| 摘要 |
<p>A method for producing a solid component which in succession includes deforming a metal bar by forging using two dies in order to obtain an intermediate component including two fins one on each side of a solid part capable of forming the base of the metal reinforcement, the two fins being at a divergent angleα; deforming the two fins of the intermediate component, altering the divergent angleα, so as to obtain the final shape of the turbomachine blade leading edge or trailing edge metal reinforcement.</p> |
