GB683555A - Improvements in or relating to combustion chamber - Google Patents

Improvements in or relating to combustion chamber

Info

Publication number
GB683555A
GB683555A GB12598/50A GB1259850A GB683555A GB 683555 A GB683555 A GB 683555A GB 12598/50 A GB12598/50 A GB 12598/50A GB 1259850 A GB1259850 A GB 1259850A GB 683555 A GB683555 A GB 683555A
Authority
GB
United Kingdom
Prior art keywords
air
combustion
casing
inlet
plate
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
GB12598/50A
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.)
Elliott Co
Original Assignee
Elliott Co
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 Elliott Co filed Critical Elliott Co
Publication of GB683555A publication Critical patent/GB683555A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
  • Air Supply (AREA)

Abstract

683,555. Generating combustion products under pressure. ELLIOTT CO. May 19, 1950 [June 2, 1949], No. 12598/50. Class 51 (i). A combustion chamber comprises a casing 1 having an air inlet 5 and an outlet 4 at one end for combustion gases, a plurality of parallel combustion tubes 15 being disposed in the casing lengthwise thereof having air inlets and burner nozzles 30. The air inlet 5 is disposed in the side wall of the casing and a plate 7 extends across the casing between the air inlet 5 and the inlet end of the casing, the plate having a plurality of openings in which the inlet ends of the combustion tubes 15 are fitted. The plate 7 also has a plurality of holes 35 and the major portion of the air from the inlet passes through the holes 35 to the inlet ends of the combustion tubes. The downstream ends of the combustion tubes are accommodated in a second plate 8 which also has openings 36 for the flow of air direct to the outlet 4, and openings 11 for the flow of air into the space 10 between the double walls of the tapered duct for cooling purposes. The combustion tubes comprise an outer shell 15 and telescopically arranged liner sections 16, 17, 18 which are spaced apart to permit air to enter the combustion zone along the length of the tube. The smallest diameter section 16 has air inlets 22 which may be adjusted by pivotally-mounted flaps. Reference has 'been directed by the Comptroller to Specification 661,864.
GB12598/50A 1949-06-02 1950-05-19 Improvements in or relating to combustion chamber Expired GB683555A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US96753A US2565843A (en) 1949-06-02 1949-06-02 Multiple tubular combustion chamber

Publications (1)

Publication Number Publication Date
GB683555A true GB683555A (en) 1952-12-03

Family

ID=22258914

Family Applications (1)

Application Number Title Priority Date Filing Date
GB12598/50A Expired GB683555A (en) 1949-06-02 1950-05-19 Improvements in or relating to combustion chamber

Country Status (2)

Country Link
US (1) US2565843A (en)
GB (1) GB683555A (en)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2885858A (en) * 1947-12-02 1959-05-12 Power Jets Res & Dev Ltd Combustion system with mixing chamber
US2608057A (en) * 1949-12-24 1952-08-26 A V Roe Canada Ltd Gas turbine nozzle box
US2673726A (en) * 1950-08-16 1954-03-30 American Mach & Foundry Jet tobacco curer
NL84788C (en) * 1951-06-12
US3073583A (en) * 1960-10-28 1963-01-15 John Wood Company Heater
DE1224095B (en) * 1962-07-24 1966-09-01 Prvni Brnenska Strojirna Zd Y Gas turbine combustor
US3958922A (en) * 1974-09-20 1976-05-25 John Zink Company Duct burner assembly
DE2950535A1 (en) * 1979-11-23 1981-06-11 BBC AG Brown, Boveri & Cie., Baden, Aargau COMBUSTION CHAMBER OF A GAS TURBINE WITH PRE-MIXING / PRE-EVAPORATING ELEMENTS
DE2949388A1 (en) * 1979-12-07 1981-06-11 Kraftwerk Union AG, 4330 Mülheim COMBUSTION CHAMBER FOR GAS TURBINES AND METHOD FOR OPERATING THE COMBUSTION CHAMBER
CA2089302C (en) * 1992-03-30 2004-07-06 Joseph Frank Savelli Double annular combustor
US7631499B2 (en) * 2006-08-03 2009-12-15 Siemens Energy, Inc. Axially staged combustion system for a gas turbine engine
US8522555B2 (en) * 2009-05-20 2013-09-03 General Electric Company Multi-premixer fuel nozzle support system
US9033699B2 (en) * 2011-11-11 2015-05-19 General Electric Company Combustor
US20130122437A1 (en) * 2011-11-11 2013-05-16 General Electric Company Combustor and method for supplying fuel to a combustor
US9134023B2 (en) * 2012-01-06 2015-09-15 General Electric Company Combustor and method for distributing fuel in the combustor
US9341376B2 (en) * 2012-02-20 2016-05-17 General Electric Company Combustor and method for supplying fuel to a combustor
US9416973B2 (en) * 2013-01-07 2016-08-16 General Electric Company Micromixer assembly for a turbine system and method of distributing an air-fuel mixture to a combustor chamber
WO2016160010A1 (en) * 2015-04-01 2016-10-06 Siemens Energy, Inc. Pre-mixing based fuel nozzle for use in a combustion turbine engine
US10890329B2 (en) 2018-03-01 2021-01-12 General Electric Company Fuel injector assembly for gas turbine engine
US10935245B2 (en) 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11156360B2 (en) 2019-02-18 2021-10-26 General Electric Company Fuel nozzle assembly

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1801007A (en) * 1926-09-23 1931-04-14 Jezler Hubert Production of gas jets for power purposes
US2078956A (en) * 1930-03-24 1937-05-04 Milo Ab Gas turbine system
US2410450A (en) * 1943-01-30 1946-11-05 Westinghouse Electric Corp Turbine apparatus
US2402377A (en) * 1943-02-09 1946-06-18 Westinghouse Electric Corp Turbine apparatus
BE489359A (en) * 1944-10-05
US2447482A (en) * 1945-04-25 1948-08-24 Westinghouse Electric Corp Turbine apparatus

Also Published As

Publication number Publication date
US2565843A (en) 1951-08-28

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