GB626275A - Improvements in or relating to flame tubes for gas turbine combustion chambers - Google Patents
Improvements in or relating to flame tubes for gas turbine combustion chambersInfo
- Publication number
- GB626275A GB626275A GB2334447A GB2334447A GB626275A GB 626275 A GB626275 A GB 626275A GB 2334447 A GB2334447 A GB 2334447A GB 2334447 A GB2334447 A GB 2334447A GB 626275 A GB626275 A GB 626275A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine combustion
- relating
- combustion chambers
- 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
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
- F23R3/005—Combined with pressure or heat exchangers
Abstract
626,275. Generating combustion products under pressure. PARSONS & CO., Ltd., C. A., VOYSEY, R. G., and HUGHES, D. F. Aug. 22, 1947, No. 23344. [Class 51 (i)] The flame tube a of a gas turbine combustion chamber has external longitudinal fins b which lie in a surrounding air duct. The fins may be bent at the exit end, or, may be helical throughout. The air duct wall d is covered by heat insulation material e enclosed in an outer shell.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2334447A GB626275A (en) | 1947-08-22 | 1947-08-22 | Improvements in or relating to flame tubes for gas turbine combustion chambers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2334447A GB626275A (en) | 1947-08-22 | 1947-08-22 | Improvements in or relating to flame tubes for gas turbine combustion chambers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB626275A true GB626275A (en) | 1949-07-12 |
Family
ID=10194118
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2334447A Expired GB626275A (en) | 1947-08-22 | 1947-08-22 | Improvements in or relating to flame tubes for gas turbine combustion chambers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB626275A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4343332A1 (en) * | 1993-12-20 | 1995-06-22 | Abb Management Ag | Convective cooling device for sealed combustion chamber |
WO1998049496A1 (en) * | 1997-04-30 | 1998-11-05 | Siemens Westinghouse Power Corporation | An apparatus for cooling a combuster, and a method of same |
EP3486431A1 (en) * | 2017-11-15 | 2019-05-22 | Ansaldo Energia Switzerland AG | Hot gas path component for a gas turbine engine |
-
1947
- 1947-08-22 GB GB2334447A patent/GB626275A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4343332A1 (en) * | 1993-12-20 | 1995-06-22 | Abb Management Ag | Convective cooling device for sealed combustion chamber |
WO1998049496A1 (en) * | 1997-04-30 | 1998-11-05 | Siemens Westinghouse Power Corporation | An apparatus for cooling a combuster, and a method of same |
EP3486431A1 (en) * | 2017-11-15 | 2019-05-22 | Ansaldo Energia Switzerland AG | Hot gas path component for a gas turbine engine |
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