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    Method for Repairing an Aircraft Structure Component
    2.
    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 of Repairing an Aircraft Structure Component
    3.
    发明申请
    Method of Repairing an Aircraft Structure Component 有权
    修理飞机结构部件的方法

    公开(公告)号：US20120152438A1

    公开(公告)日：2012-06-21

    申请号：US13311627

    申请日：2011-12-06

    申请人： Hermann Benthien ,  Axel Soeffker

    发明人： Hermann Benthien ,  Axel Soeffker

    IPC分类号： B32B43/00 ,  B32B38/10

    CPC分类号： B29C73/10 ,  B29C73/32 ,  B64F5/40

    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 an expansion body into the cavity of the aircraft structural component through an opening that has been formed by the removal of the region of the aircraft structural component having the component fault, wherein the expansion body while being introduced into the cavity of the aircraft structural component is in a non-expanded state, converting the expansion body that has been introduced into the cavity of the aircraft structural component to an expanded state, 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，通过已经通过移除具有部件的飞行器结构部件的区域形成的开口将膨胀体引入到飞机结构部件的空腔中 其中所述膨胀体在被引入到所述飞行器结构部件的空腔中时处于非膨胀状态，将已经被引入到所述飞机结构部件的空腔中的膨胀体转变为膨胀状态，并且关闭所述开口 通过修理材料。

    Method for repairing an aircraft structure component
    4.
    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。

    Method of repairing an aircraft structure component
    5.
    发明授权
    Method of repairing an aircraft structure component 有权
    修理飞机结构部件的方法

    公开(公告)号：US08623160B2

    公开(公告)日：2014-01-07

    申请号：US13311627

    申请日：2011-12-06

    申请人： Hermann Benthien ,  Axel Soeffker

    发明人： Hermann Benthien ,  Axel Soeffker

    IPC分类号： B29C73/00 ,  B32B43/00

    CPC分类号： B29C73/10 ,  B29C73/32 ,  B64F5/40

    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 an expansion body into the cavity of the aircraft structural component through an opening that has been formed by the removal of the region of the aircraft structural component having the component fault, wherein the expansion body while being introduced into the cavity of the aircraft structural component is in a non-expanded state, converting the expansion body that has been introduced into the cavity of the aircraft structural component to an expanded state, 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，通过已经通过移除具有部件的飞行器结构部件的区域形成的开口将膨胀体引入到飞机结构部件的空腔中 其中所述膨胀体在被引入到所述飞行器结构部件的空腔中时处于非膨胀状态，将已经被引入到所述飞机结构部件的空腔中的膨胀体转变为膨胀状态，并且关闭所述开口 通过修理材料。

    AIRCRAFT ASSEMBLY AND METHOD FOR PRODUCING AN AIRCRAFT ASSEMBLY
    6.
    发明申请
    AIRCRAFT ASSEMBLY AND METHOD FOR PRODUCING AN AIRCRAFT ASSEMBLY 有权
    飞机装配和生产飞机装配的方法

    公开(公告)号：US20130125354A1

    公开(公告)日：2013-05-23

    申请号：US13469822

    申请日：2012-05-11

    申请人： Hermann Benthien ,  Axel Soeffker

    发明人： Hermann Benthien ,  Axel Soeffker

    IPC分类号： B64C1/12 ,  A44B18/00

    CPC分类号： B64C1/12 ,  A44B18/0069 ,  B29C65/483 ,  B29C65/4835 ,  B29C65/5057 ,  B29C65/54 ,  B29C65/562 ,  B29C65/72 ,  B29C66/112 ,  B29C66/1122 ,  B29C66/131 ,  B29C66/524 ,  B29C66/532 ,  B29C66/61 ,  B29C66/71 ,  B29C66/721 ,  B29C66/7212 ,  B29C66/72141 ,  B29C66/72143 ,  B29C66/7394 ,  B29C66/73941 ,  B29L2031/3076 ,  B64C2001/0072 ,  Y02T50/43 ,  Y10T24/2717 ,  B29K2307/04 ,  B29K2309/08 ,  B29K2063/00

    摘要： An aircraft assembly is provided having a first aircraft component and a second aircraft component, at least one of the aircraft components being composed of a fibre-reinforced composite material, a connecting device connecting the first aircraft component to the second aircraft component, the connecting device including a first and a second section having a carrier element connected to the first and second aircraft components respectively, the first section having a first surface facing the first aircraft component and a second surface facing away from the first aircraft components, the second section having a first surface facing the second aircraft component and a second surface facing away from the second aircraft component. The first and second sections include a plurality of hook and loop elements extending from the second surface of the carrier element and cooperate to produce a hook and loop connection between the first and second aircraft components.

    摘要翻译： 提供具有第一飞行器部件和第二飞行器部件的飞行器组件，所述飞行器部件中的至少一个由纤维增强复合材料，将第一飞行器部件连接到第二飞行器部件的连接装置，连接装置 包括具有分别连接到第一和第二飞行器部件的承载元件的第一部分和第二部分，第一部分具有面向第一飞行器部件的第一表面和远离第一飞行器部件的第二表面，第二部分具有 面向第二飞行器部件的第一表面和远离第二飞行器部件的第二表面。 第一和第二部分包括从载体元件的第二表面延伸的多个钩和环元件，并且协作以在第一和第二飞行器部件之间产生钩环连接。