GB2008199A - Flame Tube - Google Patents

Flame Tube

Info

Publication number
GB2008199A
GB2008199A GB7846600A GB7846600A GB2008199A GB 2008199 A GB2008199 A GB 2008199A GB 7846600 A GB7846600 A GB 7846600A GB 7846600 A GB7846600 A GB 7846600A GB 2008199 A GB2008199 A GB 2008199A
Authority
GB
United Kingdom
Prior art keywords
flame tube
radially inwardly
inlets
annular
fuel
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.)
Withdrawn
Application number
GB7846600A
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.)
ZF International UK Ltd
Original Assignee
Lucas Industries 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 Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB7846600A priority Critical patent/GB2008199A/en
Publication of GB2008199A publication Critical patent/GB2008199A/en
Withdrawn legal-status Critical Current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
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)

Abstract

To reduce axial length a gas turbine flame tube 10 is of disc-like annular form having fuel inlets 11 in its outer periphery discharging fuel radially inwardly. An annular outlet 12 radially inwardly of inlets 11 discharges combustion gases parallel to the axis of the flame tube 10 towards turbine guide vanes 21. A plenum chamber 15 surrounding flame tube 10 and an air casing 13 is fed with compressed air via annular passage 18. The flame tube may be formed from silicon nitride segments. <IMAGE>
GB7846600A 1977-09-03 1978-11-29 Flame Tube Withdrawn GB2008199A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7846600A GB2008199A (en) 1977-09-03 1978-11-29 Flame Tube

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB3688377 1977-09-03
GB7846600A GB2008199A (en) 1977-09-03 1978-11-29 Flame Tube

Publications (1)

Publication Number Publication Date
GB2008199A true GB2008199A (en) 1979-05-31

Family

ID=26263270

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7846600A Withdrawn GB2008199A (en) 1977-09-03 1978-11-29 Flame Tube

Country Status (1)

Country Link
GB (1) GB2008199A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004150779A (en) * 2002-10-03 2004-05-27 Takashi Ikeda Gas turbine combustor
JP2007232360A (en) * 2006-03-01 2007-09-13 General Electric Co <Ge> Gas turbine engine and its combustor
WO2016174363A1 (en) * 2015-04-29 2016-11-03 Snecma Elbowed combustion chamber of a turbomachine

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004150779A (en) * 2002-10-03 2004-05-27 Takashi Ikeda Gas turbine combustor
JP2007232360A (en) * 2006-03-01 2007-09-13 General Electric Co <Ge> Gas turbine engine and its combustor
WO2016174363A1 (en) * 2015-04-29 2016-11-03 Snecma Elbowed combustion chamber of a turbomachine
FR3035707A1 (en) * 2015-04-29 2016-11-04 Snecma COMBUSTION CHAMBER WITH TURBOMACHINE
US10883720B2 (en) 2015-04-29 2021-01-05 Safran Aircraft Engines Elbowed combustion chamber of a turbomachine

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)