| 摘要 |
<p>A gas fuel turbine engine (100) may include a gaseous pilot fuel supply, a first main fuel supply, and a second main fuel supply. The first main fuel supply may provide gaseous fuel to a first plurality of fuel injectors (30), and the second main fuel supply may provide gaseous fuel to a second plurality of fuel injectors. The turbine engine may also include a flow restriction (140) provided in the first main fuel supply. The second main fuel supply may be free of the flow restriction.</p> |
