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    • 2. 发明申请
    • WINDOW STAYS
    • WO1983003634A1
    • 1983-10-27
    • PCT/SE1983000146
    • 1983-04-19
    • OLOFSSON, Gustaf, Arne, Wilhelm
    • E05C19/14
    • E05C17/04
    • The invented window stay consists of one part (1) to be attached to a window casement by a screw (4) and one on the screw flexible mounted link (9), which is eccentrically flexible mounted at a partly cylindrical fulcrum pin. This pin can be put through an opening (17), the width of which corresponds to the smallest dimension of the pin, into a tubular part (16) of a fitting (2). This fitting (2) is to be attached to the window frame. The fulcrum pin has a slip fit in the tubular part and is turnable to a position, from which it cannot be brought out through the radial opening (17) in the tubular part. In this position the casement is pulled agaisnt the frame by the eccentrically mounted link. A bolt arranged in the pin can in said position of the stay be screwed out so, that it reaches through a hole in the link, whereby the stay is blocked with its pin in the cylindrical boring of the tubular fitting. To prevent axial pulling out from the boring of the pin, a radial flange is attached to the boring, the flange fitting with a radial groove of the pin.
    • 本发明的窗户支架由通过螺钉(4)连接到窗扇的一部分(1)和螺钉柔性安装链节(9)上的一个,其偏心地安装在部分圆柱形的支点销上。 该销可以穿过其宽度对应于销的最小尺寸的开口(17)进入配件(2)的管状部分(16)中。 该配件(2)将连接到窗框。 支点销在管状部分中具有滑动配合,并且可转动到不能通过管状部分中的径向开口(17)从该位置脱出的位置。 在这种位置,通过偏心安装的链接将窗框拉开。 在所述销的所述位置处布置的销钉中的螺栓被拧出,使得其通过所述连杆中的孔到达,由此所述支柱被其销钉阻塞在所述管状配件的圆柱形钻孔中。 为了防止从销的镗孔轴向拉出,径向凸缘连接到镗孔,凸缘配件与销的径向凹槽连接。
    • 5. 发明授权
    • Rail arrangement for guiding a fitting inside guiding rails particularly in aircrafts
    • 用于将导轨特别是在飞机上引导配件的轨道布置
    • US08448911B2
    • 2013-05-28
    • US12490476
    • 2009-06-24
    • Arne WilhelmMarkus Fritz
    • Arne WilhelmMarkus Fritz
    • F16M13/00
    • B64C1/18B60N2/01575
    • The invention relates to a rail arrangement for coupling a displaceable element to a support structure, wherein the rail arrangement comprises a guiding rail and a fitting. In this arrangement the fitting is connectable to the displaceable element, and the guiding rail is connectable to the support structure. The fitting is arranged in the guiding rail in such a way that the fitting can be displaced in longitudinal direction of the guiding rail; wherein the guiding rail is formed as an open-top hollow profile with a rail base. In this arrangement the rail base comprises at least one elevation that extends upwards (i.e. towards the open-top). The fitting comprises a bottom surface which in longitudinal direction is interrupted by a continuous groove, wherein the form of the groove of the fitting is designed in such a way that the fitting is guided by the elevation along the guiding rail.
    • 本发明涉及一种用于将可移动元件联接到支撑结构的轨道装置,其中轨道装置包括导轨和配件。 在这种布置中,配件可连接到可移动元件,并且导轨可连接到支撑结构。 所述接头以这样的方式设置在所述导轨中,使得所述接头可以在所述导轨的纵向方向上移位; 其中所述导轨形成为具有轨道基座的敞开的中空型材。 在这种布置中,轨道底座包括至少一个向上延伸的仰角(即朝向敞开的顶部)。 配件包括在纵向方向上被连续的凹槽中断的底面,其中配件的凹槽的形状被设计成使得配件沿导轨被高度引导。
    • 6. 发明授权
    • Rail for positioning and locking of elements, and a corresponding fitting
    • 轨道用于定位和锁定元件,以及相应的配件
    • US08074954B2
    • 2011-12-13
    • US12011949
    • 2008-01-30
    • Arne WilhelmPeter PoppKarel Smetana
    • Arne WilhelmPeter PoppKarel Smetana
    • A47B97/00
    • B64C1/20B64D11/0696
    • A rail for fastening installations in an aircraft, the rail including a rail base section, a running-surface section that extends in a longitudinal direction with a running surface, and a connection section that connects the running-surface section to the rail base section at the face pointing away from the running surface. The running-surface section laterally on both sides, in each case spaced apart at a predetermined pitch, includes a multitude of projections projecting away from the connection section, each with a top that has substantially the same alignment as the running surface and a bottom that has an alignment that substantially is opposed to the alignment of the running surface. The bottom of the projections forms holding surfaces for holding a fitting. The rail is attached to a floor of the aircraft.
    • 一种用于航空器中的紧固装置的轨道,所述轨道包括轨道基部,沿着纵向方向延伸有行驶表面的行进面部分,以及连接部分,其将所述行进表面部分连接到所述轨道基部, 表面指向远离跑步表面。 横向地在两侧上的行进表面部分以每个预定间距间隔开,包括多个突出部分,突出部分远离连接部分突出,每个具有与运行表面基本相同的顶部的顶部,以及底部, 具有基本上与行进表面的对准相对的对准。 突起的底部形成用于保持配件的保持表面。 铁轨连接在飞机的地板上。
    • 7. 发明申请
    • RAIL ARRANGEMENT FOR GUIDING A FITTING INSIDE GUIDING RAILS PARTICULARLY IN AIRCRAFTS
    • 用于指导航空器内引导导轨的轨道布置
    • US20090321606A1
    • 2009-12-31
    • US12490476
    • 2009-06-24
    • Arne WilhelmMarkus Fritz
    • Arne WilhelmMarkus Fritz
    • B64D11/06F16M13/02
    • B64C1/18B60N2/01575
    • The invention relates to a rail arrangement for coupling a displaceable element to a support structure, wherein the rail arrangement comprises a guiding rail and a fitting. In this arrangement the fitting is connectable to the displaceable element, and the guiding rail is connectable to the support structure. The fitting is arranged in the guiding rail in such a way that the fitting can be displaced in longitudinal direction of the guiding rail; wherein the guiding rail is formed as an open-top hollow profile with a rail base. In this arrangement the rail base comprises at least one elevation that extends upwards (i.e. towards the open-top). The fitting comprises a bottom surface which in longitudinal direction is interrupted by a continuous groove, wherein the form of the groove of the fitting is designed in such a way that the fitting is guided by the elevation along the guiding rail.
    • 本发明涉及一种用于将可移动元件联接到支撑结构的轨道装置,其中轨道装置包括导轨和配件。 在这种布置中,配件可连接到可移动元件,并且导轨可连接到支撑结构。 所述接头以这样的方式设置在所述导轨中,使得所述接头可以在所述导轨的纵向方向上移位; 其中所述导轨形成为具有轨道基座的敞开的中空型材。 在这种布置中,轨道底座包括至少一个向上延伸的仰角(即朝向敞开的顶部)。 配件包括在纵向方向上被连续的凹槽中断的底面,其中配件的凹槽的形状被设计成使得配件沿导轨被高度引导。
    • 8. 发明申请
    • DEVICE FOR HOLDING LINES IN AN AIRCRAFT
    • 用于在航空器内保持线路的装置
    • US20100314505A1
    • 2010-12-16
    • US12745945
    • 2008-12-17
    • Sandra DeimerJan HarderThomas KriebischAxel KönigJean-Marie Le CorreThomas MariakArne WilhelmMarkus Fritz
    • Sandra DeimerJan HarderThomas KriebischAxel KönigJean-Marie Le CorreThomas MariakArne WilhelmMarkus Fritz
    • F16L3/08
    • H02G11/003B64D11/0624
    • The invention relates to a device for holding lines in an aircraft that comprising at least one line inlet, at least one line outlet and at least one holding space for holding at least part of a line section extending between the line inlet and the line outlet, wherein the line section has a length that is equal to or greater than the clear distance between the relevant line inlet and line outlet, and wherein the holding space comprising means for separably holding, as well as for shortening or lengthening in a reversibly guided fashion, a line end that protrudes from the line inlet and/or line outlet. Due to the devices according to the invention, lines that are individually cut to length are no longer required for connecting reconfigurable rows of passenger seats because the device according to the invention releases or takes up excess line lengths depending on the position of the rows of passenger seats.
    • 本发明涉及一种用于在航空器中保持线路的装置,其包括至少一个线路入口,至少一个线路出口和至少一个保持空间,用于保持在线路入口和线路出口之间延伸的线路段的至少一部分, 其中所述线路段具有等于或大于所述相关线路入口和线路出口之间的清除距离的长度,并且其中所述保持空间包括用于以可逆地引导的方式可分离地保持以及缩短或延长的装置, 从线入口和/或线路出口突出的线端。 由于根据本发明的装置,由于根据本发明的装置根据乘客排的位置释放或占用多余的线路长度,所以不再需要单独切割成长度的线路用于连接可重新排列的乘客座椅 座位