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    • 11. 发明申请
    • METHOD AND APPARATUS FOR THE PRODUCTION OF MITRED CORNER JOINTS BY VIBRATION WELDING
    • 用于通过振动焊接生产蓖麻角接头的方法和装置
    • US20100071834A1
    • 2010-03-25
    • US12518952
    • 2007-12-11
    • Jörg VetterPeter EugsterBeat Bruderer
    • Jörg VetterPeter EugsterBeat Bruderer
    • B29C65/06
    • B29C65/0618B29C66/1162B29C66/52431B29C66/843B29L2031/005B29L2031/778
    • A method and an apparatus are described for the production of a mitered corner joint between parts of a frame, by vibration welding. During the welding procedure, in each case two parts of a frame are displaced by oscillatory heads into mutually perpendicular straight-line translatorial oscillations, the phases of which have been matched to one another in such a way that mitered areas of the two parts of the frame oscillate perpendicularly with respect to a stationary mitered plane and through the same, while the mitered area is retained under a prescribed welding pressure in the system. The method and the apparatus can be used for the simultaneous production of the four corner joints of a frame, in particular of a frame of the moveable or fixed part of windows or of doors. For this, at least four, and preferably eight, oscillatory heads, which displace the parts of the frame into the translatorial oscillations, are synchronized in such a way that their frequencies and amplitudes are the same.
    • 描述了一种通过振动焊接来生产框架部件之间的斜角接头的方法和装置。 在焊接过程中,在每种情况下,框架的两个部分被振荡头移位成相互垂直的直线翻译振荡,其相位彼此匹配,使得两个部分的斜面 框架相对于固定的倾斜平面垂直振荡,并且通过它们,同时斜面区域保持在系统中规定的焊接压力下。 该方法和装置可用于同时生产框架的四个角接头,特别是窗户或门的可移动或固定部分的框架。 为此,至少四个,最好是八个振荡头,其将框架的各部分移位到平移振荡中,以使它们的频率和振幅相同的方式同步。
    • 15. 发明申请
    • FUSION WELDING DEVICE AND ASSEMBLING APPARATUS
    • 熔焊设备和组装设备
    • US20080223526A1
    • 2008-09-18
    • US12046877
    • 2008-03-12
    • Shinichiro MaruyamaTatsuya Maruyama
    • Shinichiro MaruyamaTatsuya Maruyama
    • B29C65/12
    • B29C66/84121B29C65/203B29C65/2061B29C65/7802B29C65/7841B29C66/1162B29C66/324B29C66/5243B29C66/52431B29C66/81431B29C66/8223B29C66/841B29C66/84123B29C66/843B29L2031/005B29L2031/3475E06B3/9608
    • A fusion welding device include: a first holder, having a first face, and adapted to hold at least an outer peripheral face of an end portion of a first work in a state where the first work is movable in a longitudinal direction thereof; a second holder, having a second face opposed to the first face, and adapted to hold at least an outer peripheral face of an end portion of a second work in a state where the second work is movable in a longitudinal direction thereof; a heater, operable to heat the first and second works; a first and second movers, adapted to move the first and second holders in such directions that the first and second faces come close to or apart from each other; and a third mover, adapted to move the first and second holders in synchronization with each other in a direction along the first and second faces. The first and second holders are moved by the third mover in a state where the first and second faces are in contact with each other, whereby end faces of the end portions of the first and second works are pressed to each other in the longitudinal directions thereof in the first and second holders.
    • 熔焊装置包括:第一保持器,具有第一面,并且适于在第一工件沿其纵向移动的状态下保持第一工件的端部的至少外周面; 第二保持器,具有与第一面相对的第二面,并且适于在第二工件沿其纵向移动的状态下保持第二工件的端部的至少外周面; 加热器,可操作以加热第一和第二工件; 第一和第二移动器,适于沿着使得第一和第二面彼此接近或分离的方向移动第一和第二保持器; 以及第三移动器,其适于在沿着所述第一和第二面的方向上彼此同步地移动所述第一和第二保持器。 第一和第二保持器在第一和第二面彼此接触的状态下被第三移动体移动,由此第一和第二工件的端部的端面在其纵向方向上被彼此挤压 在第一和第二持有人。
    • 18. 发明申请
    • Window Frame for Aircraft
    • 飞机窗框
    • US20080054122A1
    • 2008-03-06
    • US11597348
    • 2005-05-24
    • Jens Bold
    • Jens Bold
    • B64C1/14
    • B64C1/1492B29C70/48B29L2031/005Y02T50/43
    • A window frame (1) for installation in the exterior shell (5) of an aircraft comprises at least one outer flange (2), an inner flange (3), and a vertical flange (4) arranged perpendicular to and between these flanges, whereby the connection with the aircraft structure takes place via the outer flange (2) and whereby on the inner flange (3), a window element to be held is attached, which is held via the vertical flange (4). The window frame (1) comprises resin reinforced with fiber web semifinished parts, whereby the progression of the layers of the webs in the three regions of the outer flange, inner flange, and vertical flange, respectively, follow the mechanical load direction. For manufacturing, a semifinished part (10) made from reinforced web (20, 21, 22) is inserted into a molding tool (11), in which, under pressure and temperature, resin is injected, and the component made in this manner is hardened subsequently in the molding tool.
    • 用于安装在飞行器的外壳(5)中的窗框(1)包括至少一个外凸缘(2),内凸缘(3)和垂直于这些凸缘之间的垂直凸缘(4) 由此与飞机结构的连接通过外凸缘(2)进行,并且由此在内凸缘(3)上,附接有待保持的窗体元件,其通过竖直凸缘(4)保持。 窗框(1)包括用纤维网半成品加强的树脂,由此分别在外凸缘,内凸缘和垂直凸缘的三个区域中的腹板层的进行遵循机械负载方向。 为了制造,将由增强纤维网(20,21,22)制成的半成品部件(10)插入到模塑工具(11)中,其中在压力和温度下注入树脂,并且以这种方式制成的部件是 随后在模具中硬化。