GB625087A - Improvements in and relating to internal combustion turbine engines - Google Patents
Improvements in and relating to internal combustion turbine enginesInfo
- Publication number
- GB625087A GB625087A GB932345A GB932345A GB625087A GB 625087 A GB625087 A GB 625087A GB 932345 A GB932345 A GB 932345A GB 932345 A GB932345 A GB 932345A GB 625087 A GB625087 A GB 625087A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- turbine
- pressure
- low
- turbines
- 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 title abstract 2
- 235000013175 Crataegus laevigata Nutrition 0.000 abstract 1
- 239000000567 combustion gas Substances 0.000 abstract 1
- 238000001816 cooling Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
- 238000003303 reheating Methods 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
- F02C6/003—Gas-turbine plants with heaters between turbine stages
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)
Abstract
625,087. Gas turbines. POWER JETS (RESEARCH & DEVELOPMENT), Ltd.. and HAWTHORNE, W. R. April 13, 1945, No. 9323. Drawings to Specification. [Class 110(iii)] In a three-stage continuous combustion gas turbine in which the low-pressure turbine drives the low-pressure compressor,. the intermediate turbine drives the intermediate compressor and the high-pressure turbine drives the high-pressure compressor, these parts are disposed serially along their common axis in the following order:-the low-pressure turbine, the lowpressure compressor, the intermediate compressor, the intermediate turbine, the high-pressure turbine and the highpressure compressor. The ductings connecting the intermediate and high-pressure compressor surround the intermediate and high-pressure turbines and the ductings connecting the intermediate and lowpressure turbines surround the intermediate and low-pressure compressors. Reheating combustion may be provided between the turbine stages and cooling between the compressor stages. Useful power may be taken off any compressor turbine or a separate power turbine may be provided. The energy of the exhaust may be used for jet-propulsion. Specification 478,688 is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB932345A GB625087A (en) | 1945-04-13 | 1945-04-13 | Improvements in and relating to internal combustion turbine engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB932345A GB625087A (en) | 1945-04-13 | 1945-04-13 | Improvements in and relating to internal combustion turbine engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB625087A true GB625087A (en) | 1949-06-22 |
Family
ID=9869744
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB932345A Expired GB625087A (en) | 1945-04-13 | 1945-04-13 | Improvements in and relating to internal combustion turbine engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB625087A (en) |
-
1945
- 1945-04-13 GB GB932345A patent/GB625087A/en not_active Expired
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