GB1135104A - Combustion equipment - Google Patents
Combustion equipmentInfo
- Publication number
- GB1135104A GB1135104A GB44215/66A GB4421566A GB1135104A GB 1135104 A GB1135104 A GB 1135104A GB 44215/66 A GB44215/66 A GB 44215/66A GB 4421566 A GB4421566 A GB 4421566A GB 1135104 A GB1135104 A GB 1135104A
- Authority
- GB
- United Kingdom
- Prior art keywords
- vaporizing
- fuel
- air
- vaporized
- annular
- 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
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Spray-Type Burners (AREA)
Abstract
1,135,104. Gas turbine engine combustion equipment. ISHIKAWAJIMA-HARIMA JUKOGYO K.K. Oct.4, 1966 [Oct. 5, 1965], No.44215/66. Heading F1L. [Also in Division F4] Combustion equipment for example for a gas turbine engine, comprises a vaporizing surface located within the combustion chamber and defining a fuel vaporizing chamber, inlets being provided for supply of fuel and air into the vaporizing chamber and guide means for directing the mixture of vaporized fuel and air to flow from the vaporizing chamber adjacent the outer surface thereof so that when the mixture is burned, the vaporizing chamber is heated and the liquid fuel therein is vaporized. The combustion equipment shown comprises an annular flame tube 2 disposed within an annular air casing 1 having an annular air inlet 8. The flame tube comprises a pair of annular vaporizing surfaces 3, 3' between which is disposed a dividing member 5 so as to provide two fuel vaporizing chambers which are heated by combustion occurring at the vortex zones 10, 10', Fig. 3. Air flows into the vapourizing chambers between the 9, 9' and fuel is supplied thereto from manifolds 4, 4' having discharge orifices 7, 7'. As the liquid fuel flows through the vaporizing chambers it becomes vaporized and the mixture of air and vaporized fuel is directed by the guides 6, 6' to flow upstream along the outer surfaces of the vaporizing members 3, 3'. Additional air inlets 11, 11' and 12, 12' are provided in the flame tube wall. In a further embodiment Fig. 5 (not shown), six concentric vaporizing members are provided.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP6086865 | 1965-10-05 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1135104A true GB1135104A (en) | 1968-11-27 |
Family
ID=13154781
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB44215/66A Expired GB1135104A (en) | 1965-10-05 | 1966-10-04 | Combustion equipment |
Country Status (2)
Country | Link |
---|---|
US (1) | US3398528A (en) |
GB (1) | GB1135104A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4742684A (en) * | 1981-12-24 | 1988-05-10 | Rolls-Royce Plc | Fuel vaporizers for a gas turbine engine combustion engine |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3890088A (en) * | 1970-09-17 | 1975-06-17 | Advanced Tech Lab | Apparatus for reducing formation of oxides of nitrogen in combustion processes |
US4262482A (en) * | 1977-11-17 | 1981-04-21 | Roffe Gerald A | Apparatus for the premixed gas phase combustion of liquid fuels |
US4242863A (en) * | 1978-03-16 | 1981-01-06 | Caterpillar Tractor Co. | Dual phase fuel vaporizing combustor |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2541900A (en) * | 1948-12-24 | 1951-02-13 | A V Roe Canada Ltd | Multiple fuel jet burner and torch igniter unit with fuel vaporizing tubes |
US2635426A (en) * | 1949-06-29 | 1953-04-21 | A V Roe Canada Ltd | Annular vaporizer |
BE504870A (en) * | 1950-07-27 | |||
US2982098A (en) * | 1953-04-22 | 1961-05-02 | Power Jets Res & Dev Ltd | Liquid fuel vaporizing combustion systems |
-
1966
- 1966-10-03 US US583574A patent/US3398528A/en not_active Expired - Lifetime
- 1966-10-04 GB GB44215/66A patent/GB1135104A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4742684A (en) * | 1981-12-24 | 1988-05-10 | Rolls-Royce Plc | Fuel vaporizers for a gas turbine engine combustion engine |
Also Published As
Publication number | Publication date |
---|---|
US3398528A (en) | 1968-08-27 |
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