GB1060026A - Combustion equipment for a gas turbine engine - Google Patents

Combustion equipment for a gas turbine engine

Info

Publication number
GB1060026A
GB1060026A GB4246765A GB4246765A GB1060026A GB 1060026 A GB1060026 A GB 1060026A GB 4246765 A GB4246765 A GB 4246765A GB 4246765 A GB4246765 A GB 4246765A GB 1060026 A GB1060026 A GB 1060026A
Authority
GB
United Kingdom
Prior art keywords
gas turbine
turbine engine
combustion equipment
apertures
flame tubes
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
GB4246765A
Inventor
Harry Moxon
Terence Durrant
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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
Priority to GB47997/63A priority Critical patent/GB1021588A/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB4246765A priority patent/GB1060026A/en
Priority to US540636A priority patent/US3303644A/en
Priority to FR78838A priority patent/FR90891E/en
Publication of GB1060026A publication Critical patent/GB1060026A/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
    • 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
    • F23R3/60—Support 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)
  • Testing Of Engines (AREA)

Abstract

1,060,026. Gas turbine combustion chambers. ROLLS-ROYCE Ltd. Oct.6, 1965, No.42467/65. Addition to 1, 021, 588. Heading F1L. Gas turbine engine combustion equipment 15 constituting an improvement in the invention claimed in Specification 1, 021, 588 comprises outer and inner casings 11, 12 respectively, forming an annular duct 13 within which is mounted a series of angularly spaced flame tubes 20. Adjacent the upstream end of each flame tube 20 is located a plate 18 lying in a radial plane and having apertures (22), Fig. 3 (not shown), of varying size therein. The sides (23) of adjacent plates 18 abut so that the flow path for air from the engine compressor surrounding the flame tubes is blocked except through the apertures (22). The construction tends to equalize pressure differences in different parts of the duct 13 and is applicable also to annular flame tubes.
GB4246765A 1963-12-04 1965-10-06 Combustion equipment for a gas turbine engine Expired GB1060026A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB47997/63A GB1021588A (en) 1963-12-04 1963-12-04 Combustion equipment for a gas turbine engine
GB4246765A GB1060026A (en) 1965-10-06 1965-10-06 Combustion equipment for a gas turbine engine
US540636A US3303644A (en) 1963-12-04 1966-04-06 Combustion equipment for a gas turbine engine
FR78838A FR90891E (en) 1963-12-04 1966-10-05 Combustion device for gas turbine engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4246765A GB1060026A (en) 1965-10-06 1965-10-06 Combustion equipment for a gas turbine engine

Publications (1)

Publication Number Publication Date
GB1060026A true GB1060026A (en) 1967-02-22

Family

ID=10424575

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4246765A Expired GB1060026A (en) 1963-12-04 1965-10-06 Combustion equipment for a gas turbine engine

Country Status (1)

Country Link
GB (1) GB1060026A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1994028357A1 (en) * 1993-05-24 1994-12-08 Rolls-Royce Plc A gas turbine engine combustion chamber
US20120045725A1 (en) * 2009-08-13 2012-02-23 Mitsubishi Heavy Industries, Ltd. Combustor

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO1994028357A1 (en) * 1993-05-24 1994-12-08 Rolls-Royce Plc A gas turbine engine combustion chamber
US5640851A (en) * 1993-05-24 1997-06-24 Rolls-Royce Plc Gas turbine engine combustion chamber
US20120045725A1 (en) * 2009-08-13 2012-02-23 Mitsubishi Heavy Industries, Ltd. Combustor
US9863637B2 (en) * 2009-08-13 2018-01-09 Mitsubishi Heavy Industries, Ltd. Combustor

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