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公开(公告)号：US11851170B2
公开(公告)日：2023-12-26
申请号：US17002466
申请日：2020-08-25
Applicant: Intel Corporation
Inventor： Fabian Oberndorfer
CPC classification number: B64C27/006 , B64C11/205 , B64C39/024 , B64C11/00 , B64U10/00 , B64U30/20
Abstract: Disclosed is a drone rotor cage. The drone rotor cage may include a motor housing, a plurality of spars, and a plurality of ribs. The plurality of spars may extend from the motor housing. Each of the plurality of spars may have a spar height and a spar thickness. The spar height may be greater than the spar thickness. Each of the ribs may extend from a respective one of the plurality of spars. Each of the plurality of ribs may have a rib height and a rib thickness. The rib height may be greater than the rib thickness. The plurality of spars and the plurality of ribs may define a space sized to allow a rotor to spin freely when the rotor cage is attached to a drone.
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公开(公告)号：US20200012296A1
公开(公告)日：2020-01-09
申请号：US16551759
申请日：2019-08-27
Applicant: Intel Corporation
Inventor： Daniel Gurdan , Mika Ritamaeki , Fabian Oberndorfer , Tobias Gurdan , Evgeny Kalugin , Soren Friis
Abstract: An unmanned aerial vehicle comprises an image sensor, configured to detect electromagnetic radiation and to generate image sensor data representing the detected electromagnetic radiation; a filter, configured to pass image sensor data representing one or more first wavelengths of electromagnetic radiation and to block image sensor data representing one or more second wavelengths of electromagnetic radiation; and one or more processors configured to determine from the passed image sensor data an origin of the detected electromagnetic radiation; and control the unmanned aerial vehicle to travel toward the determined origin.
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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
Applicant: Intel Corporation
Inventor： Fabian Oberndorfer , Klaus Doth , Raffael Lustig , Jan Nicolaas Zelhorst
CPC classification number: 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
Abstract: 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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Patent Agency Ranking
公开(公告)号：US11054842B2
公开(公告)日：2021-07-06
申请号：US16352982
申请日：2019-03-14
Applicant: Intel Corporation
Inventor： Fabian Oberndorfer , Wolfgang Rottner , Stefan Klar
Abstract: Methods and devices are presented for controlling or reducing amount of downwash generated by a drone. A drone including a plurality of arms including rotors may be configured to operate and fly with arms in an elevated position with respect to a horizontal plane. The elevated arms may allow a drone to fly with reduced vertical downwash.
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公开(公告)号：US20190212755A1
公开(公告)日：2019-07-11
申请号：US16352982
申请日：2019-03-14
Applicant: Intel Corporation
Inventor： Fabian Oberndorfer , Wolfgang Rottner , Stefan Klar
CPC classification number: G05D1/0816 , B64C7/00 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/165
Abstract: Methods and devices are presented for controlling or reducing amount of downwash generated by a drone. A drone including a plurality of arms including rotors may be configured to operate and fly with arms in an elevated position with respect to a horizontal plane. The elevated arms may allow a drone to fly with reduced vertical downwash.
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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
Applicant: Intel Corporation
Inventor： Fabian Oberndorfer , Klaus Doth , Martin Stobbe
Abstract: 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
Applicant: Intel Corporation
Inventor： Fabian Oberndorfer , Klaus Doth , Raffael Lustig , Jan Nicolaas Zelhorst
IPC: H05K1/02 , H05K5/00 , H05K3/00 , H05K3/28 , H05K3/30 , H02K11/00 , B64C39/02 , H02K11/33 , B64D47/08 , B64C25/00
Abstract: 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
Applicant: Intel Corporation
Inventor： Fabian Oberndorfer , Klaus Doth , Martin Stobbe
CPC classification number: B64C25/62 , B64C25/06 , B64C25/10 , B64C39/024 , B64C2201/18
Abstract: 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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