Assembly for gas turbine engine

Abstract

An assembly for a gas turbine engine, the assembly including a plurality of assembly segments connected in a 360 degree arrangement, each assembly segment of the plurality of assembly segments including a first band, a second band, a first vane extending from the first band to the second band, the first vane being single-formed with the first band and the second band, and a second vane extending from the first band to the second band, wherein the second vane is joined to the first band with a first joint, and the second vane is joined to the second band with a second joint.

Dependencies are inferred from the claim text.