A late lean injection (LLI) manifold is provided and includes a central nozzle and first and second side nozzles positioned at circumferential locations defined around a vessel, a connector, a first leg, to which the connector is connected, formed to define a tube extending from the central nozzle to the first side nozzle such that fuel is communicable between the connector, the central nozzle and the first side nozzle and a second leg. The second leg is formed to define a tube extending from the central nozzle to the second side nozzle such that the fue...
1. Multiple late lean injection (LLI) manifolds for a gas turbine engine comprising multiple combustors and multiple transition pieces respectively disposed downstream from corresponding ones of the multiple combustors, each of the multiple LLI manifolds comprising: a central nozzle and first and second side nozzles positioned at circumferential locations defined around a downstream portion of a corresponding one of the multiple combustors or transition pieces;a connector receptive of fuel for the corresponding one of the multiple LLI manifolds from a pe...
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