GB758213A - Improvements in and relating to cylindrical combustion chambers or furnaces - Google Patents

Improvements in and relating to cylindrical combustion chambers or furnaces

Info

Publication number
GB758213A
GB758213A GB6208/54A GB620854A GB758213A GB 758213 A GB758213 A GB 758213A GB 6208/54 A GB6208/54 A GB 6208/54A GB 620854 A GB620854 A GB 620854A GB 758213 A GB758213 A GB 758213A
Authority
GB
United Kingdom
Prior art keywords
bricks
longitudinal
plates
end rings
perforations
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
GB6208/54A
Inventor
Robert Francis Darling
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.)
Parsons and Marine Engineering Turbine Research and Development Association
Original Assignee
Parsons and Marine Engineering Turbine Research and Development Association
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 Parsons and Marine Engineering Turbine Research and Development Association filed Critical Parsons and Marine Engineering Turbine Research and Development Association
Priority to GB6208/54A priority Critical patent/GB758213A/en
Priority to DEP13194A priority patent/DE1021647B/en
Priority to US486238A priority patent/US2915877A/en
Priority to FR1119125D priority patent/FR1119125A/en
Priority to CH330271D priority patent/CH330271A/en
Publication of GB758213A publication Critical patent/GB758213A/en
Expired 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • 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
    • F23M5/02—Casings; Linings; Walls characterised by the shape of the bricks or blocks used
    • 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)
  • Ceramic Engineering (AREA)
  • Furnace Housings, Linings, Walls, And Ceilings (AREA)
  • Air Supply (AREA)

Abstract

758,213. Generating combustion products under pressure; furnace linings. PARSONS & MARINE ENGINEERING TURBINE RESEARCH & DEVELOPMENT ASSOCIATION. Dec. 15, 1954 [March 3, 1954], No. 6208/54. Class 51(1). A cylindrical combustion chamber or furnace, for example a flame tube of a gas turbine combustion chamber comprises a plurality of longitudinal metal channel plates b secured at each end to one of a pair of metal end rings d, each channel plate supporting a set ofmutuallyabutting refractory bricks a. The thickness and cross-section of the channel plates is such that they are stiff in the longitudinal direction but flexible in the circumferential direction. The ends of each set of bricks a are disposed so as to provide a clearance from the end rings. The channel plates b have inwardly-curved longitudinal edges j and the edges of the bricks a are correspondingly shaped and are also formed with projecting lips i. Two or more cover plates f having perforations g are disposed around the f having perforations g are disposed around the plates being secured to the end rings d by the same bolts c. The two end rings d are connected together by a pair of longitudinal bridge members e. The bricks a in each longitudinal set have inter-engaging features k, m. Air passes through the perforations g and through the spaces between adjacent sets of bricks for cooling. The projecting lips i shield the edges of the channel plates from the heat of the flame.
GB6208/54A 1954-03-03 1954-03-03 Improvements in and relating to cylindrical combustion chambers or furnaces Expired GB758213A (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
GB6208/54A GB758213A (en) 1954-03-03 1954-03-03 Improvements in and relating to cylindrical combustion chambers or furnaces
DEP13194A DE1021647B (en) 1954-03-03 1954-12-13 Cylindrical heating or combustion space, especially for gas turbines
US486238A US2915877A (en) 1954-03-03 1955-02-04 Cylindrical furnaces
FR1119125D FR1119125A (en) 1954-03-03 1955-02-15 Improvements to cylindrical furnaces
CH330271D CH330271A (en) 1954-03-03 1955-02-21 Cylindrical combustion chamber

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB6208/54A GB758213A (en) 1954-03-03 1954-03-03 Improvements in and relating to cylindrical combustion chambers or furnaces

Publications (1)

Publication Number Publication Date
GB758213A true GB758213A (en) 1956-10-03

Family

ID=9810392

Family Applications (1)

Application Number Title Priority Date Filing Date
GB6208/54A Expired GB758213A (en) 1954-03-03 1954-03-03 Improvements in and relating to cylindrical combustion chambers or furnaces

Country Status (5)

Country Link
US (1) US2915877A (en)
CH (1) CH330271A (en)
DE (1) DE1021647B (en)
FR (1) FR1119125A (en)
GB (1) GB758213A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2211285A (en) * 1987-10-20 1989-06-28 Rolls Royce Plc Combustion equipment
FR2685035A1 (en) * 1991-12-16 1993-06-18 Aerospatiale Device for mounting two components made of materials with different coefficients of expansion, subjected to high temperature variations

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3380409A (en) * 1966-06-13 1968-04-30 Dresser Ind Air-cooled wall construction for incinerators
US3918255A (en) * 1973-07-06 1975-11-11 Westinghouse Electric Corp Ceramic-lined combustion chamber and means for support of a liner with combustion air penetrations
FR2245915B3 (en) * 1973-09-28 1976-08-27 Bazin Claudine
US3956886A (en) * 1973-12-07 1976-05-18 Joseph Lucas (Industries) Limited Flame tubes for gas turbine engines
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
FR2540939A1 (en) * 1983-02-10 1984-08-17 Snecma SEALING RING FOR A TURBINE ROTOR OF A TURBOMACHINE AND TURBOMACHINE INSTALLATION PROVIDED WITH SUCH RINGS
EP0539359B1 (en) * 1990-07-17 1994-04-20 Siemens Aktiengesellschaft Flame tube with a cooled supporting frame for a heat-resistant lining
US5431020A (en) * 1990-11-29 1995-07-11 Siemens Aktiengesellschaft Ceramic heat shield on a load-bearing structure
DE4200815C2 (en) * 1991-02-13 2001-03-01 Bruno Lampka Process for producing a shaped block
CA2089285C (en) * 1992-03-30 2002-06-25 Stephen Winthrop Falls Segmented centerbody for a double annular combustor
US5636508A (en) * 1994-10-07 1997-06-10 Solar Turbines Incorporated Wedge edge ceramic combustor tile
US5421158A (en) * 1994-10-21 1995-06-06 General Electric Company Segmented centerbody for a double annular combustor
US6286338B2 (en) * 1998-02-26 2001-09-11 Visteon Global Technologies, Inc. Block assembly for a gas-type lehr
DE19813897A1 (en) * 1998-03-28 1999-09-30 Bosch Gmbh Robert Segmented insulation for burners with porous media
EP1128131A1 (en) * 2000-02-23 2001-08-29 Siemens Aktiengesellschaft Heat shield element, combustion chamber and gas turbine
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
CZ15297U1 (en) * 2005-02-24 2005-04-04 Dis-R S. R. O. Burner orifice
EP2522907A1 (en) * 2011-05-12 2012-11-14 Siemens Aktiengesellschaft Heat shield assembly
EP3317584A1 (en) * 2015-06-30 2018-05-09 Siemens Energy, Inc. Hybrid component comprising a metal-reinforced ceramic matrix composite material
US20180340687A1 (en) * 2017-05-24 2018-11-29 Siemens Aktiengesellschaft Refractory ceramic component for a gas turbine engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US237339A (en) * 1881-02-01 Sectional furnace
US2530019A (en) * 1944-11-11 1950-11-14 Elliott Co Combustion chamber with side air entrance and hollow ignition cone
NL69245C (en) * 1946-01-09
CH255541A (en) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Cooled metal combustion chamber for generating heating and propellant gases.

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2211285A (en) * 1987-10-20 1989-06-28 Rolls Royce Plc Combustion equipment
FR2685035A1 (en) * 1991-12-16 1993-06-18 Aerospatiale Device for mounting two components made of materials with different coefficients of expansion, subjected to high temperature variations
US5439306A (en) * 1991-12-16 1995-08-08 Societe Nationale Industrielle Et Aerospatiale Device for assembling two elements of materials having different coefficients of thermal expansion

Also Published As

Publication number Publication date
DE1021647B (en) 1957-12-27
CH330271A (en) 1958-05-31
FR1119125A (en) 1956-06-15
US2915877A (en) 1959-12-08

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