GB2004049A - Combustion apparatus vapourizers - Google Patents
Combustion apparatus vapourizersInfo
- Publication number
- GB2004049A GB2004049A GB7830386A GB7830386A GB2004049A GB 2004049 A GB2004049 A GB 2004049A GB 7830386 A GB7830386 A GB 7830386A GB 7830386 A GB7830386 A GB 7830386A GB 2004049 A GB2004049 A GB 2004049A
- Authority
- GB
- United Kingdom
- Prior art keywords
- duct
- chamber
- combustion apparatus
- air
- outlets
- 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.)
- Withdrawn
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
- F23D11/44—Preheating devices; Vaporising devices
- F23D11/441—Vaporising devices incorporated with burners
- F23D11/443—Vaporising devices incorporated with burners heated by the main burner flame
- F23D11/445—Vaporising devices incorporated with burners heated by the main burner flame the flame and the vaporiser not coming into direct contact
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Abstract
Combustion apparatus for gas turbine engines has an air-jacketed combustion chamber, a base plate 21 at the upstream end of the chamber having an inlet for fuel and air leading to a vapourizer comprising a hollow stem 20 contiguous at one end with the inlet and leading at its other end into a duct 24 transverse to the length of the stem, the free end of the duct being closed but the duct having a number of outlets 26 facing back toward the base plate 21 so that fuel/air mixture leaving the outlets impinges on the inside of the backplate and passes from there into the interior of the chamber. <IMAGE>
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7830386A GB2004049A (en) | 1977-07-20 | 1978-07-19 | Combustion apparatus vapourizers |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3040977 | 1977-07-20 | ||
GB7830386A GB2004049A (en) | 1977-07-20 | 1978-07-19 | Combustion apparatus vapourizers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB2004049A true GB2004049A (en) | 1979-03-21 |
Family
ID=26260432
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7830386A Withdrawn GB2004049A (en) | 1977-07-20 | 1978-07-19 | Combustion apparatus vapourizers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2004049A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2519079A1 (en) * | 1981-12-24 | 1983-07-01 | Rolls Royce | FUEL SPRAYER FOR COMBUSTION CHAMBER OF TURBOMACHINES |
FR3066009A1 (en) * | 2017-05-02 | 2018-11-09 | Safran Helicopter Engines | PREVAPORIZATION ROD FOR A TURBOMACHINE |
-
1978
- 1978-07-19 GB GB7830386A patent/GB2004049A/en not_active Withdrawn
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2519079A1 (en) * | 1981-12-24 | 1983-07-01 | Rolls Royce | FUEL SPRAYER FOR COMBUSTION CHAMBER OF TURBOMACHINES |
US4742684A (en) * | 1981-12-24 | 1988-05-10 | Rolls-Royce Plc | Fuel vaporizers for a gas turbine engine combustion engine |
FR3066009A1 (en) * | 2017-05-02 | 2018-11-09 | Safran Helicopter Engines | PREVAPORIZATION ROD FOR A TURBOMACHINE |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |