Additive manufactured gear for a geared architecture gas turbine engine
A gear includes a multiple of gear teeth that extend from an outer portion of a rim about an axis and an inner portion of the rim about the axis, the inner portion of the rim additive manufactured.
1. A gear, comprising:
a multiple of gear teeth that extend from an outer portion of a rim about an axis; and
an inner portion of said rim about said axis, said inner portion of said rim additive manufactured to the outer portion at a mechanical interface.
2. The gear as recited in claim 1 , wherein said inner portion of said rim forms a journal bearing surface.
3. The gear as recited in claim 1 , wherein said inner portion of said rim includes a matrix.
4. The gear as recited in claim 3 , wherein said matrix forms a lattice structure.
5. The gear as recited in claim 1 , wherein said gear is an intermediate gear of a geared architecture for a gas turbine engine, said intermediate gear is a double helical gear.
6. The gear as recited in claim 1 , wherein said inner portion provides different characteristics along an axial length.
7. The gear as recited in claim 1 , wherein said interface is a bond layer that facilitates receipt of a dissimilar material that is applied to said outer portion of said rim via an additive manufacturing process.
8. A geared architecture for a gas turbine engine, said geared architecture, comprising:
a sun gear;
a ring gear that surrounds said sun gear; and
a multiple of intermediate gears in meshing engagement with said sun gear and said ring gear, each of said multiple of intermediate gears including an inner portion of a rim, said inner portion of said rim being additive manufactured, and a multiple of gear teeth that extend from an outer portion of said rim of each of said multiple of intermediate gears about an axis, said inner portion of said rim additive manufactured to the outer portion at a mechanical interface, said gear teeth manufactured via subtractive manufacturing.
9. The geared architecture as recited in claim 8 , wherein said inner portion of said rim forms an inner periphery.
10. The geared architecture as recited in claim 8 , wherein said mechanical interface comprises a dovetail.
11. The geared architecture as recited in claim 8 , wherein said inner portion of said rim forms a matrix that defines a lattice structure.
12. The geared architecture as recited in claim 8 , wherein each of said multiple of intermediate gears is a double helical gear.
13. The geared architecture as recited in claim 12 , wherein said inner portion provides different characteristics along an axial length.
14. A method of manufacturing a gear, comprising:
subtractive manufacturing a multiple of gear teeth from an outer portion of a rim; and
additive manufacturing an inner portion of the rim to the outer portion at a mechanical interface.
15. The method as recited in claim 14 , further comprising additive manufacturing the inner portion of the rim as a matrix structure.
16. The method as recited in claim 15 , further comprising additive manufacturing the inner portion of the rim to provide different characteristics along an axial length.