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1. 发明授权

US09359090B2 Method for producing an aircraft fuselage and aircraft fuselage 有权
标题翻译：飞机机身和飞机机身的制造方法
公开(公告)号：US09359090B2
公开(公告)日：2016-06-07
申请号：US13320278
申请日：2010-05-10
申请人： Eugen Gorr , Rolf Bense
发明人： Eugen Gorr , Rolf Bense
IPC分类号： B64C1/00 , B64F5/00 , B64C1/06
CPC分类号： B64F5/0009 , B64C1/061 , B64C1/069 , B64C2001/0081 , B64F5/10 , Y10T29/49622
摘要： Disclosed is a method for the manufacture of an aircraft fuselage with at least two fuselage barrels wherein connecting segments are firstly prepared for the formation of a transverse joint region for a later transverse joint, and the fuselage barrels are then constructed around the connecting segments; also disclosed is an aircraft fuselage with ring-type connecting segments for the formation of such a transverse joint.
摘要翻译：公开了一种用于制造具有至少两个机身筒的飞机机身的方法，其中首先准备连接段以形成用于稍后的横向接头的横向接头区域，然后将机身滚筒围绕连接段构造; 还公开了具有用于形成这种横向接头的环形连接段的飞行器机身。

2. 发明授权

US08950707B2 Connection arrangement, particularly for aircraft structure parts 有权
标题翻译：连接布置，特别适用于飞机结构件
公开(公告)号：US08950707B2
公开(公告)日：2015-02-10
申请号：US13484440
申请日：2012-05-31
申请人： Rolf Bense
发明人： Rolf Bense
IPC分类号： B64C1/06 , B21J15/02 , F16B19/08 , F16B5/04
CPC分类号： B21J15/025 , F16B5/04 , F16B19/08 , Y10T29/49956
摘要： A connection arrangement for at least two abutting components to be firmly connected to one another, includes a self-piercing rivet having a rivet head for punching of a hole and subsequent riveting of the components, wherein a washer is allocated to the self-piercing rivet at the distal end region opposite to the rivet head, with the washer including a frontal area for the insertion of a circular indentation to create a firm compression connection between a hole in the washer and the distal end region of the self-piercing rivet.
摘要翻译：用于至少两个邻接部件的连接装置彼此牢固地连接，包括具有用于冲孔的铆钉头和随后的铆接件的自穿孔铆钉，其中垫圈分配给自穿孔铆钉在与铆钉头相对的远端区域处，垫圈包括用于插入圆形凹口的前部区域，以在垫圈中的孔和自穿孔铆钉的远端区域之间产生牢固的压缩连接。

3. 发明授权

US08869374B2 Method and a device for the formation of an overlap joint 有权
标题翻译：用于形成重叠接头的方法和装置
公开(公告)号：US08869374B2
公开(公告)日：2014-10-28
申请号：US13327909
申请日：2011-12-16
申请人： Rolf Bense , Eugen Gorr , Tim Strohbach
发明人： Rolf Bense , Eugen Gorr , Tim Strohbach
IPC分类号： B21J15/02 , B21J15/14
CPC分类号： B21J15/142 , Y10T29/49622 , Y10T29/49956 , Y10T29/5177 , Y10T29/5377
摘要： Disclosed are a method and a device for the connection of two components indirectly or directly in an overlap joint, wherein component sections located in the overlap are pressed together for each drilling procedure by means of a clamping unit formed from a pressure application device on the drilling machine side and a guide on the component side, such that any penetration of chips between the component sections is prevented and temporary connecting elements can be dispensed with.
摘要翻译：公开了一种用于间接地或直接地连接在重叠接头中的两个部件的方法和装置，其中位于重叠部分的部件部分通过由钻孔上的压力施加装置形成的夹紧单元而被压在一起用于每个钻孔过程机器侧和部件侧的引导件，从而防止了部件间的切屑的任何穿透，并且可以省略临时的连接元件。

4. 发明授权

US08674705B2 Device for the contact-less detection of the degree of dryness of a coat of varnish, and method for the same 失效
标题翻译：用于无接触检测清漆涂层的干燥程度的装置及其方法
公开(公告)号：US08674705B2
公开(公告)日：2014-03-18
申请号：US13010319
申请日：2011-01-20
申请人： Rolf Bense , Rebecca Siewert
发明人： Rolf Bense , Rebecca Siewert
IPC分类号： G01R27/04
CPC分类号： G01N21/359 , F26B25/22 , G01N21/272 , G01N21/3554 , G01N21/3563 , G01N21/3581 , G01N21/4738 , G01N21/8422 , G01N33/32
摘要： A device and method for the contactless and therefore non-destructive measurement of a degree of dryness of a coat of paint applied to a substrate. The device comprises at least one transmitter for electromagnetic radiation, at least one receiver for determining the absorption of the electromagnetic radiation radiated into the coat of paint, and a measuring means. In the measuring means, the raw measured values measured by the receiver are processed and the degree of dryness, calculated therefrom, of the coat of paint is displayed. Either microwave radiation or infrared radiation in the near infrared range is used as measuring radiation, at least one time-dependent measurement of the absorption at a constant wavelength being made in both cases. In addition, the invention relates to a method for determining the degree of dryness of a coat of paint by means of the device.
摘要翻译：用于非接触且因此无损测量施加到基底上的涂料层的干燥程度的装置和方法。该装置包括用于电磁辐射的至少一个发射器，用于确定辐射到涂层中的电磁辐射的吸收的至少一个接收器和测量装置。在测量装置中，处理由接收器测量的原始测量值，并显示由其计算的油漆层的干燥程度。使用近红外范围的微波辐射或红外辐射作为测量辐射，在两种情况下都进行至少一次对恒定波长的吸收的时间依赖性测量。此外，本发明涉及一种通过该装置确定涂料层的干燥程度的方法。

5. 发明申请

US20110277924A1 METHOD AND DEVICE FOR FITTING A FUSELAGE SHELL WITH A WINDOW FRAME 有权
标题翻译：用于配有带有窗框的熔接壳的方法和装置
公开(公告)号：US20110277924A1
公开(公告)日：2011-11-17
申请号：US13105950
申请日：2011-05-12
申请人： Rolf Bense
发明人： Rolf Bense
IPC分类号： B29C70/34
CPC分类号： B64C1/1492 , Y02T50/43
摘要： A method of fitting a fuselage shell of an aircraft with at least one window frame of a cabin window includes positioning an uncured laminate including a fiber-reinforced plastic-based composite material configured to form a fuselage shell on a mold surface. A window aperture is introduced into the laminate. A window frame including a fiber-reinforced plastic-based composite material is positioned on the laminate in a region of the window aperture. The laminate is cured under the action of pressure and temperature so as to connect the window frame with the laminate by a material bond.
摘要翻译：将飞行器的机身壳体与机舱窗的至少一个窗框配合的方法包括将未固化的层压体定位成包括纤维增强的基于塑料的复合材料，其被配置成在模具表面上形成机身壳体。窗口孔被引入到层压板中。包括纤维增强塑料基复合材料的窗框位于窗口的区域中的层压板上。层压板在压力和温度的作用下固化，以通过材料粘合将窗框与层压板连接起来。

6. 发明申请

US20100319618A1 DEVICE AND METHOD FOR PRETREATING EXTERIOR SURFACES OF AN AIRCRAFT TO BE PAINTED 有权
标题翻译：用于预测待印刷飞机的外部表面的装置和方法
公开(公告)号：US20100319618A1
公开(公告)日：2010-12-23
申请号：US12819589
申请日：2010-06-21
申请人： Dirk BAUSEN , Birgit KUHLENSCHMIDT , Karl HAUSMANN , Rolf BENSE , Daniel LAHIDJANIAN
发明人： Dirk BAUSEN , Birgit KUHLENSCHMIDT , Karl HAUSMANN , Rolf BENSE , Daniel LAHIDJANIAN
IPC分类号： B05C9/12 , G05B19/00 , G06F19/00
CPC分类号： B64F5/10
摘要： A device for pretreating an exterior surface of an aircraft coated with an aircraft-specific base material so as to prepare the surface for a final painting with aircraft paint includes a pretreating tool. The pretreating tool has a laser head configured to activate the aircraft-specific base material using a laser. The device also includes a support construction including a robot device and a control unit configured to control and move the laser head over the surface using the robot device.
摘要翻译：用于预处理飞机专用基材涂覆的飞行器的外表面以便制备用于用飞机涂料进行最终涂漆的表面的装置包括预处理工具。预处理工具具有激光头，该激光头被配置为使用激光来激活飞机专用基材。该装置还包括支撑结构，其包括机器人装置和被配置为使用机器人装置来控制和移动激光头在表面上的控制单元。

7. 发明申请

US20090294018A1 Method for joining aircraft fuselage elements by friction stir welding (FSW) 有权
标题翻译：通过摩擦搅拌焊接（FSW）连接飞机机身元件的方法
公开(公告)号：US20090294018A1
公开(公告)日：2009-12-03
申请号：US12453296
申请日：2009-05-06
申请人： Dirk Gross , Robert Alexander Goehlich , Steffen Biesek , Rolf Bense
发明人： Dirk Gross , Robert Alexander Goehlich , Steffen Biesek , Rolf Bense
IPC分类号： B29C65/06 , B23K20/12
CPC分类号： B23K20/126 , B23K20/1265
摘要： The invention relates to a method for joining at least two aircraft fuselage segments (2, 3) by friction stir welding with a tool (8) generating friction heat for the partial plasticisation of an edge region (6, 7) of at least one of the two aircraft fuselage segments and a counter bearing (10) for absorbing the force exerted by the tool (8) on at least one of the two aircraft fuselage segments, wherein at least one of the two aircraft fuselage segments comprises at least one rib (17) and/or one stringer (16).In order to minimise the necessary expense incurred in association with the production aids for the FSW process, it is proposed that the at least one rib (17) and/or the at least one stringer (16) of the at least one aircraft fuselage segment (2, 3) should be used as a counter bearing (10).
摘要翻译：本发明涉及通过摩擦搅拌焊接与至少两个飞行器机身段（2,3）之间的至少一个的工件（8）接合至少两个飞行器机身段（2）的方法，所述工具（8）产生摩擦热，用于部分塑化边缘区域所述两个飞行器机身段和用于吸收由所述工具（8）施加在所述两个飞行器机身段中的至少一个上的力的反向轴承（10），其中所述两个飞行器机身段中的至少一个包括至少一个肋 17）和/或一个纵梁（16）。为了最小化与FSW过程的生产辅助相关联的必要费用，建议至少一个飞行器机身段的至少一个肋（17）和/或至少一个纵梁（16）（2,3）应用作反轴承（10）。

8. 发明授权

US08529727B2 Method and device for fitting a fuselage shell with a window frame 有权
标题翻译：用于将机身外壳与窗框配合的方法和装置
公开(公告)号：US08529727B2
公开(公告)日：2013-09-10
申请号：US13105950
申请日：2011-05-12
申请人： Rolf Bense
发明人： Rolf Bense
IPC分类号： B64C1/14 , B32B37/00
CPC分类号： B64C1/1492 , Y02T50/43
摘要： A method of fitting a fuselage shell of an aircraft with at least one window frame of a cabin window includes positioning an uncured laminate including a fiber-reinforced plastic-based composite material configured to form a fuselage shell on a mold surface. A window aperture is introduced into the laminate. A window frame including a fiber-reinforced plastic-based composite material is positioned on the laminate in a region of the window aperture. The laminate is cured under the action of pressure and temperature so as to connect the window frame with the laminate by a material bond.
摘要翻译：将飞行器的机身壳体与机舱窗口的至少一个窗框配合的方法包括将未固化的层压体定位成包括纤维增强的基于塑料的复合材料，其被配置成在模具表面上形成机身壳体。窗口孔被引入到层压板中。包括纤维增强塑料基复合材料的窗框位于窗口的区域中的层压板上。层压板在压力和温度的作用下固化，以通过材料粘合将窗框与层压板连接起来。

9. 发明授权

US08438717B2 Method for tolerance compensation between two components and a tool for execution of the method 有权
标题翻译：两个组件之间的公差补偿方法和用于执行该方法的工具
公开(公告)号：US08438717B2
公开(公告)日：2013-05-14
申请号：US12729392
申请日：2010-03-23
申请人： Eugen Gorr , Rolf Bense
发明人： Eugen Gorr , Rolf Bense
IPC分类号： B23P17/00 , B29C45/22
CPC分类号： B64F5/10 , B64C1/068 , F16B5/04 , F16B11/006 , Y10T29/4998
摘要： A method for tolerance compensation in an overlap joint between a first and a second body section of adjacent fuselage rings includes introducing a plurality of holes into a first body section corresponding to a pattern of rivets; arranging the first and second body section in an overlapping configuration so as to form an overlap; injecting a filler mass through the plurality of holes into a gap formed in the overlap; and hardening the filler mass.
摘要翻译：在相邻的机身环的第一和第二主体部分之间的重叠接头中的公差补偿方法包括将多个孔引入对应于铆钉图案的第一主体部分中; 将第一和第二主体部分布置成重叠构型以形成重叠; 将填充物通过所述多个孔注入形成在所述重叠中的间隙中; 并固化填料。

10. 发明申请

US20120159770A1 METHOD AND A DEVICE FOR THE FORMATION OF AN OVERLAP JOINT 有权
标题翻译：用于形成覆盖点的方法和装置
公开(公告)号：US20120159770A1
公开(公告)日：2012-06-28
申请号：US13327909
申请日：2011-12-16
申请人： Rolf Bense , Eugen Gorr , Tim Strohbach
发明人： Rolf Bense , Eugen Gorr , Tim Strohbach
IPC分类号： B23P19/04 , B23P19/10 , B23P11/00
CPC分类号： B21J15/142 , Y10T29/49622 , Y10T29/49956 , Y10T29/5177 , Y10T29/5377
摘要： Disclosed are a method and a device for the connection of two components indirectly or directly in an overlap joint, wherein component sections located in the overlap are pressed together for each drilling procedure by means of a clamping unit formed from a pressure application device on the drilling machine side and a guide on the component side, such that any penetration of chips between the component sections is prevented and temporary connecting elements can be dispensed with.
摘要翻译：公开了一种用于间接地或直接地连接在重叠接头中的两个部件的方法和装置，其中位于重叠部分的部件部分通过由钻孔上的压力施加装置形成的夹紧单元而被压在一起用于每个钻孔过程机器侧和部件侧的引导件，从而防止了部件间的切屑的任何穿透，并且可以省略临时的连接元件。

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