This system can use natural gas, biogas and synthesis gas to operate a recuperated gas turbine with combustion chamber inlet temperatures of up to 700 °C and a pressure ratio of around 5. For the ...

This combustion concept is characterised by the injection of air-fuel mixtures into the combustion chamber in the form of jets with high flow velocities. The arrangement of the jets results in a ...

It has provided a special combustion chamber for the micro gas turbine plant. “We have contributed to technological adaptations of the fuel system and combustion chamber technology,” said ...

Also known as gas turbines, this modern-day engineering ... to maximize the amount of air that can be sucked into the ...