A ROTARY STIRLING-CYCLE APPARATUS AND METHOD THEREOF

    公开(公告)号:US20180372022A1

    公开(公告)日:2018-12-27

    申请号:US16060277

    申请日:2016-11-03

    IPC分类号: F02G1/044 F02G1/053 F02G3/02

    摘要: A Stirling-cycle apparatus is provided comprising a hermetically sealable housing; a first rotary displacement unit in fluid communication with a second rotary fluid displacement unit, each operably mounted in a separate, fluidly sealed portion within said housing and adapted to provide a cyclic change of at least one thermodynamic state parameter of a working fluid during use. Furthermore, each one of said first and second rotary displacement unit comprises a compressor mechanism, having a first compressor working chamber that is adapted to receive a first portion of said working fluid, and at least a second compressor working chamber that is adapted to receive a second portion of said working fluid, said first compressor working chamber comprises a first outlet port and said second compressor working chamber comprises a second outlet port. Each one of said first and second rotary displacement unit further comprises an expander mechanism, having a first expander working chamber that is adapted to receive said first portion of said working fluid, and at least a second expander working chamber that is adapted to receive said second portion of said working fluid, said first expander working chamber comprises a first inlet port and said second expander working chamber comprises a second inlet port; a drive coupling assembly, adapted to operably and operatively couple said first expander mechanism to said first compressor mechanism. The drive coupling assembly further comprises a rotating valve mechanism, adapted to provide a predetermined sequence of a cyclic fluid exchange between said first compressor working chamber and said first expander working chamber, and between said second compressor working chamber and said second expander working chamber, at predetermined intervals of the angle of rotation of said first and second rotatory displacement unit. The Stirling-cycle apparatus further comprises an actuator, operably coupled to said first and second rotary displacement unit, and adapted to synchronously link the rotational movement of said first rotary displacement unit with said second rotary displacement unit, such that said first predetermined cyclic change of at least one thermodynamic state parameter of said working fluid is offset in relation to said second predetermined cyclic change of at least one thermodynamic state parameter of said working fluid by a predetermined phase angle, during use.

    THERMOACOUSTIC ELECTRIC GENERATOR SYSTEM
    8.
    发明申请

    公开(公告)号:US20180073780A1

    公开(公告)日:2018-03-15

    申请号:US15564709

    申请日:2016-03-22

    发明人: Noriyuki FUKAYA

    IPC分类号: F25B9/14 F02G1/043

    摘要: A thermoacoustic electric generator system includes: a turbine including a turbine blade provided in an inside of a branched tube in a tube component and rotating by thermoacoustic oscillation of working gas in a thermoacoustic engine, and a turbine rotational shaft configured to be coupled to the turbine blade, penetrate a tube wall of the branched tube, and extend from the inside to an outside thereof; and a generator provided on the outside of the branched tube in the tube component, coupled to the turbine rotational shaft of the turbine, and converting rotational energy of the turbine blade to electric energy.

    Micro thruster uses and improvements

    公开(公告)号:US09863364B2

    公开(公告)日:2018-01-09

    申请号:US14407814

    申请日:2013-06-14

    IPC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.