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8 条记录 (耗时 0.008 秒)

    Patch for Repairing Tires by Vulcanization
    1.
    发明申请
    Patch for Repairing Tires by Vulcanization 审中-公开
    通过硫化修复轮胎的补丁

    公开(公告)号：US20080142137A1

    公开(公告)日：2008-06-19

    申请号：US11885729

    申请日：2006-03-07

    申请人： Patric Scheungraber

    发明人： Patric Scheungraber

    IPC分类号： B29C73/06 ,  B29C73/10 ,  B32B33/00

    CPC分类号： B29C73/10 ,  B29C73/105 ,  B29K2021/00 ,  B29K2105/243 ,  B29L2030/00 ,  Y10T152/10882 ,  Y10T152/10909 ,  Y10T428/1471

    摘要： The invention relates to a patch for repairing tires, hoses and the like by vulcanization comprising at least one cover layer (1) made of a vulcanized rubber material, a joining layer (3) which is made of a rubber material and is laterally projected with respect to said cover layer (1) in an edge area (4), a protective film covering the top surface of the joining layer (3) and a thin flexible peel-off film (7) which loosely covers the surface of the cover layer (1) and adheres to the projected edge (4) of the joining layer (3), wherein said peel-off film (7) which covers the cover layer (1) and the projected edge (4) of the joining layer (3) is provided with a gripping element (8) for the removal thereof.

    摘要翻译： 本发明涉及一种用于通过硫化修复轮胎，软管等的贴片，其包括由硫化橡胶材料制成的至少一个覆盖层（1），由橡胶材料制成并且横向突出的接合层（3） 相对于边缘区域（4）中的所述覆盖层（1），覆盖接合层（3）的顶表面的保护膜和松散地覆盖覆盖层的表面的薄柔性剥离膜（7） （1）并且粘附到接合层（3）的突出边缘（4），其中覆盖覆盖层（1）的所述剥离膜（7）和接合层（3）的突出边缘（4） ）设置有用于去除它的夹紧元件（8）。

    Method for repairing fuel tanks
    2.
    发明申请
    Method for repairing fuel tanks 审中-公开
    修理燃油箱的方法

    公开(公告)号：US20030047268A1

    公开(公告)日：2003-03-13

    申请号：US09935900

    申请日：2001-08-23

    发明人： Gregory J. Korchnak ,  Kenneth J. Ritzema ,  Steven B. Swartzmiller

    IPC分类号： B32B035/00

    CPC分类号： B29C73/06 ,  B29C73/10 ,  B29C73/105 ,  B29C2073/264 ,  B29L2031/7172 ,  C09J5/00 ,  C09J2400/163 ,  C09J2400/226 ,  C09K3/12 ,  Y10T29/49732 ,  Y10T29/49734

    摘要： A method for repairing fuel tanks having detected leaks comprises (1) filling the detected leaks by applying an adhesive over the detected leaks and allowing the adhesive to cure to seal the detected leaks or (2) providing a fuel tank having a surface with detected leaks, providing a patch having a surface to be attached to the fuel tank surface having detected leaks, coating one or both surfaces with an adhesive, applying the patch over the detected leak(s) such that the adhesive is interposed between the patch surface and the tank surface, pressing the patch against the tank and allowing the adhesive to cure to bond the two surfaces together.

    摘要翻译： 用于修复具有检测到的泄漏的燃料箱的方法包括（1）通过在检测到的泄漏上施加粘合剂并使粘合剂固化以密封检测到的泄漏来填充检测到的泄漏，或（2）提供具有检测到的泄漏的表面的燃料箱 提供具有附接到具有检测到的泄漏的燃料箱表面的表面的贴片，用粘合剂涂覆一个或两个表面，将所述贴片施加在检测到的泄漏上，使得粘合剂插入在贴片表面和 罐表面，将贴片压靠在罐上并允许粘合剂固化以将两个表面粘合在一起。

    Method for Repairing an Aircraft Structure Component
    3.
    发明申请
    Method for Repairing an Aircraft Structure Component 有权
    飞机结构部件修理方法

    公开(公告)号：US20120137484A1

    公开(公告)日：2012-06-07

    申请号：US13311648

    申请日：2011-12-06

    申请人： Hermann Benthien ,  Axel Soeffker

    发明人： Hermann Benthien ,  Axel Soeffker

    IPC分类号： B23P6/00 ,  B64F5/00

    CPC分类号： B64F5/0081 ,  B29C73/10 ,  B29C73/105 ,  B29C73/30 ,  B64F5/40 ,  Y10T29/49723

    摘要： A method is provided for repairing an aircraft structural component which has a component fault in a portion adjoining a cavity of the aircraft structural component. The method includes removing a region of the aircraft structural component that has the component fault, introducing a bearing element into the cavity of the aircraft structural component through an opening, which has been formed in the aircraft structural component by the removal of the region of the aircraft structural component having the component fault, in such a way that a bearing surface of the bearing element comes to lie against a region, adjacent to the opening, of an inner surface of the aircraft structural component facing the cavity of the aircraft structural component, fixing the bearing element in its position in the cavity of the aircraft structural component, and closing the opening by means of a repair material.

    摘要翻译： 提供了一种用于修理在与飞行器结构部件的空腔相邻的部分中具有部件故障的飞行器结构部件的方法。 该方法包括去除具有部件故障的飞行器结构部件的区域，通过开口将轴承元件引入到飞行器结构部件的空腔中，该开口已经通过移除飞机结构部件的区域而形成 具有部件故障的飞行器结构部件以使得支承元件的支承表面抵靠飞机结构部件的面向飞行器结构部件的空腔的内表面的与开口相邻的区域的方式， 将轴承元件固定在飞行器结构部件的空腔中的位置，并且通过修理材料来关闭开口。

    METHOD FOR LOCATING MACHINING POSITION IN REPAIR MATERIAL, AND REPAIRING METHOD
    6.
    发明申请
    METHOD FOR LOCATING MACHINING POSITION IN REPAIR MATERIAL, AND REPAIRING METHOD 审中-公开
    用于定位修复材料中的加工位置的方法和修复方法

    公开(公告)号：US20160137316A1

    公开(公告)日：2016-05-19

    申请号：US14875982

    申请日：2015-10-06

    申请人： MITSUBISHI AIRCRAFT CORPORATION

    发明人： Toshikazu SHIGETOMI ,  Masatsugu SHIMIZU ,  Ryuichi NAGASE ,  Morimasa ISHIDA ,  Shuhei MUTO

    IPC分类号： B64F5/00 ,  G01N29/07 ,  B23P6/00

    CPC分类号： G01N29/07 ,  B23P6/00 ,  B23P2700/01 ,  B29C70/00 ,  B29C73/10 ,  B29C73/105 ,  B29C2073/264 ,  B64F5/40 ,  B64F5/60 ,  G01N29/048 ,  G01N29/4436 ,  G01N2291/2694

    摘要： The present invention provides a method for locating a machining position in a repair material that is arranged on a member including a machined portion formed by predetermined machining, the method including: a step of arranging a marker including a portion having a different propagation characteristic of an ultrasonic wave from that of a peripheral portion in the machined portion existing in the member before the repair material is arranged on the member; and a step of applying the ultrasonic wave to the member covered with the repair material and locating the machining position at a position of the marker captured by the ultrasonic wave after the repair material is arranged on the member.

    摘要翻译： 本发明提供了一种在修补材料中定位加工位置的方法，该修补材料布置在包括通过预定加工形成的加工部分的构件上，该方法包括：将包括具有不同传播特性的部分的标记 在修复材料上存在于构件中的加工部分中的周边部分的超声波布置在构件上; 以及将修复材料布置在构件上之后，将超声波施加到覆盖有修补材料的构件并将加工位置定位在由超声波捕获的标记的位置处的位置。

    Method for repairing an aircraft structure component
    7.
    发明授权
    Method for repairing an aircraft structure component 有权
    修理飞机结构部件的方法

    公开(公告)号：US09382017B2

    公开(公告)日：2016-07-05

    申请号：US13311648

    申请日：2011-12-06

    申请人： Hermann Benthien ,  Axel Soeffker

    发明人： Hermann Benthien ,  Axel Soeffker

    IPC分类号： B64F5/00 ,  B29C73/10 ,  B29C73/30

    CPC分类号： B64F5/0081 ,  B29C73/10 ,  B29C73/105 ,  B29C73/30 ,  B64F5/40 ,  Y10T29/49723

    摘要： A method is provided for repairing an aircraft structural component which has a component fault in a portion adjoining a cavity of the aircraft structural component. The method includes removing a region of the aircraft structural component that has the component fault, introducing a bearing element into the cavity of the aircraft structural component through an opening, which has been formed in the aircraft structural component by the removal of the region of the aircraft structural component having the component fault, in such a way that a bearing surface of the bearing element comes to lie against a region, adjacent to the opening, of an inner surface of the aircraft structural component facing the cavity of the aircraft structural component, fixing the bearing element in its position in the cavity of the aircraft structural component, and closing the opening by means of a repair material.

    摘要翻译： 提供了一种用于修理在与飞行器结构部件的空腔相邻的部分中具有部件故障的飞行器结构部件的方法。 该方法包括去除具有部件故障的飞行器结构部件的区域，通过开口将轴承元件引入到飞行器结构部件的空腔中，该开口已经通过移除飞机结构部件的区域而形成 具有部件故障的飞行器结构部件以使得支承元件的支承表面抵靠飞机结构部件的面向飞行器结构部件的空腔的内表面的与开口相邻的区域的方式， 将轴承元件固定在飞行器结构部件的空腔中的位置，并且通过修理材料来关闭开口。