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 ...

In the high-pressure combustion chamber test rig (HBK-S), complex and multi-stage combustion chamber systems of the next generation can be analysed under conditions typical of gas turbines, i.e. at ...

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 ...

Also known as gas turbines, this modern-day engineering ... to maximize the amount of air that can be sucked into the combustion chamber of the engine. A direct result of this design is that ...