GB586602A - Improvements in regenerative gas turbine plants - Google Patents
Improvements in regenerative gas turbine plantsInfo
- Publication number
- GB586602A GB586602A GB1414944A GB1414944A GB586602A GB 586602 A GB586602 A GB 586602A GB 1414944 A GB1414944 A GB 1414944A GB 1414944 A GB1414944 A GB 1414944A GB 586602 A GB586602 A GB 586602A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- turbine
- regenerative gas
- air
- turbine plants
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/08—Heating air supply before combustion, e.g. by exhaust gases
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
586,602. Gas turbines. SMITH, D. M., and METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. July 24, 1944, No. 14149. [Class 110 (iii)] The air from the compressor 1 driven by the gas turbine 3, is divided to flow in two channels, one to the inner or primary combustion chamber 4b wherein are located the fuel nozzles 4a and the other to the heat exchanger 6 in the turbine exhaust passage 7 and thence to the " secondary " combustion chamber, or cooling space 4c. The two streams mix at the outlet of the primary chamber and flow together to the turbine 3. In a modification, part of the " secondary " air. passes direct to the " secondary " combustion through pipes 5c. Specification 585,959 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1414944A GB586602A (en) | 1944-07-24 | 1944-07-24 | Improvements in regenerative gas turbine plants |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1414944A GB586602A (en) | 1944-07-24 | 1944-07-24 | Improvements in regenerative gas turbine plants |
Publications (1)
Publication Number | Publication Date |
---|---|
GB586602A true GB586602A (en) | 1947-03-25 |
Family
ID=10035898
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1414944A Expired GB586602A (en) | 1944-07-24 | 1944-07-24 | Improvements in regenerative gas turbine plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB586602A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2975596A (en) * | 1957-02-04 | 1961-03-21 | Adolphe C Peterson | Counter flow regenerative gas turbines |
US3705492A (en) * | 1971-01-11 | 1972-12-12 | Gen Motors Corp | Regenerative gas turbine system |
US3826078A (en) * | 1971-12-15 | 1974-07-30 | Phillips Petroleum Co | Combustion process with selective heating of combustion and quench air |
-
1944
- 1944-07-24 GB GB1414944A patent/GB586602A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2975596A (en) * | 1957-02-04 | 1961-03-21 | Adolphe C Peterson | Counter flow regenerative gas turbines |
US3705492A (en) * | 1971-01-11 | 1972-12-12 | Gen Motors Corp | Regenerative gas turbine system |
US3826078A (en) * | 1971-12-15 | 1974-07-30 | Phillips Petroleum Co | Combustion process with selective heating of combustion and quench air |
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