GB1112131A - Gas turbine engine combustion apparatus - Google Patents

Gas turbine engine combustion apparatus

Info

Publication number
GB1112131A
GB1112131A GB3557665A GB3557665A GB1112131A GB 1112131 A GB1112131 A GB 1112131A GB 3557665 A GB3557665 A GB 3557665A GB 3557665 A GB3557665 A GB 3557665A GB 1112131 A GB1112131 A GB 1112131A
Authority
GB
United Kingdom
Prior art keywords
air
flame tube
gas turbine
holes
air holes
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
GB3557665A
Inventor
Raymond Chadwick
Eric Carr
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
Joseph 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, Joseph Lucas Industries Ltd filed Critical Lucas Industries Ltd
Priority to GB3557665A priority Critical patent/GB1112131A/en
Priority to SE1112166A priority patent/SE314557B/xx
Publication of GB1112131A publication Critical patent/GB1112131A/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
    • 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)
  • Combustion Of Fluid Fuel (AREA)

Abstract

1,112,131. Gas turbine combustion chambers; gas turbine engines. JOSEPH LUCAS (INDUSTRIES) Ltd. Aug. 19, 1966 [Aug.19, 1965], No.35576/65. Headings F1G and F1L. Combustion apparatus for a gas turbine engine comprises an annular flame tube 10, 11 with its outlet 16 at the same end as the inlet 14 of the air jacket 12, 13, fuel nozzles 23 being provided at the other end. Dilution air holes 18 and primary and secondary combustion air holes 19 are provided in the outer wall 11 of the flame tube, and further dilution air holes 24 are provided in the inner wall 10. Two rows of small closely spaced holes 20 are provided, one row being between the primary and secondary air holes 19 and the other row being between the primary air holes 19 and the closed end of the flame tube. The air entering the flame tube through the holes 20 forms a substantially continuous air barrier which breaks up the flow pattern within the flame tube into a pair of toroids 21, 22. Air is supplied to the combustion apparatus by a centrifugal compressor 15, and the combustion gases are supplied to a turbine 17 having an exhaust passage 25 bounded by the inner wall 12 of the air jacket.
GB3557665A 1965-08-19 1965-08-19 Gas turbine engine combustion apparatus Expired GB1112131A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB3557665A GB1112131A (en) 1965-08-19 1965-08-19 Gas turbine engine combustion apparatus
SE1112166A SE314557B (en) 1965-08-19 1966-08-17

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3557665A GB1112131A (en) 1965-08-19 1965-08-19 Gas turbine engine combustion apparatus

Publications (1)

Publication Number Publication Date
GB1112131A true GB1112131A (en) 1968-05-01

Family

ID=10379267

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3557665A Expired GB1112131A (en) 1965-08-19 1965-08-19 Gas turbine engine combustion apparatus

Country Status (2)

Country Link
GB (1) GB1112131A (en)
SE (1) SE314557B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1705427A1 (en) * 2005-03-02 2006-09-27 General Electric Company One-piece can combustor
US7155800B2 (en) 2005-02-24 2007-01-02 General Electric Company Automated seal strip assembly method and apparatus for rotary machines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7155800B2 (en) 2005-02-24 2007-01-02 General Electric Company Automated seal strip assembly method and apparatus for rotary machines
EP1705427A1 (en) * 2005-03-02 2006-09-27 General Electric Company One-piece can combustor

Also Published As

Publication number Publication date
SE314557B (en) 1969-09-08

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