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1. 发明申请

US20100272954A1 Method for Coupling Stiffening Profile Elements and Structural Component 有权
标题翻译：耦合加强型材元件和结构部件的方法
公开(公告)号：US20100272954A1
公开(公告)日：2010-10-28
申请号：US12666605
申请日：2008-06-19
申请人： Thorsten Roming , Thorsten Schroeer , Hauke Kirstein , Hinnik Gensch , Stefan Tacke
发明人： Thorsten Roming , Thorsten Schroeer , Hauke Kirstein , Hinnik Gensch , Stefan Tacke
IPC分类号： B32B3/10 , B64F5/00 , B23P11/00
CPC分类号： B64C1/12 , B64C1/064 , B64C1/069 , B64C2001/0072 , Y02T50/43 , Y10T29/49826 , Y10T428/19 , Y10T428/192 , Y10T428/197 , Y10T428/24124 , Y10T428/24132 , Y10T428/24298 , Y10T428/24314 , Y10T428/24322 , Y10T428/24331 , Y10T428/24661 , Y10T428/24744 , Y10T428/24752 , Y10T428/24777 , Y10T428/2495 , Y10T428/249923
摘要： This invention provides a coupling method for coupling a first and a second stiffening profile element for an outer skin of an aircraft or space craft. In a first step the stiffening profile elements are arranged on the outer skin in such a manner that the stiffening profile elements oppose each other with their respective front sides and enclose within themselves a cavity. Furthermore, a fixing hole is formed through a wall of at least one of the stiffening profile elements in the cavity inside a coupling zone of the stiffening profile element. An access opening is formed through the wall in the cavity along the coupling zone. A coupling strap, which couples the stiffening profile elements together, is fastened to the coupling zone by means of a fastening element guided through the fixing hole.
摘要翻译：本发明提供了一种用于联接飞行器或航天飞机的外皮的第一和第二加强型材元件的联接方法。在第一步骤中，加强型材元件以这样的方式布置在外皮上，使得加强型材元件以它们各自的前侧彼此相对并且在它们自身内包围空腔。此外，在加强型材元件的连接区域内的空腔内的至少一个加强型材元件的壁上形成固定孔。通过沿着耦合区域的空腔中的壁形成进入开口。将加强型材元件连接在一起的联接带通过引导通过固定孔的紧固元件紧固到联接区域。

2. 发明授权

US08715808B2 Method for coupling stiffening profile elements and structural component 有权
标题翻译：耦合加强型材元件和结构件的方法
公开(公告)号：US08715808B2
公开(公告)日：2014-05-06
申请号：US12666605
申请日：2008-06-19
申请人： Thorsten Roming , Thorsten Schroeer , Hauke Kirstein , Hinnik Gensch , Stefan Tacke
发明人： Thorsten Roming , Thorsten Schroeer , Hauke Kirstein , Hinnik Gensch , Stefan Tacke
IPC分类号： B32B3/06 , B32B3/10 , B32B3/24 , B32B3/28 , B32B5/12 , B32B7/08 , B64C1/06 , B64F5/00
CPC分类号： B64C1/12 , B64C1/064 , B64C1/069 , B64C2001/0072 , Y02T50/43 , Y10T29/49826 , Y10T428/19 , Y10T428/192 , Y10T428/197 , Y10T428/24124 , Y10T428/24132 , Y10T428/24298 , Y10T428/24314 , Y10T428/24322 , Y10T428/24331 , Y10T428/24661 , Y10T428/24744 , Y10T428/24752 , Y10T428/24777 , Y10T428/2495 , Y10T428/249923
摘要： This invention provides a coupling method for coupling a first and a second stiffening profile element for an outer skin of an aircraft or space craft. In a first step the stiffening profile elements are arranged on the outer skin in such a manner that the stiffening profile elements oppose each other with their respective front sides and enclose within themselves a cavity. Furthermore, a fixing hole is formed through a wall of at least one of the stiffening profile elements in the cavity inside a coupling zone of the stiffening profile element. An access opening is formed through the wall in the cavity along the coupling zone. A coupling strap, which couples the stiffening profile elements together, is fastened to the coupling zone by means of a fastening element guided through the fixing hole.
摘要翻译：本发明提供了一种用于联接飞行器或航天飞机的外皮的第一和第二加强型材元件的联接方法。在第一步骤中，加强型材元件以这样的方式布置在外皮上，使得加强型材元件以它们各自的前侧彼此相对并且在它们自身内包围空腔。此外，在加强型材元件的连接区域内的空腔内的至少一个加强型材元件的壁上形成固定孔。通过沿着耦合区域的空腔中的壁形成进入开口。将加强型材元件连接在一起的联接带通过引导通过固定孔的紧固元件紧固到联接区域。

3. 发明申请

US20140077035A1 GUTTER PROFILE AND AIRCRAFT 有权
标题翻译： GUTTER轮廓和飞机
公开(公告)号：US20140077035A1
公开(公告)日：2014-03-20
申请号：US14116811
申请日：2012-05-14
申请人： Hinnik Gensch , Hauke Kirstein
发明人： Hinnik Gensch , Hauke Kirstein
IPC分类号： B64C1/14
CPC分类号： B64C1/1461 , B64C1/14
摘要： A gutter profile for draining liquids on an aircraft, comprising a connecting section for connecting the gutter profile to an outer skin of the aircraft and comprising a drain section for forming a drain cross-section of the gutter profile. The drain section is pre-tensioned into a ground position which opens the drain cross-section and has a flow guiding device for transferring the drain section into a flight position which closes the drain cross-section. An aircraft having such a gutter profile is also disclosed.
摘要翻译：用于排出飞机上的液体的沟槽轮廓，包括用于将沟槽轮廓连接到飞行器的外皮的连接部分，并且包括用于形成沟槽轮廓的排水横截面的排水部分。排水部分被预张紧到接地位置，该位置打开排水横截面并具有用于将排水部分转移到关闭排水横截面的飞行位置的流动引导装置。还公开了具有这种沟槽轮廓的飞机。

4. 发明申请

US20100206989A1 CORROSION-RESISTANT CONNECTION BETWEEN A FIRST COMPONENT AND SECOND COMPONENT 审中-公开
标题翻译：第一组件与第二组件之间的耐腐蚀连接
公开(公告)号：US20100206989A1
公开(公告)日：2010-08-19
申请号：US12665826
申请日：2008-06-25
申请人： Thorsten Roming , Hauke Kirstein , Thorsten Schroeer
发明人： Thorsten Roming , Hauke Kirstein , Thorsten Schroeer
IPC分类号： B64C1/12 , B32B15/04 , B32B18/00 , B32B5/00
CPC分类号： B64C1/12 , Y10T428/263
摘要： The invention relates to a connection 1 between a first component and a second component, the first component being formed from an aluminium alloy in particular and the second component being formed from a carbon-fibre-reinforced plastics material in particular. The first component is a rib 6 in particular and the second component is preferably an angle bracket 7, with which the rib 6 is connected to an aircraft fuselage skin 2 within a fuselage reinforcement structure. The connection 1 between the components comprises, according to the invention, a ceramic coating 16 which is applied for protection against corrosion at least in the region of a contact area 9 between the components, the components being riveted and/or adhesively bonded. The ceramic coating 16 is less than 0.1 mm thick and may be formed from a mixture of aluminium oxide (Al2O3) and TiO2 for example.
摘要翻译：本发明涉及第一部件和第二部件之间的连接件，第一部件特别由铝合金形成，第二部件特别由碳纤维增强塑料材料形成。第一部件特别是肋6，第二部件优选地是角架7，肋6在机身加强结构内与飞机机体皮肤2连接。根据本发明，组件之间的连接件1包括陶瓷涂层16，该陶瓷涂层16至少在部件之间的接触区域9的区域中被施加用于防止腐蚀，该部件被铆接和/或粘接。陶瓷涂层16的厚度小于0.1mm，例如可以由氧化铝（Al 2 O 3）和TiO 2的混合物形成。

5. 发明授权

US09365280B2 Gutter profile and aircraft 有权
标题翻译：沟槽轮廓和飞机
公开(公告)号：US09365280B2
公开(公告)日：2016-06-14
申请号：US14116811
申请日：2012-05-14
申请人： Hinnik Gensch , Hauke Kirstein
发明人： Hinnik Gensch , Hauke Kirstein
IPC分类号： B64C1/14
CPC分类号： B64C1/1461 , B64C1/14
摘要： A gutter profile for draining liquids on an aircraft, comprising a connecting section for connecting the gutter profile to an outer skin of the aircraft and comprising a drain section for forming a drain cross-section of the gutter profile. The drain section is pre-tensioned into a ground position which opens the drain cross-section and has a flow guiding device for transferring the drain section into a flight position which closes the drain cross-section. An aircraft having such a gutter profile is also disclosed.
摘要翻译：用于排出飞机上的液体的沟槽轮廓，包括用于将沟槽轮廓连接到飞行器的外皮的连接部分，并且包括用于形成沟槽轮廓的排水横截面的排水部分。排水部分被预张紧到接地位置，该位置打开排水横截面并具有用于将排水部分转移到关闭排水横截面的飞行位置的流动引导装置。还公开了具有这种沟槽轮廓的飞机。

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