GB839267A - Liquid fuel combustion apparatus - Google Patents
Liquid fuel combustion apparatusInfo
- Publication number
- GB839267A GB839267A GB3709557A GB3709557A GB839267A GB 839267 A GB839267 A GB 839267A GB 3709557 A GB3709557 A GB 3709557A GB 3709557 A GB3709557 A GB 3709557A GB 839267 A GB839267 A GB 839267A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- passage
- nozzle
- surrounding
- liquid fuel
- 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
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C7/00—Combustion apparatus characterised by arrangements for air supply
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
- F23C7/004—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion using vanes
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
839,267. Liquid fuel spray burners. LUCAS (INDUSTRIES) Ltd., J. Nov. 27, 1958 [Nov. 28, 1957]. No. 37095/57. Class 75(1) [Also in Group XII] A liquid fuel combustion apparatus comprising a sheet metal combustion chamber a having at its entrance end a fuel spraying nozzle c, an annular air passage b, an air jacket d surrounding the chamber a and a radial flow air swirler e located in the air jacket d adjacent the air passage b has an axially disposed member f located adjacent the air swirler e and surrounding the. nozzle c to prevent premature entrainment of the fuel into the swirling air stream. In the arrangement shown the member f is hollow and its interior is fed with air from a passage g. the air passing, in a swirling condition, through obliquely disposed slots h each slot of which has a lip k provided on one edge to promote the swirling action. A further passage m leads air to a narrow annular passage n surrounding the nozzle c and to a part o from which air. flows through passages in the body of the nozzle c.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3709557A GB839267A (en) | 1957-11-28 | 1957-11-28 | Liquid fuel combustion apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3709557A GB839267A (en) | 1957-11-28 | 1957-11-28 | Liquid fuel combustion apparatus |
Publications (1)
Publication Number | Publication Date |
---|---|
GB839267A true GB839267A (en) | 1960-06-29 |
Family
ID=10393681
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3709557A Expired GB839267A (en) | 1957-11-28 | 1957-11-28 | Liquid fuel combustion apparatus |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB839267A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3224682A (en) * | 1961-05-03 | 1965-12-21 | Paris Jean Camille Hippolyte | Oil burner apparatus |
DE1273110B (en) * | 1963-10-18 | 1968-07-18 | Kaercher Fa Alfred | Burner for fuel to be atomized |
US3767122A (en) * | 1971-08-10 | 1973-10-23 | Lucas Aerospace Ltd | Flame tubes |
FR2406726A1 (en) * | 1977-10-21 | 1979-05-18 | Rolls Royce | PERFECTED COMBUSTION EQUIPMENT FOR GAS TURBINE ENGINES |
-
1957
- 1957-11-28 GB GB3709557A patent/GB839267A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3224682A (en) * | 1961-05-03 | 1965-12-21 | Paris Jean Camille Hippolyte | Oil burner apparatus |
DE1273110B (en) * | 1963-10-18 | 1968-07-18 | Kaercher Fa Alfred | Burner for fuel to be atomized |
US3767122A (en) * | 1971-08-10 | 1973-10-23 | Lucas Aerospace Ltd | Flame tubes |
FR2406726A1 (en) * | 1977-10-21 | 1979-05-18 | Rolls Royce | PERFECTED COMBUSTION EQUIPMENT FOR GAS TURBINE ENGINES |
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