Gearbox coupling in a turbomachine

1. An engine defining an axial direction including a forward direction closer to an engine inlet and an aft direction closer to an engine exhaust, a radial direction, and a circumferential direction, the engine comprising:

a static frame member;

a spool configured to rotate relative to the static frame member during operation of the engine;

a gearbox coupled to the spool;

a gearbox coupling assembly mounting the gearbox to the static frame member using a plurality of moveable connection members; and

a bearing positioned between the static frame member and the spool at a location forward of the gearbox,

wherein each moveable connection member allows for sliding movement of the gearbox relative to the static frame member in a plane perpendicular to the axial direction of the engine,

wherein the engine defines a sump, and

wherein the bearing and the gearbox are each positioned within the sump.

2. The engine of claim 1 ,

wherein the plurality of moveable connection members comprises a forward piece and an aft piece,

wherein the forward piece is slidably coupled to the aft piece such that the forward piece is moveable relative to the aft piece in the plane perpendicular to the axial direction.

3. The engine of claim 2 ,

wherein the plurality of moveable connection member further comprises a middle piece comprising a first side and an opposite section side,

wherein the forward piece is positioned adjacent to the first side of the middle piece,

wherein the aft piece is positioned adjacent to the second side of the middle piece,

wherein the forward piece and middle piece together form a first slidable interface, and

wherein the middle piece and aft piece together form a second slidable interface.

4. The engine of claim 3 ,

wherein the first slidable interface extends in a first direction,

wherein the second slidable interface extends in a second direction, and

wherein the first direction is perpendicular to the second direction.

5. The engine of claim 4 ,

wherein the first direction is parallel to the radial direction, and

wherein the second direction is also parallel to the radial direction.

6. The engine of claim 4 , wherein the first slidable interface, the second slidable interface, or both comprise a groove and a correspondingly shaped linear ridge slidably positioned within the groove.

7. The engine of claim 1 , wherein the gearbox comprises a sun gear, a ring gear, and a plurality of planet gears.

8. The engine of claim 7 ,

wherein the spool is coupled to the sun gear, and

wherein the gearbox coupling assembly mounts the plurality of planet gears to the static frame member.

9. The engine of claim 1 ,

wherein the plurality of moveable connection members comprises a forward piece, an aft piece, and a middle piece, wherein the forward piece is coupled to the plurality of planet gears, and wherein the aft piece is coupled to the static frame member.

10. The engine of claim 1 , wherein the plurality of moveable connection members comprises a forward piece, an aft piece, and a middle piece, wherein the forward piece, the aft piece, and the middle piece together define an opening therethrough extending along the axial direction, and wherein the engine includes one or more shafts extending through the opening.

11. The engine of claim 1 , further comprising:

a lubrication oil system comprising a scavenge line, wherein the static frame member comprises a drain extension defining a drain for collecting lubrication oil from the bearing and the gearbox within the sump, and wherein the scavenge line is in fluid communication with the drain.

12. The engine of claim 11 , wherein the scavenge line extends through the gearbox.

13. The engine of claim 1 , wherein the gearbox further comprises a planet gear carrier, and wherein plurality of planet gears are coupled to the static frame member through the planet gear carrier.

14. The engine of claim 1 , wherein the engine is a turbofan engine.