| 摘要 |
<p>In one embodiment, a system includes a turbine (20) engine (10) fuel nozzle (12) having an air path, a fuel path, and a surface along the air path. The fuel path may be directed toward the surface. The turbine (20) engine (10) fuel nozzle (12) also may include a heating element (13, 79, 84, 122, 142, 152) configured to heat the surface.
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