主权项 |
1. A system for providing fuel to a combustor of a gas turbine, the system comprising:
a. an annular fuel distribution manifold, the fuel distribution manifold at least partially defining a fuel plenum, the fuel distribution manifold having a forward end axially separated from an aft end, a flange that extends radially outward and circumferentially around the forward end and an annular support ring that extends downstream from the flange; b. a LLI injection assembly that extends downstream from the fuel distribution manifold, the LLI injection assembly having a unibody liner that at least partially defines a primary combustion zone and a secondary combustion zone, a LLI injector that extends substantially radially through the unibody liner and that provides for fluid communication through the unibody liner into the combustion secondary combustion zone; and c. a fluid conduit that extends between the LLI injector and the fuel distribution manifold, the fluid conduit being in fluid communication with the fuel plenum. |