[go: up one dir, main page]

GB637223A - Improvements in and relating to combustion units particularly for use in gas turbinesystems - Google Patents

Improvements in and relating to combustion units particularly for use in gas turbinesystems

Info

Publication number
GB637223A
GB637223A GB287846A GB287846A GB637223A GB 637223 A GB637223 A GB 637223A GB 287846 A GB287846 A GB 287846A GB 287846 A GB287846 A GB 287846A GB 637223 A GB637223 A GB 637223A
Authority
GB
United Kingdom
Prior art keywords
end head
turbinesystems
relating
gas
opening
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
GB287846A
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.)
General Electric Co
Original Assignee
General Electric 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 General Electric Co filed Critical General Electric Co
Priority to GB287846A priority Critical patent/GB637223A/en
Publication of GB637223A publication Critical patent/GB637223A/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
    • F23R3/02—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
    • F23R3/54—Reverse-flow combustion chambers

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

637,223. Liquid fuel burners. BRITISH-THOMSON HOUSTON CO., Ltd. (General Electric Co.). Jan. 29, 1946, No. 2878. [Class 75 (i)!] [Also in Groups XII and XXVII] In a combustion unit, particularly for a gas turbine plant, comprising tubular inner and outer walls 10, 11 forming a combustion chamber surrounded by an air-jacket, the inner wall at one end being imperforate and fitted with an end head 17 so as to form an initial mixing and ignition chamber, two series of air inlets 42, 47 are arranged in the end head 17. The fuel nozzle casing 24 projects through an opening in the end head 17 and is provided with a boss fitting an opening in the end head 18 of the outer casing. Baffle plates 43, 44, Fig. 5, with openings 45, 46 are arranged on the fuel nozzle casing 24. Specification 610,641, [Group XII], is referred to.
GB287846A 1946-01-29 1946-01-29 Improvements in and relating to combustion units particularly for use in gas turbinesystems Expired GB637223A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB287846A GB637223A (en) 1946-01-29 1946-01-29 Improvements in and relating to combustion units particularly for use in gas turbinesystems

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB287846A GB637223A (en) 1946-01-29 1946-01-29 Improvements in and relating to combustion units particularly for use in gas turbinesystems

Publications (1)

Publication Number Publication Date
GB637223A true GB637223A (en) 1950-05-17

Family

ID=9747702

Family Applications (1)

Application Number Title Priority Date Filing Date
GB287846A Expired GB637223A (en) 1946-01-29 1946-01-29 Improvements in and relating to combustion units particularly for use in gas turbinesystems

Country Status (1)

Country Link
GB (1) GB637223A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0578048A1 (en) * 1992-07-08 1994-01-12 MAN Gutehoffnungshütte Aktiengesellschaft Cylindrical combustion chamber for gas turbine
EP2500655A1 (en) * 2009-11-10 2012-09-19 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor and gas turbine
FR2973479A1 (en) * 2011-03-30 2012-10-05 Snecma Revolution wall e.g. external revolution wall, for combustion chamber of turbomachine of commercial plane, has circumferential row of primary air holes whose regions are located away from plane along row of dilution holes

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0578048A1 (en) * 1992-07-08 1994-01-12 MAN Gutehoffnungshütte Aktiengesellschaft Cylindrical combustion chamber for gas turbine
US5363653A (en) * 1992-07-08 1994-11-15 Man Gutehoffnungshutte Ag Cylindrical combustion chamber housing of a gas turbine
EP2500655A1 (en) * 2009-11-10 2012-09-19 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor and gas turbine
EP2500655A4 (en) * 2009-11-10 2014-12-03 Mitsubishi Heavy Ind Ltd COMBUSTION CHAMBER FOR GAS TURBINE AND GAS TURBINE
US8950190B2 (en) 2009-11-10 2015-02-10 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor having contraction member on inner wall surface
FR2973479A1 (en) * 2011-03-30 2012-10-05 Snecma Revolution wall e.g. external revolution wall, for combustion chamber of turbomachine of commercial plane, has circumferential row of primary air holes whose regions are located away from plane along row of dilution holes

Similar Documents

Publication Publication Date Title
GB577972A (en) Improvements relating to liquid-fuel burners and vaporisers, and combustion engines or systems employing same
GB1489110A (en) Hot-gas generator
GB584477A (en) Improvements relating to internal combustion prime movers
GB650462A (en) Improvements in or relating to combustion apparatus
GB723015A (en) Improvements in or relating to gas turbine plant
GB904142A (en) Improvements in or relating to gas-turbine engines
GB579424A (en) Improvements relating to liquid fuel combustion apparatus for generating gases for power purposes
GB603485A (en) Liquid fuel combustion chamber
GB577865A (en) Liquid-fuel combustion-chamber
GB637223A (en) Improvements in and relating to combustion units particularly for use in gas turbinesystems
GB669751A (en) Improvements relating to combustion chambers for gas turbine plants and the like
GB616481A (en) Improvements in or relating to ignition systems for gas turbines
GB1524217A (en) Combustion chamber for a gas turbine engine
GB619251A (en) Improvements relating to combustion-equipment
GB922069A (en) Combustion chamber for a gas turbine engine
GB736823A (en) Engine combustion chambers
GB899213A (en) Combustion chambers
GB788557A (en) Main combustion chambers for gas turbine engines
GB672530A (en) Improvements in gas turbine combustion chambers
GB682778A (en) Improvements relating to combustion chambers for prime movers
GB619353A (en) Liquid-fuel combustion chamber
GB715387A (en) Improvements in or relating to combustion chambers for gas turbines or other prime movers
GB679145A (en) Improvements in combustion apparatus
GB586602A (en) Improvements in regenerative gas turbine plants
GB670968A (en) Vapourizing system for a gas turbine engine