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    Linear Electrodynamic-Type Motor, Cryocooler Including Such a Motor and Method Implementing Such a Motor
    1.
    发明申请
    Linear Electrodynamic-Type Motor, Cryocooler Including Such a Motor and Method Implementing Such a Motor 有权
    线性电动式电动机，包括这种电动机的冷却器和实施这种电动机的方法

    公开(公告)号：US20120279234A1

    公开(公告)日：2012-11-08

    申请号：US13462390

    申请日：2012-05-02

    Applicant: Gérald AIGOUY ,  James Butterworth ,  Benoit Debray ,  Jean Christophe Rey

    Inventor： Gérald AIGOUY ,  James Butterworth ,  Benoit Debray ,  Jean Christophe Rey

    IPC: F25B9/00 ,  H02K41/02

    CPC classification number: H02K33/18 ,  F04B35/045 ,  H02P25/02

    Abstract: This motor includes: a translationally movable induction coil; a power-supply circuit adapted to deliver, to at least one induction coil, an AC power-supply current; a movable mass adopting a translational movement an induction coil arranged so as to move a respective movable mass between a first position and a second position where the movable mass can compress the fluid; a secondary circuit arranged to connect the terminals of at least one induction coil in short-circuit;The secondary circuit comprises a compensation component for producing a phase shift between the power-supply voltage and the power-supply current, so as to reduce the phase difference that the inductance of the induction coil produces.

    Abstract translation: 该电动机包括：可平移的感应线圈; 电源电路，适于向至少一个感应线圈传送AC电源电流; 采用平移运动的可移动物体，感应线圈，其布置成在第一位置和第二位置之间移动相应的可移动物体，在该位置处可移动物体可以压缩流体; 二次电路，其布置成在短路中连接至少一个感应线圈的端子; 次级电路包括用于在电源电压和电源电流之间产生相移的补偿部件，以便减小感应线圈产生的电感的相位差。

    Cryogenic tank and space launcher including such a tank
    3.
    发明授权
    Cryogenic tank and space launcher including such a tank 有权
    低温坦克和空间发射器，包括这样一个坦克

    公开(公告)号：US08690000B2

    公开(公告)日：2014-04-08

    申请号：US13148101

    申请日：2010-01-28

    Applicant: Jerome Lacapere ,  James Butterworth

    Inventor： Jerome Lacapere ,  James Butterworth

    IPC: B65D88/78 ,  B64G1/40 ,  F02K9/76 ,  B65D88/12

    CPC classification number: B64G1/402 ,  B65D88/12 ,  F02K9/766 ,  F17C13/088 ,  F17C2223/0161 ,  F17C2270/0194 ,  Y10T137/86212 ,  Y10T137/86348

    Abstract: A cryogenic tank for a space launcher, comprising a partition and delimiting top and bottom volumes communicating via at least one free central opening formed in the partition, so as, on the one hand, to allow for the flow of liquid by gravity from the top volume to the bottom volume via the central opening or openings and, on the other hand, to prevent the rising of the fluid from the bottom volume to the top volume via the central opening or openings under the action of acceleration forces, the tank also comprising at least one vent forming separate from the central opening or openings and providing fluid communication between the top and bottom volumes, the vent being configured to favor the migration of vapor from the bottom volume to the top volume and to prevent the rising of liquid from the bottom volume to the top volume.

    Abstract translation: 一种用于空间发射器的低温罐，包括隔板并限定通过形成在隔板中的至少一个自由中心开口连通的顶部和底部容积，一方面允许通过重力从顶部流出液体 通过中心开口或开口的体积相对于底部容积，另一方面，为了防止流体在加速力的作用下通过中心开口或开口从底部容积升高到顶部体积，该罐还包括 至少一个通气口与中心开口或开口分开形成，并提供顶部和底部体积之间的流体连通，该排气口构造成有利于蒸汽从底部体积迁移到顶部体积，并且防止液体从 底部音量到顶部音量。

    Linear electrodynamic-type motor, cryocooler including such a motor and method implementing such a motor
    5.
    发明授权
    Linear electrodynamic-type motor, cryocooler including such a motor and method implementing such a motor 有权
    线性电动力型电动机，包括这种电动机的低温制冷机和实施这种电动机的方法

    公开(公告)号：US09000692B2

    公开(公告)日：2015-04-07

    申请号：US13462390

    申请日：2012-05-02

    Applicant: Gerald Aigouy ,  James Butterworth ,  Benoit Debray ,  Jean Christophe Rey

    Inventor： Gerald Aigouy ,  James Butterworth ,  Benoit Debray ,  Jean Christophe Rey

    IPC: H02K41/00 ,  H02K33/18 ,  F04B35/04 ,  H02P25/02

    CPC classification number: H02K33/18 ,  F04B35/045 ,  H02P25/02

    Abstract: A linear electrodynamic-type motor, for compressing a fluid circulating in a cryocooler notably using a Stirling cycle, includes a translationally movable induction coil; a power-supply circuit adapted to deliver, to at least one induction coil, an AC power-supply current; a movable mass adopting a translational movement; an induction coil arranged so as to move a respective movable mass between a first position and a second position where the movable mass can compress the fluid; and a secondary circuit arranged to connect the terminals of at least one induction coil in short-circuit. The secondary circuit comprises a compensation component for producing a phase shift between the power-supply voltage and the power-supply current, so as to reduce the phase difference that the inductance of the induction coil produces.

    Abstract translation: 用于压缩在低温冷却器中循环的流体，特别是使用斯特林循环的线性电动力型电动机包括可平移的感应线圈; 电源电路，适于向至少一个感应线圈传送AC电源电流; 采用平移运动的移动体; 感应线圈，其布置成使得可移动质量块在第一位置和第二位置之间移动，在所述第一位置和第二位置，所述可动体可以压缩所述流体; 以及二次电路，其布置成在短路中连接至少一个感应线圈的端子。 次级电路包括用于在电源电压和电源电流之间产生相移的补偿部件，以便减小感应线圈产生的电感的相位差。

    Cryogenic Tank and Space Launcher Including Such a Tank
    6.
    发明申请
    Cryogenic Tank and Space Launcher Including Such a Tank 有权
    低温坦克和空间发射器包括这样一个坦克

    公开(公告)号：US20110289942A1

    公开(公告)日：2011-12-01

    申请号：US13148101

    申请日：2010-01-28

    Applicant: Jerome Lacapere ,  James Butterworth

    Inventor： Jerome Lacapere ,  James Butterworth

    IPC: F17C13/00

    CPC classification number: B64G1/402 ,  B65D88/12 ,  F02K9/766 ,  F17C13/088 ,  F17C2223/0161 ,  F17C2270/0194 ,  Y10T137/86212 ,  Y10T137/86348

    Abstract: A cryogenic tank for a space launcher, comprising a partition and delimiting top and bottom volumes communicating via at least one free central opening formed in the partition, so as, on the one hand, to allow for the flow of liquid by gravity from the top volume to the bottom volume via the central opening or openings and, on the other hand, to prevent the rising of the fluid from the bottom volume to the top volume via the central opening or openings under the action of acceleration forces, the tank also comprising at least one vent forming separate from the central opening or openings and providing fluid communication between the top and bottom volumes, the vent being configured to favor the migration of vapor from the bottom volume to the top volume and to prevent the rising of liquid from the bottom volume to the top volume.

    Abstract translation: 一种用于空间发射器的低温罐，包括隔板并限定通过形成在隔板中的至少一个自由中心开口连通的顶部和底部容积，一方面允许通过重力从顶部流出液体 通过中心开口或开口的体积相对于底部容积，另一方面，为了防止流体在加速力的作用下通过中心开口或开口从底部容积升高到顶部体积，该罐还包括 至少一个通气口与中心开口或开口分开形成，并提供顶部和底部体积之间的流体连通，该排气口构造成有利于蒸汽从底部体积迁移到顶部体积，并且防止液体从 底部音量到顶部音量。

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