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 ...

Hydrogen burns much hotter than natural gas and has a lower flash point, which can easily damage a micro-turbine’s combustion chamber with intense heat and shockwaves. To address this ...

This resulted in a pure hydrogen gas turbine combustion chamber design and control technology with independent intellectual property rights. A 30MW pure hydrogen gas turbine unit can effectively ...