FUEL NOZZLES ASSEMBLY FOR A GAS TURBINE ENGINE

A nozzle assembly (100) includes a fuel distributor (108) for issuing a spray of fuel. A fuel conduit (106) is in fluid communication with the fuel distributor (108) and has a first end and a second end. The first end and/or the second end of the fuel conduit (106) is operatively connected to the fuel distributor (108). The fuel conduit (106) is configured to allow relative movement between the first end and the second end to accommodate dimensional variations of at least one of the nozzle assembly (100) or a combustor. A nozzle system (101) includes the nozzle assembly (100) and a combustor wall (28) having a nozzle inlet (124). The nozzle assembly (100) is positioned adjacent to the nozzle inlet (124).