METHOD & SYSTEM FOR PERFORMING A PACKAGE PRE-LOAD OPERATION IN ACCORDANCE WITH A DISPATCH PLAN
    32.
    发明申请
    METHOD & SYSTEM FOR PERFORMING A PACKAGE PRE-LOAD OPERATION IN ACCORDANCE WITH A DISPATCH PLAN 有权
    根据分配计划执行包装预加载操作的方法和系统

    公开(公告)号:US20070129842A1

    公开(公告)日:2007-06-07

    申请号:US11673891

    申请日:2007-02-12

    IPC分类号: G06F7/00

    摘要: The present invention provides systems and methods for electronically-capturing a destination address of a package and for using the destination address to automate a package pre-load operation. An embodiment of the invention includes a compression system for compressing the destination address as a compressed MaxiCode symbol, a smart shipping label system for generating a shipping label with a compressed MaxiCode and a pre-load assist system for generating package handling instructions from the electronically-captured destination address.

    摘要翻译: 本发明提供用于电子捕获包裹的目的地地址并使用目的地地址来自动化包装预加载操作的系统和方法。 本发明的实施例包括用于将目的地地址压缩为压缩MaxiCode符号的压缩系统,用于生成具有压缩MaxiCode的运输标签的智能运输标签系统和用于从电子方式生成包装处理指令的预加载辅助系统, 捕获的目的地址。

    Method and apparatus for locking a computer device

    公开(公告)号:US20060203434A1

    公开(公告)日:2006-09-14

    申请号:US11077072

    申请日:2005-03-10

    IPC分类号: H05K5/00 G06F1/16

    CPC分类号: G06F1/181

    摘要: A lock for a computer device comprises a lever operable to be positioned in a locked position and comprising at least one flange, a locking base slidably coupled to a device housing and attached to the lever, and a spring coupled to the locking base and to the device housing and operated upon by the lever, where in the locked position the at least one flange slides in a first corresponding at least one notch formed on the device housing, and where the locking base slides into a corresponding second notch formed on the device housing.

    Single-axis fin deployment system
    34.
    发明申请
    Single-axis fin deployment system 有权
    单轴翅片部署系统

    公开(公告)号:US20060163423A1

    公开(公告)日:2006-07-27

    申请号:US11043870

    申请日:2005-01-26

    IPC分类号: F42B10/14

    CPC分类号: F42B10/14

    摘要: A missile has fins that rotate about a single axis to deploy from a stowed position to a deployed position. A foil longitudinal axis of each fin is angled relative to a shaft of the fin, such that a single-axis rotation of the shaft moves the foil from the stowed position to a deployed position. A coil spring may provide both torsion and compression forces to rotate the fin into the deployed position and lock it into place. Torsion rotates the shaft until it reaches a seat on a bushing that is around the shaft. Then compression forces from the spring engage a keyed protrusion on the shaft with a corresponding keyway in the bushing, locking the shaft in place. There may be an additional lock once the fin is deployed, such as a spring-loaded pin in the missile body that engages a depression in the shaft.

    摘要翻译: 导弹具有围绕单个轴线旋转的翅片,以从收起位置部署到展开位置。 每个翅片的箔纵向轴线相对于翅片的轴成一角度,使得轴的单轴旋转将箔从收起位置移动到展开位置。 螺旋弹簧可以提供扭转和压缩力以将翅片旋转到展开位置并将其锁定到位。 扭转轴旋转直到其到达位于轴周围的衬套上的座椅。 然后,来自弹簧的压缩力将轴上的带键突起与衬套中的相应键槽接合,将轴锁定在适当位置。 一旦翅片被部署就可能有一个附加的锁,例如导弹体中的弹簧加载的销接合轴中的凹陷。

    Mechanism for at least regionally adjusting the curvature of airfoil wings

    公开(公告)号:US06644599B2

    公开(公告)日:2003-11-11

    申请号:US10008779

    申请日:2001-11-13

    申请人: Juan Perez

    发明人: Juan Perez

    IPC分类号: B64C348

    CPC分类号: B64C3/48

    摘要: A variable wing section having an adjustable profile shape extending in the wing-span direction, includes a plurality of torsion boxes, which are positioned in the longitudinal direction, are torsionally stiff about the wing-span direction, and are each constituted of a first wing skin, a second wing skin opposite to it, and at least one spar. The variable wing section includes at least one vertebra, which has a transmission element that is connected to the first wing skin by a pendulum joint in order to compensate for a relative movement between the first wing skin and the at least one vertebra, and which has a vertically spaced-apart point of connection to a drive chord, the length of which may be changed, using a control command. The length of the drive chord is changed as a function of a control signal, and the at least one vertebra is rotated about the wing-span direction, so that the shape of the torsion boxes, and thus the profile shape, are changed in a predetermined manner.

    Adjustable motor mount
    36.
    发明授权
    Adjustable motor mount 失效
    可调电机安装

    公开(公告)号:US4098477A

    公开(公告)日:1978-07-04

    申请号:US713678

    申请日:1976-08-12

    申请人: Juan Perez

    发明人: Juan Perez

    IPC分类号: F16M7/00

    CPC分类号: F16M7/00

    摘要: The specification discloses an adjustable motor mount enabling rapid movement of a motor to allow easy removal and proper tensioning of a drive belt. The motor mount moves relative to a supporting framework by means of a cable coupled to a cable take-up means.

    摘要翻译: 本说明书公开了一种可调电机安装座,可实现马达的快速移动,从而易于拆卸和适当张紧传动皮带。 电机安装座借助于耦合到电缆卷绕装置的电缆相对于支撑框架移动。