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    Geomagnetic and Atmospheric Electric Power Systems
    33.
    发明公开
    Geomagnetic and Atmospheric Electric Power Systems 审中-公开

    公开(公告)号：US20230352608A1

    公开(公告)日：2023-11-02

    申请号：US18140747

    申请日：2023-04-28

    申请人： Encarnacion Gonzalez

    发明人： Encarnacion Gonzalez

    IPC分类号： H01L31/05 ,  B64G1/44 ,  B64D41/00 ,  B60L8/00 ,  H02S30/10

    CPC分类号： H01L31/05 ,  B64G1/443 ,  B64D41/00 ,  B60L8/003 ,  H02S30/10 ,  B64D2211/00

    摘要： As it is scientifically known all or nearly all celestial bodies have magnetic fields to varying degrees including Earth. Many celestial bodies also have a gaseous atmosphere. The present invention utilizes said magnetic fields and or gaseous atmospheres in conjunction with a plurality of electric grids, coils, or super conducting slats to which varying levels of positive voltage are applied to produce electric power. A plurality of electric grids, coils, or super conducting slats may be installed on automobiles, aircraft, spacecraft, and onto the blades of a wind powered electrical generating system to produce electric power when the blades are in motion.

    CONTROL DEVICE, COMPUTER READABLE STORAGE MEDIUM, SYSTEM, AND CONTROL METHOD
    35.
    发明公开
    CONTROL DEVICE, COMPUTER READABLE STORAGE MEDIUM, SYSTEM, AND CONTROL METHOD 审中-公开

    公开(公告)号：US20230333573A1

    公开(公告)日：2023-10-19

    申请号：US18337412

    申请日：2023-06-19

    申请人： HAPSMobile Inc.

    发明人： Koji FUJIMOTO

    IPC分类号： G05D1/10 ,  H02S50/00 ,  H02S10/40 ,  B64D41/00 ,  B64D47/08

    CPC分类号： G05D1/106 ,  H02S50/00 ,  H02S10/40 ,  B64D41/00 ,  B64D47/08 ,  B64D2211/00

    摘要： Provided is a control device that controls a power supply flight vehicle, the control device including a control unit which controls the power supply flight vehicle so as to cause a light irradiation unit to radiate light toward a solar cell panel while flying following flight of a power supply target flight vehicle on which the solar cell panel is mounted. Provided is a control method to control a power supply flight vehicle, which is executed by a computer, the control method including controlling the power supply flight vehicle so as to cause a light irradiation unit to radiate light toward a solar cell panel while flying following flight of a power supply target flight vehicle on which the solar cell panel is mounted.

    ELECTRICAL SHIELDING TERMINATION SYSTEMS
    36.
    发明公开
    ELECTRICAL SHIELDING TERMINATION SYSTEMS 审中-公开

    公开(公告)号：US20230327422A1

    公开(公告)日：2023-10-12

    申请号：US17716562

    申请日：2022-04-08

    申请人： Hamilton Sundstrand Corporation

    发明人： Nhia Yang ,  Francis C. Belisle

    IPC分类号： H02G15/06 ,  H01B9/02 ,  B64D41/00

    CPC分类号： H02G15/06 ,  H01B9/02 ,  B64D41/00

    摘要： A conductor shielding termination assembly can include a housing tube defining an inner diameter housing channel therethrough. The housing tube can be made of conductive material. The assembly can include a shoulder bushing configured to insert within the inner diameter housing channel of the housing tube. The shoulder bushing can define an inner diameter bushing channel sized to receive an unshielded portion of a conductor. The assembly can include a clamping assembly configured to clamp around the housing tube and/or the conductor to axially lock the housing tube and the conductor and to trap a shielding termination between the housing tube and the clamping assembly. The clamping assembly can form a clamping inner diameter channel sized to receive a shielded portion of the conductor.

    GENERATOR SYSTEMS
    37.
    发明公开
    GENERATOR SYSTEMS 审中-公开

    公开(公告)号：US20230318497A1

    公开(公告)日：2023-10-05

    申请号：US17669742

    申请日：2022-02-11

    申请人： Hamilton Sundstrand Corporation

    发明人： Frank Z. Feng ,  Timothy R. Pieper

    IPC分类号： H02P9/30 ,  B64D41/00

    CPC分类号： H02P9/307 ,  B64D41/00 ,  H02P2101/30

    摘要： A generator system can include a dual stator generator comprising a first stator and a second stator, a first rectifier operatively connected to the first stator to receive AC from the first stator, a second rectifier operatively connected to the second stator to receive AC from the second stator, and a first DC output line and a second DC output line. The first rectifier and the second rectifier can be connected in parallel to the first DC output line and a second DC output line without an inter phase transformer (IPT) to output DC to the first DC output line and the second DC output line.

    Auxiliary power unit systems
    39.
    发明授权
    Auxiliary power unit systems 有权

    公开(公告)号：US11738881B2

    公开(公告)日：2023-08-29

    申请号：US17073216

    申请日：2020-10-16

    申请人： Hamilton Sundstrand Corporation

    发明人： Kyle Stephen Ives

    IPC分类号： B64D41/00

    CPC分类号： B64D41/00 ,  B64D2041/002 ,  B64D2221/00

    摘要： An auxiliary power unit (APU) system for an aircraft can include a fuel consuming system configured to generate and output electrical energy for use by one or more aircraft systems and a battery system configured to output stored electrical energy for use by the one or more aircraft systems. The fuel consuming system can include a fuel consuming APU, and an APU generator operatively connected to the fuel consuming APU and configured to convert APU motion into APU generator alternating current (AC). The system can include a high voltage AC line operatively connected to the generator. The battery system can include a battery configured to output battery direct current (DC).