Patent ID: 11073089

Abstract:
A gas turbine engine for an aircraft that includes an engine core, a fan, and a planetary gearbox. The planetary gearbox includes a sun gear, a plurality of planetary gears, a ring gear, a plurality of planetary pins, wherein respectively one planetary pin is arranged in a planetary gear, and an axially frontal support plate and an axially rear support plate, wherein the planetary pins are arranged in openings of the axially frontal support plate and of the axially rear support plate, and are connected to the support plates. At least one of the support plates has an axially protruding first centering collar that engages around the opening for the planetary pin, and that a second centering collar that is connected to the planetary pin or is formed in one piece with the same, engaging around the first centering collar radially outside in a form-fit manner. A planetary gearbox and an attachment arrangement.