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公开(公告)号：US20170001721A1
公开(公告)日：2017-01-05
申请号：US15197596
申请日：2016-06-29
Applicant: GoPro, Inc.
Inventor： Noriaki Saika , William H. Tolbert , Reza Yazdani
CPC classification number: B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , F16D2001/103
Abstract: Disclosed is an aerial vehicle. The aerial vehicle may include a removable battery. Various embodiments of removable battery assemblies include a pull-bar battery assembly, a latch battery assembly, and a lever battery assembly. The aerial vehicle may also include a propeller locking mechanism to which propellers may be removably coupled. The propeller locking mechanism may obviate the need for tools for coupling or decoupling propellers to the aerial vehicle. Vents in the arm of the aerial vehicle may provide an air pathway, providing convective cooling for the electronics aerial vehicle.
Abstract translation: 公开了一种航空器。 飞行器可以包括可移除的电池。 可拆卸电池组件的各种实施例包括拉杆电池组件，闩锁电池组件和杠杆电池组件。 飞行器还可以包括螺旋桨锁定机构，螺旋桨可拆卸地联接在该螺旋桨锁定机构上。 螺旋桨锁定机构可以避免需要用于将螺旋桨联接或去耦到飞行器的工具。 飞行器臂的通风口可以提供空气通道，为电子飞行器提供对流冷却。
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公开(公告)号：USD790430S1
公开(公告)日：2017-06-27
申请号：US29565618
申请日：2016-05-23
Applicant: GoPro, Inc.
Designer： Ihab A. Ali , Reza Yazdani
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公开(公告)号：US12103680B2
公开(公告)日：2024-10-01
申请号：US17130911
申请日：2020-12-22
Applicant: GoPro, Inc.
Inventor： Noriaki Saika , William H. Tolbert , Reza Yazdani
IPC: B64C39/02 , B64U10/13 , B64U20/80 , B64U30/20 , B64U50/19 , B64U101/30 , F16D1/10 , H01M50/249
CPC classification number: B64C39/024 , B64U20/80 , H01M50/249 , B64U10/13 , B64U30/20 , B64U50/19 , B64U2101/30 , F16D2001/103
Abstract: Disclosed is an aerial vehicle. The aerial vehicle may include a removable battery. Various embodiments of removable battery assemblies include a pull-bar battery assembly, a latch battery assembly, and a lever battery assembly. The aerial vehicle may also include a propeller locking mechanism to which propellers may be removably coupled. The propeller locking mechanism may obviate the need for tools for coupling or decoupling propellers to the aerial vehicle. Vents in the arm of the aerial vehicle may provide an air pathway, providing convective cooling for the electronics aerial vehicle.
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Patent Agency Ranking
公开(公告)号：US20210171199A1
公开(公告)日：2021-06-10
申请号：US17130911
申请日：2020-12-22
Applicant: GoPro, Inc.
Inventor： Noriaki Saika , William H. Tolbert , Reza Yazdani
IPC: B64C39/02
Abstract: Disclosed is an aerial vehicle. The aerial vehicle may include a removable battery. Various embodiments of removable battery assemblies include a pull-bar battery assembly, a latch battery assembly, and a lever battery assembly. The aerial vehicle may also include a propeller locking mechanism to which propellers may be removably coupled. The propeller locking mechanism may obviate the need for tools for coupling or decoupling propellers to the aerial vehicle. Vents in the arm of the aerial vehicle may provide an air pathway, providing convective cooling for the electronics aerial vehicle.
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公开(公告)号：US10315757B2
公开(公告)日：2019-06-11
申请号：US15182589
申请日：2016-06-14
Applicant: GoPro, Inc.
Inventor： Ihab A. Ali , Reza Yazdani
IPC: B64C27/467 , B64C27/08 , B64C39/02
Abstract: A propeller blade comprises a blade root coupled to a rotor hub and a blade tip. The propeller blade is composed of airfoil cross-sections, each cross-section a distance away from the rotor hub. Each airfoil is designed with particular structural characteristics that improve the overall amount of thrust generated on the quadcopter. Namely, each airfoil possesses a β angle and chord length whose values depend on the distance of that airfoil from the rotor hub. For example, the relationship between an airfoil's β angle and its distance from the rotor hub is described by a power law. Additionally, the relationship between an airfoil's chord length and its distance from the rotor hub is described using a polynomial regression. Compared to current, off the shelf propeller blades, the current propeller blade embodiment achieves the same thrust at a lower RPM, thereby yielding benefits in reduced acoustic noise and improved response time.
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公开(公告)号：US20170355454A1
公开(公告)日：2017-12-14
申请号：US15182589
申请日：2016-06-14
Applicant: GoPro, Inc.
Inventor： Ihab A. Ali , Reza Yazdani
IPC: B64C27/467 , B64C27/08 , B64C39/02
CPC classification number: B64C27/467 , B64C27/08 , B64C39/024
Abstract: A propeller blade comprises a blade root coupled to a rotor hub and a blade tip. The propeller blade is composed of airfoil cross-sections, each cross-section a distance away from the rotor hub. Each airfoil is designed with particular structural characteristics that improve the overall amount of thrust generated on the quadcopter. Namely, each airfoil possesses a β angle and chord length whose values depend on the distance of that airfoil from the rotor hub. For example, the relationship between an airfoil's β angle and its distance from the rotor hub is described by a power law. Additionally, the relationship between an airfoil's chord length and its distance from the rotor hub is described using a polynomial regression. Compared to current, off the shelf propeller blades, the current propeller blade embodiment achieves the same thrust at a lower RPM, thereby yielding benefits in reduced acoustic noise and improved response time.
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公开(公告)号：US10906642B2
公开(公告)日：2021-02-02
申请号：US16412775
申请日：2019-05-15
Applicant: GoPro, Inc.
Inventor： Noriaki Saika , William H. Tolbert , Reza Yazdani
Abstract: Disclosed is an aerial vehicle. The aerial vehicle may include a removable battery. Various embodiments of removable battery assemblies include a pull-bar battery assembly, a latch battery assembly, and a lever battery assembly. The aerial vehicle may also include a propeller locking mechanism to which propellers may be removably coupled. The propeller locking mechanism may obviate the need for tools for coupling or decoupling propellers to the aerial vehicle. Vents in the arm of the aerial vehicle may provide an air pathway, providing convective cooling for the electronics aerial vehicle.
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公开(公告)号：US10336451B2
公开(公告)日：2019-07-02
申请号：US15197596
申请日：2016-06-29
Applicant: GoPro, Inc.
Inventor： Noriaki Saika , William H. Tolbert , Reza Yazdani
Abstract: Disclosed is an aerial vehicle. The aerial vehicle may include a removable battery. Various embodiments of removable battery assemblies include a pull-bar battery assembly, a latch battery assembly, and a lever battery assembly. The aerial vehicle may also include a propeller locking mechanism to which propellers may be removably coupled. The propeller locking mechanism may obviate the need for tools for coupling or decoupling propellers to the aerial vehicle. Vents in the arm of the aerial vehicle may provide an air pathway, providing convective cooling for the electronics aerial vehicle.
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