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11.
公开(公告)号:US08998065B2
公开(公告)日:2015-04-07
申请号:US13077117
申请日:2011-03-31
申请人: Domenico Furfari , Marco Pacchione
发明人: Domenico Furfari , Marco Pacchione
CPC分类号: B23K20/129 , B23K20/002 , B23K20/122 , B23K20/123 , B23K20/124 , B23K20/1245 , B23K20/126 , B23K20/1275 , B23K20/26 , B23K31/02 , B23K37/08
摘要: A method for the friction stir welding of two components, in particular of two shell components of a fuselage structure of an aircraft and spacecraft, said method comprising the following method steps: positioning the two components relative to one another in such a way that a connection region is formed between the two components; friction stir welding the two components by means of a friction stir welding tool which penetrates the connection region in order to produce a weld which permeates the connection region with the formation of an unpenetrated weld edge portion of the connection region; and introducing internal compressive stresses, at least in the weld edge portion of the connection region. Further a device for the friction stir welding of two components, in particular of two shell components of a fuselage structure of an aircraft and spacecraft is provided.
摘要翻译: 一种用于飞行器和航天器的机身结构的两个部件,特别是两个壳体部件的摩擦搅拌焊接的方法,所述方法包括以下方法步骤:将两个部件相对于彼此定位成使得连接 两部分之间形成区域; 通过摩擦搅拌焊接工具摩擦搅拌焊接两个部件,该工具穿透连接区域,以便产生在形成连接区域的未穿透焊接边缘部分的连接区域上的焊缝; 并至少在连接区域的焊接边缘部分引入内部压缩应力。 此外,还提供了一种用于飞行器和航天器的机身结构的两个部件,特别是两个壳部件的摩擦搅拌焊接的装置。
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12.
公开(公告)号:US08770464B2
公开(公告)日:2014-07-08
申请号:US13101230
申请日:2011-05-05
申请人: Marco Pacchione , Juergen Silvanus
发明人: Marco Pacchione , Juergen Silvanus
CPC分类号: B23K20/1265 , B23K37/06
摘要: A method for manufacturing welded lap joints comprising the following steps: Providing of two components each having at least one base; allocating the components in such a way that the bases face each other and the components overlap in an overlapping area, which extends at least partially over both components; joining the components by welding in the overlapping area such that a weld joint is formed, wherein at the edge of the overlapping area non welded areas are formed; removing of the non welded areas whereby outer cutting areas are formed at the components, which are arranged at obtuse angles to the overlapping area.
摘要翻译: 一种用于制造焊接搭接接头的方法,包括以下步骤:提供每个具有至少一个基底的两个部件; 以这样的方式分配组件,使得基座彼此面对并且部件在至少部分地延伸到两个部件上的重叠区域中重叠; 通过在重叠区域中焊接来接合部件,从而形成焊接接头,其中在重叠区域的边缘形成非焊接区域; 去除非焊接区域,由此在与重叠区域成钝角配置的部件处形成外切割区域。
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公开(公告)号:US20130206817A1
公开(公告)日:2013-08-15
申请号:US13810558
申请日:2011-07-15
IPC分类号: B23K20/12
CPC分类号: B23K20/1255 , B23K20/126
摘要: A method for friction stir welding two components, with a rotating tool that comprises a rotating or non-rotating shoulder surface for subjecting the components to a process force in the region of a joining zone, and with a stirring pin for stirring plasticized material or for plasticizing and stirring the components in the region of the joining zone, in which method a stirring pin with a section slidably plunges in a slide on which the components are supported, which slide is guided along the joining zone on a side of the component, which side faces away from the tool, so that during welding an automatic relative movement between the stirring pin and the slide or the shoulder surface of the tool and a support surface of the slide, which support surface supports the components, is made possible, as well as a device for implementing such a method.
摘要翻译: 一种用于摩擦搅拌焊接两个部件的方法,具有旋转工具,其包括用于使部件在接合区域中的加工力受到旋转或非旋转的肩部表面,以及用于搅拌增塑材料的搅拌销或用于 在接合区域的区域中塑化和搅拌部件,以这种方式,一个具有滑动部分的滑块上的部分可滑动地插入到其中支撑部件的滑块的搅拌销,该滑动件沿着部件的一侧上的接合区被引导, 侧面远离工具,使得在焊接期间,搅拌销和工具的滑块或台肩表面之间的自动相对运动以及支撑表面支撑部件的滑块的支撑表面也成为可能 作为实现这种方法的装置。
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公开(公告)号:US08356772B2
公开(公告)日:2013-01-22
申请号:US12509008
申请日:2009-07-24
申请人: Rolf Bense , Steffen Biesek , Robert Alexander Goehlich , Karl-Hinrich Herbst , Michael Kreimeyer , Christian Kulik , Marco Pacchione
发明人: Rolf Bense , Steffen Biesek , Robert Alexander Goehlich , Karl-Hinrich Herbst , Michael Kreimeyer , Christian Kulik , Marco Pacchione
IPC分类号: B64C1/12
CPC分类号: B64C1/12 , B64C1/069 , B64C2001/0081 , Y02T50/42
摘要: A lightweight structure is disclosed, in particular a lightweight structure for an aircraft which is formed from a large number of components which can be joined together by weld joining processes. According to the invention, the lightweight structure has a component thickness which is increased corresponding to the loads in the joint region of the at least one welded joint compared to a thickness of the component outside the joint region.
摘要翻译: 公开了一种轻质结构,特别是用于飞机的轻型结构,其由大量可通过焊接连接工艺连接在一起的部件形成。 根据本发明,轻质结构具有相对于至少一个焊接接头的接合区域中的负载而增加的部件厚度,与组件外部的接合区域的厚度相比较。
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公开(公告)号:US20100038489A1
公开(公告)日:2010-02-18
申请号:US12509008
申请日:2009-07-24
申请人: Rolf Bense , Steffen Biesek , Robert Alexander Goehlich , Karl-Hinrich Herbst , Michael Kreimeyer , Chiristian Kulik , Marco Pacchione
发明人: Rolf Bense , Steffen Biesek , Robert Alexander Goehlich , Karl-Hinrich Herbst , Michael Kreimeyer , Chiristian Kulik , Marco Pacchione
IPC分类号: B64C1/06
CPC分类号: B64C1/12 , B64C1/069 , B64C2001/0081 , Y02T50/42
摘要: A lightweight structure is disclosed, in particular a lightweight structure for an aircraft which is formed from a large number of components which can be joined together by weld joining processes. According to the invention, the lightweight structure has a component thickness which is increased corresponding to the loads in the joint region of the at least one welded joint compared to a thickness of the component outside the joint region.
摘要翻译: 公开了一种轻质结构,特别是用于飞机的轻型结构,其由大量可通过焊接连接工艺连接在一起的部件形成。 根据本发明,轻质结构具有相对于至少一个焊接接头的接合区域中的负载而增加的部件厚度,与组件外部的接合区域的厚度相比较。
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