LOW ENERGY NUCLEAR THERMOELECTRIC SYSTEM
    31.
    发明申请
    LOW ENERGY NUCLEAR THERMOELECTRIC SYSTEM 审中-公开
    低能耗核热电系统

    公开(公告)号:WO2014146836A2

    公开(公告)日:2014-09-25

    申请号:PCT/EP2014/052961

    申请日:2014-02-14

    Applicant: LENR CARS SA

    Inventor: CHAUVIN, Nicolas

    Abstract: A low energy nuclear thermoelectric system for a vehicle which provides a cost-effective and sustainable means of transportation for long operation range with zero emission using an onboard low energy nuclear reaction thermal generator. The present invention generally includes a thermal generator within a thermal enclosure case, an energy conversion system linked with the thermal generator, an energy storage system linked with the energy conversion system, a cooling system and a central control system. The thermal generator reacts nickel powder with hydrogen within a reactor chamber to produce heat. The heat is then transferred to the energy conversion system to be converted into electricity for storage in the energy storage system. The cooling system provides cooling for the various components of the present invention and the control system regulates its overall operation. The present invention may be utilized to power a vehicle in an efficient, sustainable and cost-effective manner.

    Abstract translation: 一种用于车辆的低能量核热电系统,其使用机载低能量核反应热发电机提供具有成本效益和可持续的运输方式的长期运行范围,零排放。 本发明通常包括在热封壳壳体内的热发生器,与热发生器连接的能量转换系统,与能量转换系统连接的能量存储系统,冷却系统和中央控制系统。 热发生器将镍粉与反应器室内的氢反应产生热量。 然后将热量转移到能量转换系统中,以转换成电能以存储在能量存储系统中。 冷却系统为本发明的各种部件提供冷却,并且控制系统调节其整体操作。 本发明可以用于以有效,可持续和成本有效的方式为车辆提供动力。

    AIRCRAFT AND SYSTEM FOR SUPPLYING ELECTRICAL POWER TO AN AIRCRAFT ELECTRICAL LOAD
    32.
    发明申请
    AIRCRAFT AND SYSTEM FOR SUPPLYING ELECTRICAL POWER TO AN AIRCRAFT ELECTRICAL LOAD 审中-公开
    用于向飞机电力负载提供电力的飞机和系统

    公开(公告)号:WO2014137422A1

    公开(公告)日:2014-09-12

    申请号:PCT/US2013/071694

    申请日:2013-11-25

    Abstract: An aircraft, comprising: a wing; a fuselage coupled to the wing; an engine (34) coupled to at least one of the fuselage and the wing; an electrical load (20) associated with the aircraft during flight operations; a generator (32) coupled to the engine and configured to generate electrical power for the electrical load; a conductor (38) electrically disposed between the electrical load and the generator; a conduit (46) configured to house the conductor; and a dielectric gas (44) disposed in the conduit; wherein the conduit (46) is configured to envelop the conductor (38) in the dielectric gas (44).

    Abstract translation: 一架飞机,包括:一架翼; 机身与机翼相连; 耦合到机身和机翼中的至少一个的发动机(34); 在飞行操作期间与飞机相关联的电力负载(20); 发电机(32),其耦合到所述发动机并且被配置为产生用于所述电负载的电力; 电气设置在电负载和发电机之间的导体(38); 导管(46),其构造成容纳所述导体; 以及设置在所述导管中的电介质气体(44) 其中所述导管(46)构造成包围所述电介质气体(44)中的导体(38)。

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