公开(公告)号：US20190200736A1

公开(公告)日：2019-07-04

申请号：US15861475

申请日：2018-01-03

申请人： Thomas Tong

发明人： Thomas Tong

IPC分类号： A45F3/14 ,  A45F3/04 ,  A45F5/02

CPC分类号： A45F3/14 ,  A45F3/04 ,  A45F5/02 ,  A45F2003/142 ,  A45F2200/05 ,  B64C27/08 ,  B64C2201/203

摘要： Strapping system to enable any ordinary backpack to become a drone carrier.

公开(公告)号：US20180273166A1

公开(公告)日：2018-09-27

申请号：US15995419

申请日：2018-06-01

申请人： Paul E. ARLTON ,  David J. ARLTON

发明人： Paul E. ARLTON ,  David J. ARLTON

IPC分类号： B64C27/605 ,  B64C27/10 ,  B64C27/14 ,  B64C39/02 ,  B64C7/00 ,  B64C27/82

CPC分类号： 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

摘要： 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.

公开(公告)号：US20170225782A1

公开(公告)日：2017-08-10

申请号：US15268225

申请日：2016-09-16

申请人： Nixie Labs, Inc.

发明人： Christoph Kohstall ,  Jelena Jovanovic ,  Dylan Owens ,  Nathan Leefer ,  Ben Sampson

IPC分类号： B64C39/02 ,  B64C1/06 ,  B64F5/10 ,  B64D47/08

CPC分类号： 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

摘要： 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.

公开(公告)号：US20170101180A1

公开(公告)日：2017-04-13

申请号：US15391517

申请日：2016-12-27

申请人： Richard D. Adams

发明人： Richard D. Adams

IPC分类号： B64C39/02 ,  B64C1/26 ,  B64D17/80

CPC分类号： B64C39/024 ,  B64C1/26 ,  B64C3/56 ,  B64C2201/104 ,  B64C2201/107 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/162 ,  B64C2201/185 ,  B64C2201/203 ,  B64D17/00 ,  B64D17/80

摘要： 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.

公开(公告)号：US20160176520A1

公开(公告)日：2016-06-23

申请号：US14973466

申请日：2015-12-17

申请人： Ryan Michael Goldstein

发明人： Ryan Michael Goldstein

IPC分类号： B64C27/08 ,  B64C39/02

CPC分类号： B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/203

摘要： 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.

摘要翻译： 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。

公开(公告)号：US20140091172A1

公开(公告)日：2014-04-03

申请号：US13899252

申请日：2013-05-21

申请人： Paul E. Arlton ,  David J. Arlton

发明人： Paul E. Arlton ,  David J. Arlton

IPC分类号： B64C27/10

CPC分类号： 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

摘要： 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.

摘要翻译： 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。

公开(公告)号：US08469307B2

公开(公告)日：2013-06-25

申请号：US13270872

申请日：2011-10-11

申请人： Paul E Arlton ,  David J Arlton

发明人： Paul E Arlton ,  David J Arlton

IPC分类号： B64C27/10 ,  B64C27/54 ,  B64C27/58

CPC分类号： 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

摘要： 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.

摘要翻译： 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。

公开(公告)号：US07584925B2

公开(公告)日：2009-09-08

申请号：US11877201

申请日：2007-10-23

申请人： Stephen W. Miller ,  Matthew Velazquez

发明人： Stephen W. Miller ,  Matthew Velazquez

IPC分类号： B64C3/56 ,  B64F1/04

CPC分类号： B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64F1/06

摘要： A portable unmanned air vehicle and launcher system 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.

摘要翻译： 一种便携式无人机和发射系统，包括具有压力管的可折叠无人机; 用于发射气体的发射气藏; 操作地连接到发射气体储存器并具有位于空中载体的压力管中的自由端的发射管; 位于发射管内的自由活塞; 和自由活塞止挡件，以防止自由活塞离开发射管。 发射气体储存器中的发射气体的第一部分被释放到发射管中，并且将自由活塞从初始位置推动到自由活塞由自由活塞停止的终止位置。

公开(公告)号：US20080210818A1

公开(公告)日：2008-09-04

申请号：US11822278

申请日：2007-07-03

申请人： Tien-Seng Chiu ,  Jay Willmott ,  Kirk Jenkins

发明人： Tien-Seng Chiu ,  Jay Willmott ,  Kirk Jenkins

IPC分类号： B64C1/00 ,  B64C1/10 ,  A45C5/00

CPC分类号： B64C1/00 ,  A45C5/00 ,  A45C13/02 ,  B64C1/30 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/084 ,  B64C2201/102 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/165 ,  B64C2201/187 ,  B64C2201/201 ,  B64C2201/203

摘要： A modular unmanned aerial vehicle (UAV) having a fuselage, a nose cone, a left wing piece, a right wing piece, and a tail section. The tail section and nose cone each join to the fuselage through mating bulkhead structures that provide quick connection capability while being readily separated so as to enable the UAV to break apart at these connection points and thereby absorb or dissipate impact upon landing. The UAV is capable of rapid assembly in the field for two-man launch and data retrieval, as well as quick disassembly into these five component parts for transport and storage in a highly compact transport case that can be carried as a backpack.

摘要翻译： 具有机身，鼻锥，左翼片，右翼片和尾部的模块化无人驾驶飞行器（UAV）。 尾部和鼻锥每个通过配合的隔板结构连接到机身，提供快速的连接能力，同时易于分离，以便使UAV在这些连接点处分裂，从而吸收或消散着陆时的冲击。 无人机能够在现场快速组装两人发射和数据检索，以及快速拆卸到这五个部件中，用于运输和存储，可以作为背包携带的高度紧凑的运输箱。

公开(公告)号：US07204455B2

公开(公告)日：2007-04-17

申请号：US10481944

申请日：2002-06-28

申请人： Peter Logan Sinclair

发明人： Peter Logan Sinclair

IPC分类号： B64C33/02

CPC分类号： A63H31/08 ,  A63H27/008 ,  B64C33/02 ,  B64C39/028 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/148 ,  B64C2201/203

摘要： A drive assembly for use with a mechanical flying or walking device comprises an articulated member (7) having first and second portions (7a, 7b) arranged such that the portions move relative to each other, and a drive mechanism (9) for imparting motion to the articulated member. The drive mechanism (9) comprises: a drive member for imparting a cyclic motion on the articulated member, and a control member for controlling, in a predetermined manner, the relative position of the first and second portions during each cycle of the cyclic motion of the articulated member. In the case of a mechanical flying device, two such drive assemblies may be provided, the articulated member of each assembly forming a wing.

摘要翻译： 一种与机械飞行或步行装置一起使用的驱动组件包括铰接构件（7），其具有被布置成使得所述部分相对于彼此移动的第一和第二部分（7a，7b）以及驱动机构（9） 向铰接构件施加运动。 驱动机构（9）包括：驱动构件，用于在铰接构件上施加循环运动;以及控制构件，用于以预定方式控制第一和第二部分在循环运动的每个循环期间的相对位置 铰接构件。 在机械飞行装置的情况下，可以设置两个这样的驱动组件，每个组件的铰接构件形成翼。