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公开(公告)号：CN108945435A
公开(公告)日：2018-12-07
申请号：CN201810452187.7
申请日：2018-05-12
Applicant: 郑州航空港飘天下物联网科技有限公司
Inventor： 杨京广
CPC classification number: B64C39/026 , B64C2201/10 , B64C2201/185 , F04D29/522 , F04D29/703
Abstract: 本发明提供空中风帆及其工作原理，其包括安装架，悬浮器，固定杆，蓄电池，固定块，急救伞装置，连接管和顺风装置。安装架设置在顺风装置的下部；悬浮器安装在固定块的下部；固定杆设置在急救伞装置的下部；蓄电池固定在安装架的中间下部位置。本发明中定位器的设置，在空中风帆遗失后能够快速的进行定位并将其找到；转轴，扇叶和防护外壳设置，能够帮助空中风帆快速升空；伞体，连接绳和放置盒的设置，空中风帆在空中发生故障时能够将空中风帆安全的带回到地面，防止其直接坠落损毁，顺风装置的设置，可借助风力飞行及悬停。
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公开(公告)号：CN106828897A
公开(公告)日：2017-06-13
申请号：CN201611261420.0
申请日：2016-12-30
Applicant: 易瓦特科技股份公司
CPC classification number: B64C27/08 , B64C2201/024 , B64C2201/042 , B64C2201/10 , B64D1/18 , B64D27/24 , B64D47/00
Abstract: 本发明公开了一种防干扰无人机，属于无人机技术领域。该防干扰无人机，无人机包括机身、控制器、喷洒组件、多个旋翼、多个机臂以及内装有电池的电池仓，喷洒组件安装在机身上，多个旋翼通过机臂布置在机身外侧，用于控制无人机飞行的控制器安装在机身中，电池仓通过挂架安装在机身外部，挂架包括挂板、封闭板和多个挂杆，挂板和机身的底部相对设置，挂板朝向机身的侧面上设置有安装槽，电池仓安装在安装槽中，封闭板覆盖在安装槽上，挂杆的两端分别与挂板及机身固定连接。本发明使供控制器通讯所用的电池安装在机身外侧，即电池外置，以避免在无人机飞行时，电池对控制器产生的可能干扰，保证无人机在既定的路线上飞行。
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公开(公告)号：CN106585959A
公开(公告)日：2017-04-26
申请号：CN201610875465.0
申请日：2016-09-30
Applicant: 朱晓义
Inventor： 朱晓义
CPC classification number: B64C23/00 , B64C39/00 , B64C2201/10
Abstract: 本发明涉及一种产生更大升力的高速飞行器，包括壳体和发动机，在壳体的上部和/或机翼上部设有多个导入口与壳体内的螺旋通道相通，螺旋通道使流体围绕在螺旋中心一圈又一圈从壳体内周围经过，螺旋通道与发动机的吸气口相通，使壳体上下部之间产生压力差和更大的升力来源。本发明提供的飞行器在不增加任何动力的状态下，使上半部与下半部之间产生至少100多倍的压力差，由此发现一种比传统机翼大100多倍以上的升力来源，使飞行器的载重量显著增加，飞行速显著度提高，飞行半径成多倍增加，本发明的飞行器的功能已远远超出现在飞机的概念，由此产生一种真正高速节能的飞行器。
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公开(公告)号：CN106364667A
公开(公告)日：2017-02-01
申请号：CN201610859542.3
申请日：2016-09-28
Applicant: 韩建刚
Inventor： 韩建刚
CPC classification number: B60F5/02 , B64C21/04 , B64C39/00 , B64C39/001 , B64C2201/10
Abstract: 本发明提供了一种飞行器，包括：动力部，用于产生气流，包括一个或多个排气端；升力组件，包括翼体和一个或多个喷管，喷管设置在翼体的上翼面位置处并与排气端连接，喷管沿平行于翼体的上翼面的方向喷气或朝向翼体喷气。本发明的飞行器的升力来自于主动喷射气流，升力组件可以长时间以最佳的空气流速和迎角产生升力，受飞行状态和大气紊流影响较小，安全性好、升力效率更高；消除机翼悬臂梁结构，机翼与机身融为一体，结构简单、重量降低而强度提高；能够垂直起降，不依赖机场和跑道；飞行器水平投影尺寸接近机身尺寸，起降适应性好。
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公开(公告)号：EP2437980A4
公开(公告)日：2016-03-23
申请号：EP10784208
申请日：2010-06-04
Applicant: AEROVIRONMENT INC
Inventor： KEENNON MATTHEW TODD , KLINGEBIEL KARL ROBERT , ANDRYUKOV ALEXANDER , HIBBS BART DEAN , ZWAAN JOHN PETER
CPC classification number: B64C33/025 , B64C19/00 , B64C33/02 , B64C2201/025 , B64C2201/10 , B64C2201/146
Abstract: Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
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Patent Agency Ranking
公开(公告)号：US20180093171A1
公开(公告)日：2018-04-05
申请号：US15711695
申请日：2017-09-21
Applicant: SONY INTERACTIVE ENTERTAINMENT INC.
Inventor： Dominic Saul Mallinson
CPC classification number: A63F7/0664 , A63F7/0604 , A63F7/07 , A63F7/20 , A63F13/65 , A63F13/803 , A63H27/12 , A63H30/04 , B64C39/024 , B64C2201/10 , B64C2201/12 , B64C2201/146 , B64F1/04 , B65G51/00 , G05D1/0016
Abstract: An arena includes a porous surface through which an airflow is output, thereby providing lift for an unmanned aerial vehicle (UAV) to push the UAV away from the porous surface. The airflow may also provide thrust to push the UAV in a direction that is parallel to the porous surface. The UAV may include one or more propellers that can provide lift, thrust, or both to the UAV. The airflow may be modified over a duration of time to modify lift or thrust to the UAV. The airflow may be modified based on regions of the arena to modify lift or thrust in different regions of the arena. The arena may include a scoreboard to display a score that may be modified as a result of actions undertaken by the UAV. Two or more UAVs may be used to play a game via the arena.
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公开(公告)号：US20170129600A1
公开(公告)日：2017-05-11
申请号：US15345376
申请日：2016-11-07
Applicant: David Rancourt , Etienne Demers Bouchard
Inventor： David Rancourt , Etienne Demers Bouchard
CPC classification number: B64C39/022 , B64C1/00 , B64C19/02 , B64C29/0016 , B64C39/024 , B64C2201/042 , B64C2201/088 , B64C2201/10 , B64C2211/00 , B64D2221/00 , G05D1/104
Abstract: A vertical liftoff aircrafts system includes a plurality of unmanned wing structures configured for collective vertical liftoff; a plurality of tethers respectively connected to the plurality of wing structures; and a fuselage including a connector thereon for mechanically connecting the plurality of tethers. The fuselage includes a power pack for powering the plurality of wing structures via the plurality of tethers, whereby the plurality of wing structures is operatively interconnected to the fuselage with the plurality of tethers for lifting the fuselage. A method and a kit thereof also are disclosed.
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公开(公告)号：US08205823B2
公开(公告)日：2012-06-26
申请号：US12795539
申请日：2010-06-07
Applicant: Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
Inventor： Matthew Todd Keennon , Karl Robert Klingebiel , Alexander Andryukov , Bart Dean Hibbs , John Peter Zwaan
IPC: B64C33/00
CPC classification number: B64C33/025 , B64C19/00 , B64C33/02 , B64C2201/025 , B64C2201/10 , B64C2201/146
Abstract: Heavier-than-air, aircraft having flapping wings, e.g., ornithopters, where angular orientation control is effected by variable differential sweep angles of deflection of the flappable wings in the course of sweep angles of travel and/or the control of variable wing membrane tension.
Abstract translation: 比空中飞行器，具有扑翼的飞机，例如鸟巢飞机，其中角度定向控制是通过在扫掠角度行程和/或控制可变翼膜张力的过程中可展开的翼的偏转的可变差分扫掠角来实现的 。
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公开(公告)号：US07931239B2
公开(公告)日：2011-04-26
申请号：US11838040
申请日：2007-08-13
Applicant: Brad Pedersen , Peter Spirov
Inventor： Brad Pedersen , Peter Spirov
IPC: B64C13/20
CPC classification number: G05D1/0816 , B60V1/06 , B60V1/10 , B64C15/02 , B64C27/08 , B64C27/20 , B64C39/001 , B64C39/024 , B64C2201/042 , B64C2201/10 , B64C2201/108 , B64C2201/146 , B64D27/24 , G05D1/0016 , G05D1/0022 , G05D1/0858
Abstract: A homeostatic flying hovercraft preferably utilizes at least two pairs of counter-rotating ducted fans to generate lift like a hovercraft and utilizes a homeostatic hover control system to create a flying craft that is easily controlled. The homeostatic hover control system provides true homeostasis of the craft with a true fly-by-wire flight control and control-by-wire system control.
Abstract translation: 稳态飞行气垫船优选地使用至少两对反向旋转管道风扇来产生类似气垫船的升降机，并且利用稳态悬停控制系统来创建易于控制的飞行器。 稳态悬停控制系统通过真正的线控飞行控制和线控系统控制为飞行器提供真正的动态平衡。
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公开(公告)号：EP3363732A1
公开(公告)日：2018-08-22
申请号：EP18165126.6
申请日：2016-07-27
Applicant: Jetoptera, Inc.
Inventor： EVULET, Andrei
CPC classification number: B64D29/02 , B64C9/38 , B64C15/00 , B64C21/00 , B64C21/04 , B64C39/024 , B64C2201/10 , B64C2201/104 , B64D27/10 , B64D27/18 , B64D33/02 , B64D33/04 , B64D2033/0273 , Y02T50/166 , Y02T50/32 , Y02T50/44
Abstract: A vehicle having a main body (504), a primary airfoil (503) coupled to the main body, a gas generator (501) coupled to the main body and producing a gas stream, a conduit (505) fluidly coupled to the generator, an ejector (502) fluidly coupled to the conduit and embedded in the primary airfoil, the ejector comprising an outlet structure out of which the gas stream flows at a predetermined adjustable velocity and a secondary airfoil (506) having a leading edge (507) and located directly downstream of the outlet structure such that the gas stream from the ejector flows over the leading edge of the secondary airfoil.
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