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公开(公告)号：US3980259A
公开(公告)日：1976-09-14
申请号：US564639
申请日：1975-04-02
CPC classification number: B64C39/024 , B64D17/80 , B64C2201/048 , B64C2201/084 , B64C2201/104 , B64C2201/105 , B64C2201/107 , B64C2201/146 , B64C2201/167 , B64C2201/182 , B64C2201/205 , Y10S244/902
Abstract: A powered remotely piloted vehicle which is not controllable at the low landing speeds necessary for landing on a platform of small area is provided with a para-foil type wing deployable at the beginning of a recovery sequence, and is further provided with a rocket ejectable line which is passed to the landing platform and winched in so that the composite flight vehicle and deployed para-foil wing is drawn towards the platform after the manner of a kite.
Abstract translation: 在低平台上不能控制的低功率遥控车辆在降落在小平台的平台上所需的底盘上设置有可在恢复顺序开始时展开的对箔型翼，并且还设置有火箭弹出线 将其传递到着陆平台并绞盘，使得复合飞行器和部署的对箔翼沿着风筝的方式被吸引到平台上。
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公开(公告)号：US20180194445A1
公开(公告)日：2018-07-12
申请号：US15914162
申请日：2018-03-07
Applicant: Rujing Tang
Inventor： Rujing Tang
CPC classification number: B63C9/01 , B63C2009/0023 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/12 , B64C2201/128 , B64C2201/205 , G16H40/67
Abstract: A drone equipped with a camera, a wireless communication module, an acoustic sensor, a GPS receiver, software and collapsible floatation device patrols above swimmers. The camera and acoustic sensor capture the video and audio of the swimmers. The information is either streamed to a command center or processed by the onboard software. With audio and video analysis capabilities, software is used to detect a swimmer in distress (SID). Alternatively the information is streamed to lifeguard or volunteers all over the world to spot SID. Another detection method is to let swimmer wear a wearable emergency notification device, which sends wireless signals comprising GPS location data. A SID presses a button to indicate rescue request and the drones fly over by GPS signal guidance. Solar power is used as the optional power source of the drones, which would allow the to sustain operation for a prolonged period of time. Once a SID is identified, the drone or drones fly over the SID and drops the collapsible floatation device.
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公开(公告)号：US20180086452A1
公开(公告)日：2018-03-29
申请号：US15279133
申请日：2016-09-28
Applicant: Intel Corporation
Inventor： Simon Hunt , Neeta Srivastava
CPC classification number: B64C39/024 , B64C2201/128 , B64C2201/14 , B64C2201/205 , B64C2201/206 , B64C2201/208 , G06Q10/0835
Abstract: In an example, there is disclosed a drone operator computing apparatus having: a network interface; and one or more logic elements providing a broker agent to: communicatively couple to a drone brokerage engine via the network interface; send a carrier request comprising a request for a carrier to carry a drone through a prohibitive zone; receive a brokered carrier response comprising an engage point; and dispatch the drone to the engage point. There is also disclosed a drone having a navigation engine to proceed to the engage point and engage a carrier. There is also disclosed a brokerage engine to broker a carrier request from the drone operator, receive a carrier response from a carrier operator, and broker the carrier response.
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24.发明申请公开(公告)号：US20170369185A1
公开(公告)日：2017-12-28
申请号：US15194492
申请日：2016-06-27
Applicant: Insitu, Inc.
Inventor： Matthew Grubb
CPC classification number: B64F1/02 , B64C39/024 , B64C2201/08 , B64C2201/182 , B64C2201/205
Abstract: Locking line capture devices for unmanned aircraft, and associated systems and methods are disclosed herein. A representative system includes a line capture body having a line slot with an open end and closed end, and a retainer positioned proximate the line slot and movable between first position in which the retainer blocks access to the line slot and a second position in which the retainer allows access to the line slot. A locking device is operably coupled between the capture body and the retainer and is movable between an unlocked position to allow movement of the retainer between the first and second positions, and a locked position to block such movement. A release device is operably coupled to the locking device and movable between a secured position with the locking device secured in the locked position, and a released position with the locking device movable between the locked and unlocked positions.
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公开(公告)号：US20170291720A1
公开(公告)日：2017-10-12
申请号：US15581911
申请日：2017-04-28
Applicant: AeroVironment, Inc.
Inventor： John Peter Zwaan , Robert James Johnston , Cris James Cornell , Philip Martin Finn , Glenn Arnold Blevins , David Wayne Ganzer
CPC classification number: B64F1/02 , B63B17/00 , B63B35/52 , B64C39/024 , B64C2201/02 , B64C2201/021 , B64C2201/104 , B64C2201/182 , B64C2201/205 , B64F1/025
Abstract: Systems, devices, and methods for impacting, by a small unmanned aerial vehicle (SUAV), a net having at least three sides; and converting the kinetic energy of the SUAV into at least one of: elastic potential energy of one or more tensioned elastic cords connected to at least one corner of the net, gravitational potential energy of a frame member connected to at least one corner of the net, rotational kinetic energy of the frame member connected to at least one corner of the net, and elastic potential energy of the frame member connected to at least one corner of the net.
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Patent Agency Ranking
公开(公告)号：US09718564B1
公开(公告)日：2017-08-01
申请号：US15461038
申请日：2017-03-16
Applicant: Amazon Technologies, Inc.
Inventor： Brian C. Beckman , Nicholas Bjone
IPC: B64F5/40 , G06Q10/08 , B64C39/02 , B64F1/22 , B64F1/32 , B64D45/00 , G08G5/00 , B61D3/16 , B61D15/00 , B61L25/02 , B61D19/00 , B61D49/00 , B65D88/12 , B61D17/04 , B25J11/00
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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公开(公告)号：US20170183106A1
公开(公告)日：2017-06-29
申请号：US15372287
申请日：2016-12-07
Applicant: POSTECH ACADEMY-INDUSTRY FOUNDATION
Inventor： Son Cheol YU , Ju Hyun PYO , Han Gil JOE , Hyeon Woo CHO , Byeong Jin KIM
CPC classification number: B64F1/025 , B63B2702/12 , B63G8/001 , B63G2008/002 , B64C39/024 , B64C2201/024 , B64C2201/18 , B64C2201/182 , B64C2201/201 , B64C2201/205 , B64D45/08 , B64F1/007 , B64F1/04
Abstract: Provided is an apparatus for recovering and launching an unmanned aerial vehicle. The apparatus for recovering and launching the unmanned aerial vehicle includes a main body that includes a storage space in which the unmanned aerial vehicle is stored, an inclined platform that forms an inclined surface which is connected between a fixed bar fixed in the main body and a moving bar moved to an opened upper portion of the main body and collides with the unmanned aerial vehicle induced to approach a side of the main body, a band member of which one end is connected to the moving bar and the other end is rolled up in a roll shape and stored in the storage space of the main body, and a driving motor that rotationally drives a rotor circumscribed with the band member in a normal direction or reverse direction, so that the moving bar is moved with respect to the fixed bar, wherein the inclined surface is formed by unfolding the inclined platform, the unmanned aerial vehicle colliding with the inclined surface is recovered to the storage space, and then the inclined platform is folded.
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公开(公告)号：US20170066543A1
公开(公告)日：2017-03-09
申请号：US14845615
申请日：2015-09-04
Applicant: LOCKHEED MARTIN CORPORATION
Inventor： Russell M. SYLVIA
CPC classification number: B64F1/04 , B63G8/28 , B63G2008/008 , B64C39/024 , B64C2201/08 , B64C2201/088 , B64C2201/20 , B64C2201/201 , B64C2201/205
Abstract: A payload launch system that uses an inflatable air bag ram to launch a payload, such as an unmanned aerial vehicle, from a launch chamber of a launch tube. The air bag ram seals with the interior surface of the launch tube to isolate a dump valve that controls the flow of compressed gas from a gas storage chamber into the air bag ram. The air bag ram sealing with the interior surface of the launch tube isolates the dump valve, both pre-launch and post-launch, from any water or debris carried in with water in which the payload launch system is disposed
Abstract translation: 一种有效载荷发射系统，其使用可充气气囊冲压器从发射管的发射室发射有效载荷，例如无人驾驶飞行器。 气囊柱塞与发射管的内表面密封，以隔离一个排气阀，其将压缩气体从气体储存室流入气囊冲头。 与发射管内表面密封的气囊柱塞将排放阀（预发射和发射后）与运载有有效载荷发射系统的水携带的任何水或碎屑隔离
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公开(公告)号：US20170057635A1
公开(公告)日：2017-03-02
申请号：US14843329
申请日：2015-09-02
Applicant: THE BOEING COMPANY
Inventor： James David Strayer
CPC classification number: B64C39/024 , B63G3/04 , B63G2008/004 , B63G2008/008 , B64C2201/027 , B64C2201/088 , B64C2201/108 , B64C2201/167 , B64C2201/201 , B64C2201/205
Abstract: A drone launch system includes a canister defining an internal cavity, and a drone positioned within the internal cavity in a stowed state. The drone is configured to be ejected from the canister and transition from the stowed state into a deployed state outside of the canister. A method for launching a drone, the method includes positioning the drone in a stowed state in an internal cavity of a canister, ejecting the drone from the canister, and transitioning the drone into a deployed state after the ejecting operation.
Abstract translation: 无人机发射系统包括限定内部空腔的罐和位于收纳状态的内部空腔内的无人机。 无人机被配置为从罐排出并从收起状态转换到罐外部的展开状态。 一种用于发射无人机的方法，该方法包括将无人机处于收起状态，将其从罐中排出，将喷射器从罐排出，并且在喷射操作之后将无人机转换成展开状态。
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公开(公告)号：US09434471B2
公开(公告)日：2016-09-06
申请号：US13899252
申请日：2013-05-21
Applicant: Paul E Arlton , David J Arlton
Inventor： Paul E Arlton , David J Arlton
CPC classification number: B64C27/605 , B64C7/00 , B64C27/10 , B64C27/14 , B64C39/024 , 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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