Pilot arrangement, nozzle device, production method, and gas turbine arrangement

A pilot arrangement for use in a nozzle device of a gas turbine arrangement, in particular of an aircraft engine, comprising

• a cavity, extending along a longitudinal axis, for conducting fuel, the narrowest flow cross section of which is larger than the largest flow cross section of a pilot line of a pilot fuel nozzle, and
• the pilot fuel nozzle, which adjoins the cavity in a downstream direction and comprises the pilot line and a pilot fuel outlet arranged at the downstream end of the pilot line,
• wherein the cavity is arranged in a central body arranged on the longitudinal axis, and wherein at least one swirling element is arranged circumferentially around the central body, wherein the central body and the at least one swirling element form a swirling arrangement, wherein the pilot arrangement is made up of two components, wherein a first component comprises the at least one swirling element and the central body, and a second component comprises the pilot fuel nozzle.