公开(公告)号：US20180305011A1

公开(公告)日：2018-10-25

申请号：US15768201

申请日：2016-10-28

Applicant: BAE Systems plc

Inventor： David Julian Wright ,  Nicholas Giacomo Robert Colosimo ,  Clyde Warsop

IPC: B64C39/02 ,  B64C29/00

CPC classification number: B64C39/024 ,  A63H27/00 ,  B64C29/00 ,  B64C29/0033 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/182 ,  B64C2201/201

Abstract: A rotary-wing air vehicle comprising a main body (12) and at least two rotor devices (16a, 16b) arranged and configured to generate propulsion and thrust, in use, to lift and propel said air vehicle, said rotor devices (16a, 16b) being arranged and configured relative to said main body (12) such that the blades thereof do not cross through a central vertical axis of said main body (12) defining the centre of mass thereof, wherein said main body (12) is provided with an aperture (100) that extends therethrough to define a channel about said central vertical axis.

公开(公告)号：US11059562B2

公开(公告)日：2021-07-13

申请号：US15768744

申请日：2016-10-28

Applicant: BAE Systems plc

Inventor： Julian David Wright ,  Nicholas Giacomo Robert Colosimo ,  Clyde Warsop

IPC: B64C3/46 ,  B64C3/48 ,  B64C39/02 ,  B64C29/00

Abstract: A wing member (14b) for an air vehicle (10), said wing member comprising a core section (20) defining its longitudinal axis and having upper and lower surfaces, at least one of said surfaces comprising apparatus (22) selectively configurable between at least two positions, wherein in a fully extended position, at least portions of said apparatus extend outwardly from said respective surface so as to increase the effective cross-sectional area of said wing member and define an effective aerofoil in respect thereof.

公开(公告)号：US10556671B2

公开(公告)日：2020-02-11

申请号：US15106859

申请日：2014-12-22

Applicant: BAE SYSTEMS PLC

Inventor： Clyde Warsop ,  Nisar Ahmed Mirza

IPC: B64C21/08 ,  B64C21/02 ,  B63B1/32 ,  B63G8/00

Abstract: A tile assembly (22) which, in use, is fitted to a base structure to form at least part of a fluid washed surface. The tile assembly comprises a housing (42) with at least one plenum (45) being provided within the housing (42). A wall (44) of the housing (42) is provided with a plurality of flow passages (46) which extend from the plenum side of the wall (44) to an outer surface (48) of the wall. Flow passage closures (50) are provided which are operable to open and close at least some of the flow passages (46).

公开(公告)号：US20180297688A1

公开(公告)日：2018-10-18

申请号：US15768744

申请日：2016-10-28

Applicant: BAE Systems plc

Inventor： David Julian Wright ,  Nicholas Giacomo Robert Colosimo ,  Clyde Warsop

IPC: B64C3/46 ,  B64C3/14 ,  B64C3/48 ,  B64C39/02

Abstract: A wing member (14b) for an air vehicle (10), said wing member comprising a core section (20) defining its longitudinal axis and having upper and lower surfaces, at least one of said surfaces comprising apparatus (22) selectively configurable between at least two positions, wherein in a fully extended position, at least portions of said apparatus extend outwardly from said respective surface so as to increase the effective cross-sectional area of said wing member and define an effective aerofoil in respect thereof.

公开(公告)号：US20150142210A1

公开(公告)日：2015-05-21

申请号：US14370178

申请日：2012-12-05

Applicant: BAE SYSTEMS plc

Inventor： Clyde Warsop ,  Andrew Julian Press ,  Alan Geraint Davies

IPC: B64C39/02 ,  B64F1/04 ,  B64C3/56 ,  B64C9/08 ,  G05D1/00 ,  B64C5/06

CPC classification number: B64C39/028 ,  B64C3/56 ,  B64C5/06 ,  B64C9/08 ,  B64C2201/08 ,  B64C2201/123 ,  B64C2201/145 ,  B64C2201/146 ,  B64F1/04 ,  F42B12/365 ,  F42B15/08 ,  G05D1/0011 ,  G05D1/0088 ,  G05D1/0094

Abstract: The invention relates to a launched aerial surveillance vehicle, more specifically to a grenade or under-slung grenade launcher (UGL) aerial surveillance vehicle, a surveillance system and methods of providing rapid aerial surveillance.The vehicle once deployed is capable of autonomous flight paths, with basic inputs to change the circular flight paths, so as to build up surveillance for an area of interest. The vehicle comprises at least on optical sensor, which may be IR or visible range, to survey the area of interest, and feed the images back to at least one remote user.

Abstract translation: 本发明涉及一种发射的空中监视车辆，更具体地涉及一种手榴弹或坠落手榴弹发射器（UGL）空中监视车辆，监视系统和提供快速空中监视的方法。 一旦部署的车辆能够进行自主飞行路径，基本输入可以改变循环飞行路径，以便建立对感兴趣区域的监视。 车辆至少包括可以是IR或可见范围的光学传感器，以测量感兴趣的区域，并将图像馈送给至少一个远程用户。