GB710586A - Liquid fuel burner nozzles - Google Patents
Liquid fuel burner nozzlesInfo
- Publication number
- GB710586A GB710586A GB651052A GB651052A GB710586A GB 710586 A GB710586 A GB 710586A GB 651052 A GB651052 A GB 651052A GB 651052 A GB651052 A GB 651052A GB 710586 A GB710586 A GB 710586A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- annular
- nozzle
- liquid fuel
- march
- 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
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/38—Nozzles; Cleaning devices therefor
- F23D11/383—Nozzles; Cleaning devices therefor with swirl means
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
710,586. Nozzles. LUCAS (INDUSTRIES), Ltd., J. March 6, 1953 [March 13, 1952], No. 6510/52. Class 69 (3). [Also in Group XI] A liquid fuel burner nozzle of the swirl type has an annular discharge orifice d and coaxial therewith a fuel inlet b both disposed at the same end of the nozzle, whereby the nozzle may be used in a gas turbine engine for discharging fuel upstream whilst being supplied with fuel through an axially disposed pipe. The fuel inlet b passes axially into a cylindrical part a and communicates through radial bores j in the latter with an annular space between the part a and a sleeve h screwed thereon to hold an intermediate annular part e on the part a. From said annular space the fuel passes through tangential passages k in the part e to a swirl chamber f to discharge through the orifice d. The latter is formed between the outer end of the part e and an annular ridge c on the part a.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB651052A GB710586A (en) | 1952-03-13 | 1952-03-13 | Liquid fuel burner nozzles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB651052A GB710586A (en) | 1952-03-13 | 1952-03-13 | Liquid fuel burner nozzles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB710586A true GB710586A (en) | 1954-06-16 |
Family
ID=9815828
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB651052A Expired GB710586A (en) | 1952-03-13 | 1952-03-13 | Liquid fuel burner nozzles |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB710586A (en) |
-
1952
- 1952-03-13 GB GB651052A patent/GB710586A/en not_active Expired
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