| 摘要 |
A turbine engine augmentor (32) has a centerbody (38) within a gas flowpath. A flameholder (42) is positioned in the flowpath outboard of the centerbody (38). A burner (62) within the centerbody (38) has an outlet for expelling combustion products of a first pilot fuel. A pilot fuel conduit (100) has an outlet positioned to introduce a supplemental pilot fuel to the expelled combustion products.
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