-
公开(公告)号：EP3150483A4
公开(公告)日：2017-09-20
申请号：EP16811654
申请日：2016-06-15
Applicant: NAKAMURA KOHEI
Inventor： NAKAMURA KOHEI
CPC classification number: B64B1/30 , B64B1/58 , B64C25/06 , B64C27/08 , B64C39/02 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/101 , B64C2201/108 , B64C2201/127
Abstract: Provided is a buoyant aerial vehicle which can secure high safety by reducing the risk of crashing, and which can facilitate control of movement by suppressing the influence of wind and exhibit high mobility capability. The buoyant aerial vehicle is configured by including: a buoyant vehicle body in which gas having a specific gravity smaller than air is hermetically filled; a vertical propulsion propeller which provides vertical propulsive force to the buoyant vehicle body; and a horizontal propulsion propeller which provides horizontal propulsive force to the buoyant vehicle body, and is configured such that the buoyant vehicle body has horizontal wind passages formed in at least two directions, and has outer peripheral edges each formed into an acute angle in side view.
Abstract translation: 本发明提供一种浮力飞行器，其能够通过降低碰撞风险来确保较高的安全性，并且能够通过抑制风的影响来促进对运动的控制，并且具有高运动能力。 所述浮力飞行器通过包括：浮力车体，在所述浮力车体中气密地填充比重小于空气的气体; 向浮力车体提供垂直推进力的垂直推进螺旋桨; 以及向浮力车体提供水平推进力的水平推进螺旋桨，并且浮力车体具有形成在至少两个方向上的水平风道，并且具有在侧视图中形成为锐角的外周边缘 。
-
公开(公告)号：EP3150483A1
公开(公告)日：2017-04-05
申请号：EP16811654.9
申请日：2016-06-15
Applicant: Nakamura, Kohei
Inventor： Nakamura, Kohei
CPC classification number: B64B1/30 , B64B1/58 , B64C25/06 , B64C27/08 , B64C39/02 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/101 , B64C2201/108 , B64C2201/127
Abstract: Provided is a buoyant aerial vehicle which can secure high safety by reducing the risk of crashing, and which can facilitate control of movement by suppressing the influence of wind and exhibit high mobility capability. The buoyant aerial vehicle is configured by including: a buoyant vehicle body in which gas having a specific gravity smaller than air is hermetically filled; a vertical propulsion propeller which provides vertical propulsive force to the buoyant vehicle body; and a horizontal propulsion propeller which provides horizontal propulsive force to the buoyant vehicle body, and is configured such that the buoyant vehicle body has horizontal wind passages formed in at least two directions, and has outer peripheral edges each formed into an acute angle in side view.
Abstract translation: 本发明提供一种浮力飞行器，其能够通过降低碰撞风险来确保较高的安全性，并且能够通过抑制风的影响来促进对运动的控制，并且具有高运动能力。 所述浮力飞行器通过包括：浮力车体，在所述浮力车体中气密地填充比重小于空气的气体; 向浮力车体提供垂直推进力的垂直推进螺旋桨; 以及向浮力车体提供水平推进力的水平推进螺旋桨，并且浮力车体具有形成在至少两个方向上的水平风道，并且具有在侧视图中形成为锐角的外周边缘 。
-
公开(公告)号：EP2665651A4
公开(公告)日：2014-12-17
申请号：EP11856460
申请日：2011-12-30
Applicant: INFORMATION SYSTEMS LAB INC
Inventor： VAN STAAGEN PETER K , MCDANIEL WILLIAM DOUGLAS , BOSCHMA JAMES H JR
CPC classification number: B64B1/50 , B64B1/58 , B64C2201/022 , B64C2201/101 , B64C2201/123 , B64C2201/201 , B64C2201/208 , B64F1/14
-
公开(公告)号：JP6312038B2
公开(公告)日：2018-04-18
申请号：JP2016172646
申请日：2016-09-05
Applicant: パナソニックIPマネジメント株式会社
CPC classification number: B64C27/006 , B64B1/14 , B64B1/26 , B64B1/40 , B64B1/58 , B64C27/20 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/101 , B64C2201/108 , B64C2201/127 , B64D47/04 , B64D47/08 , B64D2203/00
-
公开(公告)号：JP2017047895A
公开(公告)日：2017-03-09
申请号：JP2016172646
申请日：2016-09-05
Applicant: パナソニックIPマネジメント株式会社
CPC classification number: B64C27/006 , B64B1/14 , B64B1/26 , B64B1/40 , B64B1/58 , B64C27/20 , B64C39/024 , B64D47/04 , B64D47/08 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/101 , B64C2201/108 , B64C2201/127 , B64D2203/00
Abstract: 【課題】飛行中に飛行体が人や物と接触した場合であっても、飛行体の安定した飛行を継続させることにある。 【解決手段】プロペラ32と、プロペラ32を駆動するモータ33とをそれぞれが有する複数のロータユニット30と、複数のロータユニット30の側方を覆う緩衝体と、を備え、緩衝体には、当該緩衝体を上下方向に貫通する複数の通気孔22が形成され、複数のロータユニット22は、それぞれ、複数の通気孔22の中に配置され、緩衝体は、中心部から周縁部へ向かって高さが次第に低くなっており、通気孔22は、緩衝体の周縁部寄りの高さが、緩衝体の中心部寄りの高さよりも低くなっている。 【選択図】図3
-
Patent Agency Ranking
公开(公告)号：KR101833920B1
公开(公告)日：2018-04-13
申请号：KR1020170137587
申请日：2017-10-23
Applicant: (주)지스페이스코리아
Inventor： 김태연
CPC classification number: B64C39/024 , B64B1/40 , B64B1/62 , B64C2201/022 , B64C2201/024 , B64C2201/101 , B64C2201/108 , B64C2201/127 , B64C2201/145
Abstract: 본발명은기촬영된항공촬영이미지와연결되기위한국소적인촬영이미지를드론을통해공중에서효율적으로획득할수 있으며, 해당드론이촬영시에는추력을정지시켜떨림없이보다정확하고선명한촬영이미지를획득할수 있는공간영상도화용이미지를확보하는드론시스템에관한것으로서, 본발명에따른공간영상도화용이미지를확보하는드론시스템은드론및 무추력촬영서포트장치를포함하여구성되며, 드론은영상도화작업을위한촬영이미지를공중에서획득하는기능을하고, 무추력촬영서포트장치는드론을통한촬영이미지의획득작업이드론의추력이정지된상태에서진행될수 있게하는기능을하는것으로서, 이러한무추력촬영서포트장치는드론을통한촬영이미지의획득을위해사전에정해지는여러위치에각각설치된다.
Abstract translation: 本发明是基于，并且可以获得一个集中式的图像要被记录在有效地通过所述无人驾驶飞机的空气连接到所记录的图像的空气，无人驾驶飞机能够获得没有一个更精确和锐利记录的图像，颤动阻止推力拍摄 根据本发明的用于保护用于空间图像映射的图像的dron系统包括无人驾驶飞机和无推力拍摄支持装置。无人驾驶飞机用于图像绘制操作 无推力拍摄支持设备具有通过无人机获取拍摄图像的功能，使得无人机的宝座能够以停止状态进行。 安装在各种预定位置以便通过无人机获取拍摄的图像。
-
公开(公告)号：US20190039427A1
公开(公告)日：2019-02-07
申请号：US15667497
申请日：2017-08-02
Applicant: The Boeing Company
Inventor： Scott Hartshorn , Keith Daniel Humfeld
IPC: B60F5/02 , G05D1/04 , B64B1/58 , B64C39/02 , B63B35/00 , B63G8/00 , B63G8/22 , B63G8/08 , C25B15/02 , C25B1/04 , C25B1/00 , H01M10/46 , H02S40/38 , H02S10/40
CPC classification number: B60F5/02 , B63B35/00 , B63B2035/007 , B63G8/001 , B63G8/08 , B63G8/22 , B63G2008/004 , B64B1/58 , B64C39/024 , B64C2201/022 , B64C2201/101 , B64C2201/141 , B64D2211/00 , C25B1/003 , C25B1/04 , C25B15/02 , G05D1/042 , H01M10/465 , H01M16/006 , H01M2220/20 , H01M2250/20 , H02S10/40 , H02S20/30 , H02S30/20 , H02S40/38
Abstract: Autonomous craft capable of extended duration operations as lighter-than-air craft, having the ability to alight on the surface of a body of water and generate hydrogen gas for lift via electrolysis using power derived from a photovoltaic system, as well as methods of launching an unmanned aerial vehicle (UAV) having a deployable envelope from a surface of a body of water.
-
公开(公告)号：US20170349260A1
公开(公告)日：2017-12-07
申请号：US15169766
申请日：2016-06-01
Applicant: James Richard Lawson
Inventor： James Richard Lawson
CPC classification number: B64C39/024 , B64B2201/00 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/101 , B64C2201/108 , B64D2211/00 , Y02T50/55
Abstract: The embodiment described herein is a hybrid balloon-multicopter invention. In a similar manner to a multicopter, it incorporates anticlockwise and clockwise rotating rotors to support maneuverability in three dimensional space. However, unlike a multicopter, maneuverability is augmented by the lift force generated by a balloon filled with a lighter than air gas. Furthermore, to support extended day and night operation, one embodiment of the invention includes photovoltaic cells to convert solar energy to electric energy recharging a battery.
-
39.发明申请Hybrid airship-drone farm robot system for crop dusting, planting, fertilizing and other field jobs 审中-公开混合飞艇 - 无人机农机机器人系统，用于作物除尘，播种，施肥等领域工作公开(公告)号：US20160307448A1
公开(公告)日：2016-10-20
申请号：US15193033
申请日：2016-06-25
Applicant: Bee Robotics Corporation
Inventor： Vladimir Salnikov , Anatoly Filin , Harm Burema
IPC: G08G5/00 , B64B1/40 , G05D1/00 , A01M9/00 , B64D1/16 , A01B79/00 , A01C7/00 , A01C21/00 , B64C39/02 , G08G5/04
CPC classification number: G08G5/0043 , A01B79/005 , A01B79/02 , A01C7/04 , A01C21/00 , B64B1/40 , B64B2201/00 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/101 , B64C2201/108 , B64C2201/12 , B64C2201/126 , B64C2201/141 , B64C2201/145 , B64C2201/146 , B64D1/00 , B64D1/16 , G05D1/104 , G08G5/04 , Y10S901/01
Abstract: Modern farming is currently being done by powerful ground equipment or aircraft that weigh several tons and treat uniformly tens of hectares per hour. Automated farming can use small, agile, lightweight, energy-efficient automated robotic equipment that flies to do the same job, even able to farm on a plant-by-plant basis, allowing for new ways of farming. A hybrid airship-drone has both passive lift provided by a gas balloon and active lift provided by propellers. A hybrid airship-drone may be cheaper, more stable in flight, and require less maintenance than other aerial vehicles such as quadrocopters. However, hybrid airship-drones may also be larger in size and have more inertia that needs to be overcome for starting, stopping and turning.
Abstract translation: 现代农业目前正在由强力的地面设备或称重数吨的飞机完成，每小时统一处理数十公顷。 自动化农业可以使用小型，敏捷，轻便，节能的自动化机器人设备，这些设备可以做同样的工作，甚至能够逐一种植，允许新的种植方式。 混合飞艇无人机具有由气球提供的被动升力和由推进器提供的主动升力。 混合飞艇无人机可能更便宜，飞行中更稳定，并且比其他空中飞行器如四轮车更需要较少的维护。 然而，混合飞艇 - 无人机的尺寸也可能更大，并且在起动，停止和转弯时需要克服更多的惯性。
-
公开(公告)号：US20160167775A1
公开(公告)日：2016-06-16
申请号：US14891153
申请日：2014-05-09
Applicant: RIDENGINEERING
Inventor： Jaques JONIOT
CPC classification number: B64C27/22 , B64B1/40 , B64B1/44 , B64C17/04 , B64C27/20 , B64C39/024 , B64C2201/022 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/101 , B64C2201/108 , B64C2201/122 , B64C2201/123 , B64D2211/00
Abstract: The invention relates to a drone comprising: two contra-rotating annular propellers (2, 4) defining a plane therebetween which is referred to as an equatorial plane and is assumed to be horizontal, means for driving the propellers, a load arranged below the equatorial plane, and means (20) for moving the load relative to the equatorial plane, an enclosure referred to as an upper enclosure (6) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially above the equatorial plane, and an enclosure referred to as a lower enclosure (8) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially below the equatorial plane, the load being placed inside the lower enclosure.
Abstract translation: 无人机技术领域本发明涉及一种无人机，包括：两个反向旋转的环形螺旋桨（2,4），在其间限定一个平面，被称为赤道平面，并被假设为水平的，用于驱动螺旋桨的装置，设置在赤道 平面和用于相对于赤道平面移动负载的装置（20），被称为上部外壳（6）的外壳，其填充有密度小于1且基本上位于赤道平面上方的气体或气体混合物 ，以及被称为下部外壳（8）的外壳，其中填充有密度小于1且基本上位于赤道平面下方的气体或气体混合物，所述负载被放置在下部外壳内。
-
-
-
-
-
-
-
-
-
Search Results
188
records
(took 0.02 seconds)
