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    Magnetic de-rotation system for a shaft fairing system
    2.
    发明授权
    Magnetic de-rotation system for a shaft fairing system 有权
    用于整流罩系统的磁旋转系统

    公开(公告)号：US08584983B2

    公开(公告)日：2013-11-19

    申请号：US12745718

    申请日：2007-12-03

    申请人： Jayant Sirohi ,  Timothy Fred Lauder

    发明人： Jayant Sirohi ,  Timothy Fred Lauder

    IPC分类号： B64C27/51

    CPC分类号： B64C27/10 ,  B64C27/04 ,  B64C27/82 ,  B64C2027/8236

    摘要： A magnetic de-rotation system includes an inner ring which supports an eddy current ring and at least one inner ring magnet and an outer ring which supports at least one outer ring magnet, attraction between the at least one inner ring magnet and the at least one outer ring magnet produces a stable rotational position for a fairing.

    摘要翻译： 磁性去旋转系统包括支撑涡流环的内圈和至少一个内环磁体和支撑至少一个外环磁体的外圈，所述至少一个内环磁体与所述至少一个内环磁体之间的吸引力 外圈磁铁为整流罩产生稳定的旋转位置。

    MAGNETIC DE-ROTATION SYSTEM FOR A SHAFT FAIRING SYSTEM
    3.
    发明申请
    MAGNETIC DE-ROTATION SYSTEM FOR A SHAFT FAIRING SYSTEM 有权
    用于制动系统的磁性转向系统

    公开(公告)号：US20100264258A1

    公开(公告)日：2010-10-21

    申请号：US12745718

    申请日：2007-12-03

    申请人： Jayant Sirohi ,  Timothy Fred Lauder

    发明人： Jayant Sirohi ,  Timothy Fred Lauder

    IPC分类号： B64C27/00 ,  F16D27/00 ,  B64C27/32 ,  F01D5/00

    CPC分类号： B64C27/10 ,  B64C27/04 ,  B64C27/82 ,  B64C2027/8236

    摘要： A magnetic de-rotation system includes an inner ring which supports an eddy current ring and at least one inner ring magnet and an outer ring which supports at least one outer ring magnet, attraction between the at least one inner ring magnet and the at least one outer ring magnet produces a stable rotational position for a fairing.

    摘要翻译： 磁性去旋转系统包括支撑涡流环的内圈和至少一个内环磁体和支撑至少一个外环磁体的外圈，所述至少一个内环磁体与所述至少一个内环磁体之间的吸引力 外圈磁铁为整流罩产生稳定的旋转位置。

    Fluid-driven artificial muscles as mechanisms for controlled actuation
    6.
    发明申请
    Fluid-driven artificial muscles as mechanisms for controlled actuation 有权
    流体驱动的人造肌肉作为受控致动的机制

    公开(公告)号：US20080035798A1

    公开(公告)日：2008-02-14

    申请号：US11502360

    申请日：2006-08-11

    申请人： Curt S. Kothera ,  Benjamin K.S. Woods ,  Jayant Sirohi ,  Norman M. Wereley ,  Peter C. Chen

    发明人： Curt S. Kothera ,  Benjamin K.S. Woods ,  Jayant Sirohi ,  Norman M. Wereley ,  Peter C. Chen

    IPC分类号： B64C9/22

    CPC分类号： B64C3/54 ,  B63B1/248 ,  B63H25/382 ,  B64C3/48 ,  B64C9/00 ,  B64C13/28 ,  B64C27/615 ,  B64C2027/7266 ,  Y02T50/34

    摘要： A fluid contact surface actuation system for a vehicle, including a first fluid contact surface constructed and arranged to act against a first fluid passing over the first fluid contact surface; and a first fluid actuator coupled to the first fluid contact surface to move the first fluid contact surface between a first position and a second position to enable control of the vehicle in a predetermined manner, the first fluid actuator having a first resilient bladder that receives a second fluid such that pressure of the second fluid moves the first bladder between a contracted configuration and an expanded configuration.

    摘要翻译： 一种用于车辆的流体接触表面致动系统，包括构造和布置成抵靠经过第一流体接触表面的第一流体作用的第一流体接触表面; 以及联接到所述第一流体接触表面的第一流体致动器，以使所述第一流体接触表面在第一位置和第二位置之间移动，以使得能够以预定方式控制所述车辆，所述第一流体致动器具有第一弹性囊， 第二流体，使得第二流体的压力在收缩构型和膨胀构型之间移动第一囊。

    Biomimetic mechanism for micro aircraft
    7.
    发明授权
    Biomimetic mechanism for micro aircraft 有权
    微型飞机的仿生机制

    公开(公告)号：US06938853B2

    公开(公告)日：2005-09-06

    申请号：US10387494

    申请日：2003-03-14

    申请人： Darryll J. Pines ,  Felipe A. Bohorquez ,  Jayant Sirohi

    发明人： Darryll J. Pines ,  Felipe A. Bohorquez ,  Jayant Sirohi

    IPC分类号： B64C33/02 ,  B64C39/02 ,  B64C33/00

    CPC分类号： B64C39/028 ,  B64C33/02 ,  B64C2201/025 ,  B64C2201/042

    摘要： A biomimetic pitching and flapping mechanism including a support member, at least two blade joints for holding blades and operatively connected to the support member. An outer shaft member is concentric with the support member, and an inner shaft member is concentric with the outer shaft member. The mechanism allows the blades of a small-scale rotor to be actuated in the flap and pitch degrees of freedom. The pitching and the flapping are completely independent from and uncoupled to each other. As such, the rotor can independently flap, or independently pitch, or flap and pitch simultaneously with different amplitudes and/or frequencies. The mechanism can also be used in a non-rotary wing configuration, such as an ornithopter, in which case the rotational degree of freedom would be suppressed.

    摘要翻译： 包括支撑构件的仿生俯仰和拍动机构，用于保持叶片并且可操作地连接到支撑构件的至少两个叶片接头。 外轴构件与支撑构件同心，并且内轴构件与外轴构件同心。 该机构允许小型转子的叶片在翼片和俯仰自由度中被致动。 投球和扑动完全独立于彼此并且脱离。 因此，转子可以独立地以不同的幅度和/或频率折叠或独立地俯仰或折叠和俯仰。 该机构也可以以非旋转翼结构使用，例如鸟笼，在这种情况下旋转自由度将被抑制。