GB703116A - Improvements in and relating to combustion chambers - Google Patents

Improvements in and relating to combustion chambers

Info

Publication number
GB703116A
GB703116A GB24866/51A GB2486651A GB703116A GB 703116 A GB703116 A GB 703116A GB 24866/51 A GB24866/51 A GB 24866/51A GB 2486651 A GB2486651 A GB 2486651A GB 703116 A GB703116 A GB 703116A
Authority
GB
United Kingdom
Prior art keywords
flame tube
openings
attached
oct
projecting
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
GB24866/51A
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.)
British Thomson Houston Co Ltd
Original Assignee
British Thomson Houston 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 British Thomson Houston Co Ltd filed Critical British Thomson Houston Co Ltd
Publication of GB703116A publication Critical patent/GB703116A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C99/00—Subject-matter not provided for in other groups of this subclass
    • 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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C2700/00—Special arrangements for combustion apparatus using fluent fuel
    • F23C2700/02—Combustion apparatus using liquid fuel
    • F23C2700/023—Combustion apparatus using liquid fuel without pre-vaporising means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
  • Gas Burners (AREA)

Abstract

703,116. Generating combustion products under pressure. BRITISH THOMSON-HOUSTON CO., Ltd. Oct. 24, 1951 [Oct. 31, 1950], No. 24866/51. Class 51 (1) In a combustion chamber having a flame tube 2 with openings 8 therein for the admission of cooling air, means for directing the air circumferentially over the inner surface of the flame tube comprises a deflecting member 9 having a portion 10 inside the flame tube close to the inner surface and parallel thereto and a second portion 12 at right angles to the first portion and projecting through an opening to outside the flame tube. The deflecting member is attached to the outer surface of the flame tube by means of bridge pieces 14 engaging slots 13 in the webs 12 and welded thereto and also welded to the outer surface of the flame tube. The openings 8 comprise five, six or seven equidistantly-spaced slots of considerable axial length and the deflector members comprise a number of sections separately attached to the flame tube and longitudinally spaced from each other, each section being attached to the flame tube near one end only, the sections being kept in alignment by pins 16 projecting into the ends. Rows' of additional combustion and dilution air inlet holes 17 are provided in the flame tube between the openings 8. Dimensions and proportions of the air inlet openings are given.
GB24866/51A 1950-10-31 1951-10-24 Improvements in and relating to combustion chambers Expired GB703116A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US193100A US2651912A (en) 1950-10-31 1950-10-31 Combustor and cooling means therefor

Publications (1)

Publication Number Publication Date
GB703116A true GB703116A (en) 1954-01-27

Family

ID=22712286

Family Applications (1)

Application Number Title Priority Date Filing Date
GB24866/51A Expired GB703116A (en) 1950-10-31 1951-10-24 Improvements in and relating to combustion chambers

Country Status (3)

Country Link
US (1) US2651912A (en)
FR (1) FR1044335A (en)
GB (1) GB703116A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1045180B (en) * 1954-02-23 1958-11-27 Gen Electric Auxiliary burner for a jet engine for aircraft

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE964191C (en) * 1957-05-02 Canadian Patents and Development Limi ted Ottawa Ontario (Kanada) Annular combustion chamber for gas turbine engines
US2874536A (en) * 1954-03-18 1959-02-24 Gen Electric Cooling means for tailpipe
BE535497A (en) * 1954-02-26
US2990686A (en) * 1955-09-29 1961-07-04 John P Longwell Combustor apparatus
DE1066385B (en) * 1956-11-21 1959-10-01 Rolls-Royce Limited, Derby (Großbritannien) Burning plant of gas tank aggregates
NL113358C (en) * 1957-02-18
US2974485A (en) * 1958-06-02 1961-03-14 Gen Electric Combustor for fluid fuels
US3064424A (en) * 1959-09-30 1962-11-20 Gen Motors Corp Flame tube
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
GB1552132A (en) * 1975-11-29 1979-09-12 Rolls Royce Combustion chambers for gas turbine engines
US4158949A (en) * 1977-11-25 1979-06-26 General Motors Corporation Segmented annular combustor
US4471623A (en) * 1982-10-15 1984-09-18 The United States Of America As Represented By The Secretary Of The Air Force Combustion chamber floatwall panel attachment arrangement
US4512159A (en) * 1984-04-02 1985-04-23 United Technologies Corporation Clip attachment
US4848089A (en) * 1988-02-18 1989-07-18 Avco Corporation Combustor attachment device
FR2646880A1 (en) * 1989-05-11 1990-11-16 Snecma THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR
EP1288578A1 (en) * 2001-08-31 2003-03-05 Siemens Aktiengesellschaft Combustor layout
GB201501817D0 (en) * 2015-02-04 2015-03-18 Rolls Royce Plc A combustion chamber and a combustion chamber segment

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB588086A (en) * 1943-04-01 1947-05-14 Power Jets Ltd Improvements relating to combustion apparatus
US2595999A (en) * 1943-11-23 1952-05-06 Westinghouse Electric Corp Power plant combustion apparatus having apertured combustion chamber walls
FR962862A (en) * 1946-10-26 1950-06-22
US2488911A (en) * 1946-11-09 1949-11-22 Surface Combustion Corp Combustion apparatus for use with turbines
BE482256A (en) * 1947-05-23
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1045180B (en) * 1954-02-23 1958-11-27 Gen Electric Auxiliary burner for a jet engine for aircraft

Also Published As

Publication number Publication date
FR1044335A (en) 1953-11-17
US2651912A (en) 1953-09-15

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