| 摘要 |
The Invention relates to a fuel Injector (1) for the supply of fuel into a g as turbine rotor (B). It solves the technical problem of injecting fuel continuously into a rotating hollow rotor (B) without loss. This is achieved by shaping the nozzle (3) of the fu el injector (1) in such a way, that fuel escaping through the gap (2) between the static fuel injector nozzle (3) and the rotating fuel intake nozzle (8) is sucked into the hollow rotor (B) via an air intake port (15).
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