发明名称 Method for fabricating composite fasteners
摘要 Composite fasteners have a high fraction of discontinuous, randomly oriented reinforcing fibers. A charge of thermoplastic fiber flakes are heated to melting temperature within a reservoir, flowed into multiple mold cavities and compression molded. The molded fasteners have high strength, exhibit quasi-isotropic properties and may be produced in high volume.
申请公布号 US9623612(B2) 申请公布日期 2017.04.18
申请号 US201313773042 申请日期 2013.02.21
申请人 THE BOEING COMPANY 发明人 Bartel Aaron William;Muntz Nathan A.
分类号 B29D1/00;B29C70/46;B29C70/12;B29L1/00 主分类号 B29D1/00
代理机构 Yee & Associates, P.C. 代理人 Yee & Associates, P.C.
主权项 1. A method of producing a composite fastener, comprising: introducing thermoplastic resin infused fiber flakes into a reservoir; heating the infused fiber flakes in the reservoir to the melting temperature of the thermoplastic resin, resulting in a mixture of melted thermoplastic resin and fiber flakes; and, flowing the mixture of the melted thermoplastic resin and fiber flakes into a mold having the shape of the fastener.
地址 Chicago IL US
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