ES353520A1 - Hot gas generators - Google Patents
Hot gas generatorsInfo
- Publication number
- ES353520A1 ES353520A1 ES353520A ES353520A ES353520A1 ES 353520 A1 ES353520 A1 ES 353520A1 ES 353520 A ES353520 A ES 353520A ES 353520 A ES353520 A ES 353520A ES 353520 A1 ES353520 A1 ES 353520A1
- Authority
- ES
- Spain
- Prior art keywords
- compressor
- rotor
- shaft
- combustion chamber
- duct
- 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
- 238000002485 combustion reaction Methods 0.000 abstract 3
- 239000000567 combustion gas Substances 0.000 abstract 2
- 238000010790 dilution Methods 0.000 abstract 2
- 239000012895 dilution Substances 0.000 abstract 2
- 239000000203 mixture Substances 0.000 abstract 2
- 230000004323 axial length Effects 0.000 abstract 1
- 238000007599 discharging Methods 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/04—Gas-turbine plants providing heated or pressurised working fluid for other apparatus, e.g. without mechanical power output
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
A combustion gas generator comprises a shaft 11 supported in bearings 10 intermediate its ends, a first radial flow compressor rotor 16 and a second radial flow compressor rotor 17 mounted in back-to-back relationship at one end of the shaft, the compressors supplying air and dilution air respectively to a combustion chamber 20, the combustion gases from which pass to a turbine 12 mounted at the other end of the shaft the gases discharging from the turbine through duct 14 to a point of use. A carburetter 25 is disposed in the inlet duct 24 of the first compressor 16 so that a fuel and air mixture is supplied to the compressor, the mixture being discharged through a burner device 21 into the combustion chamber. In Fig. 1 the two compressor rotors are mounted in separate casings in back-to-back relation whereas in Fig.2 (not shown), the two compressor rotors are mounted back-to-back on a common disc. The dilution air delivered by compressor 17 passes through duct 22 to the combustion chamber. The diameter of the first compressor rotor is greater than that of the second rotor and the axial length of the first rotor is less than that of the second rotor.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1943967A GB1222083A (en) | 1967-04-27 | 1967-04-27 | Hot gas generators |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ES353520A1 true ES353520A1 (en) | 1969-10-01 |
Family
ID=10129403
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| ES353520A Expired ES353520A1 (en) | 1967-04-27 | 1968-04-26 | Hot gas generators |
Country Status (8)
| Country | Link |
|---|---|
| AT (1) | AT293795B (en) |
| BE (1) | BE714317A (en) |
| CH (1) | CH471319A (en) |
| DE (2) | DE6606749U (en) |
| ES (1) | ES353520A1 (en) |
| FR (1) | FR1560946A (en) |
| GB (1) | GB1222083A (en) |
| NL (1) | NL6806001A (en) |
-
1967
- 1967-04-27 GB GB1943967A patent/GB1222083A/en not_active Expired
-
1968
- 1968-04-26 ES ES353520A patent/ES353520A1/en not_active Expired
- 1968-04-26 AT AT406768A patent/AT293795B/en not_active IP Right Cessation
- 1968-04-26 NL NL6806001A patent/NL6806001A/xx unknown
- 1968-04-26 CH CH622768A patent/CH471319A/en not_active IP Right Cessation
- 1968-04-26 FR FR1560946D patent/FR1560946A/fr not_active Expired
- 1968-04-26 BE BE714317D patent/BE714317A/xx unknown
- 1968-04-27 DE DE19686606749 patent/DE6606749U/en not_active Expired
- 1968-04-27 DE DE19681751253 patent/DE1751253A1/en active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| AT293795B (en) | 1971-10-25 |
| GB1222083A (en) | 1971-02-10 |
| BE714317A (en) | 1968-09-16 |
| CH471319A (en) | 1969-04-15 |
| NL6806001A (en) | 1968-10-28 |
| FR1560946A (en) | 1969-03-21 |
| DE1751253A1 (en) | 1970-09-17 |
| DE6606749U (en) | 1970-12-17 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3010281A (en) | Toroidal combustion chamber | |
| GB1135129A (en) | Gas turbine engine | |
| US2823520A (en) | Combustion equipment and gas turbine plant | |
| GB774425A (en) | Improvements in or relating to turbine engines | |
| GB801281A (en) | Improvements in or relating to reaction turbines | |
| GB1225759A (en) | ||
| GB935903A (en) | Gas turbine power plant having centripetal flow compressors and centrifugal flow turbines | |
| GB1331446A (en) | Hot gas generators | |
| GB891278A (en) | A gas turbine power unit | |
| ES353520A1 (en) | Hot gas generators | |
| US3015211A (en) | Radial turbine engine | |
| GB1222085A (en) | Hot gas generators | |
| GB931105A (en) | Improvements in combustion apparatus | |
| GB820337A (en) | Improvements in and relating to gas turbines | |
| GB1222082A (en) | Hot gas generators | |
| US3498593A (en) | Hot gas generators | |
| US2750738A (en) | Compound gas turbine plant, including simplified ducting arrangements | |
| GB1219909A (en) | Hot gas generators | |
| GB706841A (en) | Improvements relating to turbine jet propulsion power units | |
| GB1056338A (en) | Apparatus for supplying heated gases | |
| GB805003A (en) | Improvements in and relating to inlet duct arrangements for gas turbines and compressors | |
| GB694414A (en) | Improvements in or relating to internal combustion gas turbine engines | |
| GB619232A (en) | Improvements in or relating to gas turbine plants | |
| GB791917A (en) | Improvements in and relating to gas turbine plants | |
| GB780835A (en) | Improvements relating to combustion equipment for gas-turbine engines and fuel injection means therefor |