| 发明名称 |
METHOD FOR MANUFACTURING COMPOSITE PARTS |
| 摘要 |
Method for manufacturing composite parts, wherein at least a first composite part is joined to a second composite part, including providing the first composite part preform into a resin transfer mold, heating the first part into the resing transfer mold for performing a curing cycle of the first part, cooling the first part before the curing cycle is completed so that a semi-cured first part is obtained, and joining the semi-cured first part to a cured prepreg second part for obtaining the final composite part. |
| 申请公布号 |
US2016318214(A1) |
申请公布日期 |
2016.11.03 |
| 申请号 |
US201615130284 |
申请日期 |
2016.04.15 |
| 申请人 |
Airbus Operations S.L. |
发明人 |
PINILLOS MARTÍNEZ Ricardo;GARCÍA SOLARES Victor;MUÑOZ LÓPEZ Pilar;PÉREZ SÁNCHEZ Melania |
| 分类号 |
B29C35/02;B29C35/16;B29B11/00;B29C33/04 |
主分类号 |
B29C35/02 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. A method for manufacturing composite parts, wherein at least a first composite part is joined to a second composite part, the method comprising:
providing the first composite part preform into a resin transfer mold; heating the first composite part into the resin transfer mold for performing a curing cycle of the first composite part; cooling the first composite part before the curing cycle is completed so that a semi-cured first part is obtained; and joining the semi-cured first part to a cured prepreg second part for obtaining a final composite part. |
| 地址 |
Getafe ES |
