Planate dynamic isolator
    2.
    发明授权

    公开(公告)号:US11802606B2

    公开(公告)日:2023-10-31

    申请号:US16877480

    申请日:2020-05-18

    摘要: A vibration isolation system is disclosed, including a rigid retaining device having an internal space, a first external side, and a second external side. A rigid anchoring device is retained in the internal space of the rigid retaining device. The anchoring device has a linkage member that extends from the internal space to the first external side of the retaining device and is configured for rigid connection to a first apparatus. The second side of the retaining device is configured for attachment to a second apparatus. A damping material is sandwiched between the retaining device and the anchoring device, and is configured to limit transfer of vibration between the retaining device and the anchoring device.

    ADDITIVELY MANUFACTURED HEAT TRANSFER DEVICE

    公开(公告)号:US20210247140A1

    公开(公告)日:2021-08-12

    申请号:US17242204

    申请日:2021-04-27

    IPC分类号: F28D7/00

    摘要: An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.

    Additively manufactured heat transfer device

    公开(公告)号:US11015872B2

    公开(公告)日:2021-05-25

    申请号:US16024582

    申请日:2018-06-29

    IPC分类号: F28D7/00 H01Q13/00

    摘要: An additively manufactured heat transfer device is disclosed, including an enclosure portion with outer walls. The outer walls contain an inner channel configured to direct a flow of coolant fluid. The heat transfer device further includes a fluid intake port and a fluid outtake port, each connected to the first inner channel. The fluid intake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion into the inner channel, and the fluid outtake port is configured to direct a flow of coolant fluid through an outer wall of the enclosure portion out of the inner channel. The inner channel is defined by internal walls, and the enclosure portion and the internal walls form a single additively manufactured unit.

    Spacecraft with anti nadir battery radiator

    公开(公告)号:US10457425B2

    公开(公告)日:2019-10-29

    申请号:US13655224

    申请日:2012-10-18

    IPC分类号: B64G1/42 B64G1/50

    摘要: A satellite is disclosed comprising an anti-nadir panel having a first side and a second side. In one or more embodiments, the first side of the anti-nadir panel is mounted to an anti-nadir side of the main body of the satellite. The satellite further comprises at least one battery pack mounted to the second side of the anti-nadir panel, where at least one battery pack comprises at least one battery cell.