公开(公告)号：KR1020050034364A

公开(公告)日：2005-04-14

申请号：KR1020030070262

申请日：2003-10-09

Applicant: 이영욱

Inventor： 이영욱 ,  이진욱 ,  이애나

IPC: A63H27/28

CPC classification number: A63H27/008 ,  A63H29/22 ,  A63H31/08 ,  B64C2201/025

Abstract: 본 발명의 비행체를 위한 자세제어장치는, 서보혼이 구비된 서보; 일단이 상기 서보혼에 연결되고, 상기 타단이 서보혼을 통하여 상기 꼬리날개에 연결된 연결부재; 및 상기 서보혼과 상기 꼬리날개 사이에 설치되며, 상기 동체축을 골짜기로 하는 홈이 형성된 피치제어부재를 구비하여, 상기 서보혼이 상기 동체축 위치로부터 좌우로 움직임에 따라, 상기 연결부재에 의해 연결된 상기 꼬리날개가 좌우로 움직임과 동시에, 상기 꼬리날개의 앙각이 상승하도록 작동된다. 본 발명의 자세제어장치에 의하면 첫째, 방향 선회시, 하나의 서보에 의하여 수직꼬리날개의 각도 조정에 의한 요우축 제어와 수평꼬리날개의 각도 조정에 의한 피치축 제어가 동시에 이루어짐으로써, 날개짓 비행체의 방향 선회 조종이 용이하고, 선회시 고도 침하에 의한 자세 불안정 문제가 해결된다. 둘째, 방향 선회시, 수평꼬리날개 전체가 선회하고자 하는 방향으로 이동하므로, 선회 중 비행체의 좌우 공력중심점도 선회 방향으로 이동하게 되므로, 선회 중 발생하기 쉬운 롤축 불안정도 상쇄되는 효과가 있다. 세째, 하나의 서보모터 및 그 작동 기구에 의하여 비행체의 방향 선회를 제어하므로, 비행체 전체 무게를 감소시킨다. 따라서, 날개짓 비행체의 날개폭 및 전체 크기를 소형화할 수 있다. 네째, 날개짓 비행체의 제조에 있어서, 서보모터 및 그 작동 기구의 간소화로 인하여 비용감소의 효과가 있다.

公开(公告)号：EP2923945B1

公开(公告)日：2018-12-05

申请号：EP14754687.3

申请日：2014-02-19

Applicant: Mitsubishi Heavy Industries, Ltd.

Inventor： KURODA Satoshi ,  MORI Tomoyuki ,  HATTORI Kazuya ,  TAHARA Masato ,  TAKAYAMA Oki

IPC: B64C33/02 ,  A63H27/18 ,  A63H27/28

CPC classification number: B64C33/02 ,  A63H27/008 ,  B64C2201/025

Abstract: This ornithopter is provided with main wings attached to a fuselage, and a control system that controls a flapping motion of the main wings. The main wings are each provided with an inner spar, an outer spar, and a wrist configured in such a manner as to be disposed between the inner spar and the outer spar, and to have a bending angle, which is the relative angle between the inner spar and the outer spar, that varies within a prescribed variation range. The control system is provided with: an actuator that performs an upward motion and a downward motion of the inner spars by moving the inner spars upward and downward; angle sensors that measure the bending angles; and a control device that controls the actuator according to the bending angles so as to cause the inner spars to move.

公开(公告)号：EP3158558A1

公开(公告)日：2017-04-26

申请号：EP15751114.8

申请日：2015-06-19

Applicant: Kales, Jolanda Jacoba Maria

Inventor： Kales, Jolanda Jacoba Maria

IPC: G09F21/10 ,  B64C39/02 ,  G05D1/10

CPC classification number: B64C39/024 ,  B64C27/10 ,  B64C2201/024 ,  B64C2201/025 ,  B64C2201/12 ,  B64C2201/146 ,  G05D1/104 ,  G09F9/3023 ,  G09F9/33 ,  G09F9/35 ,  G09F21/10

Abstract: This invention relates to a drone, method and systems for displaying messages and/or images by using a group of one or more remotely controlled airborne drones provided with display means and controlled so the messages and/or images are created and are visual by the display means of the group of airborne drones. The display means are controlled such that the messages and/or images are 2D or 3D respectively. The display means may include LED's, OLED's or LCD based on means or DLP and/or laser projection means. The display of messages and/or images can be remotely controlled using a social gateway for airborne visualization, enabling the integration of content from end-user and marketing clients based on the drone's geographic position and social media audience profile.

Abstract translation: 通过使用由一个或多个遥控机载无人机组成的组来显示消息和/或图像的无人机，方法和系统，所述一组或多个遥控机载无人机配备有显示装置并且被控制使得所述消息和/或图像由所述组的显示装置 空中无人机。 显示装置被控制为使得所述消息和/或图像分别是2D或3D消息和/或图像。 显示装置可以包括LED，基于OLED或LCD的装置或DLP和/或激光投影装置。 消息和/或图像的显示可以使用用于机载可视化的社交网关来远程控制，使得能够基于无人机地理位置和社交媒体观众简档来整合来自最终用户和市场客户的内容。

公开(公告)号：EP2923945A4

公开(公告)日：2016-01-20

申请号：EP14754687

申请日：2014-02-19

Applicant: MITSUBISHI HEAVY IND LTD

Inventor： KURODA SATOSHI ,  MORI TOMOYUKI ,  HATTORI KAZUYA ,  TAHARA MASATO ,  TAKAYAMA OKI

IPC: B64C33/02 ,  A63H27/18 ,  A63H27/28

CPC classification number: B64C33/02 ,  A63H27/008 ,  B64C2201/025

Abstract: This ornithopter is provided with main wings attached to a fuselage, and a control system that controls a flapping motion of the main wings. The main wings are each provided with an inner spar, an outer spar, and a wrist configured in such a manner as to be disposed between the inner spar and the outer spar, and to have a bending angle, which is the relative angle between the inner spar and the outer spar, that varies within a prescribed variation range. The control system is provided with: an actuator that performs an upward motion and a downward motion of the inner spars by moving the inner spars upward and downward; angle sensors that measure the bending angles; and a control device that controls the actuator according to the bending angles so as to cause the inner spars to move.

Abstract translation: 这种鸟巢器具有附接到机身的主翼，以及控制主翼的扑动运动的控制系统。 主翼各自设置有内翼梁，外翼梁和腕部，其构造成设置在内翼梁和外翼梁之间，并且具有弯曲角度，该角度是 内部翼梁和外部翼梁，其在规定的变化范围内变化。 该控制系统设有：通过向内和向下移动内梁来执行内梁的向上运动和向下运动的致动器; 测量弯曲角度的角度传感器; 以及控制装置，其根据弯曲角度控制致动器，以使内部翼梁运动。

公开(公告)号：EP2923945A1

公开(公告)日：2015-09-30

申请号：EP14754687.3

申请日：2014-02-19

Applicant: Mitsubishi Heavy Industries, Ltd.

Inventor： KURODA Satoshi ,  MORI Tomoyuki ,  HATTORI Kazuya ,  TAHARA Masato ,  TAKAYAMA Oki

IPC: B64C33/02 ,  A63H27/18 ,  A63H27/28

CPC classification number: B64C33/02 ,  A63H27/008 ,  B64C2201/025

Abstract: This ornithopter is provided with main wings attached to a fuselage, and a control system that controls a flapping motion of the main wings. The main wings are each provided with an inner spar, an outer spar, and a wrist configured in such a manner as to be disposed between the inner spar and the outer spar, and to have a bending angle, which is the relative angle between the inner spar and the outer spar, that varies within a prescribed variation range. The control system is provided with: an actuator that performs an upward motion and a downward motion of the inner spars by moving the inner spars upward and downward; angle sensors that measure the bending angles; and a control device that controls the actuator according to the bending angles so as to cause the inner spars to move.

Abstract translation: 这个ornithopter设有连接到机身的主翼和控制主翼扑动的控制系统。 主翼分别设置有内翼梁，外翼梁和手腕，所述手腕配置成设置在内翼梁和外翼梁之间，并且具有弯曲角度，所述弯曲角度是所述内翼梁和所述外翼梁之间的相对角度 内部翼梁和外部翼梁，在规定的变化范围内变化。 控制系统设置有：致动器，其通过使内梁向上和向下移动来执行内梁的向上运动和向下运动; 测量弯曲角度的角度传感器; 以及控制装置，其根据弯曲角度控制致动器以使内梁移动。

公开(公告)号：EP2085738A2

公开(公告)日：2009-08-05

申请号：EP09000853.3

申请日：2009-01-22

Applicant: Diehl BGT Defence GmbH & Co.KG

Inventor：

IPC: F41H3/00 ,  B64C39/02

CPC classification number: F41H3/00 ,  B64C39/024 ,  B64C2201/025 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127

Abstract: Die Erfindung betrifft ein unbemanntes Fahrzeug (2, 28) mit einer Tarnvorrichtung (4).
Es wird vorgeschlagen, dass die Tarnvorrichtung (4) eine Eigenschaft eines Tieres nachbildet. Es kann trotz einer deutlichen Sichtbarkeit des unbemannten Fahrzeugs (2, 28) eine effektive Tarnung erreicht werden.

Abstract translation: 车辆（28）具有模拟动物特征的伪装装置。 鸟。 外围元件（30）通过连接单元（34）与中心元件（32）连接。 隐形装置具有以牺牲者的形式形成的外盖。 驱动单元（8）具有设置在盖的管状开口中的转子，驱动单元的前侧和侧面被隐形装置隐藏。 外围元件设置有驱动单元，并且中心元件设置有控制单元（18）。 连接单元形成为刚性杆。

公开(公告)号：US09950790B2

公开(公告)日：2018-04-24

申请号：US14198418

申请日：2014-03-05

Applicant: AeroVironment, Inc.

Inventor： Matthew Todd Keennon ,  Karl Robert Klingebiel ,  Alexander Andryukov ,  Bart Dean Hibbs ,  John Peter Zwaan

IPC: B64C33/02 ,  B64C19/00

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.

公开(公告)号：US20180099746A1

公开(公告)日：2018-04-12

申请号：US15714004

申请日：2017-09-25

Applicant: Tsinghua University ,  HON HAI PRECISION INDUSTRY CO., LTD.

Inventor： HE MA ,  YANG WEI ,  KAI LIU ,  KAI-LI JIANG ,  SHOU-SHAN FAN

IPC: B64C39/02 ,  B64C33/02

CPC classification number: B64C39/028 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/042 ,  B64C2201/127

Abstract: The disclosure relates to a biomimetic insect. The biomimetic insect includes a trunk and at least two wings connected to the trunk. The wing includes a carbon nanotube layer and a vanadium dioxide layer (VO2) layer stacked with each other. Because the drastic, reversible phase transition of vanadium dioxide, the wing has giant deformation amplitude and fast response.

公开(公告)号：US20180079504A9

公开(公告)日：2018-03-22

申请号：US14198418

申请日：2014-03-05

Applicant: AeroVironment, Inc.

Inventor： Matthew Todd Keennon ,  Karl Robert Klingebiel ,  Alexander Andryukov ,  Bart Dean Hibbs ,  John Peter Zwaan

IPC: B64C33/02 ,  B64C19/00

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.

公开(公告)号：US20170033247A1

公开(公告)日：2017-02-02

申请号：US15302277

申请日：2015-04-29

Applicant: The Regents of the University of Michigan

Inventor： Kamal Sarabandi ,  Kyusang Lee ,  Stephen R. Forrest ,  Jungsuek Oh

IPC: H01L31/046 ,  B64C39/02 ,  B64C33/00 ,  H01L31/18 ,  H01Q9/04

CPC classification number: H01L31/046 ,  B64C33/00 ,  B64C39/028 ,  B64C2201/025 ,  B64C2201/066 ,  B64D2211/00 ,  H01L27/142 ,  H01L31/022425 ,  H01L31/184 ,  H01L31/1868 ,  H01Q9/0421 ,  Y02E10/50 ,  Y02T50/55

Abstract: A device comprising a thin film solar cell with an integrated flexible antenna, such as a meander line antenna, is disclosed. In an embodiment, the device comprises a substrate and an array of solar cells disposed on the substrate, wherein the array of solar cells are interconnected by metal conductors that carry DC power from the solar cells and which form at least part of the flexible antenna. In their capacity as an antenna, the metal conductors operate cooperatively with the solar cells to radiate an RF signal, receive an RF signal, or both radiate and receive an RF signal. The device optionally comprises a choke disposed on the substrate and electrically coupled to the array of solar cells, wherein the choke operates to impede conduction of the RF signal. A method of making the disclosed device is also disclosed.

Abstract translation: 公开了一种包括具有集成柔性天线的薄膜太阳能电池的装置，例如曲折线天线。 在一个实施例中，该装置包括衬底和设置在衬底上的太阳能电池阵列，其中太阳能电池阵列由携带来自太阳能电池的DC电力并且形成柔性天线的至少一部分的金属导体互连。 以它们作为天线的能力，金属导体与太阳能电池协同工作以辐射RF信号，接收RF信号，或者两者辐射并接收RF信号。 该装置可选地包括设置在基板上并电耦合到太阳能电池阵列的扼流器，其中扼流器操作以阻止RF信号的导通。 还公开了制造所公开的装置的方法。