Invention Grant
US08205452B2 Apparatus for fuel injection in a turbine engine 有权
涡轮发动机燃料喷射装置

Apparatus for fuel injection in a turbine engine
Abstract:
In one embodiment, a system includes a fuel nozzle that includes a fuel injector configured to output a fuel flow and a premixer tube disposed about the fuel flow output from the fuel injector. The premixer tube includes a perforated portion and a non-perforated portion, and the non-perforated portion is downstream of the perforated portion.
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