公开(公告)号：US07966729B2

公开(公告)日：2011-06-28

申请号：US12635302

申请日：2009-12-10

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B21D53/88 ,  B25B27/14

CPC分类号： B64F5/10 ,  Y10T29/49622 ,  Y10T29/53961

摘要： The invention relates to a method for the economic production of entire fuselage cells of airplanes and to a site for carrying out the method. Differing from the conventional sectional assembly according to the invention separate shells (shell components) are attached to a substantially completed cockpit section and/or rear section. At this the half shell construction and the four shell construction as well as a combination hereof can be applied. Alternatively, the cockpit section and the rear section as well as the central wing box section can be aligned and positioned to each other in a site forming gaps in longitudinal direction. Subsequently, the shell components as well as the floor framework sections are adjusted circularly revolving between the sections and are ideally simultaneously connected to these by means of at least four cross-seams and a plurality of longitudinal seams.

摘要翻译： 本发明涉及一种用于经济地生产飞机的整个机身单元的方法以及用于执行该方法的部位。 与根据本发明的常规分段组件不同，分离的壳（壳组件）附接到基本上完整的驾驶舱部分和/或后部。 在这种情况下，可以应用半壳结构和四壳结构以及其组合。 或者，驾驶舱部分和后部部分以及中央翼箱部分可以在形成纵向方向上的间隙的位置彼此对准和定位。 随后，外壳部件以及底板框架部分在两部分之间循环地调节，并且理想地通过至少四个交叉接缝和多个纵向接缝同时连接到这些部件。

公开(公告)号：US20060182558A1

公开(公告)日：2006-08-17

申请号：US11286739

申请日：2005-11-22

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B65G67/00

CPC分类号： B64F5/50

摘要： A device for transporting components for transportation systems between workstations comprises a transport apparatus and a positioning frame. The positioning frame is maintained on the apparatus and has a positioning element capable of aligning the position frame in the workstation. In one example, at least one positioning element arranged on the positioning frame allows alignment of components forming a section of an aircraft that is situated on at least one positioning frame in relation to workstations. During this process, connecting members are inserted into receptacle members arranged in the region of the floor area. The members may be at least partially form-fitted fashion. In order to adapt the device to sections with different dimensions, such as sections with different cross-sectional geometries and/or lengths, the device is provided with at least one supporting device for supporting the section that is mounted on the positioning frame. After depositing at least one positioning frame in the work station, the decoupled transport device may be used for transporting other sections.

摘要翻译： 用于在工作站之间运输运输系统的部件的装置包括运输装置和定位架。 定位框架保持​​在设备上，并且具有能够对准工作站中的位置框架的定位元件。 在一个示例中，布置在定位框架上的至少一个定位元件允许形成相对于工作站位于至少一个定位框架上的飞行器的一部分的部件的对准。 在该过程中，将连接构件插入布置在地板区域的插座构件中。 这些构件可以至少部分地形式配合。 为了使装置适应具有不同尺寸的部分，例如具有不同横截面几何形状和/或长度的部分，该装置设置有至少一个支撑装置，用于支撑安装在定位框架上的部分。 在工作站中放置至少一个定位框架之后，解耦输送装置可用于运送其它部分。

公开(公告)号：US08146222B2

公开(公告)日：2012-04-03

申请号：US11286763

申请日：2005-11-22

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B21D53/88 ,  B23C1/00 ,  B23K1/14 ,  B23Q3/00 ,  B25B1/20 ,  B25B27/14

CPC分类号： B64F5/10 ,  Y10T29/49622 ,  Y10T29/49769 ,  Y10T29/49895 ,  Y10T29/5177 ,  Y10T29/53961 ,  Y10T29/53978

摘要： A device and method for joining and tacking several individual components independently of shape and/or size to form inherently rigid, transportable sections for transportation vehicles, such as an aircraft is disclosed. According to one embodiment of the invention, the individual components may be spatially positioned relative to each other independently of shape and/or size. The spatial positions of the individual components may be determined by a measuring device, such as a laser measuring device, and varied via several positioning devices until a preset spatial position of the individual components has been reached in which the individual component are tacked together to form a section. In another embodiment, the positioning devices may be designed as base positioners, a first lateral positioner, a second lateral positioner, an upper positioner as well as an inner positioner. Joining and tacking of several individual components 1 may form varying sections such as sections with varying cross sectional geometries and/or cross sectional dimensions and/or linear dimensions for different types of aircraft or for derivatives of the same aircraft types. In addition, the sections may have two working platforms on either side of the section.

摘要翻译： 公开了一种用于独立于形状和/或尺寸来连接和固定多个单独部件的装置和方法，以形成用于诸如飞机的运输车辆的固有刚性的可运输部分。 根据本发明的一个实施例，各个部件可以在空间上相对于彼此独立于形状和/或尺寸定位。 各个部件的空间位置可以由诸如激光测量装置的测量装置来确定，并且经由多个定位装置改变，直到达到各个部件的预设空间位置，其中各个部件一起固定在一起形成 一节。 在另一个实施例中，定位装置可以被设计为基座定位器，第一侧向定位器，第二横向定位器，上部定位器以及内部定位器。 几个单独部件1的接合和固定可以形成不同的部分，例如具有不同类型的飞行器或相同飞机类型的导数的具有变化的横截面几何形状和/或横截面尺寸和/或线性尺寸的部分。 此外，这些部分可以在该部分的任一侧上具有两个工作平台。

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：US20060185143A1

公开(公告)日：2006-08-24

申请号：US11286771

申请日：2005-11-22

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B23P21/00

CPC分类号： B23Q41/06 ,  B23P21/004 ,  B23P2700/01 ,  B64F5/10 ,  Y10T29/5191

摘要： A device for manufacturing sections that are composed of several individual components uses a plurality of workstations. According to an embodiment of the invention, each workstation is designed for carrying out at least one of at least three manufacturing steps. Sections may be processed in each workstation regardless of their shape and/or size. A specialized manufacturing step such as assembly and tacking, connecting, finishing or performing follow-up work is carried out in each workstation. This allows a high degree of automation in at least some of the stations and improved capacity utilization, because the sections are transferred to a downstream workstation after the completion of the respective manufacturing. In one example, a method for manufacturing sections for transportation devices, such as aircraft, by assembling several individual components in a plurality of workstations is disclosed. One of at least three manufacturing steps is carried out in each workstation and the respective sections are processed in each workstation regardless of their shape and/or size.

摘要翻译： 用于制造由几个单独部件组成的部分的装置使用多个工作站。 根据本发明的实施例，每个工作站被设计用于执行至少三个制造步骤中的至少一个。 可以在每个工作站中处理部分，而不管其形状和/或尺寸如何。 在每个工作站中进行组装和整理，连接，整理或执行后续工作的专门制造步骤。 这允许在至少一些站中的高度自动化并且提高容量利用率，这是因为在相应制造完成之后将区段传送到下游工作站。 在一个示例中，公开了一种用于通过组装多个工作站中的多个单独部件来制造诸如飞机的运输装置的部件的方法。 在每个工作站中执行至少三个制造步骤中的一个，并且在每个工作站中处理各个部分，而不管其形状和/或尺寸如何。

公开(公告)号：US20060162140A1

公开(公告)日：2006-07-27

申请号：US11286763

申请日：2005-11-22

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B23Q17/00 ,  B25B27/14 ,  B23Q3/00

CPC分类号： B64F5/10 ,  Y10T29/49622 ,  Y10T29/49769 ,  Y10T29/49895 ,  Y10T29/5177 ,  Y10T29/53961 ,  Y10T29/53978

摘要： A device and method for joining and tacking several individual components independently of shape and/or size to form inherently rigid, transportable sections for transportation vehicles, such as an aircraft is disclosed. According to one embodiment of the invention, the individual components may be spatially positioned relative to each other independently of shape and/or size. The spatial positions of the individual components may be determined by a measuring device, such as a laser measuring device, and varied via several positioning devices until a preset spatial position of the individual components has been reached in which the individual component are tacked together to form a section. In another embodiment, the positioning devices may be designed as base positioners, a first lateral positioner, a second lateral positioner, an upper positioner as well as an inner positioner. Joining and tacking of several individual components 1 may form varying sections such as sections with varying cross sectional geometries and/or cross sectional dimensions and/or linear dimensions for different types of aircraft or for derivatives of the same aircraft types. In addition, the sections may have two working platforms on either side of the section.

摘要翻译： 公开了一种用于独立于形状和/或尺寸来连接和固定多个单独部件的装置和方法，以形成用于诸如飞机的运输车辆的固有刚性的可运输部分。 根据本发明的一个实施例，各个部件可以在空间上相对于彼此独立于形状和/或尺寸定位。 各个部件的空间位置可以由诸如激光测量装置的测量装置来确定，并且经由多个定位装置改变，直到达到各个部件的预设空间位置，其中各个部件一起固定在一起形成 一节。 在另一个实施例中，定位装置可以被设计为基座定位器，第一侧向定位器，第二横向定位器，上部定位器以及内部定位器。 几个单独部件1的接合和固定可以形成不同的部分，例如具有不同类型的飞行器或相同飞机类型的导数的具有变化的横截面几何形状和/或横截面尺寸和/或线性尺寸的部分。 此外，这些部分可以在该部分的任一侧上具有两个工作平台。

公开(公告)号：US20100192376A1

公开(公告)日：2010-08-05

申请号：US12635302

申请日：2009-12-10

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B21D53/88

CPC分类号： B64F5/10 ,  Y10T29/49622 ,  Y10T29/53961

摘要： The invention relates to a method for the economic production of entire fuselage cells of airplanes and to a site for carrying out the method. Differing from the conventional sectional assembly according to the invention separate shells (shell components) are attached to a substantially completed cockpit section and/or rear section. At this the half shell construction and the four shell construction as well as a combination hereof can be applied. Alternatively, the cockpit section and the rear section as well as the central wing box section can be aligned and positioned to each other in a site forming gaps in longitudinal direction. Subsequently, the shell components as well as the floor framework sections are adjusted circularly revolving between the sections and are ideally simultaneously connected to these by means of at least four cross-seams and a plurality of longitudinal seams.

摘要翻译： 本发明涉及一种用于经济地生产飞机的整个机身单元的方法以及用于执行该方法的部位。 与根据本发明的常规分段组件不同，分离的壳（壳组件）附接到基本上完整的驾驶舱部分和/或后部。 在这种情况下，可以应用半壳结构和四壳结构以及其组合。 或者，驾驶舱部分和后部部分以及中央翼箱部分可以在形成纵向方向上的间隙的位置彼此对准和定位。 随后，外壳部件以及底板框架部分在两部分之间循环地调节，并且理想地通过至少四个交叉接缝和多个纵向接缝同时连接到这些部件。

公开(公告)号：US07735817B2

公开(公告)日：2010-06-15

申请号：US11286739

申请日：2005-11-22

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B65G35/06

CPC分类号： B64F5/50

摘要： A device for transporting components for transportation systems between workstations comprises a transport apparatus and a positioning frame. The positioning frame is maintained on the apparatus and has a positioning element capable of aligning the position frame in the workstation. In one example, at least one positioning element arranged on the positioning frame allows alignment of components forming a section of an aircraft that is situated on at least one positioning frame in relation to workstations. During this process, connecting members are inserted into receptacle members arranged in the region of the floor area. The members may be at least partially form-fitted fashion. In order to adapt the device to sections with different dimensions, such as sections with different cross-sectional geometries and/or lengths, the device is provided with at least one supporting device for supporting the section that is mounted on the positioning frame, After depositing at least one positioning frame in the work station, the decoupled transport device may be used for transporting other sections.

摘要翻译： 用于在工作站之间运输运输系统的部件的装置包括运输装置和定位架。 定位框架保持​​在设备上，并且具有能够对准工作站中的位置框架的定位元件。 在一个示例中，布置在定位框架上的至少一个定位元件允许形成相对于工作站位于至少一个定位框架上的飞行器的一部分的部件的对准。 在该过程中，将连接构件插入布置在地板区域的插座构件中。 这些构件可以至少部分地形式配合。 为了使设备适应具有不同尺寸的部分，例如具有不同横截面几何形状和/或长度的部分，该装置设置有至少一个支撑装置，用于支撑安装在定位框架上的部分。 工作站中的至少一个定位框架，去耦输送装置可以用于运送其它部分。

公开(公告)号：US20060182557A1

公开(公告)日：2006-08-17

申请号：US11286785

申请日：2005-11-22

申请人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

发明人： Holger Frauen ,  Tomas Gnauck ,  Eike Klemkow

IPC分类号： B65G67/00

CPC分类号： B23B39/006 ,  B21J15/14 ,  B21J15/142 ,  B23K37/0443 ,  B23K2101/04 ,  B25J9/026 ,  B25J9/046 ,  B64F5/50 ,  Y10T29/5118

摘要： A device with at least one manipulator system for the shape-independent and/or size-independent connection of individual components to form sections 1 for transportation vehicles, such as aircraft, is disclosed. According to one embodiment of the invention, at least one manipulator system is spatially positioned for the shape-independent and/or size-independent connection of sections by at least one positioning device that is mounted on a support base. Due to the arrangement of at least one manipulator system on at least one positioning device, individual components may be connected to form sections, regardless of the size and or shape of the sections, such as sections having substantially different cross-sectional dimensions and/or lengths. Connection of the individual components takes place by suitable processing devices that are arranged on the manipulator systems, in which processing devices, such as riveting tools, welding tools or other tools, may be spatially positioned as desired. The processing devices comprises, for example, processing elements 25, 26, 61 to 64, 75, 76 for connecting individual components.

摘要翻译： 公开了一种具有至少一个操纵器系统的装置，用于独立部件和/或尺寸独立连接各个部件以形成用于诸如飞机的运输车辆的部分1。 根据本发明的一个实施例，至少一个操纵器系统在空间上被定位成用于通过至少一个安装在支撑基座上的定位装置的部分的形状独立和/或尺寸独立的连接。 由于至少一个操纵器系统在至少一个定位装置上的布置，各个部件可以连接以形成部分，而不管部分的尺寸和形状如具有基本上不同横截面尺寸的部分和/或 长度 各个部件的连接通过布置在操纵器系统上的合适的处理装置进行，其中可以根据需要在空间上定位诸如铆接工具，焊接工具或其它工具的处理装置。 处理装置包括例如用于连接各个部件的处理元件25,26,61至64,75,76。

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。