GB603640A - Improvements in and relating to combustion turbine plants - Google Patents
Improvements in and relating to combustion turbine plantsInfo
- Publication number
- GB603640A GB603640A GB18445/45A GB1844545A GB603640A GB 603640 A GB603640 A GB 603640A GB 18445/45 A GB18445/45 A GB 18445/45A GB 1844545 A GB1844545 A GB 1844545A GB 603640 A GB603640 A GB 603640A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas
- producer
- fuel
- air
- pressure
- 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
- F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
- F02C3/26—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension
- F02C3/28—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being solid or pulverulent, e.g. in slurry or suspension using a separate gas producer for gasifying the fuel before combustion
Abstract
603,640. Gas turbines. AKT.-GES. BROWN, BOVERI, & CIE. July 18, 1945, No. 18445. Convention date, Aug. 24, 1944. [Class 110 (iii)] In a gas-turbine plant in which the fuel gas is provided by a gas-producer 7, the pressuredrop in the gas-producer is balanced in the combustion air line by the pressure-drop in an exhaust gas heat-exchanger 2. The supply of fuel to the combustion chamber is regulated by a valve 9 controlled by a speed governor 10 and the valve is arranged to be partly closed under normal working conditions. In a twostage plant with reheating, the fuel for the re-heating combustion chamber is supplied by a second gas-producer receiving air from between the compressor stages, or, working fluid tapped from a turbine stage. The lowpressure turbine and compressor set is separately governed and the governor controls the supply of combustion air to the second gas-producer In addition to the useful employment of the pressure-drop in the combustion air line, the pressure of the air supply to the gas producer may be boosted by an additional stage to the air-compressor.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH603640X | 1944-08-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB603640A true GB603640A (en) | 1948-06-21 |
Family
ID=4522903
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB18445/45A Expired GB603640A (en) | 1944-08-24 | 1945-07-18 | Improvements in and relating to combustion turbine plants |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB603640A (en) |
-
1945
- 1945-07-18 GB GB18445/45A patent/GB603640A/en not_active Expired
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