发明名称 |
Single vacuum debulk composite panel repair |
摘要 |
A method of attaching a composite member to a structure. The method including forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying vacuum at a first pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the substrate by applying heat at a second temperature and by applying vacuum at a second pressure. |
申请公布号 |
US8790485(B2) |
申请公布日期 |
2014.07.29 |
申请号 |
US200511064824 |
申请日期 |
2005.02.25 |
申请人 |
Bell Helicopter Textron Inc. |
发明人 |
Whitworth Denver;Bergerson Anthony;Marvin Michael |
分类号 |
B32B37/10;B29C65/18;B29C65/00;B29C73/10 |
主分类号 |
B32B37/10 |
代理机构 |
Pillsbury Winthrop Shaw Pittman LLP |
代理人 |
Pillsbury Winthrop Shaw Pittman LLP |
主权项 |
1. A method of attaching a composite member to a structure, comprising:
forming a laminate of fabric impregnated with resin; applying heat at a first temperature to the impregnated laminate; applying a partial vacuum at a first vacuum pressure to the impregnated laminate to degas the resin and form a degassed, impregnated laminate; positioning the degassed, impregnated laminate on a structure; and curing the degassed, impregnated laminate on the structure by applying heat at a second temperature and by applying vacuum at a second vacuum pressure, the second vacuum pressure greater than the first vacuum pressure, wherein only a same single vacuum enclosure is used when applying heat at the first temperature, when applying the partial vacuum at the first vacuum pressure, and when curing the degassed, impregnated laminate. |
地址 |
Hurst TX US |