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21. 发明申请

US20140186574A1 METHOD FOR PRODUCING AND CONNECTING FIBRE-REINFORCED COMPONENTS AND AIRCRAFT OR SPACECRAFT 审中-公开
标题翻译：生产和连接纤维增强部件和飞机或间隙的方法
公开(公告)号：US20140186574A1
公开(公告)日：2014-07-03
申请号：US14009759
申请日：2012-04-03
申请人： Robert Alexander Goehlich
发明人： Robert Alexander Goehlich
IPC分类号： B29D99/00 , B64C1/06
CPC分类号： B29D99/001 , B29C35/02 , B29C35/0266 , B29C65/42 , B29C65/425 , B29C65/4835 , B29C65/54 , B29C65/542 , B29C65/62 , B29C66/1142 , B29C66/30321 , B29C66/43 , B29C66/54 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/7392 , B29C66/7394 , B29C70/24 , B29L2031/3076 , B29L2031/3097 , B64C1/069 , Y02T50/43 , Y10T428/2405 , B29K2307/04 , B29K2309/08 , B29K2063/00 , B29K2061/04
摘要： A method for producing and connecting fibre-reinforced components, in particular for an aircraft or spacecraft. The method includes the steps of: (a) providing a textile planar structure, of which merely a first sub-region is impregnated with a matrix; (b) heating the textile planar structure which is impregnated in part, in such a way that the matrix provided in the first sub-region of the textile planar structure cures; (c) connecting the textile planar structure in a second sub-region of the textile planar structure, different from the first sub-region, by stitching the second sub-regions; (d) introducing a further matrix at least into the stitched second sub-regions of the textile planar structure; and (e) heating the impregnated textile planar structure in such a way that the further matrix present in the stitched second sub-regions of the textile planar structure cures. The present invention further relates to aircraft or spacecraft production.
摘要翻译：一种用于生产和连接纤维增强部件的方法，特别是用于飞行器或航天器。该方法包括以下步骤：（a）提供织物平面结构，其中只有第一子区浸渍有基质; （b）加热部分浸渍的织物平面结构，使得设置在织物平面结构的第一子区域中的基体固化; （c）通过拼接所述第二子区域将所述织物平面结构与所述第一子区域不同的所述纺织物平面结构的第二子区域连接; （d）至少将另外的矩阵引入到织物平面结构的缝合的第二子区域中; 和（e）以这样的方式加热浸渍的织物平面结构，使得存在于织物平面结构的缝合的第二子区域中的另一个基体固化。本发明还涉及飞机或航天器的生产。

22. 发明授权

US08496207B2 Connection of cabin components, cabin component and method for connecting cabin components 有权
标题翻译：客舱部件连接，客舱部件和连接客舱部件的方法
公开(公告)号：US08496207B2
公开(公告)日：2013-07-30
申请号：US12836641
申请日：2010-07-15
申请人： Robert Alexander Goehlich , Daniel Wenninger
发明人： Robert Alexander Goehlich , Daniel Wenninger
IPC分类号： B64C1/22 , B64D11/00
CPC分类号： B64D11/003
摘要： A connection device for a plurality of cabin components of an aircraft includes a rail extending in a longitudinal direction of an aircraft structure, wherein the plurality of cabin components is disposed on the rail; and a plurality of adjustment devices configured to self-adjust each of the plurality of cabin components in the longitudinal direction.
摘要翻译：用于飞行器的多个舱室部件的连接装置包括沿飞行器结构的纵向方向延伸的轨道，其中多个舱室部件设置在轨道上; 以及多个调整装置，其被配置为在纵向方向上自适应地调节所述多个客舱部件中的每一个。

23. 发明申请

US20120187245A1 FUSELAGE SEGMENT, AND METHOD FOR THE PRODUCTION OF A FUSELAGE SEGMENT 有权
标题翻译：熔融部分，以及生产熔融部分的方法
公开(公告)号：US20120187245A1
公开(公告)日：2012-07-26
申请号：US13262246
申请日：2010-03-30
申请人： Robert Alexander Goehlich
发明人： Robert Alexander Goehlich
IPC分类号： B64C1/00 , B23P17/04
CPC分类号： B64C1/12 , B32B1/00 , B32B3/12 , B32B3/266 , B32B5/02 , B32B5/18 , B32B5/22 , B32B5/245 , B32B5/32 , B32B7/02 , B32B15/046 , B32B27/02 , B32B27/04 , B32B2260/021 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2266/02 , B32B2266/0214 , B32B2266/045 , B32B2307/536 , B32B2307/718 , B32B2605/18 , B64C1/40 , B64C2001/0072 , B64C2211/00 , B64D11/00 , B64D13/00 , Y02T50/43 , Y02T50/44 , Y02T50/46 , Y10T29/49
摘要： A fuselage segment of an aircraft fuselage is provided with an outer skin and an inner skin that are spaced apart from one another by a core, wherein conduits for system installations are integrated into the core, as well as a method for manufacturing such a fuselage segment.
摘要翻译：飞机机身的机身部分设置有通过芯彼此间隔开的外皮和内皮，其中用于系统装置的导管被集成到芯中，以及用于制造这样的机身部分的方法。

24. 发明授权

US08100316B2 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：US08100316B2
公开(公告)日：2012-01-24
申请号：US12453296
申请日：2009-05-06
申请人： Dirk Groβ , Robert Alexander Goehlich , Steffen Biesek , Rolf Bense
发明人： Dirk Groβ , Robert Alexander Goehlich , Steffen Biesek , Rolf Bense
IPC分类号： 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过程的生产助剂相关联的必要费用，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）。

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