公开(公告)号：ES2748395T3

公开(公告)日：2020-03-16

申请号：ES16715046

申请日：2016-03-29

Applicant: BAE SYSTEMS PLC

Inventor： COLOSIMO NICHOLAS

IPC: G01S17/89 ,  G01S7/481 ,  G01S17/88

Abstract: Un aparato de formación de imágenes fantasma computacional que comprende una primera fuente de radiación electromagnética (100) y un sistema de control configurado para provocar que la radiación electromagnética de dicha primera fuente sea aplicada a una pluralidad seleccionada de porciones tridimensionales (12) de un volumen atmosférico (10) ubicado entre una segunda fuente de radiación electromagnética (110) y un objeto o región de interés (106) con el fin de calentar o ionizar el aire dentro de dichas porciones seleccionadas y crear un modulador de radiación espacial atmosférica (108) de un patrón especificado para provocar que dicho objeto o región de interés sea irradiado con una segunda radiación electromagnética espacialmente modulada en dicho patrón especificado, comprendiendo el aparato además un detector para recibir la segunda radiación electromagnética espacialmente modulada reflejada por dicho objeto o región de interés, y un módulo de procesamiento para reconstruir una imagen de dicho objeto o región de interés utilizando la salida de datos de dicho detector.

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

IPC: B64C29/00 ,  A63H27/00 ,  A63H27/14

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：SG11201803002UA

公开(公告)日：2018-05-30

申请号：SG11201803002U

申请日：2016-10-28

Applicant: BAE SYSTEMS PLC

Inventor： WRIGHT JULIAN ,  COLOSIMO NICHOLAS ,  WARSOP CLYDE

IPC: B64C29/02 ,  B64C39/02

Abstract: An air vehicle comprising a main body and a pair of opposing wing members extending substantially laterally from the main body, at least a first propulsion device associated with a first of said wing members and a second propulsion device associated with a second of said wing members, each said propulsion device being arranged and configured to generate linear thrust relative to said main body, in use, the air vehicle further comprising a control module for generating a control signal configured to change a mode of flying of said air vehicle, in use, between a fixed wing mode and a rotary wing mode, wherein, in said fixed wing mode of flying, the direction of thrust generated by the first propulsion device relative to the main body is the same as the direction of thrust generated by the second propulsion device, and in said second mode of flying, the direction of thrust generated by the first propulsion device relative to the main body is opposite to that generated by the second propulsion device.