公开(公告)号：US20180155055A1

公开(公告)日：2018-06-07

申请号：US15817826

申请日：2017-11-20

申请人： Airbus Operations, S.L.

发明人： Tamara Blanco Varela ,  José Sanchez Gomez ,  Leire Segura Martinez De Ilarduya ,  Mariano Morales Monge

IPC分类号： B64D45/02 ,  B29C70/88 ,  B32B15/02 ,  H01M2/02 ,  B32B7/06 ,  B32B15/08 ,  B32B15/14

CPC分类号： B64D45/02 ,  B29C70/885 ,  B32B3/26 ,  B32B5/00 ,  B32B5/02 ,  B32B7/00 ,  B32B7/02 ,  B32B7/04 ,  B32B7/06 ,  B32B7/10 ,  B32B9/00 ,  B32B9/04 ,  B32B15/00 ,  B32B15/02 ,  B32B15/04 ,  B32B15/08 ,  B32B15/14 ,  B32B15/20 ,  B32B27/00 ,  B32B27/06 ,  B32B27/28 ,  B32B2250/00 ,  B32B2262/00 ,  B32B2262/106 ,  B32B2307/10 ,  B32B2307/102 ,  B32B2307/20 ,  B32B2307/202 ,  B32B2307/30 ,  B32B2307/3065 ,  B32B2307/50 ,  B32B2307/558 ,  B32B2307/56 ,  B32B2307/732 ,  B32B2457/00 ,  B32B2457/10 ,  B32B2571/00 ,  B32B2605/00 ,  B32B2605/18 ,  H01M2/0267 ,  H01M2/0295

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.

公开(公告)号：US10773824B2

公开(公告)日：2020-09-15

申请号：US15817826

申请日：2017-11-20

申请人： Airbus Operations, S.L.

发明人： Tamara Blanco Varela ,  José Sanchez Gomez ,  Leire Segura Martinez De Ilarduya ,  Mariano Morales Monge

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.