Patent ID: 9500133
Filing Date: 2016-11-22
CPC Classification: F01D,F02C,F05D,Y02T,Y10T

Claim Text:
1. A turbine engine assembly, comprising: a turbine engine case extending along an axis between an upstream end and a downstream end, the turbine engine case including a plurality of discrete axial segments including a first segment and a second segment that is downstream of the first segment; a gearbox; and a plurality of gearbox mounts connecting the gearbox to the turbine engine case, and comprising an axial mount that extends axially, relative to the axis, in an upstream direction from the gearbox to the first segment of the turbine engine case; wherein the plurality of gearbox mounts further include a radial mount that extends radially towards the axis, in a direction substantially perpendicular to the axis from the gearbox to the second segment of the turbine engine case.