| 摘要 |
A fuel nozzle assembly (20) for a gas turbine, the assembly including: a cylindrical center body (50); a cylindrical shroud (46) coaxial with and extending around the center body (50), and a turning guide (42) having an downstream edge extending in a passage between the center body (50) and an inlet (56) to the shroud (46), wherein the turning guide (42) extends only partially around the center body (50). |
