Fuel nozzle for multifuel fuel delivery system

An apparatus for an aircraft powerplant, comprising:

• a fuel nozzle extending longitudinally along a centerline to a distal end, the fuel nozzle including a plurality of first fuel passages, a plurality of second fuel passages, a first fuel gallery, a second fuel gallery, an annular passage and a nozzle outlet disposed at the distal end of the fuel nozzle;
• the plurality of first fuel passages arranged circumferentially about the centerline, each of the plurality of first fuel passages extending within the fuel nozzle from the first fuel gallery to the annular passage;
• the plurality of second fuel passages arranged circumferentially about the centerline, each of the plurality of second fuel passages extending within the fuel nozzle from the second fuel gallery to the annular passage;
• and
• the annular passage extending circumferentially around the centerline, the annular passage fluidly coupling the plurality of first fuel passages and the plurality of second fuel passages to the nozzle outlet, and the annular passage radially tapering towards the centerline as the annular passage extends longitudinally towards the nozzle outlet.

An apparatus for an aircraft powerplant, comprising:

• a fuel nozzle extending longitudinally along a centerline to a distal end, the fuel nozzle including a plurality of first fuel passages, a plurality of second fuel passages, an annular passage and a nozzle outlet disposed at the distal end of the fuel nozzle;
• the plurality of first fuel passages arranged circumferentially about the centerline, each of the plurality of first fuel passages extending within the fuel nozzle, in a radial inward direction towards the centerline, to the annular passage;
• the plurality of second fuel passages arranged circumferentially about the centerline, each of the plurality of second fuel passages extending within the fuel nozzle, in a longitudinal direction towards the distal end of the fuel nozzle, to the annular passage;
• and
• the annular passage extending circumferentially around the centerline, the annular passage fluidly coupling the plurality of first fuel passages and the plurality of second fuel passages to the nozzle outlet, and the annular passage radially tapering towards the centerline as the annular passage extends longitudinally to the nozzle outlet.