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公开(公告)号：WO2014140583A3
公开(公告)日：2014-11-27
申请号：PCT/GB2014050754
申请日：2014-03-13
Applicant: BAE SYSTEMS PLC
Inventor： JONES CHRISTOPHER CHARLES RAWLINSON
IPC: B64D45/02
CPC classification number: B64D45/02
Abstract: A system comprising a low observable aircraft (2) having its surfaces oriented at a limited number of directions, and a lightning diverter strip (4, 22, 30) comprising a plurality of electrically conductive elements (8, 24, 32) arranged in a spaced apart relation, each of the electrically conductive elements (8, 24, 32) comprising an elongate portion. The lightning diverter strip (4, 22, 30) is attached to the aircraft in such a way that the conductive elements (8, 24, 32) are located on an exposed outer surface of the lightning diverter strip (4, 22, 30) and exposed to atmospheric conditions. For each conductive element (8, 24, 32), a long axis of the elongate portion of that conductive element (8, 24, 32) is substantially parallel with a surface of the aircraft.
Abstract translation: 一种包括其可观测飞行器（2）的系统，其具有以有限数量的方向定向的表面;以及雷电分流器条（4,22,30），其包括多个导电元件（8,24,32） 间隔开的关系，每个导电元件（8,24,32）包括细长部分。 闪电分流器条（4,22,30）以这样的方式附接到飞行器，使得导电元件（8,24,32）位于闪电分流器条（4,22,30）的暴露的外表面上， 并暴露于大气条件下。 对于每个导电元件（8,24,32），该导电元件（8,24,32）的细长部分的长轴基本上平行于飞行器的表面。
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公开(公告)号：WO2014140584A2
公开(公告)日：2014-09-18
申请号：PCT/GB2014050755
申请日：2014-03-13
Applicant: BAE SYSTEMS PLC
Inventor： JONES CHRISTOPHER CHARLES RAWLINSON
Abstract: A vehicle (2) comprising a vehicle part (4), the vehicle part (4) comprising: an electrically conductive core (6); a non-electrically conductive outer skin (8) made of a radar-absorbent material which surrounds, at least to some extent, the core (6) such that the core (6) is not visible from outside the vehicle (2); and one or more electrically conductive members (10) electrically connected to the core (6); each of the one or more members (10) is a tapered member having a relatively large cross sectional area where that member (10) is electrically connected to the core (6), and tapers from its end that is connected to the core (6) to a point; and the point of each member (10) is located at an outer surface of the external skin (8) such that the point of each of the members (10) is exposed.
Abstract translation: 1。一种包括车辆部件（4）的车辆（2），所述车辆部件（4）包括：导电芯（6）; 由雷达吸收材料制成的非导电外壳（8），其至少在一定程度上包围所述芯（6），使得所述芯（6）从所述车辆（2）的外部是不可见的; 和电连接到所述芯（6）的一个或多个导电构件（10）; 所述一个或多个构件（10）中的每一个是具有相对大横截面积的锥形构件，其中所述构件（10）电连接到所述芯部（6），并且从其连接到所述芯部（6）的端部逐渐变细 ）到某一点; 并且每个构件（10）的尖端位于外部蒙皮（8）的外表面处，使得每个构件（10）的尖端暴露。
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公开(公告)号：GB2511908B
公开(公告)日：2015-11-11
申请号：GB201400185
申请日：2014-01-07
Applicant: BAE SYSTEMS PLC
Inventor： ECCLES MARK , JONES CHRISTOPHER CHARLES RAWLINSON
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公开(公告)号：GB2502960A
公开(公告)日：2013-12-18
申请号：GB201210205
申请日：2012-06-11
Applicant: BAE SYSTEMS PLC
Abstract: A sensor system 2 is mounted to an aircraft fuselage 4 using an interface 6 comprising a pylon. The sensor system comprises a payload which is substantially housed within a store 8. The payload may include a ram air turbine (RAT) 10, sensors 12, processor 14 and transceiver 16. The aerodynamic properties, moments of inertia and mass distributions of the store are arranged to be the same as those for a store carrying a different payload that has already been certified for the aircraft. It is thus intended that a store can be provided which does not have to go through a certification process for a specific aircraft.
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公开(公告)号：GB2491395A
公开(公告)日：2012-12-05
申请号：GB201109297
申请日：2011-06-03
Applicant: BAE SYSTEMS PLC
Inventor： JONES CHRISTOPHER CHARLES RAWLINSON
Abstract: For each of a plurality of different time-steps in a time period, a mark is projected onto a surface in the form of a laser dot. For a first portion of the time period, a first sensor, generates a first image or image sequence of the surface with at least a portion of each of the projected marks in that image or sequence and for a second portion of the time period, a second sensor, generates a second image or image sequence of the surface with at least a portion of each of the projected marks in that image or sequence. A process that is dependent upon the respective positions of the mark in the first image or image sequence and the second image or image sequence is then performed, namely the time alignment of the image sequences to temporally align the images sequences or registering the two image sequences. The different time steps may be selected by a pseudo random sequence. The sensors may be of different types e.g. UV, Infra-red, visible light and may be mounted in an aircraft.
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Patent Agency Ranking
公开(公告)号：MY174126A
公开(公告)日：2020-03-10
申请号：MYPI2015703091
申请日：2014-03-13
Applicant: BAE SYSTEMS PLC
Inventor： JONES CHRISTOPHER CHARLES RAWLINSON
Abstract: A system comprising a low observable aircraft (2) having its surfaces oriented at a limited number of directions, and a lightning diverter strip (4, 22, 30) comprising a plurality of electrically conductive elements (8, 24, 32) arranged in a spaced apart relation, each of the electrically conductive elements (8, 24, 32) comprising an elongate portion. The lightning diverter strip (4, 22, 30) is attached to the aircraft in such a way that the conductive elements (8, 24, 32) are located on an exposed outer surface of the lightning diverter strip (4, 22, 30) and exposed to atmospheric conditions. For each conductive element (8, 24, 32), a long axis of the elongate portion of that conductive element (8, 24, 32) is substantially parallel with a surface of the aircraft.
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公开(公告)号：GB2514450B
公开(公告)日：2015-06-10
申请号：GB201404447
申请日：2014-03-13
Applicant: BAE SYSTEMS PLC
Inventor： JONES CHRISTOPHER CHARLES RAWLINSON
Abstract: A system comprising a low observable aircraft (2) having its surfaces oriented at a limited number of directions, and a lightning diverter strip (4, 22, 30) comprising a plurality of electrically conductive elements (8, 24, 32) arranged in a spaced apart relation, each of the electrically conductive elements (8, 24, 32) comprising an elongate portion. The lightning diverter strip (4, 22, 30) is attached to the aircraft in such a way that the conductive elements (8, 24, 32) are located on an exposed outer surface of the lightning diverter strip (4, 22, 30) and exposed to atmospheric conditions. For each conductive element (8, 24, 32), a long axis of the elongate portion of that conductive element (8, 24, 32) is substantially parallel with a surface of the aircraft.
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公开(公告)号：GB2514450A
公开(公告)日：2014-11-26
申请号：GB201404447
申请日：2014-03-13
Applicant: BAE SYSTEMS PLC
Inventor： JONES CHRISTOPHER CHARLES RAWLINSON
Abstract: A lightning protection system comprising a low observable aircraft 2 having its surfaces oriented at a limited number of directions and including a lightning diverter strip 4 comprising a plurality of electrically conductive elements 8 arranged in a spaced apart relation. Each of the electrically conductive elements 8 comprises an elongate portion. The lightning diverter strip 4 is attached to the aircraft in such a way that the conductive elements 8 are located on an exposed outer surface of the lightning diverter strip 4 and exposed to atmospheric conditions. For each conductive element 8 a long axis of the elongate portion of that conductive element 8 is substantially parallel with a surface of the aircraft. The conductive elements are mounted on a substrate strip 6 and may adopt one of a number of different layouts (figs 2-7).
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公开(公告)号：GB2487963A
公开(公告)日：2012-08-15
申请号：GB201102416
申请日：2011-02-10
Applicant: BAE SYSTEMS PLC
Inventor： ROWSE DAVID PAUL , PANITZ MARK , JONES CHRISTOPHER CHARLES RAWLINSON , SILLENCE COLIN DAVID , GOUGH DAVID WILLIAM
IPC: G01V3/08
Abstract: A method and apparatus for imaging hidden objects are provided. The apparatus comprises an array of magnetic field inducing elements 1 so that the array produces a combined magnetic field 3 resulting from a combination of the element fields. The combined magnetic field 3 is projected from the apparatus into an adjacent space and through a barrier or shield hiding the object. The apparatus includes means to sense a change in magnetic susceptibility of the field caused by the presence of an object in the field. Mapping of the changes in susceptibility onto individual elements in the array enables a visual image of the object to be created. The array may be a linear Halbach array of electromagnets. The strength of the field of each element may be varied in order to vary the sensitivity of the apparatus and the distance from the apparatus at which the object is detected.
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公开(公告)号：AU2016245364B2
公开(公告)日：2020-09-17
申请号：AU2016245364
申请日：2016-04-04
Applicant: BAE SYSTEMS PLC
Abstract: A method and apparatus for creating an atmospheric electromagnetic radiation path modifying element (40) operative to simulate a physical optical device, the method comprising applying electromagnetic radiation to a selected plurality of three-dimensional portions (12 –Figure 3) of an atmospheric volume (10) so as to heat and/or ionise the air within said portions, wherein said selected portions are spatially located together in a substantially unbroken three-dimensional configuration.
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