公开(公告)号：US07430792B2

公开(公告)日：2008-10-07

申请号：US11259669

申请日：2005-10-26

申请人： Henrik Linnemann ,  Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow ,  Wolfgang Ende ,  Frank Neuhaus

发明人： Henrik Linnemann ,  Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow ,  Wolfgang Ende ,  Frank Neuhaus

IPC分类号： B23P21/00

CPC分类号： B25J15/0616 ,  B23P19/00 ,  B23P2700/01 ,  B25J15/0052 ,  B25J15/0061 ,  B64F5/10 ,  Y10T29/4978 ,  Y10T29/51 ,  Y10T29/5118 ,  Y10T29/5191

摘要： A device for processing components, and in particular, sections for aircraft, includes a handling system that supports a holding frame. The holding frame includes at least one pressure stamp and/or at least one processing device or unit. By means of the handling system, the processing device is freely positionable in space in relation to the components. Preferably, in the region of the holding frame at least one connection element is arranged. Due to the connection elements, an essentially closed force ring is established between the holding frame and the components so that in an ideal case there is no longer any feedback of reaction forces to the handling system. The connection elements, the processing device and the pressure stamps can be movable by actuators and can comprise integrated force sensors and/or distance measuring sensors.

摘要翻译： 用于处理部件，特别是用于飞行器的部件的装置包括支撑保持框架的处理系统。 保持框架包括至少一个压力标记和/或至少一个处理装置或单元。 通过处理系统，处理装置可相对于部件在空间中自由定位。 优选地，在保持框架的区域中布置有至少一个连接元件。 由于连接元件，在保持框架和部件之间建立了基本上闭合的力环，使得在理想情况下不再有任何对处理系统的反作用力的反馈。 连接元件，处理装置和压力标记可以通过致动器移动，并且可以包括集成的力传感器和/或距离测量传感器。

公开(公告)号：US20060143890A1

公开(公告)日：2006-07-06

申请号：US11259669

申请日：2005-10-26

申请人： Henrik Linnemann ,  Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow ,  Wolfgang Ende ,  Frank Neuhaus

发明人： Henrik Linnemann ,  Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow ,  Wolfgang Ende ,  Frank Neuhaus

IPC分类号： B23P23/04

CPC分类号： B25J15/0616 ,  B23P19/00 ,  B23P2700/01 ,  B25J15/0052 ,  B25J15/0061 ,  B64F5/10 ,  Y10T29/4978 ,  Y10T29/51 ,  Y10T29/5118 ,  Y10T29/5191

摘要： A device for processing components, and in particular, sections for aircraft, includes a handling system that supports a holding frame. The holding frame includes at least one pressure stamp and/or at least one processing device or unit. By means of the handling system, the processing device is freely positionable in space in relation to the components. Preferably, in the region of the holding frame at least one connection element is arranged. Due to the connection elements, an essentially closed force ring is established between the holding frame and the components so that in an ideal case there is no longer any feedback of reaction forces to the handling system. The connection elements, the processing device and the pressure stamps can be movable by actuators and can comprise integrated force sensors and/or distance measuring sensors.

摘要翻译： 用于处理部件，特别是用于飞行器的部件的装置包括支撑保持框架的处理系统。 保持框架包括至少一个压力标记和/或至少一个处理装置或单元。 通过处理系统，处理装置可相对于部件在空间中自由定位。 优选地，在保持框架的区域中布置有至少一个连接元件。 由于连接元件，在保持框架和部件之间建立了基本上闭合的力环，使得在理想情况下不再有任何对处理系统的反作用力的反馈。 连接元件，处理装置和压力标记可以通过致动器移动，并且可以包括集成的力传感器和/或距离测量传感器。

公开(公告)号：US5961258A

公开(公告)日：1999-10-05

申请号：US936159

申请日：1997-09-24

申请人： Wolfgang Ende ,  Harald Schueler

发明人： Wolfgang Ende ,  Harald Schueler

IPC分类号： B21J15/10 ,  B25H1/00 ,  B23B39/00

CPC分类号： B25H1/0057 ,  B21J15/10 ,  Y10T408/5627 ,  Y10T408/563 ,  Y10T408/5653

摘要： In order to facilitate and reduce the time necessary for clamping together and boring a hole through at least two workpieces that are to be joined together, for example by rivets or bolts, a portable clamping and boring apparatus carries out all necessary operating steps once it is manually positioned at the intended location of the bored hole. The clamping and boring apparatus includes a tool body with a clamp device and a boring device mounted thereon. The clamp device includes a clamping yoke with a clamp jaw element at an end thereof, and a clamping cylinder that drives the clamping yoke in an axial direction toward the boring location, from an open starting position into a clamping position. The boring device includes a pneumatic boring machine adapted to receive a boring bit, and a boring feed advance drive connected to the boring machine to drive the boring bit in a feed advance direction opposed to and coaxial with the clamping direction of the clamp jaw element. The feed advance drive and the clamping cylinder are operatively coupled or interconnected so that the clamping step and boring step are automatically triggered together in proper sequence. The apparatus is especially suited for automatically clamping together two workpieces and boring holes therethrough, as necessary for forming a riveted connection between the workpieces, particularly in the construction of aircraft components.

摘要翻译： 为了方便和减少夹紧在一起并通过例如铆钉或螺栓连接在一起的至少两个工件镗孔所需的时间，便携式夹紧和钻孔装置一旦执行所有必要的操作步骤就执行所有必要的操作步骤 手动定位在钻孔的预期位置。 夹紧和钻孔装置包括具有夹紧装置的工具主体和安装在其上的钻孔装置。 夹紧装置包括在其一端具有夹紧爪元件的夹紧轭，以及夹紧缸，其将夹紧轭沿轴向方向从打开的起始位置驱动到夹紧位置。 钻孔装置包括适于容纳钻头的气动镗孔机，以及连接到钻孔机的钻孔进给驱动器，以与夹钳元件的夹紧方向相反并同轴的进给前进方向驱动钻头。 进给提前驱动器和夹紧缸可操作地联接或互连，使得夹紧步骤和钻孔步骤以适当的顺序自动地一起触发。 该装置特别适合于在工件之间形成铆接连接件，特别是在飞机部件的结构中，根据需要将两个工件和钻孔自动夹紧在一起。

公开(公告)号：US20090166346A1

公开(公告)日：2009-07-02

申请号：US12087095

申请日：2007-01-04

申请人： Udo Ketelhut ,  Manfred Hansen ,  Berend Andreessen ,  Wolfgang Ende

发明人： Udo Ketelhut ,  Manfred Hansen ,  Berend Andreessen ,  Wolfgang Ende

IPC分类号： B23K11/00

CPC分类号： H05B3/34 ,  B29C65/02 ,  B29C65/18 ,  B29C66/81455 ,  B29C66/81471 ,  B29C66/81821 ,  B29C66/82661 ,  B29C66/8762 ,  B29C66/91212 ,  B29C66/91231 ,  B29C66/91421 ,  B29C66/91431 ,  B29C66/961 ,  B29C73/10 ,  B29C73/12 ,  C09J5/06

摘要： The invention relates to a method for producing a bond of a first component (2) and of a second component (3) by means of a connecting mass (4), in particular with regard to large-area aircraft components of cylindrical or spherical contour, with the following method steps: (S1) connection of the components (2, 3) by means of the connecting mass (4); (S2) application of a heating element (6) to the first component (2); and (S3) curing of the connecting mass (4) by heating by means of the heating element (6) to produce the bond of the components (2, 3), wherein, during the curing of the connecting mass (4), a force is applied to the heating element (6) and the components (2, 3) by means of a first covering element (8) in the form of a vacuum film by the evacuation of a first cavity (12) in which the components (2, 3) and the heating element (6) applied to them are arranged, and to a corresponding device (1).

摘要翻译： 本发明涉及一种通过连接块（4）产生第一部件（2）和第二部件（3）的接合的方法，特别是关于圆柱形或球形轮廓的大面积飞行器部件 通过以下方法步骤：（S1）通过连接质量块（4）连接部件（2,3）; （S2）将加热元件（6）施加到第一部件（2）; 和（S3）通过加热元件（6）加热来固化连接质量块（4）以产生部件（2,3）的粘结，其中在连接质量块（4）的固化过程中， 通过排出第一空腔（12），通过真空膜形式的第一覆盖元件（8）将力施加到加热元件（6）和部件（2,3），其中部件 2，3）和施加到它们的加热元件（6）布置在相应的装置（1）上。

公开(公告)号：US06503029B1

公开(公告)日：2003-01-07

申请号：US09688568

申请日：2000-10-16

申请人： Wolfgang Ende ,  Harald Schueler

发明人： Wolfgang Ende ,  Harald Schueler

IPC分类号： B23B3500

CPC分类号： B23Q11/0046 ,  B23B47/28 ,  B23B49/02 ,  Y10T408/03 ,  Y10T408/50 ,  Y10T408/56245 ,  Y10T409/304088

摘要： A boring arrangement is connected to a boring machine equipped with a boring bit for boring a hole in overlapping workpieces. The boring arrangement includes a first sleeve connected to the boring machine, and a second sleeve that is movably connected to the first sleeve so as to allow a relative motion therebetween in a boring feed advance direction. Biasing elements such as springs apply a biasing force between the first and second sleeves so as to exert a pressing force through the second sleeve onto a pressing sleeve connected thereto. The boring bit moves through the interior of the pressing sleeve to bore the required hole in the workpiece. Thereby, the pressing sleeve surrounds the boring site and is seated and pressed against the workpiece with a pressing force that is greater than the boring feed advance force exerted by the boring bit onto the workpiece. A suction arrangement sucks away boring chips and other swarf material arising during the boring process. Thereby, the accumulation of swarf material in the joint areas between the two overlapping workpieces is avoided, and there is no need to separate the workpieces to remove swarf material.

摘要翻译： 一种钻孔装置连接到一个装有钻头的钻孔机，用于在重叠的工件上钻孔。 钻孔装置包括连接到镗床的第一套筒和可移动地连接到第一套筒的第二套筒，以允许其在镗床进给前进方向上的相对运动。 诸如弹簧的偏压元件在第一和第二套筒之间施加偏压力，以便通过第二套筒施加按压力到与其连接的按压套筒上。 钻头移动通过挤压套筒的内部，以在工件中钻出所需的孔。 由此，按压套筒围绕镗孔位置并且以比由钻头施加到工件上的镗孔进给力大的压力将其安置并压靠在工件上。 抽吸装置吸取在镗孔过程中产生的钻屑和其他切屑材料。 因此，避免了在两个重叠的工件之间的接合区域中的切屑材料的堆积，并且不需要分离工件以去除切屑材料。

公开(公告)号：US07621702B2

公开(公告)日：2009-11-24

申请号：US11246860

申请日：2005-10-07

申请人： Wolfgang Ende ,  Harald Schueler

发明人： Wolfgang Ende ,  Harald Schueler

IPC分类号： B23Q11/10

CPC分类号： F16N7/38 ,  Y10T137/7728 ,  Y10T408/03 ,  Y10T408/46

摘要： A timing element for a lubricant supply system is capable of using pneumatics for the time of delivery of lubricant for a preset duration. In one example, the timing element has a cavity having an entrance and an exit, a first piston and a second piston. The first piston and the second piston are disposed in the cavity. The first piston is coupled to the second piston in such that compressed air in the entrance of the cavity is capable of moving the second piston and closing the exit. A pneumatic timing element may be incorporated into a dosing unit that is capable of supplying an amount of lubricant in a mist to a plunger bushing of a machine tool without. The duration of the dosing may be controlled solely by pneumatics and may prevent excess pooling of lubricant in bore holes by shutting off lubricant delivery at a preset time.

摘要翻译： 用于润滑剂供应系统的定时元件能够在预定时间内使用气动输送润滑剂的时间。 在一个示例中，定时元件具有具有入口和出口的空腔，第一活塞和第二活塞。 第一活塞和第二活塞设置在空腔中。 第一活塞联接到第二活塞，使得空腔入口中的压缩空气能够移动第二活塞并关闭出口。 气动定时元件可以结合到计量单元中，该计量单元能够将一定量的雾中的润滑剂供应到机床的柱塞套管，而不需要。 计量的持续时间可以仅由气动控制，并且可以通过在预设的时间关闭润滑剂输送来防止润滑剂在钻孔中的过度积聚。

公开(公告)号：US20060075986A1

公开(公告)日：2006-04-13

申请号：US11246860

申请日：2005-10-07

申请人： Wolfgang Ende ,  Harald Schueler

发明人： Wolfgang Ende ,  Harald Schueler

IPC分类号： F01M11/02 ,  F01M1/04

CPC分类号： F16N7/38 ,  Y10T137/7728 ,  Y10T408/03 ,  Y10T408/46

摘要： A timing element for a lubricant supply system is capable of using pneumatics for the time of delivery of lubricant for a preset duration. In one example, the timing element has a cavity having an entrance and an exit, a first piston and a second piston. The first piston and the second piston are disposed in the cavity. The first piston is coupled to the second piston in such that compressed air in the entrance of the cavity is capable of moving the second piston and closing the exit. A pneumatic timing element may be incorporated into a dosing unit that is capable of supplying an amount of lubricant in a mist to a plunger bushing of a machine tool without. The duration of the dosing may be controlled solely by pneumatics and may prevent excess pooling of lubricant in bore holes by shutting off lubricant delivery at a preset time.