GB1018479A - Improvements relating to annular combustion chambers in gas turbine power plants - Google Patents

Improvements relating to annular combustion chambers in gas turbine power plants

Info

Publication number
GB1018479A
GB1018479A GB2595864A GB2595864A GB1018479A GB 1018479 A GB1018479 A GB 1018479A GB 2595864 A GB2595864 A GB 2595864A GB 2595864 A GB2595864 A GB 2595864A GB 1018479 A GB1018479 A GB 1018479A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
walls
combustion chambers
annular
power plants
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
GB2595864A
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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 Daimler Benz AG filed Critical Daimler Benz AG
Publication of GB1018479A publication Critical patent/GB1018479A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60Support structures; Attaching or mounting means

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

1,018,479. Gas turbine combustion chambers. DAIMLER BENZ A.G. June 23, 1964 [July 4, 1963], No. 25958/64. Heading F1L. The inner and outer walls of an annular gas turbine flame chamber are mounted independently of one another and mutually unconnected, the front and rear ends of both walls being engaged with fixed annular supporting parts so as to be freely movable both radially outwards and axially. The flame chamber has inner and outer annular walls 21, 11 with respective front ends 22, 12 slidably mounted on rings 16, 15. Respective rear ends 23, 13 carry L and U-section rings 23<SP>1</SP>, 13<SP>1</SP> slidably mounted on annular flanges 19, 18 attached to the turbine nozzle ring 17. Walls 21, 11 are not interconnected and can expand freely radially outwards and axially.
GB2595864A 1963-07-04 1964-06-23 Improvements relating to annular combustion chambers in gas turbine power plants Expired GB1018479A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DED41898A DE1186275B (en) 1963-07-04 1963-07-04 Arrangement of the flame chamber of annular combustion chambers for gas turbine engines

Publications (1)

Publication Number Publication Date
GB1018479A true GB1018479A (en) 1966-01-26

Family

ID=7046408

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2595864A Expired GB1018479A (en) 1963-07-04 1964-06-23 Improvements relating to annular combustion chambers in gas turbine power plants

Country Status (2)

Country Link
DE (1) DE1186275B (en)
GB (1) GB1018479A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine
WO2013060663A3 (en) * 2011-10-24 2015-02-26 Alstom Technology Ltd Gas turbine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3631674A (en) * 1970-01-19 1972-01-04 Gen Electric Folded flow combustion chamber for a gas turbine engine
WO2013060663A3 (en) * 2011-10-24 2015-02-26 Alstom Technology Ltd Gas turbine
US9708920B2 (en) 2011-10-24 2017-07-18 General Electric Technology Gmbh Gas turbine support element permitting thermal expansion between combustor shell and rotor cover at turbine inlet

Also Published As

Publication number Publication date
DE1186275B (en) 1965-01-28

Similar Documents

Publication Publication Date Title
GB1138547A (en) Improvements in cooling structure
GB790293A (en) Improvements in or relating to heat-resisting wall structures for gas-turbine enginecombustion equipment
GB1010338A (en) Means for supporting the downstream end of a combustion chamber in a gas turbine engine
GB836088A (en) Improvements in turbojet engine afterburners
GB712080A (en) Gas turbine plant
GB1494591A (en) Flexible interconnection for combustors of gas turbine engines
GB1089467A (en) Improvements in or relating to gas turbines
GB1116930A (en) Improvements in cooled flameholder assembly
GB1037923A (en) Combustion chamber for a gas turbine
GB1018479A (en) Improvements relating to annular combustion chambers in gas turbine power plants
GB1035541A (en) Combustion equipment for a gas turbine engine
GB924333A (en) Annular transition duct for a gas turbine jet propulsion engine
GB1127652A (en) A gas turbine jet propulsion engine afterburner
GB575922A (en) Improvements relating to combustion chambers for prime movers
GB1038661A (en) Improvements relating to metallic gas turbine combustion chambers
GB543918A (en) Improvements and relating to combustion chambers
GB1076367A (en) Gas turbine engine
GB595286A (en)
GB943250A (en) Improvements in or relating to gas turbine combustion chambers
GB971485A (en) Liquid fuel combustion apparatus
GB700705A (en) Combustion chambers for jet propulsion engines, gas turbines or other prime movers
GB990550A (en) Improvements in or relating to cooled burners
GB865762A (en) Internal combustion turbine units
GB580042A (en) Improvements in or relating to turbo-compressor propulsive apparatus
GB812404A (en) Internal combustion turbine units