| 摘要 |
<p>A geared architecture for a gas turbine engine according to an exemplary aspect of the present disclosure includes a fan shaft, a frame which supports the fan shaft, a gear system which drives the fan shaft, a torque frame which at least partially supports the gear system, and an input coupling to the gear system. In a further non-limiting embodiment of the foregoing geared architecture, the frame and the torque frame are mounted to a fixed structure. In a further non-limiting embodiment of the foregoing geared architecture, the frame and the torque frame are mounted to a front center body of a gas turbine engine.</p> |
