GB1060026A - Combustion equipment for a gas turbine engine - Google Patents
Combustion equipment for a gas turbine engineInfo
- 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
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.
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)
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 |
-
1965
- 1965-10-06 GB GB4246765A patent/GB1060026A/en not_active Expired
Cited By (4)
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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