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公开(公告)号：US20160075431A1
公开(公告)日：2016-03-17
申请号：US14947923
申请日：2015-11-20
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
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公开(公告)号：US20160031558A1
公开(公告)日：2016-02-04
申请号：US14836344
申请日：2015-08-26
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
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公开(公告)号：US20160016663A1
公开(公告)日：2016-01-21
申请号：US14333462
申请日：2014-07-16
Applicant: Ford Global Technologies, LLC
Inventor： Joe F. Stanek , Tony A. Lockwood
CPC classification number: G05D1/0276 , B60R16/02 , B60W30/00 , B64C29/0008 , B64C29/0091 , B64C29/02 , B64C39/00 , B64C39/02 , B64C39/022 , B64C39/024 , B64C2201/00 , B64C2201/02 , B64C2201/08 , B64C2201/086 , B64C2201/088 , B64C2201/12 , B64C2201/126 , B64C2201/127 , B64C2201/14 , B64C2201/141 , B64C2201/18 , B64C2201/182 , B64C2201/185 , B64C2201/187 , B64C2201/20 , B64C2201/208 , B64C2230/00 , G05D1/0022 , G05D1/0088 , G05D1/0094 , G05D1/0202 , G05D1/0212 , G05D1/0231 , G05D1/0242 , G05D1/0255 , G05D1/0257 , G05D1/028 , G05D2201/0213 , G08C17/00 , G08G1/012 , G08G1/091
Abstract: This disclosure generally relates to an automotive drone deployment system that includes at least a vehicle and a deployable drone that is configured to attach and detach from the vehicle. More specifically, the disclosure describes the vehicle and drone remaining in communication with each other to exchange information while the vehicle is being operated in an autonomous driving mode so that the vehicle's performance under the autonomous driving mode is enhanced.
Abstract translation: 本公开总体上涉及一种汽车无人机部署系统，该系统至少包括车辆和可部署的无人机，其配置为从车辆附接和分离。 更具体地，本公开描述了当车辆以自主驾驶模式操作时彼此保持通信的车辆和无人机交换信息，使得车辆在自主驾驶模式下的性能得到增强。
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公开(公告)号：US09233754B1
公开(公告)日：2016-01-12
申请号：US14836344
申请日：2015-08-26
Applicant: SZ DJI TECHNOLOGY CO., LTD
Inventor： Tao Wang , Tao Zhao , Shaojie Chen , Zhigang Ou
IPC: B64C29/00 , B64C27/08 , B64C27/00 , B64D43/00 , G05D1/00 , B64C25/06 , B64C39/02 , B64C25/32 , A63H27/00
CPC classification number: B64C27/08 , A63H27/12 , B64C1/30 , B64C25/06 , B64C25/32 , B64C27/00 , B64C27/54 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/123 , B64C2201/127 , B64C2201/128 , B64C2201/14 , B64C2201/141 , B64C2201/20 , B64D31/14 , B64D43/00 , G01R33/0047 , G01V3/16 , G05D1/00 , Y10T29/49117
Abstract: The present invention provides methods and apparatus for unmanned aerial vehicles (UAVs) with improved reliability. According to one aspect of the invention, interference experienced by onboard sensors from onboard electrical components is reduced. According to another aspect of the invention, user-configuration or assembly of electrical components is minimized to reduce user errors.
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公开(公告)号：US20240067357A1
公开(公告)日：2024-02-29
申请号：US17895193
申请日：2022-08-25
Applicant: Martin Daniel Holmes
Inventor： Martin Daniel Holmes
CPC classification number: B64F1/08 , B64C39/022 , B64C39/024 , B64F5/10 , B64C2201/08 , B64C2201/128 , B64C2201/20
Abstract: A system for airborne storage, assembly and launch of aircraft and spacecraft.
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Patent Agency Ranking
公开(公告)号：US20190185161A1
公开(公告)日：2019-06-20
申请号：US16323704
申请日：2017-08-08
Applicant: CLEO ROBOTICS INC.
Inventor： Omar ELERYAN , Szymon CZARNOTA
CPC classification number: B64C39/024 , B64C13/16 , B64C27/08 , B64C29/00 , B64C39/00 , B64C39/02 , B64C39/028 , B64C2201/027 , B64C2201/042 , B64C2201/08 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64C2201/146 , B64C2201/162 , B64C2201/18 , B64C2201/20 , B64D47/08
Abstract: A lightweight, pocket-sized unmanned aerial vehicle (UAV) that can be held in an outstretched hand by a user for take-off and landing of the UAV. The UAV comprises a semi-toroidal or a substantially toroidal hollow body that defines a duct. The UAV further comprises a motor for rotating a fan that directs air into and out of the duct enabling the UAV to take flight. The UAV comprises a flight-control system that comprises at least two flight control surfaces that can alter the directed air as it flows through the duct for controlling the roll and pitch and optionally the yaw of the UAV during flight. The flight control system may be controlled by a microprocessor controller. The UAV further comprises a payload, with at least a wireless transmitter and receiver unit.
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公开(公告)号：US20180327092A1
公开(公告)日：2018-11-15
申请号：US15991125
申请日：2018-05-29
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor： Yumian DENG , Rongming XIONG , Tao ZHAO , Yin TANG
CPC classification number: B64C39/024 , B64C1/30 , B64C3/56 , B64C25/52 , B64C2201/024 , B64C2201/027 , B64C2201/108 , B64C2201/20
Abstract: An unmanned aerial vehicle includes a central body, a plurality of arms extendable from the central body, and a plurality of landing stands. Each of the plurality of arms is configured to transform between a flight configuration where the arm is extending away from the central body and a compact configuration where the arm is folded against the central body. Each of the plurality of landing stands is attached to a distal end of one of the plurality of arms. A first one of the plurality of landing stands is longer than a second one of the plurality of landing stands.
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公开(公告)号：US20180319496A1
公开(公告)日：2018-11-08
申请号：US16024446
申请日：2018-06-29
Applicant: Hangzhou Zero Zero Technology Co., Ltd
Inventor： Tong Zhang , Mengqui Wang , Zhaozhe Wang , Xuyang Zhang , Guanqun Zhang , Shuang Gong , Yalin Zhang , Jinglong Wang , Lixin Liu
CPC classification number: B64C39/024 , B64C1/30 , B64C27/08 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/088 , B64C2201/108 , B64C2201/162 , B64C2201/20 , B64C2201/201 , B64C2201/203 , B64C2211/00
Abstract: An aerial vehicle, preferably including: a rotary wing and a protection housing enclosing the rotary wing. An aerial vehicle, preferably including: a first rotary wing module including a first rotary wing and a second rotary wing module including a second rotary wing, wherein the first rotary wing module and the second rotary wing module are preferably operable between a folded configuration and an unfolded configuration. A method of aerial vehicle operation.
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公开(公告)号：US20180304984A1
公开(公告)日：2018-10-25
申请号：US16016686
申请日：2018-06-25
Applicant: PowerVision Robot Inc.
Inventor： Weifeng Zheng , Hui HAN , Yi ZHENG , Buwei WEI , Guozhi ZENG
CPC classification number: B64C1/30 , B64C25/10 , B64C25/26 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/20 , B64D47/08 , H04N7/185
Abstract: An aircraft and an outer shell therefor. The aircraft includes an outer shell; and main body components, accommodated in the outer shell. The outer shell includes: an inner cavity, the inner cavity being provided with a space for at least accommodating the main body components of the aircraft; an outer surface, the outer surface enclosing the inner cavity.
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公开(公告)号：US20180297704A1
公开(公告)日：2018-10-18
申请号：US16014766
申请日：2018-06-21
Applicant: GoPro, Inc.
Inventor： Ryan Michael Goldstein
IPC: B64C39/02
CPC classification number: B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/20 , B64C2201/203
Abstract: Vehicles such as unmanned air vehicles that are capable of movement from an open, flight configuration to an enclosed configuration in which all major flight components can be protected by an outer shell are disclosed. In the enclosed configuration, the vehicles can take on standard geometric shapes such as a rectangular prism, sphere, cylinder, or another shape, so as to not be recognizable as an unmanned air vehicle. Embodiments of vehicles can also include interchangeable and/or wireless motor arms, motor arms which are electrically connected to the remainder of the vehicle only when in an open configuration, remote controllers removably attached to the remainder of the vehicle, and clip or other attachment mechanisms for attachment to objects such as backpacks.
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