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    Method and apparatus for manufacturing a shell component for an aircraft or spacecraft
    1.
    发明授权
    Method and apparatus for manufacturing a shell component for an aircraft or spacecraft 有权

    公开(公告)号：EP2905221B1

    公开(公告)日：2018-07-04

    申请号：EP14154486.6

    申请日：2014-02-10

    申请人： Airbus Operations GmbH

    发明人： Brunner, Stefan ,  Schulze, Wolfgang ,  Tiryaki, Memis ,  Eilken, Wolfgang

    IPC分类号： B64C1/12 ,  B64C3/26 ,  B64F5/00

    CPC分类号： B64C1/12 ,  B23P2700/01 ,  B64C1/068 ,  B64C3/26 ,  B64F5/10 ,  B64G1/22 ,  Y10T29/49622 ,  Y10T29/5397

    摘要： The present invention provides a method of manufacturing a shell component for an aircraft or spacecraft. The method comprises a step of positioning a skin panel (102), which includes a skin (104) of the aircraft or spacecraft and first and second stringers (111,112) stiffening the skin, opposite a frame (106) having first and second mouseholes (121,122) for receiving the first and second stringers, a step of elastically bending the skin panelm (102), a step of inserting the first stringer (111) into the first mousehole (121), and a step of releasing the elastic bend to insert the second stringer (112) into the second mousehole (122). Under a further aspect, the invention provides an apparatus (200) for manufacturing a shell component for an aircraft or spacecraft, comprising a positioning unit (203) for positioning a skin panel (102), whic h includes a skin (104) of the aircraft or spacecraft and first and second stringers (111,112) stiffening the skin, opposite a frame (106) having first and second mouseholes (121,122) for receiving the first and second stringers (111,112), a bending unit (204) for elastically bending the skin panel (102), an inserting unit (202) for inserting the first stringer (111) into the first mousehole (121), and a control unit (208), which controls the bending unit (204) to release the elastic bend in order to insert the second stringer (112) into the second mousehole (122).

    Method and apparatus for manufacturing a shell component for an aircraft or spacecraft
    3.
    发明公开
    Method and apparatus for manufacturing a shell component for an aircraft or spacecraft 有权
    用于生产壳结构用于飞行器或航天器的方法和装置

    公开(公告)号：EP2905221A1

    公开(公告)日：2015-08-12

    申请号：EP14154486.6

    申请日：2014-02-10

    申请人： Airbus Operations GmbH

    发明人： Brunner, Stefan ,  Schulze, Wolfgang ,  Tiryaki, Memis ,  Eilken, Wolfgang

    IPC分类号： B64C1/12 ,  B64C3/26 ,  B64F5/00

    CPC分类号： B64C1/12 ,  B23P2700/01 ,  B64C1/068 ,  B64C3/26 ,  B64F5/10 ,  B64G1/22 ,  Y10T29/49622 ,  Y10T29/5397

    摘要： The present invention provides a method of manufacturing a shell component for an aircraft or spacecraft. The method comprises a step of positioning a skin panel (102), which includes a skin (104) of the aircraft or spacecraft and first and second stringers (111,112) stiffening the skin, opposite a frame (106) having first and second mouseholes (121,122) for receiving the first and second stringers, a step of elastically bending the skin panelm (102), a step of inserting the first stringer (111) into the first mousehole (121), and a step of releasing the elastic bend to insert the second stringer (112) into the second mousehole (122). Under a further aspect, the invention provides an apparatus (200) for manufacturing a shell component for an aircraft or spacecraft, comprising a positioning unit (203) for positioning a skin panel (102), whic h includes a skin (104) of the aircraft or spacecraft and first and second stringers (111,112) stiffening the skin, opposite a frame (106) having first and second mouseholes (121,122) for receiving the first and second stringers (111,112), a bending unit (204) for elastically bending the skin panel (102), an inserting unit (202) for inserting the first stringer (111) into the first mousehole (121), and a control unit (208), which controls the bending unit (204) to release the elastic bend in order to insert the second stringer (112) into the second mousehole (122).

    摘要翻译： 本发明提供了制造的壳成分，用于在飞机或航天器的方法。 该方法包括定位蒙皮面板（102），其包括硬化的皮肤的飞机或航天器以及第一和第二纵梁（111112）的皮肤（104），一个框架（106）相对的具有第一的工序和第二鼠洞（ 121122），用于接收所述第一和第二纵梁的，可弹性的步骤弯曲皮肤panelm（102），将所述第一桁（111）到所述第一鼠洞（121）的步骤，和释放所述弹性弯曲，以插入的步骤 第二纵梁（112）到第二鼠洞（122）。 下一个另外的方面，本发明提供一种用于制造外壳部件用于在飞机或航天器，用于定位皮肤面板（102）包括定位部（203）的装置（200），其中H包括的皮肤（104） 飞机或航天器以及第一和第二纵梁（111112）加强皮肤，相对的具有框架（106）的第一和第二鼠标的孔（121,122），用于接收所述第一和第二纵梁（111112），弯曲部（204），用于弹性地弯曲所述 用于插入第一纵梁（111）到所述第一鼠洞（121）插入单元（202）的蒙皮壁板（102），以及控制所述弯曲部（204）的控制单元（208），以释放所述弹性弯曲在 为了插入第二纵梁（112）到第二鼠洞（122）。

    Receiving part for receiving a rod for coupling the rod to a bone anchoring element, bone anchoring device, method and tool for assembling the same
    4.
    发明公开
    Receiving part for receiving a rod for coupling the rod to a bone anchoring element, bone anchoring device, method and tool for assembling the same 有权
    接收部用于接收杆的杆联接到骨锚定元件骨锚固装置，方法和工具，其组装

    公开(公告)号：EP2384709A1

    公开(公告)日：2011-11-09

    申请号：EP10162063.1

    申请日：2010-05-05

    申请人： Biedermann Motech GmbH & Co. KG

    发明人： Biedermann, Lutz ,  Dannecker, Berthold

    IPC分类号： A61B17/70 ,  A61B17/86 ,  A61B17/88

    CPC分类号： A61B17/7037 ,  A61B17/7032 ,  A61B17/7074 ,  A61B17/866 ,  A61B17/8685 ,  A61B17/88 ,  A61B2017/00526 ,  Y10T29/49826 ,  Y10T29/49876 ,  Y10T29/49947 ,  Y10T29/53678 ,  Y10T29/53796 ,  Y10T29/5397 ,  Y10T29/53974 ,  Y10T29/53978

    摘要： A receiving part is provided for receiving a rod for coupling the rod to a bone anchoring element, the receiving part including a receiving part body (5) with a top end (9a) and a bottom end (17b); a rod receiving portion (9) with a channel (12) for receiving the rod (6), and a head receiving portion (17) for accommodating a head (3) of the bone anchoring element, the head receiving portion having an open end (19, 17b) and being flexible so as to allow introduction and clamping of the head; and a locking ring (8) embracing the head receiving portion (17), wherein the locking ring can assume a first position in which it is latched with respect to the receiving part body (5) and in which the head can be introduced into the head receiving portion (17) and a second position in which it is latched with respect to the receiving part body (5) and compresses the head receiving portion such that the head is clamped but is not locked. A method for assembling a bone anchoring device is provided, the method including providing the receiving part body with the locking ring in a first position in which it is latched with respect to the receiving part body and in which the head can be introduced into the receiving part body and can freely pivot therein; inserting the head; and moving the locking ring (8) and the receiving part body (5) relative to each other until the locking ring enters a second position in which it is latched with respect to the receiving part body and in which the bone anchoring element is held in an adjustable angular position but is not fully locked.

    摘要翻译： 的接收部被设置用于接收杆的杆联接到骨锚固元件，所述接收部分包括：接收部主体（5）具有顶端（9a）和一个底部（17b）的端部; 具有用于接收所述杆（6）用于容纳头部（3）的骨锚固元件的，具有开口端的头部接收部的通道（12），和一个头部接收部分（17）的杆接收部分（9） （19，17B），并是柔性的，以允许头部的引入和夹紧; 和锁定环（8）拥抱头部接收部分（17），worin锁定环可以假定其被锁存相对于所述接收部主体的第一位置（5），并且其中所述头部能够被引入到所述 头接收部分（17）和在其被相对于所述接收部主体（5）锁存并压缩检查的头部接收部所做的头部被夹住，但没有被锁定的第二位置。 提供了一种用于组装骨锚固装置的方法，该方法包括：提供接收部主体处于第一位置时，锁定环在它被锁存相对于所述接收部主体，并且其中所述头部能够被引入到所述接收 部本体和可自由枢转。其中; 插入头部; 和移动所述锁定环（8）和所述接收部主体（5）相对于彼此，直到锁定环进入其中它被锁存相对于所述接收部主体，并且其中所述骨锚固元件被保持在第二位置 可调整角度位置的，但没有被完全锁定。

    MACHINE TOOL
    5.
    发明公开
    MACHINE TOOL 有权
    机床

    公开(公告)号：EP2283966A1

    公开(公告)日：2011-02-16

    申请号：EP08764960.4

    申请日：2008-05-27

    申请人： MAKINO MILLING MACHINE CO. LTD.

    发明人： KAWADA, Takeshi ,  KOIKE, Sinji ,  NAGATOMO, Rintaro

    IPC分类号： B23Q1/48 ,  B23P23/00 ,  B23Q1/00

    CPC分类号： B23Q1/015 ,  B23Q1/488 ,  B23Q7/1431 ,  Y10T29/5196 ,  Y10T29/53961 ,  Y10T29/5397 ,  Y10T409/305488 ,  Y10T409/305824 ,  Y10T409/306048 ,  Y10T409/308288

    摘要： A machine tool for machining a workpiece with a tool moved relative to the workpiece is provided with a bed (13) providing a base, a column (15) vertically mounted on the bed (13), and a carriage (27) having supporting columns (27a and 27b), disposed on either side thereof, for oscillatably supporting a table (35), the carriage being oriented so that one (27b) of the supporting columns (27a and 27b) is positioned adjacent the column (15) and the other (27a) of the supporting columns is positioned away from the column (15).

    摘要翻译： 用相对于工件移动的工具加工工件的机床设置有提供底座的床（13），垂直安装在床（13）上的立柱（15），以及具有支撑柱的支架（27） （27a和27b），其设置在其任一侧上用于可摆动地支撑工作台（35），所述托架被定向为使得一个（27b）的支撑柱（27a和27b）定位在柱（15）附近，并且 其他（27a）支柱的位置远离柱（15）。

    Wall frame assembly table
    7.
    发明公开
    Wall frame assembly table 有权
    对于墙框装配表

    公开(公告)号：EP1097790A3

    公开(公告)日：2002-01-09

    申请号：EP00309701.1

    申请日：2000-11-02

    申请人： MiTek Holdings, Inc.

    发明人： Olden, Marc ,  Moore, Glenn R. ,  Dean, John C.

    IPC分类号： B27F7/15 ,  B27M3/00

    CPC分类号： B27M3/0073 ,  Y10S269/905 ,  Y10T29/5397

    摘要： A wall frame assembly table (10; 110) for rapid assembly of wall frames (W; W'; W'') at a central location for shipment to a construction site. The wall frame assembly table (10; 110) can be configured for construction of wall frames (W; W'; W'') of different shapes and sizes. The table (10; 110) is constructed to inhibit the accumulation of debris on the table (10; 110) for consistently accurate placement of the wall frame elements (B, T, S, J, C. H. O, D). Locating pins (34D, 36D; 134D, 136D) along the sides of the table (10; 110) engaging the wall frame elements (B, T, S, J, C, H. O, D) can be selectively removed as needed for driving nails through the elements (B, T, S, J, C, H. O, D). An adjustable support (40; 140) is provided for the top plate (T) of the wall frame (W; W'; W'') which can be extended to different distances from an edge of the table (10; 110) for walls of different height. In addition, the adjustable support (40; 140) can be angled in correspondence with a wall frame (W; W'; W'') which has a top plate (T) extending to an angle relative to the bottom plate (B). A laser projection system may be used to locate the elements (B, T, S, J, C, H, O, D) of the wall frame (W; W'; W''). However, the table (10; 110) may include an offset locator (205, 207) to permit entirely manual setup and assembly with minimal effort and skill.

    A MACHINE AND A METHOD FOR DRIVING INSERTS INTO PIECES OF SHEET METAL
    9.
    发明公开
    A MACHINE AND A METHOD FOR DRIVING INSERTS INTO PIECES OF SHEET METAL 失效
    一种将插入物驱入片状金属的机器和方法

    公开(公告)号：EP0814938A2

    公开(公告)日：1998-01-07

    申请号：EP96908492.0

    申请日：1996-03-08

    申请人： Amada America Inc. ,  CREA S.r.l.

    发明人： ITO, Katsuhide

    IPC分类号： B21D39 ,  B23P19

    CPC分类号： B23P19/02 ,  Y10T29/5343 ,  Y10T29/53522 ,  Y10T29/53709 ,  Y10T29/5397 ,  Y10T29/53974 ,  Y10T29/53978

    摘要： A machine for driving inserts into pieces of sheet metal includes a punch (50) and a die (46) movable relative to one another along an axis (A) along which the inserts are to be driven. The punch (50) and die (46) define a driving zone (52) therebetween, in which a hole (144) in the piece (22) in which an insert is to be driven is positioned. The axis (A) along which the inserts are to be driven is substantially horizontal and the pieces are held in a substantially vertical plane by an automatic handling device (26).

    摘要翻译： 用于将插入件驱动到金属片中的机器包括冲头（50）和冲模（46），所述冲头（50）和冲模（46）能够沿着轴线（A）相对于彼此移动，插入件沿着轴线（A）被驱动。 冲头（50）和冲模（46）在它们之间限定了一个驱动区域（52），在该驱动区域中定位有待驱动插入件的部件（22）中的孔（144）。 用于驱动插入件的轴线（A）基本上是水平的，并且通过自动处理装置（26）将这些部件保持在基本竖直的平面中。