Combustion Chamber of WERKSPOOR W72M Gas Turbine
Application:
In ferrous and non-ferrous metal industries, as a passage for the melt
Product Introduction:
In gas turbines, after leaving the compressor and distributor, the compressed air enters another part, where it is mixed with the appropriate amount of fuel and ignited, increasing the kinetic energy of the air passing through the engine.
Some of this energy is used to turn the turbine and compressor, and the rest is sent out as high-speed gases from the outlet opening and creates driving force.
The combustion chamber is one of the most important and complex parts of the gas turbine, where the heat added in the Brayton cycle enters the process.
The temperature of the air entering the combustion chamber depends on the pressure, the operating load of the turbine and the type of machine and whether or not it is regenerated and can vary between 350 and 860 degrees Celsius.
Also, the temperature of the gas exiting the combustion chamber will vary between 1000 and 1650 degrees Celsius depending on the turbine and its class in different parts of the chamber.
Technical Specifications:
Turbine power |
8530 hp |
Fuel |
Natural gas |
The mass flow rate of gas exiting the turbine |
123 lb/s |
Power turbine rotor speed |
5200 rpm |
Number per turbine |
6 sets |
Company | |
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Type | This product is a final B2B equipment. |