SHROUD DRIVEN DEPLOYABLE FLIGHT SURFACES AND METHOD

    公开(公告)号:US20210333074A1

    公开(公告)日:2021-10-28

    申请号:US16860530

    申请日:2020-04-28

    Abstract: A nose or tail assembly for a flight vehicle is provided in which the deployment of the canards or fins is driven by energy imparted by the shroud when it is released. A tip section is rotatably coupled to a base, and both are stowed in a volume between the shroud and nose/tail assembly. As the shroud is released, a drive feature engages the tip section to rotate and join the base to form a complete canard or fin. This eliminates the need for storing the canards or fins in or wrapped around the body and eliminates the need for a complex deployment mechanism occupying an internal volume of the body. Although viable for all sizes of flight vehicles, the shroud-driven deployment system scales to very small diameter vehicles in which internal volume is not available to store either flight surfaces or deployment mechanisms.

    HAND CONTROL DEVICE FOR CONRTOLLING A PERIPHERAL SYSTEM
    2.
    发明申请
    HAND CONTROL DEVICE FOR CONRTOLLING A PERIPHERAL SYSTEM 有权
    用于混合外围系统的手柄控制装置

    公开(公告)号:US20140116183A1

    公开(公告)日:2014-05-01

    申请号:US13665697

    申请日:2012-10-31

    CPC classification number: G05G9/047 G05G13/00 G06F3/0338 Y10T74/20372

    Abstract: A hand control device for controlling a peripheral system is disclosed. The hand control device can include a handle configured to be grasped by a user. The handle can comprise a body portion to be supported against a palm of the user. The hand control device can also include a finger control supported about the handle and comprising a rotatable joint to facilitate control based on flexion/extension of an index finger of the user. In addition, the hand control device can include a thumb control supported about the handle and comprising first and second rotatable joints to facilitate control based on flexion/extension and abduction/adduction of a thumb of the user.

    Abstract translation: 公开了一种用于控制外围系统的手控装置。 手控装置可以包括构造成由使用者掌握的手柄。 手柄可以包括被支撑在使用者手掌上的主体部分。 手控装置还可以包括手柄控制,其围绕手柄支撑并且包括可旋转关节,以便于基于使用者的食指的屈曲/伸展的控制。 此外,手控装置可以包括围绕手柄支撑的拇指控制器,并且包括第一和第二可旋转关节,以便于基于使用者的拇指的弯曲/伸展和外展/内收的控制。

    ROTARY ACTUATION MECHANISM
    3.
    发明申请
    ROTARY ACTUATION MECHANISM 审中-公开
    旋转执行机构

    公开(公告)号:US20140260737A1

    公开(公告)日:2014-09-18

    申请号:US13800851

    申请日:2013-03-13

    Abstract: A rotary actuation mechanism is disclosed. The rotary actuation mechanism can include an actuator having a body, and a slider movable on a linear path relative to the body. A first linkage can be pivotally coupled to the body at a first pivot having a first axis. A second linkage can be pivotally coupled to the slider at a second pivot having a second axis, and pivotally coupled to the first linkage at a third pivot. A length of the first linkage between the first pivot and the third pivot can be equal to a length of the second linkage between the second pivot and the third pivot. The slider can be movable to position the second axis in a collinear relationship with the first axis. The rotary actuation mechanism can include an anti-singularity device to constrain movement of the body when the first axis and the second axis are in the collinear relationship.

    Abstract translation: 公开了一种旋转致动机构。 旋转致动机构可以包括具有主体的致动器和可在相对于主体的线性路径上移动的滑块。 第一连杆机构可以在具有第一轴线的第一枢轴处枢转地联接到主体。 第二连杆机构可以在具有第二轴线的第二枢轴处枢转地联接到滑动件,并且在第三枢轴处枢转地联接到第一连杆机构。 第一枢轴和第三枢轴之间的第一连杆的长度可以等于第二枢轴和第三枢轴之间的第二连杆的长度。 滑块可以是可移动的,以将第二轴线定位成与第一轴线的共线关系。 当第一轴线和第二轴线处于共线关系时,旋转致动机构可以包括用于限制主体的运动的反奇异装置。

    Shroud driven deployable flight surfaces and method

    公开(公告)号:US11274907B2

    公开(公告)日:2022-03-15

    申请号:US16860530

    申请日:2020-04-28

    Abstract: A nose or tail assembly for a flight vehicle is provided in which the deployment of the canards or fins is driven by energy imparted by the shroud when it is released. A tip section is rotatably coupled to a base, and both are stowed in a volume between the shroud and nose/tail assembly. As the shroud is released, a drive feature engages the tip section to rotate and join the base to form a complete canard or fin. This eliminates the need for storing the canards or fins in or wrapped around the body and eliminates the need for a complex deployment mechanism occupying an internal volume of the body. Although viable for all sizes of flight vehicles, the shroud-driven deployment system scales to very small diameter vehicles in which internal volume is not available to store either flight surfaces or deployment mechanisms.

    LINEAR/ROTARY MOTION TRANSFORMING DEVICE
    5.
    发明申请
    LINEAR/ROTARY MOTION TRANSFORMING DEVICE 审中-公开
    线性/旋转运动变换装置

    公开(公告)号:US20140260715A1

    公开(公告)日:2014-09-18

    申请号:US13800582

    申请日:2013-03-13

    CPC classification number: F16H19/065 Y10T74/18056

    Abstract: A linear/rotary motion transforming device is disclosed. The device includes a first member, a second member, and a third member disposed along an axis such that the second member is disposed between the first member and the third member. The second member is linearly movable along the axis and rotatable about the axis. The third member is rotatable about the axis. Connecting elements pivotally couple the first member and the second member, and the second member and the third member, offset from the axis. The first member and the second member are linearly and rotatably movable relative to one another, and the second member and the third member are linearly and rotatably movable relative to one another. A load input mechanism is operably coupled to the second member or the third member. Load output is transferred via the other of the second member or the third member.

    Abstract translation: 公开了一种线性/旋转运动变换装置。 该装置包括沿轴线设置的第一构件,第二构件和第三构件,使得第二构件设置在第一构件和第三构件之间。 第二构件可沿轴线线性移动并且能够围绕轴线旋转。 第三构件可围绕轴线旋转。 连接元件枢转地联接第一构件和第二构件,并且第二构件和第三构件偏离轴。 第一构件和第二构件相对于彼此线性且可旋转地移动,并且第二构件和第三构件相对于彼此线性且可旋转地移动。 负载输入机构可操作地联接到第二构件或第三构件。 负载输出通过第二个成员或第三个成员中的另一个传送。

Patent Agency Ranking