Invention Grant
US07694899B2 Fuel injection device for an aircraft gas turbine 失效
用于飞机燃气轮机的燃油喷射装置

Fuel injection device for an aircraft gas turbine
Abstract:
A fuel injection device for fuel injection systems, e.g. for aircraft gas turbines, includes at least one fuel injection opening, through which a continuous flow of fuel 1 is issued, with the fuel injection opening having a non-circular cross-section.
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