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1. 发明授权

EP3233634B1 AERODYNAMISCH GEFORMTER, AKTIVER SCHLEPPKÖRPER 有权
公开(公告)号：EP3233634B1
公开(公告)日：2018-06-13
申请号：EP15831127.4
申请日：2015-12-04
申请人： Alfred-Wegener-Institut Helmholtz-Zentrum für Polar- und Meeresforschung
发明人： HERBER, Andreas , KALMBACH, Dirk , GERDES, Rüdiger , BAYER, Hans-Jörg
IPC分类号： B64D3/02 , B64C3/16 , F41J9/10 , B64C1/00
CPC分类号： B64D3/02 , B64C3/16 , B64C39/022 , B64C39/024 , B64C2001/0045 , B64C2201/104 , B64C2201/12 , B64C2201/126 , B64C2201/141 , B64C2201/206 , F41J9/10

2. 发明公开

EP3279088A1 MULTI-FUNCTIONAL FLYING PLATFORM 审中-公开
标题翻译：多功能飞行平台
公开(公告)号：EP3279088A1
公开(公告)日：2018-02-07
申请号：EP16771155.5
申请日：2016-01-27
申请人： Zhuhai Yuren Agricultural Aviation Co., Ltd.
发明人： CHEN, Bo
IPC分类号： B64C27/10 , B64C27/08 , B64D47/00 , H02K9/00
CPC分类号： B64C27/08 , B64C39/024 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/12 , B64C2201/126 , B64C2201/127 , B64D2203/00 , F16B2/185
摘要： The present invention is aimed to provide a multi-functional flying platform with a simple structure, which is easy to operate and can achieve the mounting of different functional equipment. It includes rotor arm system and mounting plate (1). A plurality of evenly distributed fixing devices (2) are provided on the mounting plate (1). Mounting plate (1) is fixedly connected to rotor arm (3) of the rotor arm system by fixing device (2). A plurality of mounting positions (4) are provided on the lower side of the mounting plate (1). The present invention can be used in the field of agricultural aviation.
摘要翻译：本发明的目的在于提供一种结构简单，操作方便，可实现不同功能设备安装的多功能飞行平台。它包括转子臂系统和安装板（1）。多个均匀分布的固定装置（2）设置在安装板（1）上。安装板（1）通过固定装置（2）固定连接到转子臂系统的转子臂（3）。多个安装位置（4）设置在安装板（1）的下侧。本发明可以用于农业航空领域。

3. 发明公开

EP2879954A2 UNMANNED AERIAL SYSTEMS 审中-公开
标题翻译：无人航空系统
公开(公告)号：EP2879954A2
公开(公告)日：2015-06-10
申请号：EP13845941.7
申请日：2013-07-25
申请人： Bye UAS Inc.
发明人： BYE, George , BICKEL, Matt
IPC分类号： B64C39/02
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/08 , B64C2201/086 , B64C2201/104 , B64C2201/126 , B64C2201/165 , B64C2201/167 , B64C2201/185 , B64C2211/00
摘要： The present invention provides an Unmanned Aircraft System, including an integrated unmanned aerial vehicle and all related components and subsystems that can be packaged and transported as a kit, and customized to fit desired mission profiles, and easily repaired by replacement of damaged components or subsystems. The present invention further provides unmanned aircraft system components and subsystems that facilitate low power and low noise operation, and extended flight times.

4. 发明公开

EP2879952A2 VEHICLE CAPABLE OF STABILIZING A PAYLOAD WHEN IN MOTION 无效
标题翻译： WITH可能性镇定的有效载荷在运动车辆
公开(公告)号：EP2879952A2
公开(公告)日：2015-06-10
申请号：EP13846578.6
申请日：2013-07-31
申请人： Neurosciences Research Foundation, Inc.
发明人： HUTSON, Donald B.
IPC分类号： B64C25/36
CPC分类号： B64D47/08 , B64C27/006 , B64C27/10 , B64C27/20 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/042 , B64C2201/066 , B64C2201/108 , B64C2201/121 , B64C2201/126 , B64C2201/127 , B64C2201/182 , B64D9/00 , F16M11/123 , F16M11/18 , F16M13/00 , F16M13/02 , F16M2200/041
摘要： In specific embodiments, a vehicle propellable through fluids comprises a main work section and a plurality of propulsion units. The main work section includes a payload support hub, a payload support structure rotatable in 360 about the payload support hub in at least one axis, and a core including at least one microprocessor, the core at least partially nested within the payload support hub. The at least one microprocessor is adapted to substantially maintain an orientation of the payload support structure relative to a horizon line as the vehicle is propelled. One or more payloads are mountable on the rotatable payload support structure.

5. 发明授权

EP2151379B1 Modular pods for use with an unmanned aerial vehicle 有权
标题翻译：使用模块化容器无人机
公开(公告)号：EP2151379B1
公开(公告)日：2014-03-12
申请号：EP09161737.3
申请日：2009-06-02
申请人： Honeywell International Inc.
发明人： Collette, Daniel Ross , Helsing, JR., Joseph Scott
IPC分类号： B64C27/20 , B64C39/02
CPC分类号： B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/048 , B64C2201/088 , B64C2201/108 , B64C2201/126 , B64C2201/162 , B64C2211/00

6. 发明授权

EP2147858B1 Ducted fan core for use with an unmanned aerial vehicle 失效
标题翻译：涵道的核心用在无人导弹
公开(公告)号：EP2147858B1
公开(公告)日：2013-05-08
申请号：EP09160870.3
申请日：2009-05-21
申请人： Honeywell International Inc.
发明人： Collette, Daniel Ross
IPC分类号： B64C27/20 , B64C39/02
CPC分类号： B64C39/024 , B64C27/20 , B64C2201/027 , B64C2201/048 , B64C2201/088 , B64C2201/108 , B64C2201/126 , B64C2201/162

7. 发明公开

EP2435306A2 AIR VEHICLE 有权
标题翻译： LUFTFAHRZEUG
公开(公告)号：EP2435306A2
公开(公告)日：2012-04-04
申请号：EP10732752.0
申请日：2010-05-26
申请人： Israel Aerospace Industries Ltd.
发明人： WOLFF, Amit , DEKEL, Guy , ZIVAN, Lior
IPC分类号： B64C29/00
CPC分类号： B64C29/0033 , B64C27/22 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/088 , B64C2201/126 , B64C2201/165 , B64C2211/00
摘要： In embodiments, a system and method for providing propulsion and control to an air vehicle, and for operating the vehicle, include at least three propulsion units that provide vertical thrust for vectored thrust flight, in which at least one or two of the propulsion units also provide thrust for vectored thrust cruising or aerodynamic flight by suitably tilting the respective propulsion units for changing the thrust vector thereof. At the same time, the three or more propulsion units are operated to generate controlling moments to the air vehicle about three orthogonal axes, pitch, roll and yaw, during vectored thrust flight (hover, cruising, etc.) or during aerodynamic flight for controlling the vehicle.
摘要翻译：在实施例中，用于向空中交通工具提供推进和控制以及用于操作车辆的系统和方法包括至少三个推进单元，其提供用于向量推力飞行的垂直推力，其中至少一个或两个推进单元也通过适当地倾斜相应的推进单元来改变其推力矢量，为向量推力巡航或空气动力学飞行提供推力。同时，三个或更多的推进单元被操作以在向量推力飞行（悬停，巡航等）期间或在用于控制的空气动力学飞行期间在三个正交轴线（俯仰，滚动和偏航）周围产生对空中飞行器的控制力矩机动车。

8. 发明公开

EP1175336A1 METHOD OF REDUCING A NOSE-UP PITCHING MOMENT IN A DUCTED ROTOR UNMANNED AERIAL VEHICLE 有权
标题翻译：一种减少的正击穿扭矩大衣转子无人机
公开(公告)号：EP1175336A1
公开(公告)日：2002-01-30
申请号：EP00922096.3
申请日：2000-04-12
申请人： Sikorsky Aircraft Corporation
发明人： CYCON, James , SCOTT, Mark, W. , DEWITT, Christopher, W.
IPC分类号： B64C27/10 , B64C27/22 , B64C39/02 , B64C39/06 , B64C27/20
CPC分类号： B64C27/20 , B64C27/10 , B64C39/024 , B64C2201/027 , B64C2201/104 , B64C2201/108 , B64C2201/126 , B64C2201/127 , B64C2201/162 , B64C2201/165
摘要： A method for reducing a nose-up pitching moment in an unmanned aerial vehicle (10) during forward flight. The unmanned aerial vehicle includes counter-rotating rotor assemblies (38, 40) that are mounted within a duct (18). Each rotor assembly (38, 40) includes a plurality of rotor blades. The method involves adjusting the rotor blades to have substantially zero pitch. Then rotating the rotor asemblies (38, 40) to produce a virtual plane (62) across the duct (18). The virtual plane (62) is operative for substantially deflecting air (70) passing over the fuselage (44) away from the duct (18). In one embodiment of the invention, the method involves the further step of obstructing at least a portion of the bottom of the duct (18) to inhibit air (70) that is flowing across the bottom of the duct from passing into the duct (18).

9. 发明公开

EP0167625A1 SMALL RADIO-CONTROLLED INDUSTRIAL HELICOPTER 失效
标题翻译：小型无线电遥控工业直升机
公开(公告)号：EP0167625A1
公开(公告)日：1986-01-15
申请号：EP83903825.4
申请日：1983-12-02
申请人： IZUTSUYA, Kiyonobu
发明人： IZUTSUYA, Kiyonobu
IPC分类号： A63H27/12
CPC分类号： F02B75/243 , B64C27/06 , B64C27/12 , B64C39/024 , B64C2201/024 , B64C2201/044 , B64C2201/108 , B64C2201/126 , B64C2201/127 , B64C2201/146 , F02B75/34
摘要： A small, radio-controlled helicopter with an internal- combustion engine with two opposed, simultaneous-ignition cylinders to reduce ignition vibrations applied to the helicopter body. Thus, when this small helicopter is equipped with apparatus for video recording or photography, it is possible to obtain clear picture images while preventing any unwanted movement of the camera. In addition, various other operations, such as the spreading of pharmaceuticals and the guiding of lead ropes, can be conducted stably.
摘要翻译：小型无线电控制的直升机，带有内燃机和两个相对的同步点火气缸，以减少施加在直升机机身上的点火振动。因此，当该小型直升机配备有用于视频记录或摄影的装置时，可以获得清晰的图像，同时防止摄像机的任何不需要的移动。另外，可以稳定地进行各种其他操作，例如药物的传播和引导绳的引导。

10. 发明公开

EP3401854A1 AN AGRICULTURAL SYSTEM 审中-公开
公开(公告)号：EP3401854A1
公开(公告)日：2018-11-14
申请号：EP18171544.2
申请日：2018-05-09
申请人： CNH Industrial Belgium NV
发明人： DEBBAUT, Thomas
IPC分类号： G06Q10/04 , G06Q50/02 , G06Q10/00
CPC分类号： A01B69/008 , A01D89/00 , B64C39/024 , B64C2201/126 , B64C2201/141 , G05D1/00 , G05D1/0088 , G05D1/02 , G05D1/0223 , G05D1/04 , G05D1/042 , G05D2201/0201 , G06Q10/00 , G06Q10/04 , G06Q10/047 , G06Q10/20 , G06Q50/02
摘要： A system includes a vehicle (106) configured to acquire field-data representative of a field (104) having crop material (102) that is to be picked up from the field; and a controller (108) configured to determine control-instructions for a machine (110) to pick up the crop material (102), based on the field-data. The control-instructions comprise machine-steering-instructions for automatically controlling the direction of travel of the machine (110), such that the machine follows a specific route through the field.

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