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    • 3. 发明授权
    • Device and method for joining and tacking sections for transportation vehicles
    • 运输车辆连接和固定部件的装置和方法
    • US08146222B2
    • 2012-04-03
    • US11286763
    • 2005-11-22
    • Holger FrauenTomas GnauckEike Klemkow
    • Holger FrauenTomas GnauckEike Klemkow
    • B21D53/88B23C1/00B23K1/14B23Q3/00B25B1/20B25B27/14
    • B64F5/10Y10T29/49622Y10T29/49769Y10T29/49895Y10T29/5177Y10T29/53961Y10T29/53978
    • 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.
    • 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。
    • 5. 发明授权
    • Method and device for producing a fuselage cell of an airplane
    • 用于生产飞机的机身单元的方法和装置
    • US07966729B2
    • 2011-06-28
    • US12635302
    • 2009-12-10
    • Holger FrauenTomas GnauckEike Klemkow
    • Holger FrauenTomas GnauckEike Klemkow
    • B21D53/88B25B27/14
    • B64F5/10Y10T29/49622Y10T29/53961
    • 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.
    • 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。
    • 6. 发明申请
    • Device for transporting components for transportation systems
    • 运输系统部件运输装置
    • US20060182558A1
    • 2006-08-17
    • US11286739
    • 2005-11-22
    • Holger FrauenTomas GnauckEike Klemkow
    • Holger FrauenTomas GnauckEike Klemkow
    • B65G67/00
    • B64F5/50
    • 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.
    • 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。
    • 7. 发明申请
    • Method and device for manufacturing sections for transportation systems
    • 运输系统制造方法和装置
    • US20060185143A1
    • 2006-08-24
    • US11286771
    • 2005-11-22
    • Holger FrauenTomas GnauckEike Klemkow
    • Holger FrauenTomas GnauckEike Klemkow
    • B23P21/00
    • B23Q41/06B23P21/004B23P2700/01B64F5/10Y10T29/5191
    • 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.
    • 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。
    • 8. 发明申请
    • Device and method for joining and tacking sections for transportation vehicles
    • 运输车辆连接和固定部件的装置和方法
    • US20060162140A1
    • 2006-07-27
    • US11286763
    • 2005-11-22
    • Holger FrauenTomas GnauckEike Klemkow
    • Holger FrauenTomas GnauckEike Klemkow
    • B23Q17/00B25B27/14B23Q3/00
    • B64F5/10Y10T29/49622Y10T29/49769Y10T29/49895Y10T29/5177Y10T29/53961Y10T29/53978
    • 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.
    • 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。
    • 9. 发明申请
    • METHOD AND DEVICE FOR PRODUCING A FUSELAGE CELL OF AN AIRPLANE
    • 用于生产机场的熔融池的方法和装置
    • US20100192376A1
    • 2010-08-05
    • US12635302
    • 2009-12-10
    • Holger FrauenTomas GnauckEike Klemkow
    • Holger FrauenTomas GnauckEike Klemkow
    • B21D53/88
    • B64F5/10Y10T29/49622Y10T29/53961
    • 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.
    • 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。
    • 10. 发明授权
    • Device for transporting components for transportation systems
    • 运输系统部件运输装置
    • US07735817B2
    • 2010-06-15
    • US11286739
    • 2005-11-22
    • Holger FrauenTomas GnauckEike Klemkow
    • Holger FrauenTomas GnauckEike Klemkow
    • B65G35/06
    • B64F5/50
    • 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.
    • 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。