| 摘要 |
<p>The method involves a yoke with two arms (18-1, 18-2), where each arm is equipped with a hole (20-1, 20-2) that is designed to work with a pin. An area (34) of less rigidity is produced in the end fitting upstream from the holes. The area of less rigidity is produced on the arms of the yoke. The area of less rigidity is not produced symmetrically to an inside surface (40) and an outside surface (42) of the arm that receives the inside surface. The area is provided with reduced thickness (36-1, 36-2). An independent claim is also included for an aeronautical rod.</p> |
