FR939630A - Improvements to linings for combustion chambers - Google Patents

Improvements to linings for combustion chambers

Info

Publication number
FR939630A
FR939630A FR939630DA FR939630A FR 939630 A FR939630 A FR 939630A FR 939630D A FR939630D A FR 939630DA FR 939630 A FR939630 A FR 939630A
Authority
FR
France
Prior art keywords
linings
combustion chambers
chambers
combustion
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
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.)
Anglo Saxon Petroleum Co Ltd
Original Assignee
Anglo Saxon Petroleum Co Ltd
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 Anglo Saxon Petroleum Co Ltd filed Critical Anglo Saxon Petroleum Co Ltd
Application granted granted Critical
Publication of FR939630A publication Critical patent/FR939630A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/08—Cooling thereof; Tube walls
    • F23M5/085—Cooling thereof; Tube walls using air or other gas as the cooling medium
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S60/00—Power plants
    • Y10S60/909—Reaction motor or component composed of specific material
    • 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

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)
FR939630D 1946-01-09 1947-01-09 Improvements to linings for combustion chambers Expired FR939630A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB830/46A GB602149A (en) 1946-01-09 1946-01-09 Improvements in and relating to combustion chamber linings

Publications (1)

Publication Number Publication Date
FR939630A true FR939630A (en) 1948-11-19

Family

ID=9711219

Family Applications (1)

Application Number Title Priority Date Filing Date
FR939630D Expired FR939630A (en) 1946-01-09 1947-01-09 Improvements to linings for combustion chambers

Country Status (5)

Country Link
US (1) US2548485A (en)
CH (1) CH268030A (en)
FR (1) FR939630A (en)
GB (1) GB602149A (en)
NL (1) NL69245C (en)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2686655A (en) * 1949-09-02 1954-08-17 Maschf Augsburg Nuernberg Ag Joint between ceramic and metallic parts
US2658332A (en) * 1951-03-21 1953-11-10 Carborundum Co Fluid cooled, refractory, ceramic lined rocket structure
US2823103A (en) * 1952-04-02 1958-02-11 Koppers Co Inc High pressure gas producers
BE535497A (en) * 1954-02-26
GB758213A (en) * 1954-03-03 1956-10-03 Parsons & Marine Eng Turbine Improvements in and relating to cylindrical combustion chambers or furnaces
US2787457A (en) * 1954-05-14 1957-04-02 Westinghouse Electric Corp High temperature furnace
US3170289A (en) * 1962-07-05 1965-02-23 Bruce E Kramer Lightweight refractory metal structure
US3229359A (en) * 1962-07-05 1966-01-18 Bruce E Kramer Method of forming a refractory metal rocket nozzle
DE1173734B (en) * 1962-10-11 1964-07-09 Siemens Ag Combustion chamber, especially for gas turbines, with a lining made of refractory bricks
US3321922A (en) * 1964-10-29 1967-05-30 Jr William T Latto Small rocket engine
US3429973A (en) * 1965-09-02 1969-02-25 Frederick H N Carter Furnace construction
GB1320482A (en) * 1971-01-25 1973-06-13 Secr Defence Cooling of hot fluid ducts
US3797236A (en) * 1971-06-11 1974-03-19 Rolls Royce Annular combustion chamber with ceramic annular ring
US3897200A (en) * 1974-03-04 1975-07-29 Howe Baker Eng Cyclonic multi-fuel burner
FR2400681A1 (en) * 1977-08-18 1979-03-16 Nord Pas Calais Houilleres NEW OVEN WALLS USED AT HIGH TEMPERATURES
JPS5857658B2 (en) * 1980-04-02 1983-12-21 工業技術院長 Heat shielding structure for walls exposed to high heat using ceramics
US4499946A (en) * 1981-03-10 1985-02-19 Mason & Hanger-Silas Mason Co., Inc. Enhanced oil recovery process and apparatus
US4490110A (en) * 1983-05-20 1984-12-25 Jones William R Plenum arrangement
US4664618A (en) * 1984-08-16 1987-05-12 American Combustion, Inc. Recuperative furnace wall
US4637550A (en) * 1985-10-01 1987-01-20 The United States Of America As Represented By The Secretary Of The Air Force Dual material exhaust nozzle flap
US4898000A (en) * 1986-04-14 1990-02-06 Allied-Signal Inc. Emergency power unit
US5553455A (en) * 1987-12-21 1996-09-10 United Technologies Corporation 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
RU2076275C1 (en) * 1990-07-17 1997-03-27 Сименс АГ Length of pipe, flame tube in particular, with inner volume for direction of hot gas and thermal shield
US5431020A (en) * 1990-11-29 1995-07-11 Siemens Aktiengesellschaft Ceramic heat shield on a load-bearing structure
US5224539A (en) * 1991-06-14 1993-07-06 Coen Company, Inc. Cooling system for air heaters and the like
CA2089285C (en) * 1992-03-30 2002-06-25 Stephen Winthrop Falls Segmented centerbody for a double annular combustor
DE4343319A1 (en) * 1993-12-18 1995-06-22 Abb Patent Gmbh Combustion chamber with a ceramic lining
US5636508A (en) * 1994-10-07 1997-06-10 Solar Turbines Incorporated Wedge edge ceramic combustor tile
DE19602731C1 (en) * 1996-01-26 1997-07-10 Daimler Benz Aerospace Ag Reduced thermal stress wall structure for a rocket drive mechanism
DE19704976C2 (en) * 1997-01-29 1999-02-25 Siemens Ag Gas turbine system with a combustion chamber casing lined with ceramic stones
US6021570A (en) * 1997-11-20 2000-02-08 Caterpillar Inc. Annular one piece combustor liner
EP1072573A1 (en) 1999-07-30 2001-01-31 Siemens Aktiengesellschaft Method of making a refractory body and ceramic combustion chamber stone
EP1288601B1 (en) * 2001-08-28 2006-10-25 Siemens Aktiengesellschaft Heat shield brick and its use in a combustion chamber
EP1302723A1 (en) * 2001-10-15 2003-04-16 Siemens Aktiengesellschaft Lining for combustion chamber inside walls
ES2307702T3 (en) * 2002-11-22 2008-12-01 Siemens Aktiengesellschaft COMBUSTION CHAMBER FOR THE COMBUSTION OF A FUEL FLUID MIX.
GB0305025D0 (en) * 2003-03-05 2003-04-09 Alstom Switzerland Ltd Method and device for efficient usage of cooling air for acoustic damping of combustion chamber pulsations
US7553385B2 (en) * 2004-11-23 2009-06-30 United Technologies Corporation Cold gas dynamic spraying of high strength copper
US8359865B2 (en) * 2010-02-04 2013-01-29 United Technologies Corporation Combustor liner segment seal member
US9494081B2 (en) 2013-05-09 2016-11-15 Siemens Aktiengesellschaft Turbine engine shutdown temperature control system with an elongated ejector
WO2015022222A1 (en) * 2013-08-15 2015-02-19 Siemens Aktiengesellschaft Heat shield having at least one helmholtz resonator
CN106247400B (en) * 2015-06-08 2020-01-31 A.S.En.安萨尔多开发能源有限责任公司 Fixing device for heat-insulating tiles of a combustion chamber of a gas turbine
US10260750B2 (en) * 2015-12-29 2019-04-16 United Technologies Corporation Combustor panels having angled rail
US10619854B2 (en) * 2016-11-30 2020-04-14 United Technologies Corporation Systems and methods for combustor panel
US11204204B2 (en) * 2019-03-08 2021-12-21 Toyota Motor Engineering & Manufacturing North America, Inc. Acoustic absorber with integrated heat sink

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US792667A (en) * 1902-11-01 1905-06-20 J S Rogers Process of burning hydrocarbons or other combustibles.
US1757698A (en) * 1927-08-15 1930-05-06 Allen Sherman Hoff Co Side-wall seal
US2092537A (en) * 1935-10-14 1937-09-07 Andrew H Stewart Furnace wall
US2183313A (en) * 1938-07-07 1939-12-12 Robert H Goddard Combustion chamber for aircraft
US2186740A (en) * 1939-02-17 1940-01-09 Teeters Thomas Furnace construction
US2348754A (en) * 1942-08-06 1944-05-16 Allis Chalmers Mfg Co Turbine apparatus
US2451146A (en) * 1944-06-05 1948-10-12 Kellogg M W Co Internally insulation lined vessel
US2468902A (en) * 1944-10-20 1949-05-03 Tech Studien Ag Double-walled body for hot gases or vapors under superatmospheric pressure

Also Published As

Publication number Publication date
NL69245C (en)
CH268030A (en) 1950-04-30
GB602149A (en) 1948-05-20
US2548485A (en) 1951-04-10

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