GB597992A - Improvements in or relating to the pre-heating and vapourization of fuel for internal combustion reaction motors - Google Patents
Improvements in or relating to the pre-heating and vapourization of fuel for internal combustion reaction motorsInfo
- Publication number
- GB597992A GB597992A GB2197145A GB2197145A GB597992A GB 597992 A GB597992 A GB 597992A GB 2197145 A GB2197145 A GB 2197145A GB 2197145 A GB2197145 A GB 2197145A GB 597992 A GB597992 A GB 597992A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- combustion chamber
- vapourization
- perforated
- relating
- 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)
Abstract
597,992. Gas turbines. KNUDSEN, H. Aug. 27, 1945, No. 21971. [Class 110 (iii)] Liquid fuel is heated and vaporized before introduction to the combustion chamber of a continuous combustion gas turbine. Air from the compressor passes through an annular passage 12 to a combustion chamber 21. The fuel is pumped through a coiled pipe 16, where it receives heat from the compressed air, to a pipe 18 closed at the end but perforated as at 22 on both sides. The fuel escaping through the perforations falls on to the outside of the wall 20 of the combustion chamber and is vaporized. The vapour is drawn into the airstrea.m by means of venturi tubes 26 enclosing perforated nozzle parts 25. Many spaced and upwardly-inclined perforated baffles 29 are located on the outside of the combustion chamber.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB597992A true GB597992A (en) | 1948-02-09 |
Family
ID=1736616
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2197145A Expired GB597992A (en) | 1945-08-27 | Improvements in or relating to the pre-heating and vapourization of fuel for internal combustion reaction motors |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB597992A (en) |
-
1945
- 1945-08-27 GB GB2197145A patent/GB597992A/en not_active Expired
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