- 专利标题： Structural composite component and method for configuring a structural composite component
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申请号： US15817826申请日： 2017-11-20
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公开(公告)号： US10773824B2公开(公告)日： 2020-09-15
- 发明人: Tamara Blanco Varela , José Sanchez Gomez , Leire Segura Martinez De Ilarduya , Mariano Morales Monge
- 申请人： Airbus Operations, S.L.
- 申请人地址： ES
- 专利权人： Airbus Operations, S.L.
- 当前专利权人： Airbus Operations, S.L.
- 当前专利权人地址： ES
- 代理机构： Lerner, David, Littenberg, Krumholz & Mentlik, LLP
- 优先权： com.zzzhc.datahub.patent.etl.us.BibliographicData$PriorityClaim@153457df
- 主分类号： B64D45/02
- IPC分类号： B64D45/02 ; B29C70/88 ; B32B15/02 ; H01M2/02 ; B32B7/06 ; B32B15/08 ; B32B15/14 ; B32B15/00 ; B32B27/00 ; B32B9/04 ; B32B7/02 ; B32B5/00 ; B32B9/00 ; B32B3/26 ; B32B27/06 ; B32B7/04 ; B32B27/28 ; B32B7/10 ; B32B15/04 ; B32B5/02 ; B32B7/00 ; B32B15/20
摘要：
A structural composite component, in particular for an aircraft or spacecraft, includes: a lightning strike protection layer; and a composite battery including a cathode layer and a separation layer, wherein the lightning strike protection layer is formed integrated with the cathode layer, and wherein the separation layer is configured for providing acoustic damping, and/or fire barrier, and/or impact resistance to the structural composite component. A method for configuring such a structural composite component; and an aircraft or spacecraft including such a structural composite component are also described.
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