Patent ID: 9599161
Date: 2017-03-21
CPC Classifications: F01D,F02C,F05D,F16C

Claim:
1. An assembly for a turbine engine, comprising: a rolling element bearing and a turbine engine component arranged along an axis, the bearing including an inner ring; the inner ring including a plurality of first passages and a first channel that extends axially into the inner ring; the first passages arranged circumferentially around the axis, and respectively extending axially through the inner ring from a plurality of first passage inlets to the first channel; and the turbine engine component including a component channel that extends axially into the turbine engine component and is fluidly coupled with the first channel; wherein an outer radius of the component channel is less than an outer radius of the first channel, and the first channel extends axially to and is partially formed by an axial end of the turbine engine component.