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    • 54. 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.
    • 55. 发明申请
    • COMPRESSOR MODULE
    • US20210388730A1
    • 2021-12-16
    • US17282044
    • 2019-10-09
    • BAE SYSTEMS plc
    • James William Spain
    • F01D9/04F04D19/00F04D29/58F01D25/12
    • A compressor module (200) wherein the compressor module (200) defines a working fluid flow duct (60) between a compressor module inlet (210) and a compressor module outlet (214). The compressor module comprises: a first heat exchanger (37) and a compressor rotor stage (24) each provided in the working fluid flow duct (60). The first heat exchanger (37) is provided in flow series between the compressor module inlet (210) and the compressor rotor stage (24). The compressor stage (24) is provided in flow series between the first heat exchanger (37) and the compressor module outlet (214). The first heat exchanger (37) is defined by a wall (226) having an external surface (282) which is located in the working fluid flow duct (60). There is provided a heat sink unit (236) which defines a portion (240) of the working fluid flow duct (60) in flow series between the compressor rotor stage (24) and compressor module outlet (214). The first heat exchanger (37) is in heat transfer communication with the heat sink unit (236). The first heat exchanger (37) is configured such that it is operable to transfer heat to the heat sink unit (236) from the working fluid (250) passing the first heat exchanger (37).