The project contains the design and validation of a dual-fuel capable combustion chamber as well as the necessary dual-fuel injector. The injector requires two separate fuel paths and have to be ...

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 ...

From there, it's pushed into the combustion chamber, where the hot air is mixed with jet fuel and ignited. Ignition creates an explosion that generates thrust through one or more turbines and ...