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公开(公告)号：EP2691300B1
公开(公告)日：2015-01-21
申请号：EP12717216.1
申请日：2012-03-26
Applicant: Prox Dynamics AS
Inventor： MUREN, Petter
CPC classification number: B64C39/024 , A63H27/12 , B64C39/028 , B64C2201/024 , B64C2201/127 , B64C2201/201 , B64C2201/203 , B64C2203/00 , B64D47/08
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公开(公告)号：EP1594736B1
公开(公告)日：2012-12-19
申请号：EP04809283.7
申请日：2004-02-19
Applicant: AAI CORPORATION
Inventor： MILLER, Stephen, W. , VELAZQUEZ, Matthew, T.
IPC: B64F1/04
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/084 , B64C2201/102 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64F1/06
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公开(公告)号：EP1761430A2
公开(公告)日：2007-03-14
申请号：EP05761246.7
申请日：2005-04-14
Applicant: Arlton, Paul E. , Arlton, David J.
Inventor： Arlton, Paul E. , Arlton, David J.
IPC: B64C27/10
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.
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公开(公告)号：EP1594736A2
公开(公告)日：2005-11-16
申请号：EP04809283.7
申请日：2004-02-19
Applicant: AAI CORPORATION
Inventor： MILLER, Stephen, W. , VELAZQUEZ, Matthew, T.
IPC: B64B1/00
CPC classification number: B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/084 , B64C2201/102 , B64C2201/165 , B64C2201/201 , B64C2201/203 , B64F1/06
Abstract: A portable unmanned air vehicle and launcher system is provided that includes a foldable unmanned air vehicle having a pressure tube; a launch gas reservoir for holding launch gas; a launch tube operatively connected to the launch gas reservoir and having a free end that is positioned in the pressure tube of the air vehicle; a free piston positioned within the launch tube; and a free piston stop to prevent the free piston from leaving the launch tube. A first portion of the launch gas in the launch gas reservoir is released into the launch tube and forces the free piston from an initial position to an end position at which the free piston is stopped by the free piston stop.
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公开(公告)号：KR101863157B1
公开(公告)日：2018-06-07
申请号：KR20180014680
申请日：2018-02-06
CPC classification number: B64C39/024 , A45C11/00 , B64C1/30 , B64C25/10 , B64C27/08 , B64C2025/325 , B64C2201/024 , B64C2201/108 , B64C2201/203
Abstract: 본발명은, 무인비행체에있어서, 배터리를포함하는상기무인비행체의제어, 전원공급을위한제어부를수용가능하게상하방향으로설정된높이를갖는본체와; 접혀지는프로펠러와상기프로펠러를구동시키는구동부를지지가능하게상기본체에결합된복수의아암과; 상기본체가착륙할수 있도록상기각 아암에결합된랜딩부와: 상기아암은, 상기본체에결합된고정아암과, 상기고정아암에서연장된폴딩아암을구비하되, 상기폴딩아암은인접한상기고정아암을향하여순차적으로접혀지도록상기폴딩아암및 상기고정아암에결합된아암폴딩부;를포함하는것을특징으로한다. 이에, 본발명에따르면, 보다간단하고편리하게무인비행체의구성을접어서휴대용가방에보관하여운반이가능한접이식무인비행체를제공할수 있다.
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Patent Agency Ranking
公开(公告)号：US20190200736A1
公开(公告)日：2019-07-04
申请号：US15861475
申请日：2018-01-03
Applicant: Thomas Tong
Inventor： Thomas Tong
CPC classification number: A45F3/14 , A45F3/04 , A45F5/02 , A45F2003/142 , A45F2200/05 , B64C27/08 , B64C2201/203
Abstract: Strapping system to enable any ordinary backpack to become a drone carrier.
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公开(公告)号：US20180273166A1
公开(公告)日：2018-09-27
申请号：US15995419
申请日：2018-06-01
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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公开(公告)号：US20170225782A1
公开(公告)日：2017-08-10
申请号：US15268225
申请日：2016-09-16
Applicant: Nixie Labs, Inc.
Inventor： Christoph Kohstall , Jelena Jovanovic , Dylan Owens , Nathan Leefer , Ben Sampson
CPC classification number: B64C39/024 , B64C1/063 , B64C1/30 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/20 , B64C2201/203 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64D47/08 , B64F5/10
Abstract: Stowable and deployable unmanned aerial vehicles (UAVs), and associated systems and methods are disclosed. A UAV in accordance with a particular embodiment includes a main body, frames carried by the main body, and motors carried by the frames. At least two frames are positioned to move relative to each other between a stowed configuration in which the frames are generally aligned proximate to each other and a deployed configuration different from the stowed configuration. The main body can include a first body portion pivotably connected to a second body portion. In a stowed configuration, the body portions can generally overlap each other. A UAV in accordance with particular embodiments includes a modular electronics unit carried by the UAV and including a camera, a battery, and a vehicle controller. Modular electronics units can be configured to be removably connected to and disconnected from the UAV and other vehicles.
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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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公开(公告)号：US20160176520A1
公开(公告)日：2016-06-23
申请号：US14973466
申请日：2015-12-17
Applicant: Ryan Michael Goldstein
Inventor： Ryan Michael Goldstein
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.
Abstract translation: 公开了能够从打开的飞行结构移动到封闭构造的无人驾驶飞行器的车辆，其中所有主要飞行部件都可以被外壳保护。 在封闭结构中，车辆可以采取标准的几何形状，例如矩形棱柱，球形，圆柱体或另一种形状，从而不能被识别为无人机。 车辆的实施例还可以包括可互换的和/或无线的电动机臂，仅当处于开放构造时电动连接到车辆的其余部分的电动机臂，可拆卸地附接到车辆的其余部分的遥控器以及夹子或其他附接机构 用于附着到诸如背包的物体上。
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