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WO2012168636A3 - Chambre de combustion annulaire de turbomachine - Google Patents

Chambre de combustion annulaire de turbomachine Download PDF

Info

Publication number
WO2012168636A3
WO2012168636A3 PCT/FR2012/051240 FR2012051240W WO2012168636A3 WO 2012168636 A3 WO2012168636 A3 WO 2012168636A3 FR 2012051240 W FR2012051240 W FR 2012051240W WO 2012168636 A3 WO2012168636 A3 WO 2012168636A3
Authority
WO
WIPO (PCT)
Prior art keywords
combustion chamber
turbomachine
annular wall
annular combustion
annular
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.)
Ceased
Application number
PCT/FR2012/051240
Other languages
English (en)
Other versions
WO2012168636A2 (fr
Inventor
Bernard CARRERE
Nicolas SAVARY
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 Helicopter Engines SAS
Original Assignee
Turbomeca SA
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 Turbomeca SA filed Critical Turbomeca SA
Priority to EP12731106.6A priority Critical patent/EP2718627B1/fr
Priority to RU2013158179/06A priority patent/RU2600829C2/ru
Priority to CN201280028205.XA priority patent/CN103597285B/zh
Priority to KR1020137034350A priority patent/KR102001690B1/ko
Priority to CA2838168A priority patent/CA2838168C/fr
Priority to JP2014514132A priority patent/JP6073299B2/ja
Priority to ES12731106.6T priority patent/ES2548697T3/es
Priority to US14/124,511 priority patent/US8925331B2/en
Priority to PL12731106T priority patent/PL2718627T3/pl
Publication of WO2012168636A2 publication Critical patent/WO2012168636A2/fr
Publication of WO2012168636A3 publication Critical patent/WO2012168636A3/fr
Anticipated expiration legal-status Critical
Ceased 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
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00017—Assembling combustion chamber liners or subparts
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T403/00—Joints and connections
    • Y10T403/70—Interfitted members
    • Y10T403/7005—Lugged member, rotary engagement

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)

Abstract

Chambre de combustion annulaire (10) de turbomachine présentant une direction axiale (X), une direction radiale (R) et une direction azimutale (Y), comprenant une première paroi annulaire (12) et une deuxième paroi annulaire (14), chaque paroi annulaire délimitant au moins une partie de l'enceinte de la chambre de combustion (10). La première paroi annulaire (12) et la deuxième paroi annulaire (14) présentent des moyens complémentaires d'assemblage (12b, 14b) qui coopèrent par emboîtement azimutal.
PCT/FR2012/051240 2011-06-08 2012-06-04 Chambre de combustion annulaire de turbomachine Ceased WO2012168636A2 (fr)

Priority Applications (9)

Application Number Priority Date Filing Date Title
EP12731106.6A EP2718627B1 (fr) 2011-06-08 2012-06-04 Chambre de combustion annulaire de turbomachine
RU2013158179/06A RU2600829C2 (ru) 2011-06-08 2012-06-04 Кольцевая камера сгорания для турбомашины
CN201280028205.XA CN103597285B (zh) 2011-06-08 2012-06-04 涡轮机的环形燃烧室
KR1020137034350A KR102001690B1 (ko) 2011-06-08 2012-06-04 터보머신을 위한 환형 연소실
CA2838168A CA2838168C (fr) 2011-06-08 2012-06-04 Chambre de combustion annulaire de turbomachine
JP2014514132A JP6073299B2 (ja) 2011-06-08 2012-06-04 ターボ機械用の環状燃焼室
ES12731106.6T ES2548697T3 (es) 2011-06-08 2012-06-04 Cámara de combustión anular de turbomáquina
US14/124,511 US8925331B2 (en) 2011-06-08 2012-06-04 Annular combustion chamber of a turbomachine
PL12731106T PL2718627T3 (pl) 2011-06-08 2012-06-04 Pierścieniowa komora spalania maszyny wirowej

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1154984A FR2976346B1 (fr) 2011-06-08 2011-06-08 Chambre de combustion annulaire de turbomachine
FR1154984 2011-06-08

Publications (2)

Publication Number Publication Date
WO2012168636A2 WO2012168636A2 (fr) 2012-12-13
WO2012168636A3 true WO2012168636A3 (fr) 2013-03-28

Family

ID=46420420

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2012/051240 Ceased WO2012168636A2 (fr) 2011-06-08 2012-06-04 Chambre de combustion annulaire de turbomachine

Country Status (11)

Country Link
US (1) US8925331B2 (fr)
EP (1) EP2718627B1 (fr)
JP (1) JP6073299B2 (fr)
KR (1) KR102001690B1 (fr)
CN (1) CN103597285B (fr)
CA (1) CA2838168C (fr)
ES (1) ES2548697T3 (fr)
FR (1) FR2976346B1 (fr)
PL (1) PL2718627T3 (fr)
RU (1) RU2600829C2 (fr)
WO (1) WO2012168636A2 (fr)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2484064B (en) * 2010-08-26 2016-01-06 Rotite Ltd Connector and method of connecting two items together
FR3017693B1 (fr) * 2014-02-19 2019-07-26 Safran Helicopter Engines Chambre de combustion de turbomachine
US9513011B2 (en) * 2014-06-03 2016-12-06 Siemens Energy, Inc. Gas turbine engine combustor top hat cover attachment system with lugged interlocking backing plate
FR3022613B1 (fr) * 2014-06-24 2019-04-19 Safran Helicopter Engines Bossage pour chambre de combustion.
WO2016032515A1 (fr) * 2014-08-29 2016-03-03 Siemens Energy, Inc. Agencement à baïonnette d'un élément carcasse utilisant des crochets inclinés et procédé pour fixer et retirer cet élément
UA119005C2 (uk) * 2015-04-02 2019-04-10 Бті Гумковскі Сп. З О.О. Сп. К. Пальник твердопаливного котла
RU186048U1 (ru) * 2018-10-08 2018-12-27 Публичное Акционерное Общество "Одк-Сатурн" Узел упругого соединения жаровой трубы и газосборника камеры сгорания газотурбинного двигателя
US10895170B2 (en) * 2018-10-22 2021-01-19 Raytheon Technologies Corporation Shear wave resistant flange assembly
FR3095499B1 (fr) 2019-04-23 2021-06-11 Safran Helicopter Engines Injecteur d’un melange d’air et de carburant pour une chambre de combustion d’une turbomachine
FR3119881B1 (fr) * 2021-02-18 2023-12-22 Safran Ceram Sous ensemble comportant des moyens de compensation d'une difference de dilatation

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5145276A (en) * 1989-12-27 1992-09-08 Societe Nationale Industrielle Et Aerospatiale System for coaxial assembly of two bodies of revolution
US5737913A (en) * 1996-10-18 1998-04-14 The United States Of America As Represented By The Secretary Of The Air Force Self-aligning quick release engine case assembly
US20050076643A1 (en) * 2003-10-08 2005-04-14 Honeywell International Inc. Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engine
US20070031188A1 (en) * 2005-06-23 2007-02-08 Siemens Westinghouse Power Corporation Attachment device for removable components in hot gas paths in a turbine engine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4411134A (en) * 1981-10-26 1983-10-25 Moir David L Apparatus for the repair and replacement of transition ducts on jet engines and bracket therefor
JPH087246Y2 (ja) * 1989-08-03 1996-03-04 トヨタ自動車株式会社 セラミック製燃焼器の組立構造
FR2679010B1 (fr) * 1991-07-10 1993-09-24 Snecma Chambre de combustion de turbomachine a bols de prevaporisation demontables.
US7152411B2 (en) * 2003-06-27 2006-12-26 General Electric Company Rabbet mounted combuster
RU2287115C1 (ru) * 2005-04-15 2006-11-10 Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") Кольцевая камера сгорания газотурбинного двигателя
FR2885201B1 (fr) * 2005-04-28 2010-09-17 Snecma Moteurs Chambre de combustion aisement demontable a performance aerodynamique amelioree
FR2897145B1 (fr) * 2006-02-08 2013-01-18 Snecma Chambre de combustion annulaire de turbomachine a fixations alternees.
FR2897922B1 (fr) * 2006-02-27 2008-10-10 Snecma Sa Agencement pour une chambre de combustion de turboreacteur
US7623940B2 (en) * 2006-06-02 2009-11-24 The Boeing Company Direct-manufactured duct interconnects
US7984615B2 (en) * 2007-06-27 2011-07-26 Honeywell International Inc. Combustors for use in turbine engine assemblies
US8579538B2 (en) * 2010-07-30 2013-11-12 United Technologies Corporation Turbine engine coupling stack

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5145276A (en) * 1989-12-27 1992-09-08 Societe Nationale Industrielle Et Aerospatiale System for coaxial assembly of two bodies of revolution
US5737913A (en) * 1996-10-18 1998-04-14 The United States Of America As Represented By The Secretary Of The Air Force Self-aligning quick release engine case assembly
US20050076643A1 (en) * 2003-10-08 2005-04-14 Honeywell International Inc. Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engine
US20070031188A1 (en) * 2005-06-23 2007-02-08 Siemens Westinghouse Power Corporation Attachment device for removable components in hot gas paths in a turbine engine

Also Published As

Publication number Publication date
EP2718627A2 (fr) 2014-04-16
PL2718627T3 (pl) 2015-12-31
CN103597285B (zh) 2015-09-30
KR102001690B1 (ko) 2019-07-18
EP2718627B1 (fr) 2015-08-26
RU2013158179A (ru) 2015-07-20
WO2012168636A2 (fr) 2012-12-13
JP6073299B2 (ja) 2017-02-01
RU2600829C2 (ru) 2016-10-27
ES2548697T3 (es) 2015-10-20
US8925331B2 (en) 2015-01-06
CA2838168A1 (fr) 2012-12-13
FR2976346A1 (fr) 2012-12-14
KR20140037885A (ko) 2014-03-27
US20140109595A1 (en) 2014-04-24
FR2976346B1 (fr) 2013-07-05
CN103597285A (zh) 2014-02-19
CA2838168C (fr) 2018-10-23
JP2014516152A (ja) 2014-07-07

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