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公开(公告)号:US20190248486A1
公开(公告)日:2019-08-15
申请号:US16261590
申请日:2019-01-30
Applicant: Coretronic Intelligent Robotics Corporation
Inventor: Ying-Chieh Chen , Shih-Hang Lin , Chi-Tong Hsieh
CPC classification number: B64C39/024 , B64C27/006 , B64C2201/027 , B64C2201/108
Abstract: A flight device including a device main body and a plurality of lift force providing modules is provided. The lift force providing modules are connected to the device main body. Each of the lift force providing modules includes two propellers, and each of the propellers rotates to lift the device main body. Two propellers of each of the lift force providing modules may rotate around the same rotation axis. The flight device has an enhanced lift force and good efficiency in lifting, and the flight device has a reduced device volume and improved flight reliability.
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公开(公告)号:US20190248471A1
公开(公告)日:2019-08-15
申请号:US16395464
申请日:2019-04-26
Applicant: SZ DJI TECHNOLOGY CO., LTD.
CPC classification number: B64C11/02 , A63H27/12 , B64C27/08 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/20
Abstract: A propulsion system assembly includes a propeller and a motor configured to drive the propeller to rotate. The propeller includes one of a first body and a second body. The motor comprises the other one of the first body and the second body. The propulsion system assembly also includes a locking mechanism configured to detachably connecting the first body and the second body. The locking mechanism includes a locking member and a position limiting lock catch. The locking member is configured to lock the first body and the second body. The locking member includes locking parts located at at least two sides of the locking member. When the locking parts of the locking member rotate to a locking position, the position limiting lock catch is mounted to a side of the locking parts, to restrain the locking member from rotating relative to the first body.
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公开(公告)号:US20190248464A1
公开(公告)日:2019-08-15
申请号:US16394966
申请日:2019-04-25
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Fangming YE , Zhao YANG , Di OU , Hongshan LI
CPC classification number: B64C1/063 , B64C1/061 , B64C39/02 , B64C39/024 , B64C2201/024 , B64C2201/042 , B64C2201/102 , B64C2201/108 , B64C2201/126
Abstract: An unmanned aerial vehicle includes a fuselage and an arm coupled to the fuselage. The arm includes a first segment, a second segment, and a connecting assembly coupling and locking the first segment and the second segment to each other. The connecting assembly includes a first connecting member and a second connecting member. The first connecting member is rotatably coupled to one of the first segment or the second segment. The second connecting member is coupled to another one of the first segment or the second segment. The first connecting member is rotatable relative to the arm and engages with the second connecting member to lock the first segment and the second segment.
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公开(公告)号:US20190217952A1
公开(公告)日:2019-07-18
申请号:US16324656
申请日:2016-08-19
Applicant: MOTOROLA SOLUTIONS, INC.
Inventor: Artur ZAWADZKI , Rafal Leszek ADAMSKI , Michal SLUSARCZYK
CPC classification number: B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/143 , B64C2201/148 , B64C2201/162 , B64D1/02 , B64D1/22 , B64D47/08 , B64F3/02 , G05D1/0866 , G05D1/104 , H02G11/00 , H02G11/02
Abstract: Methods and systems are described for an aerial drone system including a drone system controller, at least one working drone (101), and a plurality of support drones (103). The working drone (101) is operated by the drone system controller (125) to adjust a position of the working drone (101). A tether line (105) coupled to the working drone (101) provides electrical power to the working drone (101). The support drones (103) are each coupled to the tether line (105) at a different location along the tether line (105) forming a tethered aerial drone system. Each support (drone 103) supports a portion of the weight of the tether line (105) and is operated by the drone system controller (125) to adjust the position of the tether line (105) by adjusting the position of one or more of the support drones (103).
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公开(公告)号:US20190132557A1
公开(公告)日:2019-05-02
申请号:US16219607
申请日:2018-12-13
Applicant: Avigilon Corporation
Inventor: Mahesh SAPTHARISHI
CPC classification number: H04N7/181 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/127 , G06K9/00221 , G06K9/0063 , G06K9/00771 , G06K9/4652 , H04N5/232 , H04N5/23216 , H04N5/23241 , H04N5/23293 , H04N5/23296 , H04N5/23299 , H04N7/185
Abstract: A video surveillance system having a plurality of aerial camera devices such as cameras on drones operable from a plurality of docking stations. Each station has a dock for receiving, charging, and controlling the aerial camera devices.
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公开(公告)号:US20190011932A1
公开(公告)日:2019-01-10
申请号:US15641735
申请日:2017-07-05
Applicant: QUALCOMM Incorporated
Inventor: Gary MCGRATH
CPC classification number: G05D1/0808 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/141 , B64D47/08 , B64G1/244 , G01C23/00 , G05D1/0094 , G05D1/0875 , G05D1/0891
Abstract: Various embodiments involve controlling rotational maneuvers of a robotic vehicle (e.g., an unmanned aerial vehicle or UAV) so that commanded changes in vehicle attitude (e.g., pitch, roll, and/or yaw) may be performed as rotations about a center of sensing of a sensor instead of the vehicle's center of gravity. Maneuvers performed according to various embodiments may reduce or eliminate translational movements in the sensor output that occur when the robotic vehicle rotates about the center of gravity and the sensor is mounted some distance from the center of gravity.
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公开(公告)号:US20190009885A1
公开(公告)日:2019-01-10
申请号:US16066178
申请日:2016-12-20
Applicant: GoerTek Technology Co., Ltd.
Inventor: Zhongyu Cai
CPC classification number: B64C9/00 , B64C27/10 , B64C27/82 , B64C39/024 , B64C2027/8272 , B64C2201/108 , B64D27/24
Abstract: A single-shaft aerial vehicle comprises a propeller, an aerial vehicle body and a wing driver unit constituting a portion of the aerial vehicle body. The aerial vehicle body has a streamlined shape. A ring-shaped wing extending out of the wing driver unit is provided at a central position of the wing driver unit. The ring-shaped wing is movable horizontally under the drive of the wing drive unit. When drag areas of the ring-shaped wing extending out of an outer circumference of the wing drive unit are the same in all directions, the single-shaft aerial vehicle maintains its current flying posture. When the ring-shaped wing moves toward a certain direction to increase the drag area extending out of the wing drive unit in the certain direction, and contracts into the wing drive unit in its opposite direction to reduce the drag area in the opposite direction, the single-shaft aerial vehicle changes its current flying posture.
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公开(公告)号:US20190004176A1
公开(公告)日:2019-01-03
申请号:US15443173
申请日:2017-02-27
Applicant: Raytheon BBN Technologies Corp.
Inventor: Brian R. Van Voorst
CPC classification number: G01S17/026 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/12 , B64C2201/121 , B64C2201/141 , B64C2201/146 , F41H11/02 , F41H13/0006 , G01S7/4817 , G01S7/495 , G01S7/51 , G01S17/023 , G01S17/66 , G01S17/87 , G01S17/89 , G01S17/933 , G05D1/0016 , G05D1/0088 , G05D1/0094 , G05D1/101 , G05D1/12 , G06K9/0063 , G06K2209/21 , G06T17/05 , G08G5/0026 , G08G5/0069 , G08G5/0082 , H04W4/021
Abstract: A system comprising includes a plurality of three dimensional line-scanner LIDAR sensors disposed to provide a set of fanned beams that travel from one horizon into the air to the other horizon arranged to provide a light fence to detect an object that breaks the light fence and a sensor processor connected to the plurality of three dimensional multi-beam line-scanner LIDAR sensors to establish a vector of travel and a velocity of the object that passes through the multi-beam light fence at the location of where the beams are broken.
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公开(公告)号:US20180327087A1
公开(公告)日:2018-11-15
申请号:US16049768
申请日:2018-07-30
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor: Tao Wang , Tao Zhao , Zhi Gang Ou
CPC classification number: B64C27/32 , A63H27/001 , A63H27/02 , B64C11/02 , B64C11/04 , B64C27/08 , B64C27/14 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/108 , F01D5/021 , F01D5/025
Abstract: Systems, methods, and devices for propelling self-propelled movable objects are provided. In one aspect, a rotor assembly for a self-propelled movable object comprises: a hub comprising a first fastening feature; a drive shaft comprising a second fastening feature and directly coupled to the hub by a mating connection of the first and second fastening features, wherein the drive shaft is configured to cause rotation of the hub such that the mating connection of the first and second fastening features is tightened by the rotation; and a plurality of rotor blades coupled to the hub and configured to rotate therewith to generate a propulsive force.
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公开(公告)号:US20180319497A1
公开(公告)日:2018-11-08
申请号:US16029564
申请日:2018-07-07
Applicant: ETAK Systems, LLC
Inventor: Lee Priest , Charlie Terry , Joshua Godwin
CPC classification number: B64C39/024 , B60L11/1822 , B64C17/02 , B64C2201/108 , B64C2201/127 , B64C2201/128 , B64C2201/141 , B64D1/02
Abstract: Systems and methods using an Unmanned Aerial Vehicle (UAV) to supply one or more batteries include loading the UAV with the one or more batteries as cargo; causing the UAV to fly to a remote location; and at the remote location, inserting the one or more batteries in a battery system for powering thereof. The method can further include, at the remote location, retrieving a second set of one or more batteries from the battery system; and causing the UAV to fly back with the retrieved second set.
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