Method of fixing a plurality of lower members each having a reference bore for installing an upper member, and fixing jigs
    91.
    发明公开
    Method of fixing a plurality of lower members each having a reference bore for installing an upper member, and fixing jigs 审中-公开
    一种用于安装多个下部元件,每个具有用于安装一个上部元件和附接装置的一个基准孔方法

    公开(公告)号:EP1384925A3

    公开(公告)日:2004-02-18

    申请号:EP03024656.5

    申请日:1998-10-13

    IPC分类号: H01L21/00

    摘要: First and second two spacing jigs 81 are used each having a rectangular parallelepipedal body 81a formed on the bottom surface thereof with projections 82 which are arranged side by side at a spacing equal to a predetermined interval between reference bores 106. First, the projections 82 of the first jig 81 are fitted in front reference bores 106 of respective lower members 31, 32, 33, and the projections 82 of the second jig 82 in rear reference bores 106 of the lower members. A right angle holding jig 84 in the form of a rectangular frame and having inner side faces positionable respectively in contact with the front side face of the first jig 81, the rear side face of the second jig 81 and the left and right side faces of the two jigs 81 is fitted around the bodies 81a of the two jigs 81 to adjust the arrangement of bores 106 to right angles. The lower members are fixed to a support member in this state by tightening up screw members 110.

    Method of fixing a plurality of lower members each having a reference bore for installing an upper member, and fixing jigs
    92.
    发明公开
    Method of fixing a plurality of lower members each having a reference bore for installing an upper member, and fixing jigs 审中-公开
    一种用于安装多个下部元件,每个具有用于安装一个上部元件和附接装置的一个基准孔方法

    公开(公告)号:EP1384925A2

    公开(公告)日:2004-01-28

    申请号:EP03024656.5

    申请日:1998-10-13

    IPC分类号: F16K27/00 H01L21/00

    摘要: First and second two spacing jigs 81 are used each having a rectangular parallelepipedal body 81a formed on the bottom surface thereof with projections 82 which are arranged side by side at a spacing equal to a predetermined interval between reference bores 106. First, the projections 82 of the first jig 81 are fitted in front reference bores 106 of respective lower members 31, 32, 33, and the projections 82 of the second jig 82 in rear reference bores 106 of the lower members. A right angle holding jig 84 in the form of a rectangular frame and having inner side faces positionable respectively in contact with the front side face of the first jig 81, the rear side face of the second jig 81 and the left and right side faces of the two jigs 81 is fitted around the bodies 81a of the two jigs 81 to adjust the arrangement of bores 106 to right angles. The lower members are fixed to a support member in this state by tightening up screw members 110.

    摘要翻译: 第一和第二两个限位夹具81被用于各具有长方体体81A与并排在等于106首先,82突起参考孔之间具有预定间隔的间距排列侧突起82形成在其底表面上 第一夹具81被装配在前面参考孔respectivement下部构件31,32,33的106,并且突出在后方参照第二夹具82的孔82的下构件106。 直角保持夹具84为矩形框架的形式,并且具有内侧面定位的分别与所述第一夹具81的前侧面相接触,该第二夹具81的后侧面和左右侧面 的两个夹具81被嵌合在两个夹具81的本体81a至腔106的配置调整为直角。 下部构件通过收紧螺丝部件110 固定到在该状态下的支撑部件

    A METHOD OF AND APPARATUS FOR ASSEMBLING AN AIRCRAFT WHEEL OR BRAKE COMPONENT ON AN AXLE OF AN UNDERCARRIAGE
    93.
    发明公开
    A METHOD OF AND APPARATUS FOR ASSEMBLING AN AIRCRAFT WHEEL OR BRAKE COMPONENT ON AN AXLE OF AN UNDERCARRIAGE 有权
    方法和装置以进行组装飞机轮或部分刹车片在底盘AXLE

    公开(公告)号:EP1322517A1

    公开(公告)日:2003-07-02

    申请号:EP01967540.4

    申请日:2001-09-21

    申请人: Airbus UK Limited

    IPC分类号: B64F5/00 B60B29/00

    摘要: A method of and apparatus for assembling an aircraft wheel or brake (10) component on an axle (26) of an undercarriage in which a holder (12) is provided for the component along with a lifting device (28). The lifting device is used to lift the holder with the component therein to a position where the component is substantially in axial alignment with the axle. Once in that position, assembly of the component on the axle can take place by moving the component axially on to the axle. The holder can then be lowered away from the assembled component.

    摘要翻译: 的对,其中一个保持架(12)与提升装置(28),沿着规定的成分的起落架的轮轴(26)的飞机轮或制动器(10)组件的组装方法和装置。 升降装置在其中使用与组件解除保持器的位置,其中该组件基本上与所述轴轴向对准。 一旦就位那样,在轴部件的组件可以通过在到所述轴沿轴向移动部件发生。 保持器然后可以从已组装部件降低了。

    Apparatus for corking bottles
    94.
    发明公开
    Apparatus for corking bottles 有权
    Vorrichtung zum Verschliessen von Flaschen mit Korken

    公开(公告)号:EP1314683A1

    公开(公告)日:2003-05-28

    申请号:EP02021008.4

    申请日:2002-09-20

    申请人: Arol S.p.A.

    发明人: Cirio, Sergio

    IPC分类号: B67B1/00 B67B1/04

    摘要: In an apparatus for corking bottles, the corks (T) are fed in succession within the cavities of a plurality of vice-like devices (8), which are driven in rotation by a carousel device and which are designed to be radially compressed by said vice-like devices before their insertion into the respective bottles. The cavity (17) of the vice-like device (8) that each time comes to occupy the position for receiving the cork T is set in communication with a negative-pressure source, which sucks the cork T downwards, causing it to drop into the cavity (17), and maintains it in the correct vertical position. Preferably, similar suction means are further provided at the outlet end of a feed channel (15) for feeding the corks, which brings the corks to a loading station (C). A transfer wheel (13) with a vertical axis transfers the corks (T) in succession from the loading station (C) to the starting station (A) of the corking apparatus, where the corks are received within the respective vice-like devices (8).

    摘要翻译: 在用于塞瓶的装置中,软木塞(T)连续地供给在多个类似装置(8)的空腔内,这些装置由转盘装置旋转驱动,并被设计成被所述 在类似设备插入相应的瓶子之前。 每次进入用于接收软木T的位置的副装置(8)的空腔(17)设置成与负压源连通,负压源向下吸入软木T,使其下降到 空腔(17),并将其保持在正确的垂直位置。 优选地,类似的抽吸装置进一步设置在供给通道(15)的出口端,用于供给软木塞,将软木塞带到装载站(C)。 具有垂直轴的传送轮(13)将软木塞(T)从加载站(C)连续地传送到软木塞装置的起始站(A),其中软木塞接收在相应的类似装置内 8)。

    REIBWERKZEUG MIT FÜHRUNGSSCHAFT
    97.
    发明公开
    REIBWERKZEUG MIT FÜHRUNGSSCHAFT 有权
    铰刀,并具领导PARTNERSHIP

    公开(公告)号:EP1259350A1

    公开(公告)日:2002-11-27

    申请号:EP01919294.7

    申请日:2001-02-17

    申请人: Dihart AG

    IPC分类号: B23B31/11

    摘要: The invention relates to a reaming tool for reaming out several axially interspaced borings (14) of a workpiece (12). The reaming tool comprises a guide shank (16) which can be clamped into a machine spindle and which can be supported in prepared borings (14) of the workpiece (12) to be machined using external supporting elements (18). The reaming tool also comprises a reaming head (26) which coaxially connects on the front end thereof. In order to be able to easily change a worn tool, the invention provides that the reaming head (26) can be connected to the guide shank (16) by means of an auto-centering clamping mechanism (30), and that the supporting elements (18) positioned in the proximity of the clamping mechanism (30) can, during a clamping process, be radially spread in an at least partial manner from a dimension smaller than that of the diameter to a predetermined diameter guide dimension.

    AIRCRAFT ASSEMBLY TOOL AND METHOD OF MANUFACTURING THE SAME
    99.
    发明公开
    AIRCRAFT ASSEMBLY TOOL AND METHOD OF MANUFACTURING THE SAME 有权
    FLUGZEUGMONTAGEWERKZEUG UND METHODE ZU DESSEN HERSTELLUNG

    公开(公告)号:EP1230124A1

    公开(公告)日:2002-08-14

    申请号:EP00976160.2

    申请日:2000-11-16

    申请人: BAE SYSTEMS plc

    IPC分类号: B64F5/00

    摘要: This invention provides a method of producing an aircraft assembly tool for supporting an aircraft component comprising: a) determining a plurality of predetermined positions and orientations in space at which the component should be supported; b) designing a fixture frame (12) configured to provide support at predetermined locations of the frame associated with said predetermined positions; c) constructing the fixture frame by selecting elongate members (14) having predetermined lengths and connecting the elongate members together by means of releasable fastening means (32); d) constructing a plurality of pick-up devices (20), each having a receiving element (76) for carrying the component, by selecting further elongate members (66) having predetermined lengths and connecting the further elongate members together by means of clamping elements (68) adapted selectively to allow at least three degrees of freedom of movement of each receiving element along at least two orthogonal axes and around at least one axis coplanar with the orthogonal axes; e) mounting the pick-up devices to the fixture frame at the predetermined locations; and f) moving each receiving element about/around the orthogonal axes to align the receiving element with a respective predetermined position and orientation. The invention further provides an aircraft assembly tool resulting from such a method.

    摘要翻译: 本发明提供一种用于支撑飞行器部件的飞行器组装工具。 装配工具包括固定框架(12),其被配置成在分别与预定计算位置相关联的框架的预定位置处提供支撑,并且在飞行器部件将被支撑的空间中相应计算出的取向,固定框架包括细长构件 )具有通过可释放的紧固装置(32)连接在一起的预定长度的多个拾取装置(20),每个拾取装置被夹紧到基本平坦或平面 相关联的所述细长构件的表面。 每个拾取装置包括用于承载飞行器部件的接收元件,具有预定长度的多个另外的细长构件(66),以及多个将另外的细长构件连接在一起并将接收元件连接到一个的夹紧元件(68) 所述另外的细长构件。 该装置选择性地允许接收元件沿着三个正交轴线和围绕三个正交轴线的六个自由度的移动自由度,以便将接收元件相对于相关联的预定位置和相应的取向三维对准,并且构成组装工具以接收 飞机部件。