BE535497A - - Google Patents

Info

Publication number
BE535497A
BE535497A BE535497DA BE535497A BE 535497 A BE535497 A BE 535497A BE 535497D A BE535497D A BE 535497DA BE 535497 A BE535497 A BE 535497A
Authority
BE
Belgium
Application number
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.)
Publication of BE535497A publication Critical patent/BE535497A/xx

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)
BE535497D 1954-02-26 BE535497A (enrdf_load_html_response)

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
BE535497A true BE535497A (enrdf_load_html_response)

Family

ID=26258006

Family Applications (1)

Application Number Title Priority Date Filing Date
BE535497D BE535497A (enrdf_load_html_response) 1954-02-26

Country Status (6)

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

Families Citing this family (75)

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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
DE1957147A1 (de) * 1968-11-15 1970-06-04 Rolls Royce Flammrohr fuer Verbrennungsanlagen von Gasturbinentriebwerken
US3545202A (en) * 1969-04-02 1970-12-08 United Aircraft Corp Wall structure and combustion holes for a gas turbine engine
GB1283953A (en) * 1969-06-19 1972-08-02 Rolls Royce Wall for hot fluid streams
US4174608A (en) * 1972-08-15 1979-11-20 Stal-Laval Turbin Ab Combustion chamber for a gas turbine
US4480436A (en) * 1972-12-19 1984-11-06 General Electric Company Combustion chamber construction
US4614082A (en) * 1972-12-19 1986-09-30 General Electric Company Combustion chamber construction
SE375583B (enrdf_load_html_response) * 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
CH643050A5 (de) * 1979-10-01 1984-05-15 Proizv Ob Nevsky Z Im V I Gasturbinentriebwerk mit ringbrennkammer.
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
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
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
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
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
EP0224817B1 (de) * 1985-12-02 1989-07-12 Siemens Aktiengesellschaft Hitzeschildanordnung, insbesondere für Strukturteile von Gasturbinenanlagen
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
DE59810637D1 (de) 1998-11-30 2004-02-26 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
RU2212587C2 (ru) * 2001-08-16 2003-09-20 Открытое акционерное общество "Научно-производственное объединение "Сатурн" Жаровая труба камеры сгорания газотурбинного двигателя
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
US20100229565A1 (en) * 2006-12-19 2010-09-16 Arne Boman Wall of a rocket engine
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
US8894363B2 (en) 2011-02-09 2014-11-25 Siemens Energy, Inc. Cooling module design and method for cooling components of a gas turbine system
US8959886B2 (en) * 2010-07-08 2015-02-24 Siemens Energy, Inc. Mesh cooled conduit for conveying combustion gases
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
US20180292090A1 (en) * 2015-06-30 2018-10-11 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
WO2019177598A1 (en) * 2018-03-14 2019-09-19 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
CN117917530A (zh) 2022-10-20 2024-04-23 通用电气公司 用于涡轮发动机的联接组件

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 (enrdf_load_html_response) * 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
FR1034669A (fr) * 1949-12-12 1953-07-29 Babcock & Wilcox France Perfectionnements aux appareils de combustion
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

Also Published As

Publication number Publication date
US2919549A (en) 1960-01-05
GB790293A (en) 1958-02-05
GB790292A (en) 1958-02-05
DE1052750B (de) 1959-03-12
CH331954A (de) 1958-08-15
FR1122030A (fr) 1956-08-30

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