GB674641A - Fuel-burning means for a gaseous-fluid propulsion jet - Google Patents
Fuel-burning means for a gaseous-fluid propulsion jetInfo
- Publication number
- GB674641A GB674641A GB30699/49A GB3069949A GB674641A GB 674641 A GB674641 A GB 674641A GB 30699/49 A GB30699/49 A GB 30699/49A GB 3069949 A GB3069949 A GB 3069949A GB 674641 A GB674641 A GB 674641A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- casing
- disposed
- pilot
- main
- 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
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
- F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Combustion Of Fluid Fuel (AREA)
Abstract
674,641. Jet propulsion plant. ARMSTRONG SIDDELEY MOTORS, Ltd., and ALLEN, S. Aug. 21, 1950 [Nov. 30, 1949], No. 30699/49. Class 110(iii) [Also in Groups XI and XII] In a fuel burning means for a gaseous propulsion jet, a casing 11 is axially disposed within the jet pipe 13 upstream of the combustion zone and swirl vanes 16 are disposed at the upstream end of the casing through which passes sufficient gaseous fluid containing oxygen for the combustion of a pilot supply of fuel, an igniter 17 for the pilot fuel supply being disposed within the casing and the main portion of the fuel being supplied to the gaseous fluid outside the casing. The casing 11 is frustro-conical in shape gradually diverging downstream and has a baffle 15 at the upstream end connected with the casing by the swirl vanes, the igniter 17 being disposed centrally in the baffle. The casing is connected to the jet pipes by three or more webs 12 and fuel is supplied from the annular pipe 26 through the pipe 21 to the pilot jets 22, and through radially-disposed pipes 25 to the main fuel jets 27. The main fuel pipes 25 may be disposed at the downstream end of the casing, and the supporting webs 12 may have spoilers at their downstream edges to promote turbulence. A plurality of similar casings 11 may be used' in the case of a larger diameter jet pipe. Both the main and pilot supplies of fuel may be admixed with a portion of the gaseous fluid or with air from the compressor; alternatively only the main supply may be supplied in either of these ways, the pilot supply being delivered as neat fuel. Specifications 624,726, [Group XI], and 659,859 are referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB295488X | 1949-11-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB674641A true GB674641A (en) | 1952-06-25 |
Family
ID=10293275
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30699/49A Expired GB674641A (en) | 1949-11-30 | 1949-11-30 | Fuel-burning means for a gaseous-fluid propulsion jet |
Country Status (4)
Country | Link |
---|---|
CH (1) | CH295488A (en) |
DE (1) | DE846343C (en) |
FR (1) | FR1024777A (en) |
GB (1) | GB674641A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3931707A (en) * | 1975-01-08 | 1976-01-13 | General Electric Company | Augmentor flameholding apparatus |
FR2429326A1 (en) * | 1978-06-22 | 1980-01-18 | Snecma | IMPROVEMENTS IN FLAME-HANGING DEVICES FOR COMBUSTION CHAMBERS, IN PARTICULAR FOR TURBO-JET POST-COMBUSTION CHANNELS |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1074920B (en) * | 1955-07-07 | 1960-02-04 | Ing habil Fritz A F Schmidt Murnau Dr (Obb) | Method and device for regulating gas turbine combustion chambers with subdivided combustion and several pressure levels |
DE1051071B (en) * | 1955-07-13 | 1959-02-19 | Sud Aviation | Combustion device for supersonic ramjet engines |
DE1053872B (en) * | 1957-03-20 | 1959-03-26 | Armstrong Siddeley Motors Ltd | Combustion device for fuel, especially for afterburning in jet engines |
US2958196A (en) * | 1959-01-02 | 1960-11-01 | Gen Electric | Flame igniter for gas turbine combustor |
-
1949
- 1949-11-30 GB GB30699/49A patent/GB674641A/en not_active Expired
-
1950
- 1950-09-14 CH CH295488D patent/CH295488A/en unknown
- 1950-09-21 FR FR1024777D patent/FR1024777A/en not_active Expired
- 1950-10-19 DE DEA4724A patent/DE846343C/en not_active Expired
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3931707A (en) * | 1975-01-08 | 1976-01-13 | General Electric Company | Augmentor flameholding apparatus |
FR2429326A1 (en) * | 1978-06-22 | 1980-01-18 | Snecma | IMPROVEMENTS IN FLAME-HANGING DEVICES FOR COMBUSTION CHAMBERS, IN PARTICULAR FOR TURBO-JET POST-COMBUSTION CHANNELS |
Also Published As
Publication number | Publication date |
---|---|
CH295488A (en) | 1953-12-31 |
FR1024777A (en) | 1953-04-07 |
DE846343C (en) | 1952-08-11 |
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