AERIAL PLATFORM LIGHTER THAN AIR EQUIPPED WITH TRAJECTORY CONTROL SYSTEMS AND INFLATABLE ANTENNAS FOR DATA AND POWER TRANSMISSION

    公开(公告)号:WO2022237995A1

    公开(公告)日:2022-11-17

    申请号:PCT/EP2021/066922

    申请日:2021-06-22

    摘要: A lighter-than-air aerial platform is consisting of two or more inflatable elements (100), balloons or dirigibles, a propulsion system (400), aerodynamic lifting and flight surfaces (500) which are optionally inflatable, an on-board electronic system (303) and a release actuator that separates or deflates at least one of the inflatable elements or balloons or airships; wherein the release actuator is located at the apex of the platform, and allows the rest of the system to descend in a controlled manner to be then recovered on land or at sea; wherein at least two of the inflatable elements, balloons or dirigibles that compose it are connected together by one or more cables (200) which place them at two different flight altitudes and wherein at least one of the inflatable elements, balloons or dirigibles that generates its own vertical force due to the Archimedes effect is an antenna (600) for receiving or sending radio, light or radiation signals through the use of specific sensors or cameras.

    可折叠电子设备
    2.
    发明申请

    公开(公告)号:WO2021249014A1

    公开(公告)日:2021-12-16

    申请号:PCT/CN2021/087193

    申请日:2021-04-14

    发明人: 赵宁

    摘要: 一种可折叠电子设备,包括:第一主体,包括第一金属边框;第二主体,包括第二金属边框;当第二主体与第一主体转动至展开状态时形成第一辐射结构,第一辐射结构用于以二分之一波长模态辐射第一射频信号;当第二主体与第一主体转动至折叠状态时形成第二辐射结构,第二辐射结构用于以四分之一波长模态辐射第一射频信号。

    REMOTE ELECTRONIC TILT BASE STATION ANTENNAS AND MECHANICAL CALIBRATION FOR SUCH ANTENNAS

    公开(公告)号:WO2021046149A1

    公开(公告)日:2021-03-11

    申请号:PCT/US2020/049096

    申请日:2020-09-03

    发明人: EVEREST, Paul D.

    摘要: The RET adjuster includes a drive assembly with a rotatable drive member operatively connected to a phase shifter assembly such that rotation of the drive member adjusts the phase shifter assembly. A first connector is coupled to the drive member where the first connector occupies a rest positon when the drive member is at rest. A drive system has a second connector occupying a rest positon when the drive system is at rest where the second connector is releasably engageable with the first connector such that actuation of the drive system rotates the drive member. A mechanical calibration system locates the second connector at the second rest position.

    ANTENNA SYSTEM FOR SATELLITE APPLICATIONS
    7.
    发明申请

    公开(公告)号:WO2020239865A1

    公开(公告)日:2020-12-03

    申请号:PCT/EP2020/064752

    申请日:2020-05-27

    申请人: TICRA FOND

    摘要: An antenna system for satellite applications is provide, the antenna system comprising an antenna array and a feed structure, and the antenna array is a passive antenna array configured to have a first state and a second state, the second state being a first deployed state. The feed structure is configured to provide a linearly polarized incident field for the antenna array in the first deployed state. The antenna array comprises a plurality of array elements, and the plurality of array elements forms a polarization conversion surface configured for converting the linearly polarized incident field to a reflected/transmitted circular polarized field. The antenna array is configured so that the radiation pattern of the reflected/transmitted circular polarized field corresponds to a predetermined radiation pattern and an array element geometry and an array element position of each of the plurality array elements are configured to provide the predetermined radiation pattern.

    COMPACTABLE RF MEMBRANE ANTENNA AND METHODS OF MAKING

    公开(公告)号:WO2020033279A1

    公开(公告)日:2020-02-13

    申请号:PCT/US2019/045036

    申请日:2019-08-04

    申请人: L'GARDE, INC

    IPC分类号: H01Q1/08 B29C70/40 H01Q15/161

    摘要: Exemplary embodiments are described herein for compactable antennas and methods of making such an antenna. Exemplary compactable antennas include a support structure and a reflector surface. The support structure may directly or indirectly define the reflector shape. Exemplary embodiments comprise deployable support structures to permit the compactable antenna to have a smaller volume stowed configuration and a larger volume deployed configuration.

    SYSTEMS AND METHODS RELATED TO FLEXIBLE ANTENNAS

    公开(公告)号:WO2019191415A1

    公开(公告)日:2019-10-03

    申请号:PCT/US2019/024564

    申请日:2019-03-28

    发明人: WONG, Serena H.

    IPC分类号: H01Q1/08 H01Q1/38

    摘要: A flexible instrument comprises an antenna having a distal tip portion, a proximal base, and an antenna body therebetween. The antenna body comprises a patterned cylindrical structure having a proximal end coupled to the proximal base and a distal end coupled to the distal tip portion. The flexible instrument is configured to generate a radiation pattern from the antenna to ablate tissue.