发明名称 Method and apparatus for assembling composite structures using a composite rivet
摘要 Method and apparatus for mechanically-joining components (514,516,518) to assemble a composite structure. A first component and a second component are provided. At least one of the first and second components may comprise a composite component. A hole (510,512) is formed in each of the first and second components. A metallic sleeve (504) is placed in the holes in the first and second components such that the metallic sleeve is in contact with the first and second components, and a composite rivet (502) is placed in the metallic sleeve. Heat and a deforming force (530,532) are applied to the composite rivet to join the first and second components to form an assembled composite structure.
申请公布号 EP2058111(A1) 申请公布日期 2009.05.13
申请号 EP20080253594 申请日期 2008.11.04
申请人 THE BOEING COMPANY 发明人 KEENER, STEVEN G.
分类号 B29C70/88 主分类号 B29C70/88
代理机构 代理人
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