-
公开(公告)号：NO20025705A
公开(公告)日：2002-11-27
申请号：NO20025705
申请日：2002-11-27
Applicant: BAE SYSTEMS PLC
Inventor： WARSOP CLYDE , WOODS MIKE , HENDERSON JAMES , LOCK GARY
CPC classification number: B64C39/062 , B64C2201/028 , B64C2201/042 , B64C2201/162
-
公开(公告)号：AU2023244547A1
公开(公告)日：2024-10-10
申请号：AU2023244547
申请日：2023-03-02
Applicant: BAE SYSTEMS PLC
Inventor： WARSOP CLYDE , AMOR DOMINIC , JOHNSON GRAHAM , JOHNS JOSEPH , WEST MICHAEL
IPC: G06F30/17 , G06F30/15 , G06F111/04 , G06F111/06
Abstract: A computer-implemented method of generating one or more designs for a vehicle, using a vehicle modelling application arranged to generate a three-dimensional model of a vehicle from a vehicle model definition, the vehicle model definition defining a set of values for geometric properties of the vehicle. A set of vehicle model definitions is generated, each vehicle model definition satisfying a set of geometric constraints. The set of vehicle model definitions is then filtered by generating the three-dimensional model of a vehicle from a vehicle model definition using the vehicle modelling application, determining whether the three-dimensional model satisfies a first set of physical constraints, and if the three-dimensional model does not satisfy the set of physical constraints, removing the vehicle model definition from the set of vehicle model definitions.
-
公开(公告)号：AU2016344526B2
公开(公告)日：2020-10-01
申请号：AU2016344526
申请日：2016-10-28
Applicant: BAE SYSTEMS PLC
Inventor： WRIGHT JULIAN DAVID , COLOSIMO NICHOLAS GIACOMO ROBERT , WARSOP CLYDE
Abstract: An air vehicle (10) comprising a main body (12) and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body(12) having a principal axis orthogonal to the longitudinal axis(20) of said wing members, at least a first propulsion device (16a) associated with a first of said wing members arranged and configured to generate a linear thrust relative to the main body in a first direction, and a second propulsion device (16b) associated with a second of said wing members arranged and configured to generate linear thrust relative to said main body in a second, substantially opposite, direction such that said wing members and said main body are caused to rotate about said principal axis, in use, the air vehicle further comprising an imaging system (100) configured to cover a substantially 360o imaging area about said principal axis and comprising at least one electro-optic sensor (102) mounted on a support member (104) and having a field of view (102a) covering a portion of said imaging area, said support member being mounted on said air vehicle, said imaging system (100) further comprising a control module (400) configured to define an object or region of interest in relation to said air vehicle, determine a nominal sensor field of view incorporating said object or region of interest, and obtain sequential image data from a sensor having a field of view matching said nominal field of view as said air vehicle completes a rotary cycle.
-
公开(公告)号：SG11201803015RA
公开(公告)日：2018-05-30
申请号：SG11201803015R
申请日：2016-10-28
Applicant: BAE SYSTEMS PLC
Inventor： WRIGHT JULIAN , COLOSIMO NICHOLAS , WARSOP CLYDE
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：AU2016344526A1
公开(公告)日：2018-05-10
申请号：AU2016344526
申请日：2016-10-28
Applicant: BAE SYSTEMS PLC
Inventor： WRIGHT JULIAN DAVID , COLOSIMO NICHOLAS GIACOMO ROBERT , WARSOP CLYDE
Abstract: An air vehicle (10) comprising a main body (12) and a pair of opposing wing members (14a, 14b) extending substantially laterally from the main body(12) having a principal axis orthogonal to the longitudinal axis(20) of said wing members, at least a first propulsion device (16a) associated with a first of said wing members arranged and configured to generate a linear thrust relative to the main body in a first direction, and a second propulsion device (16b) associated with a second of said wing members arranged and configured to generate linear thrust relative to said main body in a second, substantially opposite, direction such that said wing members and said main body are caused to rotate about said principal axis, in use, the air vehicle further comprising an imaging system (100) configured to cover a substantially 360o imaging area about said principal axis and comprising at least one electro-optic sensor (102) mounted on a support member (104) and having a field of view (102a) covering a portion of said imaging area, said support member being mounted on said air vehicle, said imaging system (100) further comprising a control module (400) configured to define an object or region of interest in relation to said air vehicle, determine a nominal sensor field of view incorporating said object or region of interest, and obtain sequential image data from a sensor having a field of view matching said nominal field of view as said air vehicle completes a rotary cycle.
-
Patent Agency Ranking36.发明专利
公开(公告)号：BRPI0914608A2
公开(公告)日：2015-12-08
申请号：BRPI0914608
申请日：2009-06-23
Applicant: BAE SYSTEMS PLC
Inventor： WARSOP CLYDE
-
公开(公告)号：ES2374545T3
公开(公告)日：2012-02-17
申请号：ES09772827
申请日：2009-06-23
Applicant: BAE SYSTEMS PLC
Inventor： WARSOP CLYDE
Abstract: Aparato de empuje vectorial para un motor (300) de reacción, pudiendo hacerse funcionar el motor de reacción para expulsar un chorro (115) principal para generar empuje; y comprendiendo el aparato: (i) una carcasa 112, 114 que define una salida (110) principal para emitir el chorro (115) principal; (ii) superficies (140) de Coanda primera y segunda que se extienden desde zonas opuestas de un extremo de escape de dicha carcasa, separándose cada superficie (140) de Coanda hacia fuera con respecto a la salida (110) principal de tal manera que se define un paso entre cada respectiva superficie (140) de Coanda y la salida (110) principal; de modo que, cuando se expulsa un chorro (115) principal a través de la salida (110) principal, se forman zonas de baja presión en la proximidad de dichos pasos; y (iii) conductos (124, 134) que conducen desde una fuente de fluido hacia salidas (120, 130) secundarias primera y segunda, estando situada la primera salida secundaria adyacente a la primera superficie de Coanda y estando situada la segunda salida secundaria adyacente a la segunda superficie de Coanda, estando dispuestas las salidas (120, 130) secundarias cada una para emitir un respectivo flujo secundario hacia la zona de baja presión en la proximidad del paso definido entre la respectiva superficie (140) de Coanda y la salida (110) principal; caracterizado porque el aparato comprende además: (iv) medios (126, 136) de control de flujo que pueden hacerse funcionar para controlar el flujo másico a través de una primera salida (120, 130) secundaria para que se encuentre dentro del intervalo del 0% al 5% del flujo másico en el chorro (115) principal de tal manera que, cuando el primer flujo secundario se emite desde la primera salida (120, 130) secundaria, el chorro (115) principal se arrastra por la segunda superficie (140) de Coanda.
-
公开(公告)号：AT533935T
公开(公告)日：2011-12-15
申请号：AT09772827
申请日：2009-06-23
Applicant: BAE SYSTEMS PLC
Inventor： WARSOP CLYDE
-
公开(公告)号：AT494536T
公开(公告)日：2011-01-15
申请号：AT05801578
申请日：2005-11-02
Applicant: BAE SYSTEMS PLC
Inventor： PARFITT ALEXANDER ROY , STURLAND IAN MICHAEL , WARSOP CLYDE , DAWSON PAUL JAMES
Abstract: A particle sampling device is disclosed for separating and collecting particles of at least first and second mass/size ranges from an ambient fluid (e.g. gaseous) medium in which they are present, particles of the first range being of generally larger size/mass than particles of the second range. The separator is especially designed for use in an air sampling device which is designed for rapid detection of micro-organisms such as bacteria, viruses, pathogens and the like, and is designed to be portable so that it can be readily and rapidly deployed in both civilian and military environments and can be used indoors and outdoors; it can also be designed for personal use.
-
公开(公告)号：AU2009265340A1
公开(公告)日：2010-01-07
申请号：AU2009265340
申请日：2009-06-23
Applicant: BAE SYSTEMS PLC
Inventor： WARSOP CLYDE
-
-
-
-
-
-
-
-
-
Search Results
55
records
(took 0.069 seconds)
