FLIGHT CONTROL USING DISTRIBUTED MICRO-THRUSTERS
    2.
    发明公开
    FLIGHT CONTROL USING DISTRIBUTED MICRO-THRUSTERS 审中-公开
    飞行控制分布式使用MICRO推力JETS

    公开(公告)号:EP2681116A1

    公开(公告)日:2014-01-08

    申请号:EP12752329.8

    申请日:2012-03-02

    IPC分类号: B64D27/00 F25B21/02 B64C19/00

    CPC分类号: B64C19/00 B64C9/00 B64C15/14

    摘要: A method and apparatus to control movement of a vehicle using a plurality of thrust-producing devices formed in at least one control surface is disclosed. A supply of power to the plurality of thrust-producing devices that are configured to propel gas through the control surface to produce thrust is controlled such that a physical displacement of the control surface is generated. The physical displacement is in accordance with the supply of power to the plurality of thrust-producing devices and controls the movement of the vehicle.

    MICRO THRUSTER USES AND IMPROVEMENTS
    3.
    发明公开
    MICRO THRUSTER USES AND IMPROVEMENTS 有权
    一个MICROTHRUSTERS和改进使用应该

    公开(公告)号:EP2861859A4

    公开(公告)日:2016-05-04

    申请号:EP13833411

    申请日:2013-06-14

    申请人: GAME CHANGERS LLC

    IPC分类号: F03H99/00 H01L31/00

    CPC分类号: F02G1/043 F03H99/00 H02S99/00

    摘要: NMSET and related device uses and improvements to the forces generated. Laminar flow control systems benefit from NMSET and related devices as they simplify installation and are easier to retrofit on existing aircraft. Necessary temperature gradients can me generated by using a heated material with the sides at different energy accommodation coefficients. Surface geometries can be used to increase the force generated. Photovoltaic film can be embedded into the membrane, providing a source of energy that can offset the power required for desired thrust. Intake scoops improve the air flow through the micro thrusters and surface geometries, and airflow diffusers increase air flow interaction with the hotter surface resulting in higher thrust outputs.

    NANOMOLECULAR SOLID STATE ELECTRODYNAMIC THRUSTER
    9.
    发明公开
    NANOMOLECULAR SOLID STATE ELECTRODYNAMIC THRUSTER 有权
    NANO分子电气动态立体DRIVE

    公开(公告)号:EP2473785A4

    公开(公告)日:2015-04-29

    申请号:EP10814092

    申请日:2010-09-03

    申请人: GAME CHANGERS LLC

    IPC分类号: F03H99/00 H01L35/00

    摘要: A method and device for creating a temperature gradient among a plurality of temperature gradient devices. Each device is formed of a first layer of conductive material having a top surface and a bottom surface. The first layer is adjacent to a second layer of conductive material and has electrical resistive heating properties. A power supply is used to provide a current flow through at least the first layer when the power supply is activated. When activated, the resulting current flow causes the second layer to heat and thus create a temperature gradient between the bottom surface of the second layer and the top surface of the first layer. Activation of the power supply is controlled by a control unit so that activation of adjacent temperature gradient devices is avoided for a predetermined time after activation of the first temperature gradient device.

    AIR CUSHION TRANSPORT
    10.
    发明公开
    AIR CUSHION TRANSPORT 有权
    气垫运输

    公开(公告)号:EP2681088A1

    公开(公告)日:2014-01-08

    申请号:EP12752278.7

    申请日:2012-03-01

    IPC分类号: B60V1/04 F02K99/00 F25B21/02

    摘要: A movable support platform is disclosed that includes a platform, a skirt coupled to a periphery of the platform that provides an enclosed space below the platform that retains pressurized gas, and a thrust propulsion device coupled to the platform for pressurizing gas in the enclosed space. The thrust propulsion device includes an array of gas-propelling devices "distributed thrusters" that propel gas into the enclosed space below the platform. The distributed thrusters may be comprised of Nano Molecular Solid-state Electrodynamic Thrusters ("NMSET").