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

Applicant: Neurosciences Research Foundation, Inc.

Inventor： HUTSON, Donald B.

IPC: B64C25/36

CPC classification number: 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

Abstract: 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.

公开(公告)号：EP2778598A1

公开(公告)日：2014-09-17

申请号：EP13275062.1

申请日：2013-03-14

Applicant: BAE Systems PLC

Inventor： The designation of the inventor has not yet been filed

IPC: F41H7/00 ,  B64C39/02 ,  F41H13/00 ,  F42B12/36

CPC classification number: B64C39/024 ,  B64C2201/121 ,  B64C2201/146 ,  F41H7/005 ,  F41H13/00 ,  F42B12/365

Abstract: Disclosed is a method performed by apparatus. The apparatus comprises a first module (18) and a second module (32). The first module is mounted on an unmanned vehicle (2) and arranged to act upon a payload (16) also mounted on the vehicle (2). The second module (32) is remote from the unmanned vehicle. The method comprises: receiving, by the second module (32), an instruction to activate the payload (16); generating, by the second module (32), a plurality of activation codes and sending those codes to the first module (18); determining, by the first module (18), whether or not each of the received activation codes is valid; and if the codes are valid, activating the payload (16), or, if the codes are not valid, preventing activation of the payload (16). Each code comprises: a time dependent portion, a single-use portion, and an identifier for the unmanned vehicle (2).

Abstract translation: 公开了一种由装置执行的方法。 该装置包括第一模块（18）和第二模块（32）。 第一模块安装在无人驾驶车辆（2）上并被布置成作用在也安装在车辆（2）上的有效载荷（16）上。 第二模块（32）远离无人驾驶车辆。 该方法包括：由第二模块（32）接收激活有效载荷（16）的指令; 通过第二模块（32）生成多个激活码并将这些代码发送到第一模块（18）; 由所述第一模块（18）确定所接收的激活码是否有效; 并且如果代码有效，则激活有效载荷（16），或者如果代码无效，则防止有效载荷（16）的激活。 每个代码包括：时间依赖部分，一次性部分和无人驾驶车辆（2）的标识符。

公开(公告)号：EP2391863A4

公开(公告)日：2014-07-02

申请号：EP10767467

申请日：2010-02-02

Applicant: AEROVIRONMENT INC

Inventor： MIRALLES CARLOS

IPC: F42B15/01 ,  F41G7/00 ,  F41G7/22 ,  F41G9/00 ,  G08G5/00

CPC classification number: F41G7/2246 ,  B64C39/024 ,  B64C2201/121 ,  B64C2201/141 ,  F41G7/008 ,  F41G7/2206 ,  F41G7/2253 ,  F41G7/2293 ,  F41G9/002 ,  G05D1/0094 ,  G05D1/12 ,  G08G5/0069

Abstract: A system comprising an unmanned aerial vehicle (UAV) configured to transition from a terminal homing mode to a target search mode, responsive to an uplink signal and/or an autonomous determination of scene change.

Abstract translation: 一种系统，包括被配置为响应于上行链路信号和/或场景变化的自主确定从终端归属模式转换到目标搜索模式的无人驾驶飞行器（UAV）。

公开(公告)号：EP2532588A1

公开(公告)日：2012-12-12

申请号：EP12004166.0

申请日：2012-05-31

Applicant: EADS Deutschland GmbH

Inventor： Dornwald, Jochen ,  Bichler, Bartholomäus

IPC: B64D7/00 ,  B64C1/00 ,  B64C39/02

CPC classification number: B64C39/10 ,  B64C25/10 ,  B64C25/16 ,  B64C39/024 ,  B64C2201/028 ,  B64C2201/121 ,  B64C2201/22 ,  B64D1/06 ,  B64D7/00 ,  B64D7/02 ,  B64D7/06 ,  B64D27/10 ,  B64D27/14

Abstract: Ein Fluggerät 10 mit geringer Radarsignatur weist eine erste Seite 12 auf, auf der Turbinenöffnung 14, 16 und Nutzlast- oder Fahrwerkschächte 20, 24, 26 angeordnet sind. Eine zweite Seite 30 des Fluggeräts ist derart ausgeführt, dass sie eine geringere Radarsignatur als die erste Seite 12 aufweist.

Abstract translation: 飞行器（10）具有设置有孔（14,16）的涡轮机（18）。 飞行器部件通过有效负载轴（20）和起落架轴（24,26）在飞行器主体部分内移动。 涡轮机孔和轴布置在飞机主体部分的顶表面（12）上。 飞行器主体部分的底面（30）的雷达标记被设定为小于飞机主体部分顶表面的雷达标记。 底面设置有不间断的表面。 航空器运行方法包括独立的索赔。

公开(公告)号：EP1734333B1

公开(公告)日：2008-07-02

申请号：EP06019954.4

申请日：2005-11-02

Applicant: NEXTER Munitions

Inventor： Brunet, Luc ,  Regis, Muriel

IPC: F42B12/36 ,  C06B25/12 ,  C06C15/00 ,  C06D3/00 ,  F42C19/08 ,  F41J9/08 ,  B64C3/00 ,  B64C39/02 ,  F42B10/04

CPC classification number: F42B3/28 ,  B64C39/024 ,  B64C2201/121 ,  B64C2201/127 ,  B64C2201/165 ,  C06B23/001 ,  C06B23/003 ,  C06B45/00 ,  F41J9/08 ,  F42B5/18 ,  F42B5/192 ,  F42B10/04 ,  F42B12/36 ,  F42B12/365 ,  F42B12/76 ,  F42C19/0803 ,  F42C19/0842

公开(公告)号：EP1444476A4

公开(公告)日：2008-04-02

申请号：EP02771875

申请日：2002-10-24

Applicant: METAL STORM LTD

Inventor： O'DWYER JAMES MICHAEL

IPC: F41A9/72 ,  F41A23/00 ,  B63G1/00 ,  B64C39/02 ,  B64D7/00 ,  B64D7/04 ,  B64D7/08 ,  F41A21/08 ,  F41A21/20 ,  F41A21/36 ,  F41A21/48 ,  F42B5/03

CPC classification number: B64D7/00 ,  B64C2201/121 ,  B64D7/04 ,  B64D7/08 ,  F41A21/48 ,  F41A23/00 ,  F42B5/035

Abstract: A vehicular weapons platform (30) including a plurality of barrel assemblies (10), wherein each barrel assembly includes a barrel (11), a plurality of projectiles (14) axially disposed within the barrel for operative sealing engagement with the bore of the barrel (11) and discrete propellant charges (15) for propelling respective projectiles sequentially through the muzzle of the barrel; and at least one of said plurality of barrel assemblies (10) includes a barrel which also forms a structural member of the weapons platform. In one preferred form, the weapons platform takes the form of a small combat aerial vehicle (SCAV) (30), wherein the barrel assemblies (10) form the airframe. A method of constructing a weapons platform from the barrel assemblies is also described.

公开(公告)号：EP1444476A1

公开(公告)日：2004-08-11

申请号：EP02771875.8

申请日：2002-10-24

Applicant: Metal Storm Limited

Inventor： O'DWYER, James, Michael

IPC: F41A23/00 ,  F41A21/48 ,  B64D7/04 ,  B63G1/00

CPC classification number: B64D7/00 ,  B64C2201/121 ,  B64D7/04 ,  B64D7/08 ,  F41A21/48 ,  F41A23/00 ,  F42B5/035

Abstract: A vehicular weapons platform (30) including a plurality of barrel assemblies (10), wherein each barrel assembly includes a barrel (11), a plurality of projectiles (14) axially disposed within the barrel for operative sealing engagement with the bore of the barrel (11) and discrete propellant charges (15) for propelling respective projectiles sequentially through the muzzle of the barrel; and at least one of said plurality of barrel assemblies (10) includes a barrel which also forms a structural member of the weapons platform. In one preferred form, the weapons platform takes the form of a small combat aerial vehicle (SCAV) (30), wherein the barrel assemblies (10) form the airframe. A method of constructing a weapons platform from the barrel assemblies is also described.

公开(公告)号：US20180251218A1

公开(公告)日：2018-09-06

申请号：US15760259

申请日：2016-09-16

Applicant: Christopher Wilkinson

Inventor： Christopher Wilkinson

IPC: B64C39/02 ,  B64D1/04

CPC classification number: B64C39/024 ,  B64C2201/02 ,  B64C2201/046 ,  B64C2201/082 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/206 ,  B64C2201/22 ,  B64D1/04

Abstract: An unmanned aerial combat vehicle system is disclosed. The system provides for an unmanned aerial combat vehicle that is capable of performing reconnaissance, disrupting enemy communications, or delivering a weaponized payload. The unmanned aerial combat vehicle may also be equipped with a cloaking mechanism, where it can mask it's heat signature, or simulate an image on its outer surface.

公开(公告)号：US20180162527A1

公开(公告)日：2018-06-14

申请号：US15293020

申请日：2016-10-13

Applicant: THE BOEING COMPANY

Inventor： Ryan L. Hupp ,  Sean R. Wakayama

IPC: B64C39/02 ,  G05D1/00 ,  F41G9/00

CPC classification number: B64C39/024 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/14 ,  B64C2201/146 ,  B64D7/04 ,  F41G9/002 ,  G05D1/0016 ,  G05D1/0038 ,  G05D1/0094

Abstract: An unmanned aerial system (UAS) includes a body and a lift and propulsion system coupled to the body. The UAS includes a weapon coupled to the body. The weapon has an aiming axis oriented in a fixed direction relative to the body. The UAS includes a control system operatively coupled to the lift and propulsion system and the weapon. The control system is configured to determine a roll angle and a flight path such that the aiming axis is directed at a target when the UAS moves according to at least a portion of the flight path at the roll angle. The control system is further configured to control the lift and propulsion system such that the UAS moves according to the at least the portion of the flight path at the roll angle.

公开(公告)号：US20180022423A1

公开(公告)日：2018-01-25

申请号：US15694215

申请日：2017-09-01

Applicant: Lockheed Martin Corporation

Inventor： Nathan E. Low ,  Peter J. Demas

IPC: B63B25/00 ,  B63B35/00 ,  B64C39/02

CPC classification number: B63B25/002 ,  B63B35/00 ,  B63H11/00 ,  B63H2011/006 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/121

Abstract: A water-propelled or water-powered unmanned aerial vehicle including a base configured to carry a payload, and at least one nozzle attached thereto. The at least one nozzle is configured to selectively receive pressurized fluid from a source located remotely from the vehicle. The vehicle includes a control system configured to alter or otherwise selectively dictate the flow of fluid through the at least one nozzle and/or the orientation of the at least one nozzle with respect to the base in response to a received control signal for providing controlled unmanned vehicle flight.