- 专利标题: Fiber composite laminate and method for producing a fiber composite laminate
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申请号: US15478298申请日: 2017-04-04
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公开(公告)号: US10213972B2公开(公告)日: 2019-02-26
- 发明人: Christopher Buchmann , Christian Weimer , Christoph Meier , Jonas Gruenewald
- 申请人: Airbus Defence and Space GmbH
- 申请人地址: DE Taufkirchen
- 专利权人: AIRBUS DEFENCE AND SPACE GMBH
- 当前专利权人: AIRBUS DEFENCE AND SPACE GMBH
- 当前专利权人地址: DE Taufkirchen
- 代理机构: Greer, Burns & Crain, Ltd.
- 优先权: DE102016206325 20160414
- 主分类号: B29C70/42
- IPC分类号: B29C70/42 ; B32B27/08 ; B32B27/20 ; B29C70/40 ; B29C70/50 ; B29B15/10 ; B32B5/14 ; B32B3/26 ; B29K21/00 ; B29K105/08 ; B29K307/04 ; B29K309/08 ; B29L31/30 ; B29L31/52 ; B29K101/10 ; B29K101/12
摘要:
A method for producing a fiber composite laminate, including the steps of applying pressure and/or heat to a first preform, which has one or more dry fiber layers and a thermoplastic elastomer, such that the thermoplastic portion of the thermoplastic elastomer completely impregnates the dry fiber layers of the first preform in at least one first region and only partially impregnates the dry fiber layers in at least one second region and, in a thermosetting polymer matrix, impregnating and curing the fiber layers of the second region of the first preform that are still dry and have not been impregnated with the thermoplastic portion of the thermoplastic elastomer.
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