专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

1. 发明授权

US08968500B2 Method and device for adhesively joining large-surface components in vehicle construction 有权
标题翻译：在车辆结构中粘接大面积部件的方法和装置
公开(公告)号：US08968500B2
公开(公告)日：2015-03-03
申请号：US13221279
申请日：2011-08-30
申请人： Dirk Niermann , Holger Frauen
发明人： Dirk Niermann , Holger Frauen
IPC分类号： B32B41/00 , B64F5/00 , B05C11/10 , B64C1/06 , B05C5/02 , B05C13/02 , B62D27/02 , B62D65/02
CPC分类号： B64F5/0009 , B05C5/0216 , B05C11/1021 , B05C13/02 , B62D27/026 , B62D65/028 , B64C1/068 , B64F5/10
摘要： A method for joining, by adhesive bonding, at least two large joining partners in vehicle construction, in particular in aircraft construction, comprises the following steps: detecting the geometric data of the joining partners in an automated manner, detecting the joint gap dimensions of the joining partners from the geometric data, applying adhesive to one or both joint faces of the two joining partners to be joined as a function of the joint gap dimensions, joining the joining partners in the joining position, and sequentially applying joining pressure to the joint faces along the joint gap to bring the joining partners into the final joining position.
摘要翻译：一种用于通过粘合剂粘合在车辆结构中，特别是飞机结构中的至少两个大的接合伙伴的方法包括以下步骤：以自动方式检测接合伙伴的几何数据，检测接合伙伴的接合间隙尺寸从所述几何数据接合伙伴，根据所述接合间隙尺寸将所述两个接合伙伴的一个或两个接合面施加粘合剂，将所述接合部件接合在所述接合位置，以及将接合压力依次施加到所述接合面沿着联合差距，使加盟伙伴进入最终加盟的位置。

2. 发明授权

US08468699B2 Method for producing a fuselage cell of an aircraft 有权
标题翻译：一种生产机身机身的方法
公开(公告)号：US08468699B2
公开(公告)日：2013-06-25
申请号：US12085268
申请日：2006-11-15
申请人： Holger Frauen , Dirk Gross , Oliver Kraatz , Eckart Frankenberger
发明人： Holger Frauen , Dirk Gross , Oliver Kraatz , Eckart Frankenberger
IPC分类号： B21D53/88
CPC分类号： B64F5/10 , Y10T29/49622
摘要： The invention relates to a method for producing at least one fuselage cell of an aircraft with the following steps: at least partial production of surface protection and thermal insulation in the region of the at least one shell part, at least partial introduction of technical outfitting systems 1-3, 10-12, 22-24, 46-48, in particular of electrical and hydraulic lines, air-conditioning lines, electrical and hydraulic appliances, sanitary and catering equipment or the like, into the at least one shell part and/or the at least one floor grid 13, 41, and assembly of the at least one shell part and of the at least one floor grid 13, 41 into the at least one fuselage section 32.
摘要翻译：本发明涉及一种用于生产飞行器的至少一个机身单元的方法，其具有以下步骤：在至少一个壳体部分的区域中至少部分地产生表面保护和绝热，至少部分引入技术out装系统 1-3,10-12,22-24,46-48，特别是电气和液压管线，空调线路，电气和液压设备，卫生和餐饮设备等，至少一个壳体部分和 /或至少一个地板网格41,41，以及至少一个壳体部分和至少一个地板栅极13,41的组装到至少一个机身部分32中。

3. 发明授权

US08167231B2 Shielding arrangement for lines, in particular electrical lines, in aircraft 有权
标题翻译：飞机上线路，特别是电线的屏蔽布置
公开(公告)号：US08167231B2
公开(公告)日：2012-05-01
申请号：US12316201
申请日：2008-12-10
申请人： Volker Leisten , Frank Falow , Holger Frauen
发明人： Volker Leisten , Frank Falow , Holger Frauen
IPC分类号： B64D45/00
CPC分类号： B64C1/18 , B64D45/02
摘要： A shielding arrangement for the lightning protection of electrical lines and components in an aircraft includes a protected installation space for receiving the lines that is arranged in the region of a floor framework, at least one delimiting surface of the installation space being provided at least in certain regions with an electrically conductive shielding, the at least one delimiting surface of the installation space being formed with at least one floor panel and a further delimiting surface of the installation space being formed with at least one ceiling panel.
摘要翻译：用于飞机中的电线和部件的防雷保护的屏蔽装置包括用于接收布置在地板框架区域中的线路的受保护的安装空间，至少一定的至少一个设置空间的限定表面具有导电屏蔽的区域，所述安装空间的所述至少一个限定表面形成有至少一个地板镶板，并且所述安装空间的另外的限定表面形成有至少一个天花板面板。

4. 发明申请

US20100031509A1 Method for Producing a Fuselage Cell of an Aircraft 有权
标题翻译：制造飞机机身细胞的方法
公开(公告)号：US20100031509A1
公开(公告)日：2010-02-11
申请号：US12085268
申请日：2006-11-15
申请人： Holger Frauen , Dirk Gross , Oliver Kraatz , Eckart Frankenberger
发明人： Holger Frauen , Dirk Gross , Oliver Kraatz , Eckart Frankenberger
IPC分类号： B21D53/88
CPC分类号： B64F5/10 , Y10T29/49622
摘要： The invention relates to a method for producing at least one fuselage cell of an aircraft with the following steps: at least partial production of surface protection and thermal insulation in the region of the at least one shell part, at least partial introduction of technical outfitting systems 1-3, 10-12, 22-24, 46-48, in particular of electrical and hydraulic lines, air-conditioning lines, electrical and hydraulic appliances, sanitary and catering equipment or the like, into the at least one shell part and/or the at least one floor grid 13, 41, and assembly of the at least one shell part and of the at least one floor grid 13, 41 into the at least one fuselage section 32.
摘要翻译：本发明涉及一种用于生产飞行器的至少一个机身单元的方法，其具有以下步骤：在至少一个壳体部分的区域中至少部分地产生表面保护和绝热，至少部分引入技术out装系统 1-3,10-12,22-24,46-48，特别是电气和液压管线，空调线路，电气和液压设备，卫生和餐饮设备等，至少一个壳体部分和 /或至少一个地板网格41,41，以及至少一个壳体部分和至少一个地板栅极13,41的组装到至少一个机身部分32中。

5. 发明授权

US08667689B2 Method and arrangement for supplying essentially hollow bodies with equipment 有权
标题翻译：用于为基本上空心体供给设备的方法和装置
公开(公告)号：US08667689B2
公开(公告)日：2014-03-11
申请号：US11786927
申请日：2007-04-13
申请人： Eckart Frankenberger , Eike Klemkow , Horst Zapp , Gerhard Muller , Holger Frauen
发明人： Eckart Frankenberger , Eike Klemkow , Horst Zapp , Gerhard Muller , Holger Frauen
IPC分类号： B21D39/03
CPC分类号： B64F5/50 , B64F5/10 , Y10T29/49622 , Y10T29/49828 , Y10T29/49829 , Y10T29/53548
摘要： Method and arrangement for supplying essentially hollow bodies with equipment wherein the hollow bodies each have a transverse dimension and a longitudinal dimension being larger than the transverse dimension. The bodies have at least one opening for accessing their interior from outside along their longitudinal dimension. The hollow bodies are arranged essentially side-by-side along the longitudinal dimension and they are moved along their transverse dimension in a clocked fashion. An arrangement comprises a plurality of conveyor means for moving hollow bodies, wherein the conveyor means are arranged such that the hollow bodies are arranged side-by-side along their longitudinal dimension and moved along their transverse dimension in a clocked fashion.
摘要翻译：用于向基本上具有中空体的设备供应设备，其中中空体各自具有横向尺寸和纵向尺寸大于横向尺寸。主体具有至少一个开口，用于沿其纵向尺寸从外部进入其内部。中空体沿着纵向尺寸基本上并排布置，并且它们以其时钟方式沿其横向尺寸移动。一种装置包括用于移动中空体的多个传送装置，其中传送装置被布置成使得中空体沿着它们的纵向尺寸并排布置，并且以它们的横向尺寸以时钟方式移动。

6. 发明授权

US08146222B2 Device and method for joining and tacking sections for transportation vehicles 有权
标题翻译：运输车辆连接和固定部件的装置和方法
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。

7. 发明授权

US07430792B2 Device for processing components for means of transport, in particular for processing sections for aircraft 有权
标题翻译：用于处理运输工具的部件的装置，特别是用于飞机的处理部件
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。

8. 发明授权

US08765042B2 Fuselage section of an aircraft and method for the production of the fuselage section 有权
标题翻译：飞机的机身部分和生产机身部分的方法
公开(公告)号：US08765042B2
公开(公告)日：2014-07-01
申请号：US13154899
申请日：2011-06-07
申请人： Holger Frauen , Robert Alexander Goehlich
发明人： Holger Frauen , Robert Alexander Goehlich
IPC分类号： B32B37/16 , B29C70/30 , B64C1/00
CPC分类号： B29C70/202 , B29D99/001 , B29L2031/3082 , B64C1/068 , B64C2001/0072 , Y02T50/43
摘要： In accordance with the method, an inside layer of a fuselage section skin made from first fibers is placed on a manufacturing surface, the first fibers being placed in one or more first fiber directions. On the inside layer, a stiffening structure is formed from stiffening fibers, the stiffening fibers being placed in one or more stiffening fiber directions. An outside layer of the fuselage section skin, comprising fourth fibers, is placed on the stiffening structure formed from stiffening fibers, the fourth fibers being placed in one or more fourth fiber directions. The stiffening structure is designed and developed in such a way that the fuselage section does not require an additional stiffening structure, is connected with the fuselage section skin, and comprises the inside layer, the stiffening structure, and the outside layer; in particular, an additional stiffening structure in the form of stringers and frames is not required.
摘要翻译：根据该方法，将由第一纤维制成的机身部分皮肤的内层放置在制造表面上，将第一纤维放置在一个或多个第一纤维方向上。在内层中，加强结构由加强纤维形成，加强纤维被放置在一个或多个加强纤维方向上。包括第四纤维的机身部分皮肤的外层被放置在由加强纤维形成的加强结构上，第四纤维被放置在一个或多个第四纤维方向上。加固结构的设计和开发方式使得机身部分不需要额外的加强结构，与机身部分皮肤相连，并且包括内层，加强结构和外层; 特别地，不需要桁条和框架形式的附加加强结构。

9. 发明申请

US20120043008A1 METHOD AND DEVICE FOR ADHESIVELY JOINING LARGE-SURFACE COMPONENTS IN VEHICLE CONSTRUCTION 有权
标题翻译：车辆结构中粘合大面积部件的方法和装置
公开(公告)号：US20120043008A1
公开(公告)日：2012-02-23
申请号：US13221279
申请日：2011-08-30
申请人： Dirk Niermann , Holger Frauen
发明人： Dirk Niermann , Holger Frauen
IPC分类号： B32B37/02 , B29C65/00
CPC分类号： B64F5/0009 , B05C5/0216 , B05C11/1021 , B05C13/02 , B62D27/026 , B62D65/028 , B64C1/068 , B64F5/10
摘要： A method for joining, by adhesive bonding, at least two large joining partners in vehicle construction, in particular in aircraft construction, comprises the following steps: detecting the geometric data of the joining partners in an automated manner, detecting the joint gap dimensions of the joining partners from the geometric data, applying adhesive to one or both joint faces of the two joining partners to be joined as a function of the joint gap dimensions, joining the joining partners in the joining position, and sequentially applying joining pressure to the joint faces along the joint gap to bring the joining partners into the final joining position.
摘要翻译：一种用于通过粘合剂粘合在车辆结构中，特别是飞机结构中的至少两个大的接合伙伴的方法包括以下步骤：以自动方式检测接合伙伴的几何数据，检测接合伙伴的接合间隙尺寸从所述几何数据接合伙伴，根据所述接合间隙尺寸将所述两个接合伙伴的一个或两个接合面施加粘合剂，将所述接合部件接合在所述接合位置，以及将接合压力依次施加到所述接合面沿着联合差距，使加盟伙伴进入最终加盟的位置。

10. 发明申请

US20080250626A1 Method and arrangement for supplying essentially hollow bodies with equipment 有权
标题翻译：用于为基本上空心体供给设备的方法和装置
公开(公告)号：US20080250626A1
公开(公告)日：2008-10-16
申请号：US11786927
申请日：2007-04-13
申请人： Eckart Frankenberger , Eike Klemkow , Horst Zapp , Gerhard Muller , Holger Frauen
发明人： Eckart Frankenberger , Eike Klemkow , Horst Zapp , Gerhard Muller , Holger Frauen
IPC分类号： B64F5/00
CPC分类号： B64F5/50 , B64F5/10 , Y10T29/49622 , Y10T29/49828 , Y10T29/49829 , Y10T29/53548
摘要： Method and arrangement for supplying essentially hollow bodies with equipment wherein the hollow bodies each have a transverse dimension and a longitudinal dimension being larger than the transverse dimension. The bodies have at least one opening for accessing their interior from outside along their longitudinal dimension. The hollow bodies are arranged essentially side-by-side along the longitudinal dimension and they are moved along their transverse dimension in a clocked fashion. An arrangement comprises a plurality of conveyor means for moving hollow bodies, wherein the conveyor means are arranged such that the hollow bodies are arranged side-by-side along their longitudinal dimension and moved along their transverse dimension in a clocked fashion.
摘要翻译：用于向基本上具有中空体的设备供应设备，其中中空体各自具有横向尺寸和纵向尺寸大于横向尺寸。主体具有至少一个开口，用于沿其纵向尺寸从外部进入其内部。中空体沿着纵向尺寸基本上并排布置，并且它们以它们的横向尺寸以时钟方式移动。一种装置包括用于移动中空体的多个传送装置，其中传送装置被布置成使得中空体沿其纵向尺寸并排布置，并且以它们的横向尺寸方式移动。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式