| 摘要 |
<p>An aircraft power generating assembly (1) having a mechanical gear transmission (12), and an electric machine (13) integrated in the mechanical transmission (12); the electric machine (13) having a stator (28) connected directly to a fixed frame (10) of the mechanical transmission, and a rotor (22) surrounding and rotated by a rotary shaft (15) of the mechanical transmission; and the opposite ends of the rotary shaft (15) being connected to respective further rotary input/output shafts (3)(6).</p> |
