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1. 发明授权

US07437807B2 Tufted backing and method of manufacturing same 失效
标题翻译：簇绒背衬及其制造方法
公开(公告)号：US07437807B2
公开(公告)日：2008-10-21
申请号：US10074404
申请日：2002-02-12
申请人： Rudolf Gärtner , Peter Sander , Detlef Barbier , Ulrike Maaβ , Engelbert Löcher , Ararad Emirze , Klaus Klein , Christine König
发明人： Rudolf Gärtner , Peter Sander , Detlef Barbier , Ulrike Maaβ , Engelbert Löcher , Ararad Emirze , Klaus Klein , Christine König
IPC分类号： D04H3/00 , D04H3/08 , D04H3/10 , D04H3/14 , D06C3/00
CPC分类号： D04H3/11 , D04H1/48 , D04H1/54 , D04H3/011 , D04H3/02 , D04H3/033 , D04H3/105 , D04H3/14 , D04H3/16 , D05C17/023 , D06N7/0068 , D06N2201/02 , D06N2201/0254 , D06N2207/04 , D06N2209/1628 , Y10T442/3187
摘要： A tufted backing and a method of manufacturing a tufted backing from thermoplastic polymer fibers or filaments that are processed to yield a spunbonded nonwoven are described, the spunbonded nonwoven containing only fibers or filaments having a titer of 1 to 15 dtex, the mass per unit area of the tufted backing being 70 to 110 g/m2, its density being 0.18 to 0.28 g/cm3 and the 5% modulus value in the machine direction being >60 N/5 cm, but at least 0.6 Nm2/g.
摘要翻译：描述了由热塑性聚合物纤维或长丝制成簇绒背衬的簇绒背衬和方法，所述热塑性聚合物纤维或长丝被处理以产生纺粘非织造布，纺粘非织造物仅含有滴定度为1至15分特的纤维或长丝，每单位面积的质量簇绒背衬为70〜110g / m 2，密度为0.18〜0.28g / cm 3，机器方向的5％模数值为> 60 N / 5cm，但至少为0.6Nm 2 / g。

2. 发明授权

US08574391B2 Method for joining a profiled first structural component to a second structural component 失效
标题翻译：将成型的第一结构部件接合到第二结构部件的方法
公开(公告)号：US08574391B2
公开(公告)日：2013-11-05
申请号：US11904312
申请日：2007-09-26
申请人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
发明人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
IPC分类号： B32B37/10
CPC分类号： B29C66/001 , B29C65/02 , B29C65/48 , B29C65/483 , B29C66/1122 , B29C66/43441 , B29C66/47 , B29C66/721 , B29C66/82423 , B29C66/82661 , B29C70/443 , B29C2043/3644 , B29K2105/06 , B29L2031/3076 , Y02T50/43
摘要： The invention relates to a method for joining precured stringers to at least one structural component of an aircraft or spacecraft. A vacuum arrangement required for the joining is produced in two parts. In a first step, each precured stringer is covered in advance by a covering vacuum film. The stringers prepared in this manner are arranged on the structural component. Vacuum film strips are subsequently arranged in each case on adjacent stringers and over an intermediate space between the adjacent stringers. With the use of a vacuum sealing means, the vacuum film strips and the covering vacuum films 8 form a continuous vacuum arrangement. The stringers are subsequently joined under pressurization to the structural component with the use of this vacuum arrangement.
摘要翻译：本发明涉及一种用于将预固化桁条连接到飞行器或航天器的至少一个结构部件的方法。连接所需的真空布置分两部分制造。在第一步中，每个预固化的桁条预先被覆盖的真空膜覆盖。以这种方式制备的桁条被布置在结构部件上。随后在相邻的桁条上并且在相邻的桁条之间的中间空间上，每个情况下布置真空薄膜带。通过使用真空密封装置，真空膜条和覆盖真空膜8形成连续的真空装置。随后使用该真空装置，将桁条随后在加压下结合到结构部件。

3. 发明申请

US20080083494A1 Method for joining precured or cured stringers to at least one structural component of an aircraft or spacecraft 有权
标题翻译：将预固化或固化的桁条连接到飞行器或航天器的至少一个结构部件的方法
公开(公告)号：US20080083494A1
公开(公告)日：2008-04-10
申请号：US11904310
申请日：2007-09-26
申请人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
发明人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
IPC分类号： B29C65/00
CPC分类号： B29C66/721 , B29C65/02 , B29C66/1122 , B29C66/474 , B29C66/532 , B29C66/61 , B29C66/73751 , B29C66/73753 , B29C66/7394 , B29C66/81455 , B29D99/0014 , B29K2105/06 , B29K2105/24 , B29L2031/3076 , B29L2031/766 , Y10T156/1089
摘要： The invention relates to a method for joining precured stringers to at least one structural component of an aircraft or spacecraft. A vacuum arrangement necessary for the joining is produced in two parts. In a first step, each precured stringer is covered in advance with a covering vacuum film. The stringers prepared in this manner are arranged on the structural component. Respective vacuum film strips are subsequently arranged on adjacent stringers and over an intermediate space between the adjacent stringers. With the use of a vacuum sealing means, the vacuum film strips and the covering vacuum films 8 form a continuous vacuum arrangement. The stringers are subsequently joined under pressurization to the structural component with the use of this vacuum arrangement.
摘要翻译：本发明涉及一种用于将预固化桁条连接到飞行器或航天器的至少一个结构部件的方法。连接所需的真空布置分两部分。在第一步中，每个预固化的桁条预先用覆盖真空膜覆盖。以这种方式制备的桁条被布置在结构部件上。随后将各真空薄膜条布置在相邻的桁条上并在相邻桁条之间的中间空间上。通过使用真空密封装置，真空膜条和覆盖真空膜8形成连续的真空装置。随后使用该真空装置，将桁条随后在加压下结合到结构部件。

4. 发明授权

US5953725A Networked multimedia information system 失效
标题翻译：网络多媒体信息系统
公开(公告)号：US5953725A
公开(公告)日：1999-09-14
申请号：US903235
申请日：1997-07-12
申请人： Peter Agha Eprahim , Doris Meschzan , Peter Sander
发明人： Peter Agha Eprahim , Doris Meschzan , Peter Sander
IPC分类号： G06F17/30 , H04L29/06
CPC分类号： H04L29/06 , G06F17/3056 , G06F17/30861 , H04L29/06027 , Y10S707/99944 , Y10S707/99945
摘要： The invention concerns multimedia kiosk (newsstand) systems where single system units are interconnected via a telecommunication network. The objective is to enable updating of all information and/or the network interconnection structure between the system units during run-time.The invention solves this problem, by common dynamic management of both the configuration data and the information contents in an object-oriented database. The provision of all system functionalities as an object-oriented database enables the kiosk contents in an individual kiosk to be updated, or configuration data, e.g. network addresses to be notified-during run-time. For updating it is only necessary to transfer a so-called "version file" at a particular point in time to one or more terminals via the network. The database operations indicated in the version file are then executed at the terminal in the background, step by step. The step by step procedure for updating the information contents of a kiosk system unit guarantees--in contrast to a total replacement of the information--shorter updating times and a lower network load, since a much smaller amount of data has to be sent.It should be emphasized that the updating of a system take place ONLINE, i.e. the kiosk application does not have to be shut down.
摘要翻译：本发明涉及其中单个系统单元经由电信网络互连的多媒体信息亭（报亭）系统。目的是在运行期间更新系统单元之间的所有信息和/或网络互连结构。本发明通过对面向对象数据库中的配置数据和信息内容的共同动态管理来解决这个问题。将所有系统功能作为面向对象的数据库的提供使得可以更新各个信息亭中的信息亭内容，或者配置数据。在运行期间通知网络地址。为了更新，仅需要在特定时间点将所谓的“版本文件”传送到经由网络的一个或多个终端。然后，逐步在后台在终端上执行版本文件中指定的数据库操作。由于必须发送少得多的数据量，所以用于更新信息站系统单元的信息内容的逐步过程保证了与信息更短更新时间的总体替换和较低的网络负载相反。应该强调的是，系统的更新是在线上进行的，即报亭应用不必被关闭。

5. 发明申请

US20110308714A1 METHOD AND SHAPING DEVICE FOR PRODUCING A COMPOSITE FIBRE COMPONENT FOR AIR AND SPACE TRAVEL 有权
标题翻译：用于生产用于空气和空间旅行的复合纤维部件的方法和形成装置
公开(公告)号：US20110308714A1
公开(公告)日：2011-12-22
申请号：US12989813
申请日：2009-03-13
申请人： Peter Sander , Hauke Lengsfeld , Hans Marquardt
发明人： Peter Sander , Hauke Lengsfeld , Hans Marquardt
IPC分类号： B29C70/08
CPC分类号： B29C70/44 , B29C33/30 , B29C70/443 , B29C70/46 , B29C70/54 , B29D99/0003 , B29D99/0014 , B29K2707/04 , B29L2031/003 , B29L2031/3076 , Y02T50/43
摘要： A forming tool with a predefined mould portion is provided in a method for producing a reinforced fibre composite component for aviation and aerospace. A forming/support element is moulded by means of the mould portion of the forming tool. A semi-finished fibre product is then deposited at least in portions on the shaped forming/support element. The deposited semi-finished fibre product is deformed by means of the forming/support element to form at least one reinforcing portion. The forming/support element is then removed from the forming tool together with the reinforcing section formed on this element, followed by defined positioning of the reinforcing section thus formed with respect to an associated fibre composite component portion by supporting with the forming/support element. The reinforcing portion is cured to form the reinforced fibre composite component. A forming device is provided with a predefined mould portion which holds a forming/support element such that it can be removed.
摘要翻译：在制造用于航空和航空航天的增强纤维复合材料部件的方法中提供了具有预定义的模具部分的成型工具。成形/支撑元件通过成形工具的模具部分模制。然后将半成品纤维产品至少部分沉积在成形/支撑元件上。沉积的半成品纤维产品通过成形/支撑元件变形以形成至少一个增强部分。然后将成形/支撑元件与形成在该元件上的加强部分一起从成形工具中移除，然后通过与成形/支撑元件的支撑相对于相关联的纤维复合部件部分形成的加强部分的定位。固化增强部分以形成增强纤维复合部件。成形装置设置有预定的模具部分，其保持成形/支撑元件，使得其可以被移除。

6. 发明授权

US07993479B2 Method for joining precured or cured stringers to at least one structural component of an aircraft or spacecraft 有权
标题翻译：将预固化桁条连接到飞行器或航天器的至少一个结构部件的方法
公开(公告)号：US07993479B2
公开(公告)日：2011-08-09
申请号：US11904310
申请日：2007-09-26
申请人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
发明人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
IPC分类号： B29C65/00 , B32B37/00
CPC分类号： B29C66/721 , B29C65/02 , B29C66/1122 , B29C66/474 , B29C66/532 , B29C66/61 , B29C66/73751 , B29C66/73753 , B29C66/7394 , B29C66/81455 , B29D99/0014 , B29K2105/06 , B29K2105/24 , B29L2031/3076 , B29L2031/766 , Y10T156/1089
摘要： The invention relates to a method for joining precured stringers to at least one structural component of an aircraft or spacecraft. A vacuum arrangement necessary for the joining is produced in two parts. In a first step, each precured stringer is covered in advance with a covering vacuum film. The stringers prepared in this manner are arranged on the structural component. Respective vacuum film strips are subsequently arranged on adjacent stringers and over an intermediate space between the adjacent stringers. With the use of a vacuum sealing means, the vacuum film strips and the covering vacuum films 8 form a continuous vacuum arrangement. The stringers are subsequently joined under pressurization to the structural component with the use of this vacuum arrangement.
摘要翻译：本发明涉及一种用于将预固化桁条连接到飞行器或航天器的至少一个结构部件的方法。连接所需的真空布置分两部分。在第一步中，每个预固化的桁条预先用覆盖真空膜覆盖。以这种方式制备的桁条被布置在结构部件上。随后将各真空薄膜条布置在相邻的桁条上并在相邻桁条之间的中间空间上。通过使用真空密封装置，真空膜条和覆盖真空膜8形成连续的真空装置。随后使用该真空装置，将桁条随后在加压下结合到结构部件。

7. 发明申请

US20100065760A1 METHOD FOR DETERMINING A CHARACTERISTIC PARAMETER OF A CRP SPECIMEN 有权
标题翻译：用于确定CRP样本特征参数的方法
公开(公告)号：US20100065760A1
公开(公告)日：2010-03-18
申请号：US12308013
申请日：2007-07-20
申请人： Hauke Lengsfeld , Peter Sander , Han Marquardt , Rudolf Duwald
发明人： Hauke Lengsfeld , Peter Sander , Han Marquardt , Rudolf Duwald
IPC分类号： G01N21/95
CPC分类号： G01N33/44 , G01N21/8914 , G01N21/9515 , G01N2021/8472
摘要： The invention relates to a method for determining at least one characteristic parameter of a CRP specimen (3, 4), in particular a specimen of prepreg material, for aerospace, comprising the following method steps: presenting the specimen (3, 4), irradiating the. specimen (3, 4) with a predetermined spectrum of electromagnetic radiation, recording the interaction between the specimen (3, 4) and the electromagnetic radiation in a data record (20) and determining the at least one characteristic parameter from the recorded data record (20).
摘要翻译：本发明涉及一种确定用于航空航天的CRP试样（3,4）特别是预浸料材料试样的至少一个特性参数的方法，包括以下方法步骤：将样品（3,4）照射的。在具有预定的电磁辐射光谱的样本（3,4）上记录样本（3,4）与数据记录（20）中的电磁辐射之间的相互作用，并根据记录的数据记录确定至少一个特性参数（ 20）。

8. 发明申请

US20080083850A1 METHOD FOR JOINING A PROFILED FIRST STRUCTURAL COMPONENT TO A SECOND STRUCTURAL COMPONENT 失效
标题翻译：将第一个结构部件配置成第二个结构部件的方法
公开(公告)号：US20080083850A1
公开(公告)日：2008-04-10
申请号：US11904312
申请日：2007-09-26
申请人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
发明人： Peter Sander , Hans Marquardt , Hauke Lengsfeld
IPC分类号： B64C1/00 , B64C1/06
CPC分类号： B29C66/001 , B29C65/02 , B29C65/48 , B29C65/483 , B29C66/1122 , B29C66/43441 , B29C66/47 , B29C66/721 , B29C66/82423 , B29C66/82661 , B29C70/443 , B29C2043/3644 , B29K2105/06 , B29L2031/3076 , Y02T50/43
摘要： The invention relates to a method for joining precured stringers to at least one structural component of an aircraft or spacecraft. A vacuum arrangement required for the joining is produced in two parts. In a first step, each precured stringer is covered in advance by a covering vacuum film. The stringers prepared in this manner are arranged on the structural component. Vacuum film strips are subsequently arranged in each case on adjacent stringers and over an intermediate space between the adjacent stringers. With the use of a vacuum sealing means, the vacuum film strips and the covering vacuum films 8 form a continuous vacuum arrangement. The stringers are subsequently joined under pressurization to the structural component with the use of this vacuum arrangement.
摘要翻译：本发明涉及一种用于将预固化桁条连接到飞行器或航天器的至少一个结构部件的方法。连接所需的真空布置分两部分制造。在第一步中，每个预固化的桁条预先被覆盖的真空膜覆盖。以这种方式制备的桁条被布置在结构部件上。随后在相邻的桁条上并且在相邻的桁条之间的中间空间上，每个情况下布置真空薄膜带。通过使用真空密封装置，真空膜条和覆盖真空膜8形成连续的真空装置。随后使用该真空装置，将桁条随后在加压下结合到结构部件。

9. 发明申请

US20070137788A1 Method and system for position control of webs and corrugated board with a natural edge 审中-公开
标题翻译：具有自然边缘的腹板和瓦楞纸板的位置控制方法和系统
公开(公告)号：US20070137788A1
公开(公告)日：2007-06-21
申请号：US11300888
申请日：2005-12-15
申请人： Harald Loffler , Peter Sander , Franz Guenter
发明人： Harald Loffler , Peter Sander , Franz Guenter
IPC分类号： B32B37/00
CPC分类号： B32B38/1841 , B31F1/2836 , B32B2317/12 , Y10T156/1018
摘要： The invention relates to a method and a system for position control of one or more webs, particularly of paper-like or board-like webs, which are preferably used in manufacturing corrugated board and corrugated board which has a natural edge. For controlling the web position by means of position manipulation apparatuses, position information is used, which is detected downstream by position detection means.
摘要翻译：本发明涉及一种用于一个或多个幅材，特别是纸状或板状幅材的位置控制的方法和系统，其优选用于制造具有天然边缘的瓦楞纸板和瓦楞纸板。为了通过位置操纵装置控制卷筒纸位置，使用位置信息，其由位置检测装置在下游检测。

10. 发明申请

US20070001091A1 Method for sensing a marking on a running web of material 有权
标题翻译：用于感测运行的材料网上的标记的方法
公开(公告)号：US20070001091A1
公开(公告)日：2007-01-04
申请号：US11479351
申请日：2006-06-30
申请人： Andrea Wittmann , Juergen Eisen , Martin Zeh , Dominik Schild , Peter Sander
发明人： Andrea Wittmann , Juergen Eisen , Martin Zeh , Dominik Schild , Peter Sander
IPC分类号： C12Q1/68
CPC分类号： G06Q10/08 , G01C11/00
摘要： In the case of a method for sensing a marking (2) of a running web of material (3), the web of material is optically scanned by an image recording device (6). This generates in successive measuring cycles image signals which are fed to an image processing device (7). This image processing device (7) determines the positional values of the marking (2) of the web of material (3). A validity signal is generated from these positional values by applying a position-dependent weighting function and is output. This validity signal indicates whether the currently determined positional value is valid.
摘要翻译：在用于感测材料（3）的运行卷材的标记（2）的方法的情况下，材料卷材由图像记录装置（6）光学扫描。这在连续的测量周期中产生被馈送到图像处理装置（7）的图像信号。该图像处理装置（7）确定材料卷材（3）的标记（2）的位置值。通过应用位置相关加权函数从这些位置值产生有效性信号并输出。该有效信号指示当前确定的位置值是否有效。

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