FR1122030A - Perfectionnements aux parois réfractaires - Google Patents

Perfectionnements aux parois réfractaires

Info

Publication number
FR1122030A
FR1122030A FR1122030DA FR1122030A FR 1122030 A FR1122030 A FR 1122030A FR 1122030D A FR1122030D A FR 1122030DA FR 1122030 A FR1122030 A FR 1122030A
Authority
FR
France
Prior art keywords
refractory walls
refractory
walls
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
Application number
Other languages
English (en)
French (fr)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of FR1122030A publication Critical patent/FR1122030A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/16—Two dimensionally sectional layer
    • Y10T428/163—Next to unitary web or sheet of equal or greater extent
    • Y10T428/164—Continuous two dimensionally sectional layer
    • Y10T428/166—Glass, ceramic, or metal sections [e.g., floor or wall tile, etc.]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gasket Seals (AREA)
FR1122030D 1954-02-26 1955-02-02 Perfectionnements aux parois réfractaires Expired FR1122030A (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB331954X 1954-02-26
GB260155X 1955-01-26

Publications (1)

Publication Number Publication Date
FR1122030A true FR1122030A (fr) 1956-08-30

Family

ID=26258006

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1122030D Expired FR1122030A (fr) 1954-02-26 1955-02-02 Perfectionnements aux parois réfractaires

Country Status (6)

Country Link
US (1) US2919549A (es)
BE (1) BE535497A (es)
CH (1) CH331954A (es)
DE (1) DE1052750B (es)
FR (1) FR1122030A (es)
GB (2) GB790293A (es)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666251A (en) * 1969-06-19 1972-05-30 Rolls Royce Wall for hot fluid streams
FR2468073A1 (fr) * 1979-10-01 1981-04-30 Proizv Obiedine Nevsky Chambre de combustion annulaire de turbomoteur

Families Citing this family (71)

* Cited by examiner, † Cited by third party
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US3082601A (en) * 1958-05-08 1963-03-26 Daimler Benz Ag Rocket combustion chamber
DE1168929B (de) * 1959-03-06 1964-04-30 Summa Kessel G M B H Und Co K Rohrfoermiges Waermetauscherelement
US3154914A (en) * 1959-12-12 1964-11-03 Bolkow Entwicklungen Kg Rocket engine construction
DE1159694B (de) * 1960-08-26 1963-12-19 United Aircraft Corp Einspritzkopf fuer eine Fluessigkeitsrakete
GB1038661A (en) * 1961-12-05 1966-08-10 Ass Elect Ind Improvements relating to metallic gas turbine combustion chambers
CH399075A (de) * 1962-07-26 1966-03-31 Bbc Brown Boveri & Cie Brennkammer, insbesondere für magnetogasdynamische Maschinen
DE1225331B (de) * 1962-07-26 1966-09-22 Bbc Brown Boveri & Cie Gekuehlte Brennkammer fuer hoechste Temperaturen
GB1055234A (en) * 1963-04-30 1967-01-18 Hitachi Ltd Ultra-high temperature combustion chambers
US3899876A (en) * 1968-11-15 1975-08-19 Secr Defence Brit Flame tube for a gas turbine combustion equipment
US3545202A (en) * 1969-04-02 1970-12-08 United Aircraft Corp Wall structure and combustion holes for a gas turbine engine
US4174608A (en) * 1972-08-15 1979-11-20 Stal-Laval Turbin Ab Combustion chamber for a gas turbine
US4614082A (en) * 1972-12-19 1986-09-30 General Electric Company Combustion chamber construction
US4480436A (en) * 1972-12-19 1984-11-06 General Electric Company Combustion chamber construction
SE375583B (es) * 1973-05-22 1975-04-21 United Turbine Ab & Co
US3910036A (en) * 1974-04-05 1975-10-07 Gen Motors Corp Igniter installation for combustor with ceramic liner
GB1550368A (en) * 1975-07-16 1979-08-15 Rolls Royce Laminated materials
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
GB1564608A (en) * 1975-12-20 1980-04-10 Rolls Royce Means for cooling a surface by the impingement of a cooling fluid
US4158949A (en) * 1977-11-25 1979-06-26 General Motors Corporation Segmented annular combustor
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
GB2049152B (en) * 1979-05-01 1983-05-18 Rolls Royce Perforate laminated material
JPS5857658B2 (ja) * 1980-04-02 1983-12-21 工業技術院長 セラミツクスによる高熱曝露壁面の熱遮断構造
US4414816A (en) * 1980-04-02 1983-11-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combustor liner construction
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
GB2087065B (en) * 1980-11-08 1984-11-07 Rolls Royce Wall structure for a combustion chamber
US4422300A (en) * 1981-12-14 1983-12-27 United Technologies Corporation Prestressed combustor liner for gas turbine engine
GB2117506B (en) * 1982-03-25 1985-06-19 Nu Way Energy Ltd Burners for gaseous fuels
US4664618A (en) * 1984-08-16 1987-05-12 American Combustion, Inc. Recuperative furnace wall
JPH0660740B2 (ja) * 1985-04-05 1994-08-10 工業技術院長 ガスタービンの燃焼器
US4642993A (en) * 1985-04-29 1987-02-17 Avco Corporation Combustor liner wall
DE3519938A1 (de) * 1985-06-04 1986-12-04 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Brennkammereinrichtung
DE3664374D1 (en) * 1985-12-02 1989-08-17 Siemens Ag Heat shield arrangement, especially for the structural components of a gas turbine plant
US4773356A (en) * 1986-07-24 1988-09-27 W B Black & Sons Limited Lining a furnace with a refractory material
US5639531A (en) * 1987-12-21 1997-06-17 United Technologies Corporation Process for making a hybrid ceramic article
US5113660A (en) * 1990-06-27 1992-05-19 The United States Of America As Represented By The Secretary Of The Air Force High temperature combustor liner
US5233798A (en) * 1991-03-06 1993-08-10 Shaw Clive A Enabling assembly
US5184455A (en) * 1991-07-09 1993-02-09 The United States Of America As Represented By The Secretary Of The Air Force Ceramic blanket augmentor liner
US5216886A (en) * 1991-08-14 1993-06-08 The United States Of America As Represented By The Secretary Of The Air Force Segmented cell wall liner for a combustion chamber
US5331816A (en) * 1992-10-13 1994-07-26 United Technologies Corporation Gas turbine engine combustor fiber reinforced glass ceramic matrix liner with embedded refractory ceramic tiles
US5333443A (en) * 1993-02-08 1994-08-02 General Electric Company Seal assembly
US5758503A (en) * 1995-05-03 1998-06-02 United Technologies Corporation Gas turbine combustor
US5605046A (en) * 1995-10-26 1997-02-25 Liang; George P. Cooled liner apparatus
TW360744B (en) * 1996-07-15 1999-06-11 Siemens Ag Equipment for fixing a covering sheet metal in the waste-gas flue of a gas turbine as well as halting
US5758504A (en) * 1996-08-05 1998-06-02 Solar Turbines Incorporated Impingement/effusion cooled combustor liner
FR2752916B1 (fr) * 1996-09-05 1998-10-02 Snecma Chemise de protection thermique pour chambre de combustion de turboreacteur
DE59706557D1 (de) * 1997-07-28 2002-04-11 Alstom Keramische Auskleidung
EP1006315B1 (de) 1998-11-30 2004-01-21 ALSTOM (Switzerland) Ltd Keramische Auskleidung für einen Brennraum
US6213714B1 (en) * 1999-06-29 2001-04-10 Allison Advanced Development Company Cooled airfoil
US6402470B1 (en) * 1999-10-05 2002-06-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
GB9926257D0 (en) * 1999-11-06 2000-01-12 Rolls Royce Plc Wall elements for gas turbine engine combustors
EP1284390A1 (de) * 2001-06-27 2003-02-19 Siemens Aktiengesellschaft Hitzeschildanordnung für eine Heissgas führende Komponente, insbesondere für Strukturteile von Gasturbinen
US6830437B2 (en) * 2002-12-13 2004-12-14 General Electric Company Assembly containing a composite article and assembly method therefor
EP1528343A1 (de) * 2003-10-27 2005-05-04 Siemens Aktiengesellschaft Keramischer Hitzeschildstein mit eingebetteten Verstärkungselementen zur Auskleidung einer Gasturbinenbrennkammerwand
DE102004044852A1 (de) * 2004-09-10 2006-03-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Heißgaskammer und Schindel für eine Heißgaskammer
GB0601413D0 (en) * 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
EP2094964A4 (en) * 2006-12-19 2013-05-01 Volvo Aero Corp MOTOR-FUSE WALL
US8435007B2 (en) * 2008-12-29 2013-05-07 Rolls-Royce Corporation Hybrid turbomachinery component for a gas turbine engine
EP2233835A1 (en) * 2009-03-23 2010-09-29 Siemens Aktiengesellschaft Combustion chamber brazed with ceramic inserts
GB0913580D0 (en) * 2009-08-05 2009-09-16 Rolls Royce Plc Combustor tile
US8959886B2 (en) * 2010-07-08 2015-02-24 Siemens Energy, Inc. Mesh cooled conduit for conveying combustion gases
US8894363B2 (en) 2011-02-09 2014-11-25 Siemens Energy, Inc. Cooling module design and method for cooling components of a gas turbine system
US9243801B2 (en) * 2012-06-07 2016-01-26 United Technologies Corporation Combustor liner with improved film cooling
GB201403404D0 (en) * 2014-02-27 2014-04-16 Rolls Royce Plc A combustion chamber wall and a method of manufacturing a combustion chamber wall
GB201501817D0 (en) * 2015-02-04 2015-03-18 Rolls Royce Plc A combustion chamber and a combustion chamber segment
EP3317584A1 (en) * 2015-06-30 2018-05-09 Siemens Energy, Inc. Hybrid component comprising a metal-reinforced ceramic matrix composite material
GB201514390D0 (en) * 2015-08-13 2015-09-30 Rolls Royce Plc A combustion chamber and a combustion chamber segment
US10577944B2 (en) * 2017-08-03 2020-03-03 General Electric Company Engine component with hollow turbulators
US11208899B2 (en) * 2018-03-14 2021-12-28 General Electric Company Cooling assembly for a turbine assembly
US10968750B2 (en) 2018-09-04 2021-04-06 General Electric Company Component for a turbine engine with a hollow pin
US11506383B2 (en) * 2020-10-09 2022-11-22 Pratt & Whitney Canada Corp Combustor liner and method of operating same

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US814949A (en) * 1903-10-27 1906-03-13 Ellis F Edgar Boiler-furnace.
US2061822A (en) * 1935-04-12 1936-11-24 Chicago Retort & Fire Brick Co Furnace wall and block unit for making the same
GB597151A (en) * 1943-03-13 1948-01-20 Claude Albert Bonvillian Improvements in apparatus for the combustion of fuel
NL69245C (es) * 1946-01-09
CH255541A (de) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Gekühlte metallische Brennkammer zur Erzeugung von Heiz- und Treibgasen.
US2564497A (en) * 1947-11-26 1951-08-14 Gen Electric Combustion chamber liner
US2544538A (en) * 1948-12-01 1951-03-06 Wright Aeronautical Corp Liner for hot gas chambers
GB680641A (en) * 1949-12-08 1952-10-08 George Jendrassik Improvements relating to gas pressure exchangers
GB700004A (en) * 1949-12-12 1953-11-25 Babcock & Wilcox Ltd Improvements in or relating to combustion apparatus
CH284190A (de) * 1950-09-04 1952-07-15 Bbc Brown Boveri & Cie Metallene Brennkammer zur Erzeugung heisser Gase, insbesondere Treibgase für Gasturbinenanlagen.
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
FR1053232A (fr) * 1952-03-31 1954-02-01 Paroi de four

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3666251A (en) * 1969-06-19 1972-05-30 Rolls Royce Wall for hot fluid streams
FR2468073A1 (fr) * 1979-10-01 1981-04-30 Proizv Obiedine Nevsky Chambre de combustion annulaire de turbomoteur

Also Published As

Publication number Publication date
BE535497A (es)
CH331954A (de) 1958-08-15
DE1052750B (de) 1959-03-12
GB790293A (en) 1958-02-05
GB790292A (en) 1958-02-05
US2919549A (en) 1960-01-05

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