公开(公告)号：EP3055208A4

公开(公告)日：2017-05-31

申请号：EP13895435

申请日：2013-11-08

Applicant: DE SILVA SHELTON GAMINI

Inventor： DE SILVA SHELTON GAMINI

IPC: B64C39/02 ,  B64D5/00 ,  G05D1/00

CPC classification number: B64D5/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/082 ,  B64C2201/122 ,  B64C2201/126 ,  B64C2201/143 ,  B64C2201/145 ,  B64C2201/206 ,  B64D47/08 ,  G05D1/0011 ,  G05D1/104

Abstract: This invention relates to an Unmanned Aerial Vehicle hereinafter called “Mother UAV” member (11) capable of carrying modules of Sub Unmanned Aerial Vehicle members (12) hereinafter called “Sub UAV” member. More particularly, the method and system that is capable of communicating via satellite and remote control technology wherein ejecting said Sub UAV members (12) from the Mother UAV member (11) wherein Sub UAV members (12) autonomously fly in sequence in a coordinated manner with the Mother UAV member (11), and capable of engaging in multiple missions in high, medium, low altitude, and surface, also communication with under sea submarines (27). Further, comprises of a method and system that the Sub UAV members (12) are able to return back to the Mother UAV member (11) after the mission is completed and be firmly secured to the flatbed (14) of the Mother UAV member (11). The present invention is specifically designed for multifunctional and multipurpose applications where humans and other vehicles are unable to access, for civil, commercial and military purposes.

Abstract translation: 本发明涉及一种能够承载以下称为“Sub UAV”成员的子无人驾驶飞机构件（12）的模块的以下称为“母亲UAV”构件（11）的无人驾驶飞行器（11）。 更具体地说，能够通过卫星和远程控制技术进行通信的方法和系统，其中从UAV无人机构件（11）中弹出所述无人驾驶飞行器构件（12），其中无人机UAV构件（12）以协调的方式 与母亲无人机成员（11），并能够在高，中，低海拔和水面进行多项任务，并且还可以与海底潜艇进行通信（27）。 此外，包括一种方法和系统，使得在完成任务后Sub UAV部件（12）能够返回到母机（11）并牢固地固定到母UAV部件（11）的平板（14） 11）。 本发明特别设计用于人和其他车辆无法进入的用于民用，商业和军事目的的多功能和多用途应用。

公开(公告)号：EP3127809A1

公开(公告)日：2017-02-08

申请号：EP16179595.0

申请日：2016-07-15

Applicant: Lockheed Martin Corporation

Inventor： GAMBLE, Dustin ,  CURRAN, Matthew

IPC: B64C39/02 ,  B64D5/00 ,  B64C27/08

CPC classification number: B64D5/00 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/082 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/182 ,  B64C2201/206

Abstract: In one embodiment, a system includes an unmanned, multirotor helicopter and a fixed-wing aircraft. The multirotor helicopter may couple to the fixed-wing aircraft to support and hold the fixed-wing aircraft. The multirotor helicopter may then elevate the fixed-wing aircraft from a launch site to a release altitude. The multirotor helicopter may also accelerate the fixed-wing aircraft to a release speed and upon reaching the release speed, release the fixed-wing aircraft. The unmanned, multirotor helicopter may then return to the launch site.

Abstract translation: 在一个实施例中，系统包括无人驾驶的多旋翼直升机和固定翼飞机。 多旋翼直升机可以耦合到固定翼飞机，以支撑和固定固定翼飞机。 然后，多旋翼直升机可以将固定翼飞机从发射场提升到释放高度。 多转直升机也可以将固定翼飞机加速到释放速度，达到释放速度后，释放固定翼飞机。 无人驾驶的多旋翼直升机然后可以返回发射场。

公开(公告)号：EP2957978A1

公开(公告)日：2015-12-23

申请号：EP14461542.4

申请日：2014-06-20

Applicant: Patents Factory Ltd. Sp. z o.o.

Inventor： Paczkowski, Jacek ,  Nalewa, Tomasz ,  Kramek, Krzysztof

IPC: G05D1/10 ,  B64D5/00

CPC classification number: G05D1/104 ,  B64C19/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/206 ,  B64D5/00

Abstract: A method for supporting maneuvers of an all-wing carrier aircraft by its parasite flying units, comprising the steps of: selecting (20) a maneuver to be performed; determining (21) sensor values (25) corresponding to selected maneuver; selecting (22) flight control surfaces of parasites to support the maneuver; activating (23) said flight control surfaces so that sensor values (25) are matched.

Abstract translation: 一种用于通过其寄生虫飞行单位支持全翼航空母舰的机动，包括以下步骤的方法：选择（20）的操纵被执行; 确定（21）的传感器值（25），以选择相应的机动; 选择（22）的寄生虫飞行控制面以支撑机动; 激活（23）所述的飞行控制面象传感器值（25）相匹配。

公开(公告)号：EP2727835A2

公开(公告)日：2014-05-07

申请号：EP13189903.1

申请日：2013-10-23

Applicant: The Boeing Company

Inventor： Hanna, Mark ,  Poling, David R

IPC: B64C39/02 ,  B64D1/10 ,  B64D1/12

CPC classification number: B64C39/024 ,  B64C2201/082 ,  B64C2201/126 ,  B64C2201/182 ,  B64C2201/206

Abstract: An aircraft system incorporates a first aircraft 48a, 48b having a grappling device 26 including a first gripper 30 with a first actuator 36a and a second gripper 32 with a second actuator 36b. The first gripper and the second gripper are movable between an open and a closed position to engage a hooking device 18 and pivot together to change a capture angle. A first controller 72 receives a command and operates the actuators in response to open and close the first and second grippers of the grappling device. The controller also receives a second command and operates the first and second actuators to pivot the grippers and provide grappling at a range of capture angles. A second aircraft 10, which may be a UAV, incorporates the hooking device 18. The hooking device includes a ring 20 rotatable from the surface and a third actuator 22 to rotate the ring between a stowed and an extended position.

Abstract translation: 飞机系统包括具有抓斗装置26的第一飞行器48a，48b，其包括具有第一致动器36a的第一夹持器30和具有第二致动器36b的第二夹持器32。 第一夹持器和第二夹持器可在打开位置和关闭位置之间移动以接合钩装置18并枢转在一起以改变捕获角度。 第一控制器72接收命令并响应于打开和关闭抓斗装置的第一和第二夹持器来操作致动器。 控制器还接收第二命令并操作第一和第二致动器以枢转夹持器并在捕获角度范围内提供抓斗。 可以是UAV的第二飞行器10结合有钩装置18.钩装置包括从表面可旋转的环20和第三致动器22，以在收起和延伸位置之间旋转环。

公开(公告)号：EP2314508A4

公开(公告)日：2014-03-05

申请号：EP09808231

申请日：2009-08-13

Applicant: MITSUBISHI HEAVY IND LTD

Inventor： SUZUKI SATOSHI

IPC: B64C37/02 ,  B64D5/00 ,  B64D47/08

CPC classification number: B64C39/024 ,  B64C37/02 ,  B64C2201/082 ,  B64C2201/206

Abstract: An unmanned aircraft system includes a manned aircraft and an unmanned aircraft. The manned aircraft includes a manned aircraft main wing, a manned aircraft fuselage, a manned aircraft landing system, and a manned aircraft joining mechanism provided at a bottom portion of the manned aircraft fuselage. The unmanned aircraft includes an unmanned aircraft main wing, an unmanned aircraft fuselage, an unmanned aircraft landing system, and an unmanned aircraft joining mechanism provided at a roof portion of the unmanned aircraft fuselage. The manned aircraft joining mechanism and the unmanned aircraft joining mechanism are detachably joined. The unmanned aircraft system can take off or land in a state that the unmanned aircraft and the manned aircraft are joined.

公开(公告)号：EP2354000A1

公开(公告)日：2011-08-10

申请号：EP11290030.3

申请日：2011-01-19

Applicant: MBDA France

Inventor： Jaurand, Benoît

IPC: B64D1/10 ,  B64D1/12 ,  B64D1/02

CPC classification number: B64D1/02 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/201 ,  B64C2201/206

Abstract: - Système d'emport de charge pour avion de transport.
- Le système (1) comporte un conteneur externe (15) qui est fixé, directement et complètement, dans la soute de l'avion de transport (AC), et dans lequel est agencé un conteneur interne (4) qui peut être déplacé longitudinalement et être amené d'une première position d'emport, dans laquelle il est entièrement situé à l'intérieur dudit conteneur externe (15), à une seconde position (P2) de déchargement, dans laquelle il est décalé longitudinalement vers l'arrière de l'aéronef (AC) de sorte qu'une partie (7) dudit conteneur interne (4) est alors située à l'extérieur de l'avion de transport (AC).

Abstract translation: 系统（1）固定在运输飞机（AC）的货舱中的外部容器（15）。 内部容器（4）布置在外部容器中，以使内部容器从内部容器完全位于外部容器内部的位置到另一个位置（P2），其中内部容器朝向后部侧 飞机相对于前一位置使得内部容器的释放部分（7）通过在隔室的后侧处的开口（8）位于飞机外部。

公开(公告)号：EP1924495A2

公开(公告)日：2008-05-28

申请号：EP06851409.0

申请日：2006-06-28

Applicant: Sommer, Geoffrey S.

Inventor： Sommer, Geoffrey S.

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C37/02 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/143 ,  B64C2201/165 ,  B64C2201/206

Abstract: Systems and/or methods for forming a multiple-articulated flying system (skybase) having a high aspect ratio wing platform, operable to loiter over an area of interest at a high altitude are provided. In certain exemplary embodiments, autonomous modular flyers join together in a wingtip-to-wingtip manner. Such modular flyers may derive their power from insolation. The autonomous flyers may include sensors which operate individually, or collectively after a skybase is formed. The skybase preferably may be aggregated, disaggregated, and/or re-aggregated as called for by the prevailing conditions. Thus, it may be possible to provide a “forever-on-station” aircraft.

公开(公告)号：EP1370461A1

公开(公告)日：2003-12-17

申请号：EP02700439.9

申请日：2002-02-20

Applicant: BAE Systems PLC

Inventor： HARRISON, Richard George,Bae Systems plc

IPC: B64D5/00 ,  B64D3/00 ,  B64D39/00

CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/048 ,  B64C2201/082 ,  B64C2201/206 ,  B64D3/00 ,  B64D5/00 ,  B64D39/02 ,  B64D39/06

Abstract: A system for launching, refuelling and recovering in flight an aircraft (10) such as an unmanned aerial vehicle (UAV) from a larger carrier aircraft (16) comprising a holder (22) on the carrier aircraft (16) to which the UAV (10) is detachably connectable and an extendable and retractable refuelling device (23, 24) on the carrier aircraft (16) detachably connectable to the UAV (10) whereby to launch the UAV it is disconnected from the holder (22), the refuelling device (23, 24) is extended with the UAV connected thereto to cause the UAV to trail behind the carrier aircraft and the UAV is then disconnected from the refuelling device.

公开(公告)号：EP0786403A1

公开(公告)日：1997-07-30

申请号：EP97100748.9

申请日：1997-01-18

Applicant: Daimler-Benz Aerospace Aktiengesellschaft

Inventor： Karg, Josef, Ing.

IPC: B64D5/00

CPC classification number: B64D3/02 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/182 ,  B64C2201/206

Abstract: Für eine Vorrichtung 2 zum Absetzen und Wiederaufnehmen einer Drohne 3 von einem Transportflugzeug 1 während des Fluges ist im Flugzeug 1 ein durch Heckklappen 9, 11 aus dem Flugzeug 1 ausschwenkbarer Kran 5 angeordnet, an dem zum Befestigen der Drohne 3 ein Fesselungskopf 8 montiert ist. An der Drohne 3 sind eine ausklappbare Führungsstange 21, die in einen im Fesselungskopf 8 eingebauten Trichter 30 einfahrbar ist, und Schienen 23 angeordnet, um die am Trichter 30 angebaute Klauen 44 greifen können. Im Flugzeug 1, im Fesselungskopf 8 und in der Drohne 3 sind Sensoren vorhanden, welche die Drohne 3 zum Wiederaufnehmen an den Fesselungskopf 8 heranführen und in den Trichter 30 einführen.

Abstract translation: 用于在飞行中从飞机（1）起飞和取出无人机（3）的装置（2）包括可通过尾门（9,11）摆动的起重机（5），具有固定头（8） 无人机。无人机具有延伸的导杆，其可以进入固定头中的漏斗。 无人机还具有用于通过漏斗夹爪的轨道。 传感器安装在飞机上，固定头和无人机，无人机被引导到位置，以便通过固定头进入漏斗。

公开(公告)号：US10081425B2

公开(公告)日：2018-09-25

申请号：US15905572

申请日：2018-02-26

Applicant: International Business Machines Corporation

Inventor： Jeanette L. Blomberg ,  Eric K. Butler ,  Anca A. Chandra ,  Pawan R. Chowdhary ,  Thomas D. Griffin ,  Divyesh Jadav ,  Sunhwan Lee ,  Robert J. Moore ,  Hovey R. Strong, Jr.

IPC: B64C39/02 ,  B64F1/36 ,  B64F1/22 ,  B64F1/32 ,  B64F1/00

CPC classification number: B64C39/024 ,  B64C2201/128 ,  B64C2201/201 ,  B64C2201/205 ,  B64C2201/206 ,  B64C2201/208 ,  B64F1/007 ,  B64F1/222 ,  B64F1/32 ,  B64F1/36 ,  B64F1/368

Abstract: Embodiments of the present invention provide an apparatus comprising a body including a cavity for storing one or more packages, and a conveyor belt disposed above a top surface of the body. The belt is shaped to receive one or more packages, and the belt is controllable to rotate a package placed on the belt either from the top surface to the cavity for storage or from the cavity to the top surface for dispatch. A package comprises at least one of a drone and a payload transported by the drone. The apparatus further comprises a landing mechanism for stabilizing a drone landing on the apparatus.