001-07-31 General Electric Company Film cooled combustor liner and method of making the same
FR2925147B1 (en) * 2007-12-14 2012-07-13 Snecma DEVICE FOR GUIDING AN ELEMENT IN AN ORIFICE OF A TURBOMACHINE COMBUSTION CHAMBER WALL

Also Published As

Publication number Publication date
FR2958372A1 (en) 2011-10-07

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