FR2752916B1 - Chemise de protection thermique pour chambre de combustion de turboreacteur - Google Patents

Chemise de protection thermique pour chambre de combustion de turboreacteur

Info

Publication number
FR2752916B1
FR2752916B1 FR9610824A FR9610824A FR2752916B1 FR 2752916 B1 FR2752916 B1 FR 2752916B1 FR 9610824 A FR9610824 A FR 9610824A FR 9610824 A FR9610824 A FR 9610824A FR 2752916 B1 FR2752916 B1 FR 2752916B1
Authority
FR
France
Prior art keywords
turboreactor
combustion chamber
thermal protective
protective shirt
shirt
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 - Fee Related
Application number
FR9610824A
Other languages
English (en)
Other versions
FR2752916A1 (fr
Inventor
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
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
Priority to FR9610824A priority Critical patent/FR2752916B1/fr
Priority to GB9717702A priority patent/GB2317005B/en
Priority to US08/919,353 priority patent/US6029455A/en
Publication of FR2752916A1 publication Critical patent/FR2752916A1/fr
Application granted granted Critical
Publication of FR2752916B1 publication Critical patent/FR2752916B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F23R3/002—Wall structures

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR9610824A 1996-09-05 1996-09-05 Chemise de protection thermique pour chambre de combustion de turboreacteur Expired - Fee Related FR2752916B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR9610824A FR2752916B1 (fr) 1996-09-05 1996-09-05 Chemise de protection thermique pour chambre de combustion de turboreacteur
GB9717702A GB2317005B (en) 1996-09-05 1997-08-22 Gas turbine engine combustion chamber with thermal protective lining
US08/919,353 US6029455A (en) 1996-09-05 1997-08-28 Turbojet engine combustion chamber with heat protecting lining

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9610824A FR2752916B1 (fr) 1996-09-05 1996-09-05 Chemise de protection thermique pour chambre de combustion de turboreacteur

Publications (2)

Publication Number Publication Date
FR2752916A1 FR2752916A1 (fr) 1998-03-06
FR2752916B1 true FR2752916B1 (fr) 1998-10-02

Family

ID=9495456

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9610824A Expired - Fee Related FR2752916B1 (fr) 1996-09-05 1996-09-05 Chemise de protection thermique pour chambre de combustion de turboreacteur

Country Status (3)

Country Link
US (1) US6029455A (fr)
FR (1) FR2752916B1 (fr)
GB (1) GB2317005B (fr)

Families Citing this family (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2776713B1 (fr) * 1998-03-26 2000-06-02 Aerospatiale Structure de protection thermique
US6145319A (en) * 1998-07-16 2000-11-14 General Electric Company Transitional multihole combustion liner
GB2361303B (en) 2000-04-14 2004-10-20 Rolls Royce Plc Wall structure for a gas turbine engine combustor
WO2003023281A1 (fr) * 2001-09-07 2003-03-20 Alstom Technology Ltd Ensemble amortisseur concu pour reduire les pulsations d'une chambre de combustion dans une installation de turbine a gaz
DE10158548A1 (de) * 2001-11-29 2003-06-12 Rolls Royce Deutschland Brennkammerschindel für eine Gasturbine mit mehreren Kühllöchern mit unterschiedlicher Winkelausrichtung
EP1507116A1 (fr) * 2003-08-13 2005-02-16 Siemens Aktiengesellschaft Ensemble bouclier thermique pour un composant acheminant un gaz chaud, notamment pour une chambre de combustion de turbine à gaz
US7363763B2 (en) * 2003-10-23 2008-04-29 United Technologies Corporation Combustor
US7464554B2 (en) * 2004-09-09 2008-12-16 United Technologies Corporation Gas turbine combustor heat shield panel or exhaust panel including a cooling device
EP1650503A1 (fr) * 2004-10-25 2006-04-26 Siemens Aktiengesellschaft Méthode de refroidissement d'un bouclier thermique et bouclier thermique
GB2444947B (en) * 2006-12-19 2009-04-08 Rolls Royce Plc Wall elements for gas turbine engine components
US8281600B2 (en) * 2007-01-09 2012-10-09 General Electric Company Thimble, sleeve, and method for cooling a combustor assembly
FR2920525B1 (fr) * 2007-08-31 2014-06-13 Snecma Separateur pour alimentation de l'air de refroidissement d'une turbine
US8166764B2 (en) * 2008-07-21 2012-05-01 United Technologies Corporation Flow sleeve impingement cooling using a plenum ring
US8359865B2 (en) * 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
US20120180492A1 (en) * 2011-01-14 2012-07-19 General Electric Company Apparatus for vibration support in combustors and method for forming apparatus
US8973376B2 (en) * 2011-04-18 2015-03-10 Siemens Aktiengesellschaft Interface between a combustor basket and a transition of a gas turbine engine
EP2522907A1 (fr) * 2011-05-12 2012-11-14 Siemens Aktiengesellschaft Agencement de bouclier thermique
US8745988B2 (en) 2011-09-06 2014-06-10 Pratt & Whitney Canada Corp. Pin fin arrangement for heat shield of gas turbine engine
US20130074471A1 (en) * 2011-09-22 2013-03-28 General Electric Company Turbine combustor and method for temperature control and damping a portion of a combustor
DE102012204103A1 (de) * 2012-03-15 2013-09-19 Siemens Aktiengesellschaft Hitzeschildelement für einen Verdichterluftbypass um die Brennkammer
DE102012213637A1 (de) * 2012-08-02 2014-02-06 Siemens Aktiengesellschaft Brennkammerkühlung
WO2014143209A1 (fr) * 2013-03-15 2014-09-18 Rolls-Royce Corporation Chemisage de chambre de combustion de moteur à turbine à gaz
WO2014149119A2 (fr) * 2013-03-15 2014-09-25 Rolls-Royce Corporation Chemise de chambre de combustion d'une turbine à gaz
US9651258B2 (en) 2013-03-15 2017-05-16 Rolls-Royce Corporation Shell and tiled liner arrangement for a combustor
WO2015050603A2 (fr) * 2013-07-16 2015-04-09 United Technologies Corporation Bords arrondis pour des composants d'acheminement de gaz
EP2837887B1 (fr) * 2013-08-15 2019-06-12 Ansaldo Energia Switzerland AG Chambre de combustion d'une turbine à gaz avec refroidissement de doublure optimisée de chute de pression
WO2015034861A1 (fr) * 2013-09-04 2015-03-12 United Technologies Corporation Écran thermique pour cloison de chambre de combustion
US20160169515A1 (en) * 2013-09-10 2016-06-16 United Technologies Corporation Edge cooling for combustor panels
US10222064B2 (en) 2013-10-04 2019-03-05 United Technologies Corporation Heat shield panels with overlap joints for a turbine engine combustor
EP3066386B1 (fr) * 2013-11-04 2020-04-29 United Technologies Corporation Bouclier thermique de chambre de combustion de moteur à turbine doté de rails à hauteurs multiples
EP3071816B1 (fr) * 2013-11-21 2019-09-18 United Technologies Corporation Refroidissement d'une structure à parois multiples d'un moteur à turbine
WO2015116360A1 (fr) 2014-01-30 2015-08-06 United Technologies Corporation Flux de refroidissement pour un panneau principal dans une chambre de combustion de moteur à turbine à gaz
US9410702B2 (en) * 2014-02-10 2016-08-09 Honeywell International Inc. Gas turbine engine combustors with effusion and impingement cooling and methods for manufacturing the same using additive manufacturing techniques
EP2952812B1 (fr) * 2014-06-05 2018-08-08 General Electric Technology GmbH Chambre de combustion annulaire d'une turbine á gaz et segment de manchon
US20160290642A1 (en) * 2015-03-30 2016-10-06 United Technologies Corporation Combustor configurations for a gas turbine engine
CN106247399B (zh) * 2015-06-08 2020-01-31 A.S.En.安萨尔多开发能源有限责任公司 用于燃气轮机的燃烧室的具有较薄的厚度的绝热陶瓷砖瓦
DE102015225505A1 (de) * 2015-12-16 2017-06-22 Rolls-Royce Deutschland Ltd & Co Kg Wand eines mittels Kühlluft zu kühlenden Bauteils, insbesondere einer Gasturbinenbrennkammerwand
GB2545459B (en) * 2015-12-17 2020-05-06 Rolls Royce Plc A combustion chamber
US10260750B2 (en) * 2015-12-29 2019-04-16 United Technologies Corporation Combustor panels having angled rail
GB201603166D0 (en) * 2016-02-24 2016-04-06 Rolls Royce Plc A combustion chamber
GB201610122D0 (en) * 2016-06-10 2016-07-27 Rolls Royce Plc A combustion chamber
JP6650849B2 (ja) * 2016-08-25 2020-02-19 三菱日立パワーシステムズ株式会社 ガスタービン
US10935236B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10655853B2 (en) 2016-11-10 2020-05-19 United Technologies Corporation Combustor liner panel with non-linear circumferential edge for a gas turbine engine combustor
US10935235B2 (en) 2016-11-10 2021-03-02 Raytheon Technologies Corporation Non-planar combustor liner panel for a gas turbine engine combustor
US10830433B2 (en) 2016-11-10 2020-11-10 Raytheon Technologies Corporation Axial non-linear interface for combustor liner panels in a gas turbine combustor
US10739001B2 (en) 2017-02-14 2020-08-11 Raytheon Technologies Corporation Combustor liner panel shell interface for a gas turbine engine combustor
US10718521B2 (en) 2017-02-23 2020-07-21 Raytheon Technologies Corporation Combustor liner panel end rail cooling interface passage for a gas turbine engine combustor
US10677462B2 (en) 2017-02-23 2020-06-09 Raytheon Technologies Corporation Combustor liner panel end rail angled cooling interface passage for a gas turbine engine combustor
US10823411B2 (en) 2017-02-23 2020-11-03 Raytheon Technologies Corporation Combustor liner panel end rail cooling enhancement features for a gas turbine engine combustor
US10830434B2 (en) 2017-02-23 2020-11-10 Raytheon Technologies Corporation Combustor liner panel end rail with curved interface passage for a gas turbine engine combustor
US10941937B2 (en) 2017-03-20 2021-03-09 Raytheon Technologies Corporation Combustor liner with gasket for gas turbine engine
US20180299126A1 (en) * 2017-04-18 2018-10-18 United Technologies Corporation Combustor liner panel end rail
US20180306113A1 (en) * 2017-04-19 2018-10-25 United Technologies Corporation Combustor liner panel end rail matching heat transfer features
US10473331B2 (en) 2017-05-18 2019-11-12 United Technologies Corporation Combustor panel endrail interface
US10551066B2 (en) * 2017-06-15 2020-02-04 United Technologies Corporation Combustor liner panel and rail with diffused interface passage for a gas turbine engine combustor
US10663168B2 (en) 2017-08-02 2020-05-26 Raytheon Technologies Corporation End rail mate-face low pressure vortex minimization
US11248791B2 (en) 2018-02-06 2022-02-15 Raytheon Technologies Corporation Pull-plane effusion combustor panel
US11009230B2 (en) * 2018-02-06 2021-05-18 Raytheon Technologies Corporation Undercut combustor panel rail
US10830435B2 (en) 2018-02-06 2020-11-10 Raytheon Technologies Corporation Diffusing hole for rail effusion
US11022307B2 (en) 2018-02-22 2021-06-01 Raytheon Technology Corporation Gas turbine combustor heat shield panel having multi-direction hole for rail effusion cooling
US10995955B2 (en) 2018-08-01 2021-05-04 Raytheon Technologies Corporation Combustor panel
US11326518B2 (en) * 2019-02-07 2022-05-10 Raytheon Technologies Corporation Cooled component for a gas turbine engine
US11073285B2 (en) * 2019-06-21 2021-07-27 Raytheon Technologies Corporation Combustor panel configuration with skewed side walls
CN114046212B (zh) * 2021-11-30 2023-06-27 西安航天动力研究所 一种具有热变形补偿功能的复合隔热结构

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE535497A (fr) * 1954-02-26
GB1451436A (en) * 1972-11-02 1976-10-06 Lucas Industries Ltd Flame tubes
US4912922A (en) * 1972-12-19 1990-04-03 General Electric Company Combustion chamber construction
US3965066A (en) * 1974-03-15 1976-06-22 General Electric Company Combustor-turbine nozzle interconnection
US4567730A (en) * 1983-10-03 1986-02-04 General Electric Company Shielded combustor
FR2567250A1 (fr) * 1984-07-06 1986-01-10 Gen Electric Chambre de combustion pour moteur a turbine a gaz
US4622821A (en) * 1985-01-07 1986-11-18 United Technologies Corporation Combustion liner for a gas turbine engine
JPH0660740B2 (ja) * 1985-04-05 1994-08-10 工業技術院長 ガスタービンの燃焼器
DE3664374D1 (en) * 1985-12-02 1989-08-17 Siemens Ag Heat shield arrangement, especially for the structural components of a gas turbine plant
US4944151A (en) * 1988-09-26 1990-07-31 Avco Corporation Segmented combustor panel
FR2644209B1 (fr) * 1989-03-08 1991-05-03 Snecma Chemise de protection thermique pour canal chaud de turboreacteur
GB9106085D0 (en) * 1991-03-22 1991-05-08 Rolls Royce Plc Gas turbine engine combustor
DE4314160A1 (de) * 1992-05-13 1993-11-18 Siemens Ag Fügeverbindung und Verfahren zu ihrer Herstellung
US5528904A (en) * 1994-02-28 1996-06-25 Jones; Charles R. Coated hot gas duct liner
FR2723177B1 (fr) * 1994-07-27 1996-09-06 Snecma Chambre de combustion comportant une double paroi
WO1996004511A1 (fr) * 1994-08-05 1996-02-15 Yanovsky, Ilya Yakovlevich Chambre a combustion a tube a feu en ceramique
GB2298267B (en) * 1995-02-23 1999-01-13 Rolls Royce Plc An arrangement of heat resistant tiles for a gas turbine engine combustor
GB2298266A (en) * 1995-02-23 1996-08-28 Rolls Royce Plc A cooling arrangement for heat resistant tiles in a gas turbine engine combustor
US5755093A (en) * 1995-05-01 1998-05-26 United Technologies Corporation Forced air cooled gas turbine exhaust liner

Also Published As

Publication number Publication date
GB2317005A (en) 1998-03-11
US6029455A (en) 2000-02-29
FR2752916A1 (fr) 1998-03-06
GB9717702D0 (en) 1997-10-29
GB2317005B (en) 1999-12-15

Similar Documents

Publication Publication Date Title
FR2752916B1 (fr) Chemise de protection thermique pour chambre de combustion de turboreacteur
FR2644209B1 (fr) Chemise de protection thermique pour canal chaud de turboreacteur
FR2770283B1 (fr) Chambre de combustion pour turbomachine
DE69716614D1 (de) Flamenschutzzusammensetzung
FR2773051B1 (fr) Perfectionnement pour casque de protection
BR9701959A (pt) Esquema de proteção de sobrecorrente do acionador do cabeçote de jato de tinta térmica
HK1068366A1 (en) Thermal protective compositions
GB2379520B (en) Engine over temperature protection
ATA168493A (de) Thermokammer
ITUD950053A0 (it) Combinazione di componenti per piastre elettriche di riscaldamento dispositivi di accensione, sensori di temperatura o simili
DE60022364D1 (de) Wärmeschutzzusammensetzung
NO941913D0 (no) Frostsikringsanordning for varmegjenvinnere
FR2756704B1 (fr) Machine de desherbage thermique
FR2716933B1 (fr) Elément de chemise de protection thermique pour turbomachine et ses procédés de fabrication.
FR2752145B1 (fr) Effeuilleuse thermique perfectionnee
DE69941873D1 (de) Zigarrenanzünder mit PTC thermischer Absicherung
DE59509000D1 (de) Thermoschutz-Bauelement
KR960037978U (ko) 고온파이프용 보온 보호커버
ITMI942125A0 (it) Gruppo di protezione termica per interruttore automatico
UA2650S (uk) Термозахисний комбінезон
FR2727700B3 (fr) Dalle de protection des surfaces herbeuses
FR2715497B1 (fr) Buse de disjoncteur à chambre d'expansion thermique.
DE59801762D1 (de) Thermischer schutz
KR950033070U (ko) 오토바이 방한·방풍장치
ATE245613T1 (de) Thermisch schützende beschichtungszusammensetzung des ablativen typs

Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
CL Concession to grant licences
CD Change of name or company name
ST Notification of lapse

Effective date: 20090529