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公开(公告)号：US20180065745A1
公开(公告)日：2018-03-08
申请号：US15698341
申请日：2017-09-07
Applicant: Flytrex Aviation Ltd.
Inventor： Yariv BASH , Amit REGEV , Vadim ZLOTNIK
CPC classification number: B64C39/024 , B64C2201/185 , B64D17/80 , B64D31/04 , B64D31/06
Abstract: A navigation termination system of an unmanned vehicle (UV) is provided. The system includes a plurality of sensors connected to the UV and configured to detect motion of the UV; a power supply configured to power the movement of the UV; a processing circuitry; and a memory, the memory containing instructions that, when executed by the processing circuitry, configure the system to: determine, based on sensory signals captured by the plurality of sensors, a navigation termination event; and disrupt a connection between the power supply and a motion mechanism of the UV when the navigation termination event occurs.
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公开(公告)号：US20180050805A1
公开(公告)日：2018-02-22
申请号：US15556649
申请日：2016-03-10
Applicant: KAPI electronics GmbH
Inventor： Holger Kalinka
CPC classification number: B64D17/72 , B64C39/024 , B64C2201/185 , B64D17/80 , B64D25/12 , B64D45/00 , B64D2045/0085
Abstract: The invention relates to a method and a device for an intelligent parachute rescue system for manned and unmanned aerial vehicles (14), wherein no pyrotechnic propellants are used, but compressed air (4a) extracted from a pressure bottle (4).
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公开(公告)号：US20170225792A1
公开(公告)日：2017-08-10
申请号：US15503089
申请日：2015-08-11
Applicant: DroneTech Studio, LLC
Inventor： Liang Wang , Daniel Joseph Bodenstein , Ryan Michael Welsh , Kevin Ian McWilliams
CPC classification number: B64D17/70 , B64C39/024 , B64C2201/185 , B64D17/80
Abstract: Various embodiments of the present disclosure relate to a parachute deployment system for an unmanned aerial vehicle (UAV). In some examples, the parachute deployment system includes a base attached to the unmanned aerial vehicle, a deployment tray mechanically connected to the base, an acceleration mechanism for propelling the deployment tray away from the base, a parachute cover releasably secured over the deployment tray, a parachute stowed between the deployment tray and the parachute cover, and a triggering mechanism. Upon activation of the triggering mechanism, the parachute cover is released and the deployment tray is propelled away from the base, which rapidly deploys the parachute away from the UAV.
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公开(公告)号：US09716862B1
公开(公告)日：2017-07-25
申请号：US13668397
申请日：2012-11-05
Applicant: The Boeing Company
Inventor： Joseph Wilbur Evans
IPC: H04N7/18
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/046 , B64C2201/082 , B64C2201/088 , B64C2201/12 , B64C2201/123 , B64C2201/185 , H04N7/185
Abstract: Systems and methods for capturing situational awareness information are provided. The systems and methods include a portable aircraft configured to obtain situational awareness information. The portable aircraft includes a body including deployable wings, a stability device coupled to the body, the stability device including deployable tail fins, a propulsion device configured to propel the portable aircraft aloft, a capture device configured to selectively capture situational information, and a communications device configured to transmit captured situational information to a ground based receiver.
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公开(公告)号：US20170101180A1
公开(公告)日：2017-04-13
申请号：US15391517
申请日：2016-12-27
Applicant: Richard D. Adams
Inventor： Richard D. Adams
CPC classification number: B64C39/024 , B64C1/26 , B64C3/56 , B64C2201/104 , B64C2201/107 , B64C2201/123 , B64C2201/127 , B64C2201/162 , B64C2201/185 , B64C2201/203 , B64D17/00 , B64D17/80
Abstract: A remotely controlled or autonomously controlled UAV is disclosed. The UAV has both wings and a deployable parachute to enable both fixed wing flight and paraglider flight. The UAV can fly at a higher speed to a mission area as a fixed wing craft, and loiter over the area as a powered paraglider. In some embodiments, the wings are jettisoned over the mission area and the UAV configured as a powered paraglider completes its mission. In other embodiments the UAV flies to the mission area as a fixed wing craft, deploys the parachute to loiter as a powered paraglider and then jettisons the parachute to fly under a fixed wing back to a base. The former embodiment cannot fly back to a base, they may be used to carry and deploy bombs or grenades, while the latter may be used for surveillance, deliver supplies or the like.
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Patent Agency Ranking
公开(公告)号：US09611044B2
公开(公告)日：2017-04-04
申请号：US15111147
申请日：2015-10-12
Applicant: Skycat Oy
Inventor： Henri Hiisilä
CPC classification number: B64D17/70 , B64C39/024 , B64C2201/128 , B64C2201/146 , B64C2201/185 , B64D1/04 , B64D1/12 , B64D7/08 , B64D17/64 , B64D25/00 , F41A19/58 , F41B7/00 , F41F1/00
Abstract: The object of this invention is a method to shoot an object from a flying apparatus. Into an flying apparatus, into certain part of it, like a container that consists at least of a bottom and a shell a spring will be placed, like a push spring that has been loaded in a tense state and that is locked in this position using a fixing organ and further there will be put as an extension of the spring an object to be shot out from the flying apparatus. The fixing organ is thread, metal cord, bar, strip, rope, line, or some combination of these and tension strength (T) is greater than the tension load of the push force (F) to the mentioned fixing organ. the tension strength (T) of the fixing organ is weakened to be less than the mentioned tension load by heating, burning, or melting the mentioned fixing organ by electric energy when the fixing organ breaks, the spring expands into the direction of the object and the push force (F) pushes the object out of the container and off the flying apparatus. The apparatus that is used in the present method is also an object of the invention.
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公开(公告)号：US20160001878A1
公开(公告)日：2016-01-07
申请号：US14768476
申请日：2014-02-06
Applicant: NES&TEC CO.,LTD.
Inventor： Ki-Seong LEE
CPC classification number: B64C27/28 , B64C3/38 , B64C3/58 , B64C9/323 , B64C39/024 , B64C2201/088 , B64C2201/108 , B64C2201/185 , B64C2201/187
Abstract: Disclosed is an easy landing drone. The drone includes: a propeller changing direction; a propeller tower supporting the propeller; a body connected to the propeller tower; a main wing arranged left-right symmetrically with respect to a horizontal axis of the body and having a pair of holes around a center of gravity of the body; a pair of auxiliary wings disposed in the pair of holes, respectively; and an actuator connected to a base shaft fixed to the main wing through the pair of auxiliary wings and controlling angles of the pair of auxiliary wings.
Abstract translation: 披露了一个简单的降落无人机。 无人机包括：螺旋桨改变方向; 支撑螺旋桨的螺旋桨塔; 连接到螺旋桨塔的主体; 主翼相对于主体的水平轴对称地布置，并且具有围绕主体的重心的一对孔; 一对辅助翼分别设置在该对孔中; 以及致动器，其通过所述一对辅助翼连接到固定到所述主翼的基轴，并且控制所述一对辅助翼的角度。
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公开(公告)号：US20120175468A1
公开(公告)日：2012-07-12
申请号：US13026061
申请日：2011-02-11
Applicant: Eric Zerof
Inventor： Eric Zerof
CPC classification number: B64D1/16 , A62C3/0228 , A62C3/0242 , B64C39/024 , B64C2201/042 , B64C2201/145 , B64C2201/185 , G05D1/101
Abstract: A system for delivering cooling water to building roofs by means of drone aircraft is disclosed. Control systems for navigation and precisely targeting a water spray are disclosed.
Abstract translation: 公开了一种通过无人驾驶飞机将冷却水输送到建筑物屋顶的系统。 公开了用于导航和精确瞄准喷水的控制系统。
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9.发明申请公开(公告)号：US20060102798A1
公开(公告)日：2006-05-18
申请号：US11030379
申请日：2005-01-06
Applicant: Beverly Cox , Hampton Dews , Nicholas Nyroth
Inventor： Beverly Cox , Hampton Dews , Nicholas Nyroth
CPC classification number: B64C39/024 , B64C1/26 , B64C3/14 , B64C13/20 , B64C39/08 , B64C2201/021 , B64C2201/102 , B64C2201/104 , B64C2201/123 , B64C2201/126 , B64C2201/127 , B64C2201/128 , B64C2201/141 , B64C2201/146 , B64C2201/165 , B64C2201/185
Abstract: The present invention provides an unmanned airborne reconnaissance vehicle having a fuselage, a forward wing pair and a rearward wing pair vertically separated by a gap and staggered fore and aft therebetween such that a general biplane configuration is formed. The present invention provides a pair of wing tip plates for joining the wing tips of the forward and rearward wings. The unmanned airborne reconnaissance vehicle of the present invention includes a power plant to propel the vehicle through the air and a generally T-shaped tail having a vertical stabilizer including a rudder and a full span elevator.
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公开(公告)号：US06685140B2
公开(公告)日：2004-02-03
申请号：US10255185
申请日：2002-09-26
Applicant: Ernest A. Carroll
Inventor： Ernest A. Carroll
IPC: B64C2556
CPC classification number: B64C39/028 , B64C39/024 , B64C2201/044 , B64C2201/104 , B64C2201/123 , B64C2201/127 , B64C2201/146 , B64C2201/165 , B64C2201/185 , B64D17/80 , F02B75/34 , F02D35/0069 , F02D41/2406 , F02D2200/0414 , F02D2200/703 , F02D2400/06 , F02D2400/11 , G05D1/101
Abstract: A miniature, unmanned aircraft having a parachute which deploys automatically under certain conditions. The aircraft has a flight control system based on remotely generated signals, potentially achieves relatively high altitude flight for a remotely controlled aircraft, and can thus operate well beyond line-of-sight control. For safety, an automatically deployed parachute system is provided. The parachute deployment system includes a folded parachute and a propulsion system for expelling the parachute from the aircraft. Preferably, a microprocessor for flight management sends intermittent inhibitory signals to prevent unintended deployment. A deployment signal is generated, illustratively, when the microprocessor fails, when engine RPM fall below a predetermined threshold, and when the aircraft strays from predetermined altitude and course.
Abstract translation: 具有降落伞的微型无人机在某些条件下自动部署。 该飞机具有基于远程产生的信号的飞行控制系统，可能为远程控制的飞机实现相对高的高度飞行，并且因此可以远远超出视线控制。 为了安全起见，提供了自动部署的降落伞系统。 降落伞部署系统包括折叠的降落伞和用于从降落伞排出飞机的推进系统。 优选地，用于飞行管理的微处理器发送间歇性抑制信号以防止意外部署。 例如，当微处理器发生故障时，当发动机转速低于预定阈值时，以及当飞行器从预定高度和当然时间偏离时，产生部署信号。
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