Turbomachines and epicyclic gear assemblies with axially offset sun and ring gears

A turbomachine engine comprising:

• a fan assembly comprising a plurality of fan blades;
• a core engine comprising a turbine and an input shaft rotatable with the turbine;
• and
• a gear assembly configured to drive an input shaft at a first speed and drive an output shaft at a second speed that is slower than the first speed, the gear assembly comprising:
• a sun gear rotating about a longitudinal centerline of the gear assembly;
• a plurality of planet gears;
• a ring gear;
• a sun gear-mesh region along the longitudinal centerline of the gear assembly where the sun gear is configured to contact the plurality of planet gears;
• a ring gear-mesh region along the longitudinal centerline of the gear assembly where the ring gear is configured to contact the plurality of planet gears,
• wherein the sun gear-mesh region is axially offset from the ring gear-mesh region along the longitudinal centerline such that at least 50% of a width of the sun gear-mesh region does not axially overlap with the ring gear-mesh region,
• wherein the sun gear, the plurality of planet gears, and the ring gear mesh comprise double helical gears, and the sun gear comprises a first sun gear set and a second sun gear set, each of the plurality of planet gears comprise a first planet gear set and a second planet gear set, and the ring gear comprises a first ring gear set and a second ring gear set,
• wherein the first sun gear set and the second sun gear set are axially spaced apart from one another along the longitudinal centerline, and the first sun gear set and the second sun gear set are positioned between the first ring gear set and the second ring gear set, and
• wherein the fan assembly has a fan pressure ratio (FPR) for the fan assembly that is 1.04 to 1.10, as measured across the fan blades at a cruise flight condition.

A turbomachine engine comprising:

• a fan assembly comprising a plurality of fan blades;
• a core engine comprising a turbine and an input shaft rotatable with the turbine;
• and
• a single-stage epicyclic gear assembly that receives the input shaft at a first speed and drives an output shaft coupled to the fan assembly at a second speed, the second speed being slower than the first speed, the gear assembly comprising:
• a sun gear, a plurality of planet gears, and a ring gear, the sun gear rotating about a longitudinal centerline of the gear assembly;
• a sun gear-mesh region along the longitudinal centerline of the gear assembly where the sun gear is configured to contact the plurality of planet gears;
• a ring gear-mesh region along the longitudinal centerline of the gear assembly where the ring gear is configured to contact the plurality of planet gears,
• wherein the sun gear-mesh region is axially offset from the ring gear-mesh region along the longitudinal centerline such that at least 50% of a width of the sun gear-mesh region does not axially overlap with the ring gear-mesh region,
• wherein the sun gear, the plurality of planet gears, and the ring gear comprise double helical gears, and the sun gear comprises a first sun gear set and a second sun gear set, each of the plurality of planet gears comprise a first planet gear set and a second planet gear set, and the ring gear comprises a first ring gear set and a second ring gear set,
• wherein the first ring gear set and the second ring gear set are axially spaced apart from one another along the longitudinal centerline, and the first sun gear set and the second sun gear set are positioned between the first ring gear set and the second ring gear set,
• wherein the sun gear-mesh region comprises a first sun gear-mesh region where the first sun gear set meshes with the first planet gear sets and a second sun gear-mesh region where the second sun gear set meshes with the second planet gear sets,
• the ring gear-mesh region comprises a first ring gear-mesh region where the first ring gear set meshes with the first planet gear sets and a second ring gear-mesh region where the second ring gear set meshes with the second planet gear sets, and
• wherein there is an axial overlap between the first sun gear-mesh region and the first ring gear-mesh region, and an amount of the axial overlap is less than 15% of a width of the first planet gear set.