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16 条记录 (耗时 0.011 秒)

    Cookie press
    5.
    外观设计
    Cookie press 失效

    公开(公告)号：USD485137S1

    公开(公告)日：2004-01-13

    申请号：US29173703

    申请日：2003-01-03

    申请人： Jeff Bull

    设计人： Jeff Bull

    Baked Good Marking Device and Method of Using the Same
    6.
    发明申请
    Baked Good Marking Device and Method of Using the Same 审中-公开
    烘烤好的标记装置及其使用方法

    公开(公告)号：US20120045557A1

    公开(公告)日：2012-02-23

    申请号：US13159494

    申请日：2011-06-14

    申请人： Traci Chapple ,  Stephanie Goode ,  Jeff Bull ,  Hugh Melling ,  David Starr

    发明人： Traci Chapple ,  Stephanie Goode ,  Jeff Bull ,  Hugh Melling ,  David Starr

    IPC分类号： A21C15/00 ,  G01B1/00 ,  A23P1/00

    CPC分类号： A47G23/08 ,  A21C11/106 ,  A21C15/00 ,  B26B25/005 ,  B26B29/06 ,  B26B29/063 ,  B26F1/36 ,  B26F1/3846 ,  B26F1/44 ,  Y10T83/7487

    摘要： A baked good marking device assembly comprises a base, an elongated marking arm, and a marker. The base has a top surface and a bottom surface. The elongated marking arm is generally perpendicular to the base. The elongated marking arm has a first side and a second side. At least one of the first side and the second side includes one of either a first channel and a first rail. The elongated marking arm has measuring indicia proximate the one of either the first channel and the first rail. The elongated marking arm is removably fixed to the base. The marker has a body portion. The marker is moveable along the first channel or the first rail of the elongated marking arm. The marker has a marking portion protruding outward from the body portion. The marking portion is disposed in a generally perpendicular relationship to the elongated marking arm.

    摘要翻译： 烘烤好的标记装置组件包括基部，细长标记臂和标记。 底座具有顶面和底面。 细长的标记臂通常垂直于基座。 细长的标记臂具有第一侧和第二侧。 第一侧和第二侧中的至少一个包括第一通道和第一轨道中的一个。 细长的标记臂具有靠近第一通道和第一轨道中的一个的测量标记。 细长的标记臂可拆卸地固定在基座上。 标记具有主体部分。 标记可以沿着细长标记臂的第一通道或第一轨道移动。 标记具有从主体部分向外突出的标记部分。 标记部分以与细长标记臂大致垂直的关系设置。

    Integrated thermal insulation system for spacecraft
    9.
    发明授权
    Integrated thermal insulation system for spacecraft 失效
    航天器综合保温系统

    公开(公告)号：US5803406A

    公开(公告)日：1998-09-08

    申请号：US656144

    申请日：1996-04-22

    申请人： Paul Kolodziej ,  Jeff Bull ,  Thomas Kowalski ,  Matthew Switzer

    发明人： Paul Kolodziej ,  Jeff Bull ,  Thomas Kowalski ,  Matthew Switzer

    IPC分类号： B64G1/58

    CPC分类号： B64G1/58

    摘要： An integrated thermal protection system (TPS) for a spacecraft includes a grid that is bonded to skin of the spacecraft, e.g., to support the structural loads of the spacecraft. A plurality of thermally insulative, relatively large panels are positioned on the grid to cover the skin of the spacecraft to which the grid has been bonded. Each panel includes a rounded front edge and a front flange depending downwardly from the front edge. Also, each panel includes a rear edge formed with a rounded socket for receiving the rounded front edge of another panel therein, and a respective rear flange depends downwardly from each rear edge. Pins are formed on the front flanges, and pin receptacles are formed on the rear flanges, such that the pins of a panel mechanically interlock with the receptacles of the immediately forward panel. To reduce the transfer to the skin of heat which happens to leak through the panels to the grid, the grid includes stringers that are chair-shaped in cross-section.

    摘要翻译： 用于航天器的集成热保护系统（TPS）包括结合到航天器的皮肤的网格，例如以支持航天器的结构负载。 多个绝热的，相对较大的面板位于网格上以覆盖已经结合网格的航天器的皮肤。 每个面板包括圆形前边缘和从前边缘向下悬垂的前凸缘。 此外，每个面板包括形成有圆形插座的后边缘，用于接收其中另一个面板的圆形前边缘，并且相应的后凸缘从每个后边缘向下。 引脚形成在前法兰上，并且引脚插座形成在后凸缘上，使得面板的销与立即前面板的插座机械联锁。 为了减少碰到通过面板泄漏到网格的热量的皮肤，网格包括横截面呈椅子状的桁条。