FR2909163B1 - Carenage de chambre de combustion de turbomachine. - Google Patents

Carenage de chambre de combustion de turbomachine.

Info

Publication number
FR2909163B1
FR2909163B1 FR0610380A FR0610380A FR2909163B1 FR 2909163 B1 FR2909163 B1 FR 2909163B1 FR 0610380 A FR0610380 A FR 0610380A FR 0610380 A FR0610380 A FR 0610380A FR 2909163 B1 FR2909163 B1 FR 2909163B1
Authority
FR
France
Prior art keywords
combustion chamber
turbomachine combustion
fairing
chamber fairing
turbomachine
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
FR0610380A
Other languages
English (en)
Other versions
FR2909163A1 (fr
Inventor
Denis Jean Maurice Sandelis
Christophe Pieussergues
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 FR0610380A priority Critical patent/FR2909163B1/fr
Publication of FR2909163A1 publication Critical patent/FR2909163A1/fr
Application granted granted Critical
Publication of FR2909163B1 publication Critical patent/FR2909163B1/fr
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
    • F23R3/42—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
    • 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
    • F23R3/60—Support structures; Attaching or mounting means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR0610380A 2006-11-28 2006-11-28 Carenage de chambre de combustion de turbomachine. Active FR2909163B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0610380A FR2909163B1 (fr) 2006-11-28 2006-11-28 Carenage de chambre de combustion de turbomachine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0610380A FR2909163B1 (fr) 2006-11-28 2006-11-28 Carenage de chambre de combustion de turbomachine.

Publications (2)

Publication Number Publication Date
FR2909163A1 FR2909163A1 (fr) 2008-05-30
FR2909163B1 true FR2909163B1 (fr) 2011-02-25

Family

ID=38191358

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0610380A Active FR2909163B1 (fr) 2006-11-28 2006-11-28 Carenage de chambre de combustion de turbomachine.

Country Status (1)

Country Link
FR (1) FR2909163B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2527932C2 (ru) * 2009-03-17 2014-09-10 Снекма Камера сгорания турбомашины, содержащая улучшенные средства питания воздухом

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3011317B1 (fr) * 2013-10-01 2018-02-23 Safran Aircraft Engines Chambre de combustion pour turbomachine a admission d'air homogene au travers de systemes d'injection
GB2548585B (en) * 2016-03-22 2020-05-27 Rolls Royce Plc A combustion chamber assembly
DE102017100984B4 (de) 2017-01-19 2019-03-07 Karlsruher Institut für Technologie Gasturbinenbrennkammeranordnung
US10619856B2 (en) * 2017-03-13 2020-04-14 Rolls-Royce Corporation Notched gas turbine combustor cowl
RU2670858C9 (ru) * 2017-11-17 2018-11-13 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Кольцевая камера сгорания газотурбинного двигателя
US10982852B2 (en) 2018-11-05 2021-04-20 Rolls-Royce Corporation Cowl integration to combustor wall

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5289687A (en) * 1992-03-30 1994-03-01 General Electric Company One-piece cowl for a double annular combustor
FR2706021B1 (fr) * 1993-06-03 1995-07-07 Snecma Chambre de combustion comprenant un ensemble séparateur de gaz.
FR2751054B1 (fr) * 1996-07-11 1998-09-18 Snecma Chambre de combustion anti-nox a injection de carburant de type annulaire
US5970716A (en) * 1997-10-02 1999-10-26 General Electric Company Apparatus for retaining centerbody between adjacent domes of multiple annular combustor employing interference and clamping fits

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2527932C2 (ru) * 2009-03-17 2014-09-10 Снекма Камера сгорания турбомашины, содержащая улучшенные средства питания воздухом

Also Published As

Publication number Publication date
FR2909163A1 (fr) 2008-05-30

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