GB802477A - Improvements in hot air turbines - Google Patents
Improvements in hot air turbinesInfo
- Publication number
- GB802477A GB802477A GB2804655A GB2804655A GB802477A GB 802477 A GB802477 A GB 802477A GB 2804655 A GB2804655 A GB 2804655A GB 2804655 A GB2804655 A GB 2804655A GB 802477 A GB802477 A GB 802477A
- Authority
- GB
- United Kingdom
- Prior art keywords
- passage
- flow
- blading
- combustion chamber
- gas turbine
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/045—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
- F02C3/05—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
802,477. Gas turbine plant. JOHNSTON, J. Oct. 2, 1956 [Oct. 3, 1955], No. 28046/55. Class 110 (3). [Also in Groups XII and XXIX] In a gas turbine plant of the type in which jets of fuel are injected into a mechanically produced stream of air, and in which the fuel ignition is such as to cause successive explosions in the stream, the flow passage ahead of the turbine divides into two branches, one of which passes through a device for preventing back flow and then through a combustion chamber and ends in a nozzle which discharges centrally into the other branch, the passage then continuing as a single straight passage. In the intermittentcombustion gas turbine engine shown, centrifugal compressor blading 6 supplies air through a tangential passage 13 to a combustion chamber 14. Fuel is supplied through an injector 16 and ignited by a plug 17. An aerodynamic valve 15 at the inlet to the flame tube 21 of the combustion chamber opposes back flow during combustion. After leaving the flame tube, the combustion gases are joined, at an injector-like portion 20 of the flow passage, by air which has by-passed the flame tube, and flow tangentially into an annular passage 18. In rotating around the passage 18, the gases acquire a uniform condition free from pulsation before entering inward-flow turbine blading 7. The blading 6, 7 are arranged on opposite sides of a common rotor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2804655A GB802477A (en) | 1955-10-03 | 1955-10-03 | Improvements in hot air turbines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB2804655A GB802477A (en) | 1955-10-03 | 1955-10-03 | Improvements in hot air turbines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB802477A true GB802477A (en) | 1958-10-08 |
Family
ID=10269386
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB2804655A Expired GB802477A (en) | 1955-10-03 | 1955-10-03 | Improvements in hot air turbines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB802477A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2301630A (en) * | 1995-06-01 | 1996-12-11 | Bridge Butler James Alexander | Internal combustion turbine engine |
-
1955
- 1955-10-03 GB GB2804655A patent/GB802477A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2301630A (en) * | 1995-06-01 | 1996-12-11 | Bridge Butler James Alexander | Internal combustion turbine engine |
| GB2301630B (en) * | 1995-06-01 | 1999-12-29 | Bridge Butler James Alexander | Internal combustion turbine engine |
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