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公开(公告)号：WO2005099415A2
公开(公告)日：2005-10-27
申请号：PCT/US2005/012560
申请日：2005-04-14
Applicant: ARLTON, Paul, E. , ARLTON, David, J.
Inventor： ARLTON, Paul, E. , ARLTON, David, J.
CPC classification number: B64C27/10 , B64C27/22 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
Abstract: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
Abstract translation: 旋转翼车辆包括具有细长管状骨架或芯体的主体结构，以及具有转子的反向旋转同轴转子系统，每个转子具有单独的电动机，以围绕公共转子旋转轴线驱动转子。 转子系统用于在定向飞行中移动旋翼机。
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公开(公告)号：WO2005042342A2
公开(公告)日：2005-05-12
申请号：PCT/US2004/036349
申请日：2004-11-01
Applicant: THE INSITU GROUP , SLIWA, Steven, M. , VON FLOTOW, Andreas, H. , DENNIS, Brian, D.
Inventor： SLIWA, Steven, M. , VON FLOTOW, Andreas, H. , DENNIS, Brian, D.
IPC: B63H
CPC classification number: B64C11/003 , A63H27/02 , B64C11/04 , B64C11/14 , B64C11/28 , B64C39/024 , B64C2201/044 , B64C2201/082 , B64C2201/102 , B64C2201/165 , B64C2201/182 , B64C2201/201 , B64C2201/206 , B64D41/007 , F02K5/023 , F05D2260/85 , Y02T50/44 , Y02T50/672
Abstract: Methods and systems for starting propeller driven aircraft and other devices are disclosed. A system in accordance with one embodiment of the invention includes a removable fixture that is coupled to the propeller and has at least one portion exposed to a flowstream to rotate the propeller during engine start-up. The fixture is configured to separate from the propeller after the engine begins to turn over (e.g., after the engine starts and/or rotates above a threshold rate). Accordingly, the system can include a releasable link between the fixture and the propeller.
Abstract translation: 公开了用于启动螺旋桨驱动的飞机和其他装置的方法和系统。 根据本发明的一个实施例的系统包括可拆卸的固定装置，其连接到螺旋桨并且具有暴露于流动流中的至少一个部分以在发动机起动期间旋转螺旋桨。 发动机开始翻转后（例如在发动机起动和/或旋转高于阈值速率之后），该固定装置构造成与螺旋桨分离。 因此，系统可以包括夹具和螺旋桨之间的可释放的连接。
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公开(公告)号：US11649051B2
公开(公告)日：2023-05-16
申请号：US17007647
申请日：2020-08-31
Applicant: Paul E. Arlton , David J. Arlton
Inventor： Paul E. Arlton , David J. Arlton
CPC classification number: B64C39/024 , B64C7/00 , B64C27/10 , B64C27/14 , B64C27/605 , B64C2027/8236 , B64C2027/8281 , B64C2201/027 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/108 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64C2201/205
Abstract: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
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公开(公告)号：US20190152599A1
公开(公告)日：2019-05-23
申请号：US16260828
申请日：2019-01-29
Applicant: SZ DJI TECHNOLOGY CO., LTD.
Inventor： Xumin WU , Xiaolong WU , Sungki LEE , Jiyuan AO , Zhuang FENG
CPC classification number: B64C39/024 , B64C1/30 , B64C27/08 , B64C27/12 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/201 , B64D47/08
Abstract: An unmanned aerial vehicle (UAV) includes a central body, a plurality of arms extending out from the central body, and a plurality of propulsion units. Each of the plurality of arms includes a stem portion, one or more branch portions, and a joint connecting the stem portion with the one or more branch portions. The joint includes a sleeve configured to lock a position of one of the one or more branch portions relative to the stem portion. Each of the propulsion units is attached to one of the one or more branch portions of one of the plurality of arms.
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公开(公告)号：US20180354621A1
公开(公告)日：2018-12-13
申请号：US16048076
申请日：2018-07-27
Applicant: International Business Machines Corporation
Inventor： Jeanette L. Blomberg , Eric K. Butler , Anca A. Chandra , Pawan R. Chowdhary , Thomas D. Griffin , Divyesh Jadav , Sunhwan Lee , Robert J. Moore , Hovey R. Strong, Jr.
CPC classification number: B64C39/024 , B64C2201/128 , B64C2201/201 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64F1/007 , B64F1/222 , B64F1/32 , B64F1/36 , B64F1/368
Abstract: Embodiments of the present invention provide an apparatus comprising a body including a cavity for storing one or more packages, and a conveyor belt disposed above a top surface of the body. The belt is shaped to receive one or more packages, and the belt is controllable to rotate a package placed on the belt either from the top surface to the cavity for storage or from the cavity to the top surface for dispatch. A package comprises at least one of a drone and a payload transported by the drone. The apparatus further comprises a landing mechanism for stabilizing a drone landing on the apparatus.
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Patent Agency Ranking
公开(公告)号：US10079497B2
公开(公告)日：2018-09-18
申请号：US15414636
申请日：2017-01-25
Applicant: Coretronic Intelligent Robotics Corporation
Inventor： Hsu-Chih Cheng , Ying-Chieh Chen , Chi-Tong Hsieh
CPC classification number: H02J7/0044 , B64C39/024 , B64C2201/108 , B64C2201/201 , H02J7/0052
Abstract: A charge device for a drone includes a base and a covering mechanism. The base has a charge portion. The covering mechanism includes two covers, two first position-limiting components and two second position-limiting components. The two covers are movably disposed on the base. The covers are adapted to move toward each other to become a closed state and cover the charge portion, and the covers are adapted to move away from each other to become an expanded state and expose the charge portion. The first position-limiting components are connected to the covers respectively. Each of the second position-limiting components is connected between the covers. When the covers are in the closed state, the first position-limiting components and the second position-limiting components are located above the charge portion. When the covers are in the expanded state, the first position-limiting components and the second position-limiting components are away from the charge portion.
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公开(公告)号：US10053217B2
公开(公告)日：2018-08-21
申请号：US14845988
申请日：2015-09-04
Applicant: LG ELECTRONICS INC.
Inventor： Taehoon Cho , Choonghwan Shin
IPC: B64C39/02 , B60P3/11 , B64F1/22 , A62C3/02 , G05D1/00 , G05D1/10 , G08G1/09 , G08G1/16 , B60Q1/52 , G08G1/04 , G08G1/0955 , G08G1/00
CPC classification number: B64C39/024 , A62C3/0242 , B60P3/11 , B60Q1/525 , B60Q7/00 , B60Q7/005 , B64C2201/027 , B64C2201/042 , B64C2201/08 , B64C2201/108 , B64C2201/122 , B64C2201/123 , B64C2201/126 , B64C2201/127 , B64C2201/128 , B64C2201/141 , B64C2201/185 , B64C2201/201 , B64C2201/208 , B64D1/16 , B64F1/222 , G05D1/0088 , G05D1/0094 , G05D1/101 , G08G1/04 , G08G1/09 , G08G1/0955 , G08G1/16 , G08G1/162 , G08G1/205 , G08G7/00
Abstract: An unmanned aerial vehicle according to the present invention includes a housing mounted on a vehicle and having an inner space, the housing provided with a launching unit, an unmanned aerial vehicle accommodated in the housing and configured to be launched from the housing when a driving state of the vehicle meets a preset condition, wing units mounted to the unmanned aerial vehicle and configured to allow the flight of the unmanned aerial vehicle in response to the launch from the housing, an output unit disposed on the unmanned aerial vehicle, and a controller configured to control the wing units to move the unmanned aerial vehicle to a position set based on information related to the driving state when the unmanned aerial vehicle is launched, and control the output unit to output warning information related to the driving state.
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公开(公告)号：US20180178912A1
公开(公告)日：2018-06-28
申请号：US15905572
申请日：2018-02-26
Applicant: International Business Machines Corporation
Inventor： Jeanette L. Blomberg , Eric K. Butler , Anca A. Chandra , Pawan R. Chowdhary , Thomas D. Griffin , Divyesh Jadav , Sunhwan Lee , Robert J. Moore , Hovey R. Strong, Jr.
CPC classification number: B64C39/024 , B64C2201/128 , B64C2201/201 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64F1/007 , B64F1/222 , B64F1/32 , B64F1/36 , B64F1/368
Abstract: Embodiments of the present invention provide an apparatus comprising a body including a cavity for storing one or more packages, and a conveyor belt disposed above a top surface of the body. The belt is shaped to receive one or more packages, and the belt is controllable to rotate a package placed on the belt either from the top surface to the cavity for storage or from the cavity to the top surface for dispatch. A package comprises at least one of a drone and a payload transported by the drone. The apparatus further comprises a landing mechanism for stabilizing a drone landing on the apparatus.
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189.发明授权公开(公告)号：US09977435B2
公开(公告)日：2018-05-22
申请号：US15040985
申请日：2016-02-10
Applicant: AeroVironment, Inc.
Inventor： Christopher Eugene Fisher , Jason Sidharthadev Mukherjee , William Arden Lott , Eric James Aagaard
IPC: G05D1/10 , B64C29/02 , B64D47/08 , G05D1/00 , B60L11/18 , B64D1/02 , G08G5/00 , B64C39/02 , B64F1/22 , G06T11/60
CPC classification number: G05D1/102 , B60L11/1824 , B60L2200/10 , B60L2230/22 , B64C29/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/088 , B64C2201/104 , B64C2201/127 , B64C2201/141 , B64C2201/165 , B64C2201/201 , B64D1/02 , B64D47/08 , B64F1/222 , G05D1/0088 , G06Q10/08 , G06T11/60 , G08G5/0034 , G08G5/0039 , G08G5/0069 , G08G5/0091
Abstract: A method of migrating unmanned aerial vehicle (UAV) operations between geographic survey areas, including: uploading a first plurality of flight missions into a first UAV pod; deploying the UAV pod; autonomously launching the UAV from the UAV pod a plurality of times to perform the first plurality of flight missions; providing first survey data from the UAV to the UAV pod; autonomously migrating the UAV from the first UAV pod to a second UAV pod; receiving a second plurality of flight missions in a second UAV pod; providing the UAV with one of the second plurality of flight missions from the second UAV pod; autonomously launching the UAV from the second UAV pod a plurality of times to perform the second plurality of flight missions; and providing a second survey data from the UAV to the second UAV pod; where the autonomous migrating of the UAV to accomplish the first and second survey data happens autonomously and without active human intervention.
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公开(公告)号：US09950814B1
公开(公告)日：2018-04-24
申请号：US15658080
申请日：2017-07-24
Applicant: Amazon Technologies, Inc.
Inventor： Brian C. Beckman , Nicholas Bjone
IPC: B61D15/00 , B60L11/18 , B64F5/40 , B65D88/12 , B61D49/00 , B61D19/00 , B61L25/02 , B61D3/16 , G08G5/00 , B64D45/00 , B64F1/32 , B64F1/22 , B64C39/02 , G06Q10/08 , B25J11/00 , B61D17/04
CPC classification number: B64F5/40 , B60L11/1822 , B60L2200/10 , B61D3/16 , B61D15/00 , B61D17/04 , B61D19/001 , B61D49/00 , B61L15/0027 , B61L23/00 , B61L23/04 , B61L25/025 , B61L2205/04 , B64C39/024 , B64C2201/027 , B64C2201/128 , B64C2201/201 , B64C2201/205 , B64C2201/208 , B64D45/00 , B64D2045/0085 , B64F1/22 , B64F1/32 , G06Q10/0832 , G08G5/0069
Abstract: Intermodal vehicles may be loaded with items and an aerial vehicle, and directed to travel to areas where demand for the items is known or anticipated. The intermodal vehicles may be coupled to locomotives, container ships, road tractors or other vehicles, and equipped with systems for loading one or more items onto the aerial vehicle, and for launching or retrieving the aerial vehicle while the intermodal vehicles are in motion. The areas where the demand is known or anticipated may be identified on any basis, including but not limited to past histories of purchases or deliveries to such areas, or events that are scheduled to occur in such areas. Additionally, intermodal vehicles may be loaded with replacement parts and/or inspection equipment, and configured to conduct repairs, servicing operations or inspections on aerial vehicles within the intermodal vehicles, while the intermodal vehicles are in motion.
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