GB819065A - Improvements in or relating to combustion equipment for example of gas turbine engines - Google Patents

Improvements in or relating to combustion equipment for example of gas turbine engines

Info

Publication number
GB819065A
GB819065A GB3287655A GB3287655A GB819065A GB 819065 A GB819065 A GB 819065A GB 3287655 A GB3287655 A GB 3287655A GB 3287655 A GB3287655 A GB 3287655A GB 819065 A GB819065 A GB 819065A
Authority
GB
United Kingdom
Prior art keywords
dilution air
flame tube
baffle
combustion
air
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
GB3287655A
Inventor
Frederick Reginald Murray
Francis Murray Johnson
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
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB3287655A priority Critical patent/GB819065A/en
Publication of GB819065A publication Critical patent/GB819065A/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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/045Air inlet arrangements using pipes

Abstract

819,065. Generating combustion products under pressure. ROLLS-ROYCE Ltd. Nov. 16, 1956 [Nov. 16, 1955], No. 32876/55. Class 51 (1). In combustion equipment comprising an outer easing and an inner flame tube, for example for use in gas turbine engines in which large openings are provided in the flame tube for admission of dilution air which is mixed with the combustion gases to cool them, baffles are provided in association with the dilution air admission holes, the baffles being spaced from the wall of the flame tube towards the centre-line of the combustion space therein and lying across the paths of the dilution air flowing through the dilution air openings. The combustion equipment shown is of the annular kind comprising an annular flame tube formed by outer and inner annular walls 10a, 10b enclosed within an air casing formed by outer and inner annular walls 11a, 11b, the upstream end of the flame tube being substantially closed by structure 14 in which fuel injectors 15 are mounted. Primary air is admitted to the combustion zone through inlet 18 as disclosed in Specifications 744,593, 744,657 and 744,659. Large openings 19 are provided towards the downstream end of the flame tube for admission of dilution air. A supporting plate member 22 is mounted in the dilution air hole 19, a baffle plate 21 being secured to the radially inner end of the plate 22. Dilution air flowing through the opening 19 flows on either side of the plate 22 and impinges on the baffle 21 whereby mixing of the dilution air with the combustion gases is improved. In a second embodiment, the baffle supporting member comprises a pair of plates which are bowed outwardly along the central portions thereof so as to form a tubular air passage through the member, the baffle plate having a corresponding opening. In this arrangement, dilution air flows both through and over the outer surfaces of the baffle supporting members. In another arrangement, the baffle is of annular form being supported by a plurality of support members.
GB3287655A 1955-11-16 1955-11-16 Improvements in or relating to combustion equipment for example of gas turbine engines Expired GB819065A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3287655A GB819065A (en) 1955-11-16 1955-11-16 Improvements in or relating to combustion equipment for example of gas turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3287655A GB819065A (en) 1955-11-16 1955-11-16 Improvements in or relating to combustion equipment for example of gas turbine engines

Publications (1)

Publication Number Publication Date
GB819065A true GB819065A (en) 1959-08-26

Family

ID=10345347

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3287655A Expired GB819065A (en) 1955-11-16 1955-11-16 Improvements in or relating to combustion equipment for example of gas turbine engines

Country Status (1)

Country Link
GB (1) GB819065A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2018641B1 (en) * 1970-04-18 1971-10-14 Motoren Turbinen Union Reversing combustion chamber for gas turbine engines
EP0348097A1 (en) * 1988-06-22 1989-12-27 Secretary Of State For Defence In Her Britannic Majesty's Gov. Of The United Kingdom Of Great Britain And Northern Ireland Gas turbine engine combustors
FR3019586A1 (en) * 2014-04-03 2015-10-09 Turbomeca COMBUSTION CHAMBER COMPRISING DILUTION PIPES WITH FLOOR OUTPUTS.
EP2993404A1 (en) * 2014-09-08 2016-03-09 Alstom Technology Ltd Dilution gas or air mixer for a combustor of a gas turbine
US20230204212A1 (en) * 2021-12-29 2023-06-29 Hanwha Aerospace Co., Ltd. Combustor

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2018641B1 (en) * 1970-04-18 1971-10-14 Motoren Turbinen Union Reversing combustion chamber for gas turbine engines
DE2018641C2 (en) * 1970-04-18 1972-05-10 Motoren Turbinen Union REVERSE COMBUSTION CHAMBER FOR GAS TURBINE ENGINES
EP0348097A1 (en) * 1988-06-22 1989-12-27 Secretary Of State For Defence In Her Britannic Majesty's Gov. Of The United Kingdom Of Great Britain And Northern Ireland Gas turbine engine combustors
WO1989012788A1 (en) * 1988-06-22 1989-12-28 The Secretary Of State For Defence In Her Britanni Gas turbine engine combustors
GB2238864A (en) * 1988-06-22 1991-06-12 Secr Defence Gas turbine engine combustors
GB2238864B (en) * 1988-06-22 1992-04-22 Secr Defence Gas turbine engine combustors
US5187937A (en) * 1988-06-22 1993-02-23 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Gas turbine engine combustors
FR3019586A1 (en) * 2014-04-03 2015-10-09 Turbomeca COMBUSTION CHAMBER COMPRISING DILUTION PIPES WITH FLOOR OUTPUTS.
EP2993404A1 (en) * 2014-09-08 2016-03-09 Alstom Technology Ltd Dilution gas or air mixer for a combustor of a gas turbine
US10443847B2 (en) 2014-09-08 2019-10-15 Ansaldo Energia Switzerland AG Dilution gas or air mixer for a combustor of a gas turbine
US20230204212A1 (en) * 2021-12-29 2023-06-29 Hanwha Aerospace Co., Ltd. Combustor

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