发明名称 |
Forming a composite reinforcement preform |
摘要 |
<p>An assembly and method for manufacturing a composite reinforcement perform for unitizing a structure are provided. The assembly includes a base 34 having a plurality of pins 32 extending outwardly from the base to define a structure about which a composite fiber is wound to define a composite reinforcement perform 14. The assembly also includes a plurality of mandrels 36 positioned adjacent to the base 32 and at least a portion of the composite reinforcement preform. A cap 40 is positioned over at least a portion of the plurality of mandrels 36 to engage each of the mandrels to support the mandrels and the composite reinforcement preform during a curing process to form the composite reinforcement. The backside of each mandrel has a tapered surface extending along it. The cap comprises as tapered surface corresponding with each of the tapered surfaces on the mandrels. The taper may be 5 degrees. Each mandrel may comprise a key or keyway 38 configured to mate with a keyway or key 45 defined in the cap.</p> |
申请公布号 |
GB2462941(A) |
申请公布日期 |
2010.03.03 |
申请号 |
GB20090015400 |
申请日期 |
2009.09.03 |
申请人 |
THE BOEING COMPANY |
发明人 |
DAVID T MISCIAGNA;JESSICA J FUHRER;ROBERT S FUNK;WILLIAM S TOLOTTA |
分类号 |
B29C69/00;B29C53/56;B29C70/08;B29C70/34;B29D99/00 |
主分类号 |
B29C69/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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