[go: up one dir, main page]

ES2548697T3 - Cámara de combustión anular de turbomáquina - Google Patents

Cámara de combustión anular de turbomáquina Download PDF

Info

Publication number
ES2548697T3
ES2548697T3 ES12731106.6T ES12731106T ES2548697T3 ES 2548697 T3 ES2548697 T3 ES 2548697T3 ES 12731106 T ES12731106 T ES 12731106T ES 2548697 T3 ES2548697 T3 ES 2548697T3
Authority
ES
Spain
Prior art keywords
annular wall
combustion chamber
annular combustion
annular
azimuthal
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
ES12731106.6T
Other languages
English (en)
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
Application granted granted Critical
Publication of ES2548697T3 publication Critical patent/ES2548697T3/es
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
    • F23R3/60—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

Cámara de combustión anular (10, 110, 210) de turbomáquina que presenta una dirección axial (X), una dirección radial (R) y una dirección acimutal (Y), que comprende una primera pared anular (12) y una segunda pared anular (14), delimitando cada pared anular al menos una parte del recinto de la cámara de combustión anular (10, 110, 210), presentando la primera pared anular (12) y la segunda pared anular (14) unos medios complementarios de ensamble (12b, 14b) que cooperan por encaje acimutal, caracterizada por que los medios complementarios de ensamble comprenden una pluralidad de primeras lengüetas (12b), que parten acimutalmente en un primer sentido desde la primera pared anular (12), y una pluralidad de segundas lengüetas (14b), que parten acimutalmente en un segundo sentido, opuesto al primer sentido, desde la segunda pared anular (14), cooperando las primeras y segundas lengüetas (12b, 14b) por encaje acimutal

Description

imagen1
imagen2
imagen3
imagen4
imagen5
imagen6
imagen7

Claims (1)

  1. imagen1
ES12731106.6T 2011-06-08 2012-06-04 Cámara de combustión anular de turbomáquina Active ES2548697T3 (es)

Applications Claiming Priority (3)

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
PCT/FR2012/051240 WO2012168636A2 (fr) 2011-06-08 2012-06-04 Chambre de combustion annulaire de turbomachine

Publications (1)

Publication Number Publication Date
ES2548697T3 true ES2548697T3 (es) 2015-10-20

Family

ID=46420420

Family Applications (1)

Application Number Title Priority Date Filing Date
ES12731106.6T Active ES2548697T3 (es) 2011-06-08 2012-06-04 Cámara de combustión anular de turbomáquina

Country Status (11)

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

Families Citing this family (9)

* 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
WO2016032515A1 (en) * 2014-08-29 2016-03-03 Siemens Energy, Inc. Bayonet arrangement of a casing component using inclined hooks and method for attaching and removing this component
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

Family Cites Families (15)

* 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
FR2656391B1 (fr) * 1989-12-27 1992-04-03 Aerospatiale Systeme pour l'assemblage coaxial de deux pieces de revolution.
FR2679010B1 (fr) * 1991-07-10 1993-09-24 Snecma Chambre de combustion de turbomachine a bols de prevaporisation demontables.
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
US7152411B2 (en) * 2003-06-27 2006-12-26 General Electric Company Rabbet mounted combuster
US7093448B2 (en) * 2003-10-08 2006-08-22 Honeywell International, Inc. Multi-action on multi-surface seal with turbine scroll retention method in gas turbine engine
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
US7334960B2 (en) * 2005-06-23 2008-02-26 Siemens Power Generation, Inc. Attachment device for removable components in hot gas paths in a turbine engine
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

Also Published As

Publication number Publication date
WO2012168636A3 (fr) 2013-03-28
RU2013158179A (ru) 2015-07-20
CA2838168C (fr) 2018-10-23
JP6073299B2 (ja) 2017-02-01
PL2718627T3 (pl) 2015-12-31
US20140109595A1 (en) 2014-04-24
KR102001690B1 (ko) 2019-07-18
KR20140037885A (ko) 2014-03-27
EP2718627A2 (fr) 2014-04-16
RU2600829C2 (ru) 2016-10-27
WO2012168636A2 (fr) 2012-12-13
US8925331B2 (en) 2015-01-06
FR2976346A1 (fr) 2012-12-14
EP2718627B1 (fr) 2015-08-26
FR2976346B1 (fr) 2013-07-05
JP2014516152A (ja) 2014-07-07
CN103597285B (zh) 2015-09-30
CA2838168A1 (fr) 2012-12-13
CN103597285A (zh) 2014-02-19

Similar Documents

Publication Publication Date Title
ES2548697T3 (es) Cámara de combustión anular de turbomáquina
WO2015065550A3 (en) Fuel igniter assembly having heat-dissipating element and methods of using same
ES2483865T3 (es) Máquina eléctrica giratoria de turbina eólica
BR112015010702A2 (pt) suporte de tubo de evacuação de ar em uma turbomáquina
BR112016028953A8 (pt) turbomáquina e conjunto propulsivo
EP2562086A3 (en) Nacelle assembly having integrated afterbody mount case
EP2474707A3 (en) Multi-function heat shield for a gas turbine engine
ES2551262T3 (es) Dispositivo de esterilización con haces de electrones para recipientes de pared delgada y método de esterilización
EP2613021A3 (en) Stator vane spring damper
RU2012157717A (ru) Подшипник качения для авиационного турбореактивного двигателя, оборудованный средствами осевого удержания своего наружного кольца
RU2012107522A (ru) Сектор наружной обечайки для лопаточного кольца статора турбомашины летательного аппарата, включающий в себя демпфирующие вибрацию клинья
BR112015010701A2 (pt) suporte de tubo de evacuação de ar em uma turbomáquina
RU2014145861A (ru) Способ и инструмент для сборки ступени выпрямления
WO2015147938A3 (en) A cooled grommet for a combustor wall assembly
WO2015147929A3 (en) Cooling an aperture body of a combustor wall
RU2012126095A (ru) Изоляция окружного выступающего края внешнего корпуса турбомашины относительно соответствующего кольцевого сектора
RU2008149155A (ru) Устройство отбора воздуха в компрессоре газотурбинного двигателя
RU2016137127A (ru) Кольцевая камера сгорания турбомашины
EP2565398A3 (en) Shaft assembly for a gas turbine engine
JP2015083835A5 (es)
RU2016140620A (ru) Радиальная турбомашина
IN2014DN10840A (es)
RU2016125485A (ru) Устройство для центровки и направления во вращении вала газотурбинного двигателя, содержащее усовершенствованные средства удержания наружного кольца опорного подшипника
BR112016022162A2 (pt) Alojamento de suporte de mancal e aparelho de mancal de um motor de turbina a gás
BR112018000928A2 (pt) ?anel de estator, gerador elétrico, e, instalação de energia eólica?