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公开(公告)号：US20180103543A1
公开(公告)日：2018-04-12
申请号：US15782269
申请日：2017-10-12
申请人： Intel Corporation
CPC分类号： H05K1/0278 , B64C25/00 , B64C39/024 , B64C2201/108 , B64D47/08 , H02K11/0094 , H02K11/33 , H05K1/0271 , H05K3/0044 , H05K3/285 , H05K3/303 , H05K5/0017 , H05K5/0039 , H05K2201/09063 , H05K2201/09263 , H05K2201/1009 , H05K2201/10189 , H05K2201/10318 , H05K2203/0228
摘要： Flexible printed circuit boards and related methods are disclosed herein. An example printed circuit board includes a controller interface coupled to a surface of the printed circuit board between a first end of the printed circuit board and a second end of the printed circuit board. The example printed circuit board includes a connector coupled to the surface proximate to the first end. The example printed circuit board includes a notch formed between the controller interface and the connector. The notch is to form a narrowed portion of the printed circuit board to enable the printed circuit board to bend at the narrowed portion.
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公开(公告)号：US10787249B2
公开(公告)日：2020-09-29
申请号：US15782660
申请日：2017-10-12
申请人： Intel Corporation
发明人： Fabian Oberndorfer , Klaus Doth , Martin Stobbe
摘要： Multi-stage reduction of impact forces are disclosed. An example apparatus to reduce impact energy of an aircraft during landing includes a rotatable landing leg having a proximal end near an axis of rotation and a distal end opposite the proximal end, a first flexible portion of the proximal end, where the first flexible portion is to engage a first engaging portion at a first rotation angle of the rotatable landing leg, and a second flexible portion of the distal end, where the second flexible portion is to engage a second engaging portion at a second rotation angle of the rotatable landing leg.
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公开(公告)号：US10212809B2
公开(公告)日：2019-02-19
申请号：US15782269
申请日：2017-10-12
申请人： Intel Corporation
IPC分类号： H05K1/02 , H05K5/00 , H05K3/00 , H05K3/28 , H05K3/30 , H02K11/00 , B64C39/02 , H02K11/33 , B64D47/08 , B64C25/00
摘要： Flexible printed circuit boards and related methods are disclosed herein. An example printed circuit board includes a controller interface coupled to a surface of the printed circuit board between a first end of the printed circuit board and a second end of the printed circuit board. The example printed circuit board includes a connector coupled to the surface proximate to the first end. The example printed circuit board includes a notch formed between the controller interface and the connector. The notch is to form a narrowed portion of the printed circuit board to enable the printed circuit board to bend at the narrowed portion.
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公开(公告)号：US20180099741A1
公开(公告)日：2018-04-12
申请号：US15782660
申请日：2017-10-12
申请人： Intel Corporation
发明人： Fabian Oberndorfer , Klaus Doth , Martin Stobbe
CPC分类号： B64C25/62 , B64C25/06 , B64C25/10 , B64C39/024 , B64C2201/18
摘要： Multi-stage reduction of impact forces are disclosed. An example apparatus to reduce impact energy of an aircraft during landing includes a rotatable landing leg having a proximal end near an axis of rotation and a distal end opposite the proximal end, a first flexible portion of the proximal end, where the first flexible portion is to engage a first engaging portion at a first rotation angle of the rotatable landing leg, and a second flexible portion of the distal end, where the second flexible portion is to engage a second engaging portion at a second rotation angle of the rotatable landing leg.
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