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 enginesInfo
- 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
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
- F23R3/045—Air 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.
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)
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 |
-
1955
- 1955-11-16 GB GB3287655A patent/GB819065A/en not_active Expired
Cited By (11)
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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