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    • 22. 发明申请
    • OPTICAL ARRANGEMENT FOR A DISPLAY
    • US20220179217A1
    • 2022-06-09
    • US17594418
    • 2020-03-18
    • BAE SYSTEMS plc
    • Ian Thomas MackenJonathan Paul FreemanRory Thomas Alexander Mills
    • G02B27/01G02B17/08
    • A folded optical arrangement for use in a look-through display to transmit an image from an image plane to a user's eye, the arrangement providing a folded optical transmission path and comprising: an optical system having a first optical element comprising a first plurality of optically powered surfaces; and a second optical element comprising at least one optically powered surface, the optical system configured to receive light forming the image from an image source, and to focus the light to have an apparent optical focus between a predetermined distance and optical infinity and output the light; wherein the first plurality of optically powered surfaces and the at least one optically powered surface of the second optical element are arranged to define a plurality of interfaces along the folded optical path and wherein a refractive index change at each interface is predetermined to control the direction of light passing through the or each interface; and wherein one surface of the first optical element and one surface of the second optical element are adjacent to one another and the adjacent surfaces are dissimilar and each define an angle with a respective other surface of the relevant optical element at opposing ends of the adjacent surfaces and wherein the opposing angles are not equal; and a combiner element located to receive the output light from the optical system and a further external image for combination for transmission to the user.
    • 26. 发明授权
    • Flight simulation
    • US11302211B2
    • 2022-04-12
    • US16964024
    • 2019-01-14
    • BAE SYSTEMS plc
    • Richard Stephen Hadfield
    • G09B9/44G09B9/20G09B9/24G09B9/30
    • There is provided a method and apparatus for simulating a flight scenario during a live flight of an aircraft. The method comprises:
      (i) generating (60) images comprising scenes relevant to the simulated flight scenario at a simulated altitude;
      (ii) calculating, using live flight data received for the aircraft and with reference to a predetermined flight model (65), simulated flight data for the simulated flight scenario at the simulated altitude; and
      (iii) displaying, on a display system (35) of the aircraft, the calculated simulated flight data while controlling the display of said generated scene images to simulate movement of the aircraft through the displayed scene at a rate and in a direction corresponding to the displayed simulated flight data.
      The method and apparatus may optionally alter the response of the aircraft to control actions (70) by a pilot to simulate the response expected of the aircraft having the simulated flight characteristics.
    • 30. 发明授权
    • Payload mechanism
    • US11235877B2
    • 2022-02-01
    • US17290923
    • 2019-10-29
    • BAE Systems plc
    • James David CushingAndrew Charles White
    • B64D1/06
    • A payload mechanism for a vehicle is provided. The payload mechanism comprises: a door (2) operable to be in a closed configuration or an open configuration within a recess of the vehicle, the recess having an aperture (10); a first bearing unit comprising a first bearing (3a) and a second bearing (4a), the first bearing unit being coupled to one end of the door such that the door can rotate about the axis of rotation (y) of the first bearing and wherein the first bearing unit can rotate about the axis of rotation (x) of the second bearing, wherein the axis of rotation of the first bearing is offset from the axis of rotation of the second bearing; and a drive unit arranged to selectively drive either: the first bearing and the second bearing simultaneously at opposite and equal angular rates of motion to rotate the door in a first direction about the axis of rotation of the first bearing and to rotate the first bearing unit in a second direction about the axis of rotation of the second bearing to move the door closer to or away from the aperture, or the first bearing but not the second bearing to rotate the door about the axis of rotation of the first bearing. Methods of operating said payload mechanism are also provided, along with a vehicle having the payload mechanism.