GB827741A - Improvements in or relating to gas turbine plant - Google Patents
Improvements in or relating to gas turbine plantInfo
- Publication number
- GB827741A GB827741A GB1718556A GB1718556A GB827741A GB 827741 A GB827741 A GB 827741A GB 1718556 A GB1718556 A GB 1718556A GB 1718556 A GB1718556 A GB 1718556A GB 827741 A GB827741 A GB 827741A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas
- turbine
- combustion chamber
- pressure exchanger
- exchanger
- 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
- F02C3/02—Gas-turbine plants characterised by the use of combustion products as the working fluid using exhaust-gas pressure in a pressure exchanger to compress combustion-air
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Cyclones (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
827,741. Gas turbine plant. SPALDING, D. B. May 28, 1957 [June 4, 1956], No. 17185/56. Drawings to Specification. Class 110 (3). [Also in Group XXVIII] A gas turbine is supplied with motive gas substantially free from impurities harmful to the turbine by a pressure exchanger which feeds gas to a combustion chamber which in one embodiment feeds combustion products to a gas cleaner, in the form of a cyclone separator, which passes clean gas to the turbine and polluted gas to the pressure exchanger. In another embodiment the combustion products pass through the hot pass of a heat exchanger while clean gas from the pressure exchanger passes through the cold pass to the turbine. The heat exchanger and combustion chamber may be structurally combined. Further heat exchangers may be provided to heat the gas to the combustion chamber by the exhaust gases from the turbine and pressure exchanger.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1718556A GB827741A (en) | 1956-06-04 | 1956-06-04 | Improvements in or relating to gas turbine plant |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1718556A GB827741A (en) | 1956-06-04 | 1956-06-04 | Improvements in or relating to gas turbine plant |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB827741A true GB827741A (en) | 1960-02-10 |
Family
ID=10090754
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1718556A Expired GB827741A (en) | 1956-06-04 | 1956-06-04 | Improvements in or relating to gas turbine plant |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB827741A (en) |
-
1956
- 1956-06-04 GB GB1718556A patent/GB827741A/en not_active Expired
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