JP2016510701A5 - - Google Patents

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Publication number
JP2016510701A5
JP2016510701A5 JP2015561367A JP2015561367A JP2016510701A5 JP 2016510701 A5 JP2016510701 A5 JP 2016510701A5 JP 2015561367 A JP2015561367 A JP 2015561367A JP 2015561367 A JP2015561367 A JP 2015561367A JP 2016510701 A5 JP2016510701 A5 JP 2016510701A5
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JP
Japan
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resin
substrate
fiber
segments
applicator
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JP2015561367A
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English (en)
Japanese (ja)
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JP6453250B2 (ja
JP2016510701A (ja
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Priority claimed from US13/789,965 external-priority patent/US20140255646A1/en
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JP2015561367A 2013-03-08 2014-02-14 案内された不連続繊維プリプレグを用いる複合特徴部の形成 Active JP6453250B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US13/789,965 US20140255646A1 (en) 2013-03-08 2013-03-08 Forming Composite Features Using Steered Discontinuous Fiber Pre-Preg
US13/789,965 2013-03-08
PCT/US2014/016533 WO2014137568A2 (en) 2013-03-08 2014-02-14 Forming composite features using steered discontinuous fiber pre-preg

Related Child Applications (1)

Application Number Title Priority Date Filing Date
JP2018230731A Division JP6612958B2 (ja) 2013-03-08 2018-12-10 案内された不連続繊維プリプレグを用いる複合特徴部の形成

Publications (3)

Publication Number Publication Date
JP2016510701A JP2016510701A (ja) 2016-04-11
JP2016510701A5 true JP2016510701A5 (cg-RX-API-DMAC7.html) 2017-03-23
JP6453250B2 JP6453250B2 (ja) 2019-01-16

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JP2015561367A Active JP6453250B2 (ja) 2013-03-08 2014-02-14 案内された不連続繊維プリプレグを用いる複合特徴部の形成
JP2018230731A Active JP6612958B2 (ja) 2013-03-08 2018-12-10 案内された不連続繊維プリプレグを用いる複合特徴部の形成

Family Applications After (1)

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JP2018230731A Active JP6612958B2 (ja) 2013-03-08 2018-12-10 案内された不連続繊維プリプレグを用いる複合特徴部の形成

Country Status (9)

Country Link
US (2) US20140255646A1 (cg-RX-API-DMAC7.html)
EP (1) EP2964451B1 (cg-RX-API-DMAC7.html)
JP (2) JP6453250B2 (cg-RX-API-DMAC7.html)
KR (1) KR102119435B1 (cg-RX-API-DMAC7.html)
CN (2) CN110920093A (cg-RX-API-DMAC7.html)
BR (1) BR112015019511A2 (cg-RX-API-DMAC7.html)
CA (2) CA2898224C (cg-RX-API-DMAC7.html)
MX (1) MX388975B (cg-RX-API-DMAC7.html)
WO (1) WO2014137568A2 (cg-RX-API-DMAC7.html)

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GB2556065B (en) * 2016-11-16 2020-09-16 Ge Aviat Systems Ltd Method for forming stiffened composite parts
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