GB670968A - Vapourizing system for a gas turbine engine - Google Patents
Vapourizing system for a gas turbine engineInfo
- Publication number
- GB670968A GB670968A GB5028/49A GB502849A GB670968A GB 670968 A GB670968 A GB 670968A GB 5028/49 A GB5028/49 A GB 5028/49A GB 502849 A GB502849 A GB 502849A GB 670968 A GB670968 A GB 670968A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wall
- space
- air
- combustion
- combustion chamber
- 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
-
- 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)
- Pre-Mixing And Non-Premixing Gas Burner (AREA)
Abstract
670,968. Generating combustion products under pressure. MESCHINO, R. G., and ROE CANADA, Ltd., A. V. Feb. 15, 1950 [Feb. 24, 1949], No. 5028/49. Class 51 (i). [Also in Group XI] A vaporizing system for use in a gas turbine combustion chamber comprises an annular vaporizing space 25 formed between the wall 24 bounding the flame zone and another wall which may be the wall 20 of the flame tube, air and fuel being led into the vaporizing space and the vaporized mixture discharged therefrom being reversed in direction by the annular baffle 27 and flange 28. The combustion chamber shown is of the annular type and air enters the space 25 through the swirl vanes 26 and fuel enters through the nozzles 30, the mixture being heated by contact with the wall 24 which is heated by the combustion occurring at E. Further air enters the flame tube through the swirl vanes 26a and also through the holes 32, 33 in the downstream portion. The air-fuel mixture discharging from the space 25 as indicated by the arrows D, together with the air flowing in the direction of the arrows C, causes the vortex E which forms the core of combustion taking place in the flame tube. A tubular type combustion chamber may be employed.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB310945X | 1949-02-24 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB670968A true GB670968A (en) | 1952-04-30 |
Family
ID=10317866
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB5028/49A Expired GB670968A (en) | 1949-02-24 | 1949-02-24 | Vapourizing system for a gas turbine engine |
Country Status (2)
| Country | Link |
|---|---|
| CH (1) | CH310945A (en) |
| GB (1) | GB670968A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0074196A1 (en) * | 1981-09-04 | 1983-03-16 | General Motors Corporation | Gas turbine prechamber and fuel manifold structure |
| CN112082176A (en) * | 2020-09-14 | 2020-12-15 | 清华大学 | Combustion chamber structure of micro turbojet engine |
| CN115143489A (en) * | 2022-06-15 | 2022-10-04 | 南京航空航天大学 | Combustion chamber suitable for full-ring large-scale cyclone air intake |
-
1949
- 1949-02-24 GB GB5028/49A patent/GB670968A/en not_active Expired
-
1950
- 1950-02-23 CH CH310945D patent/CH310945A/en unknown
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0074196A1 (en) * | 1981-09-04 | 1983-03-16 | General Motors Corporation | Gas turbine prechamber and fuel manifold structure |
| CN112082176A (en) * | 2020-09-14 | 2020-12-15 | 清华大学 | Combustion chamber structure of micro turbojet engine |
| CN112082176B (en) * | 2020-09-14 | 2024-06-04 | 清华大学 | Combustion chamber of miniature turbojet engine |
| CN115143489A (en) * | 2022-06-15 | 2022-10-04 | 南京航空航天大学 | Combustion chamber suitable for full-ring large-scale cyclone air intake |
| CN115143489B (en) * | 2022-06-15 | 2023-08-11 | 南京航空航天大学 | Combustion chamber suitable for full-ring large-scale rotational flow air intake |
Also Published As
| Publication number | Publication date |
|---|---|
| CH310945A (en) | 1955-11-15 |
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