| 摘要 |
The present invention relates to a method for manufacturing composite parts and to manufacturing equipment. The invention is useful in the field of aircraft construction. During a first phase, the part is designed, the geometry is computed, and the fabric architecture of the fabric preform and a mandrel for forming the first state of the preform are calculated. During a second phase, the preform fabric (21) and the mandrel (20) are produced. During a third phase, the mandrel is wrapped with the fabric, the preform is extracted from the mandrel thereof in order to collapse (R) a portion (29b") of the preform, and the preform is impregnated in order to obtain the desired part. |
