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1. 发明申请

US20100108252A1 PROCESS AND DEVICE FOR MANUFACTURING A PREFORM FOR A LOAD PATH ALIGNED FIBER COMPOSITE STRUCTURE 有权
标题翻译：用于制造负载路径对准纤维复合结构的预处理和装置
公开(公告)号：US20100108252A1
公开(公告)日：2010-05-06
申请号：US12530607
申请日：2008-03-13
申请人： Andreas Gessler , Oliver Meyer
发明人： Andreas Gessler , Oliver Meyer
IPC分类号： B32B38/04 , B32B37/00
CPC分类号： B29B11/16 , B29C70/20 , B29C70/382 , B29C70/386 , B29C70/545 , B65H49/18 , B65H51/005 , B65H57/16 , B65H2701/314 , B65H2701/38 , D02J1/18 , D04H1/4242 , D04H1/60 , D04H1/655 , D04H3/002 , D04H3/04 , D04H3/12 , D04H13/00 , Y10T156/1062 , Y10T156/1075
摘要： The invention relates to a process and a device for manufacturing a perform (42) for a load path aligned fiber composite structure. The process includes cutting off relatively short fiber band pieces (40, 40′, 40″) from a spread fiber band (14), placing the fiber band pieces (40, 40′, 40″) at a predetermined position and fixing them at this position by means of a binder material (38).
摘要翻译：本发明涉及用于制造负载路径对准的纤维复合结构的执行（42）的方法和装置。该方法包括从扩展的纤维带（14）切断相对较短的纤维带片（40,40'，40“），将纤维带片（40,40'，40”）放置在预定位置并将它们固定在该位置借助于粘合剂材料（38）。

2. 发明申请

US20070193439A1 Method For Producing Fiber Composite Semi-Finished Products By Means Of A Round Braiding Technique 有权
标题翻译：通过圆形编织技术生产纤维复合半成品的方法
公开(公告)号：US20070193439A1
公开(公告)日：2007-08-23
申请号：US10592678
申请日：2005-04-06
申请人： Andreas Gessler , Franz Maidl
发明人： Andreas Gessler , Franz Maidl
IPC分类号： D04C1/00
CPC分类号： D04C1/02 , D10B2505/02
摘要： Method of producing fiber composite semifinished products by means of a circular braiding technique, a braiding core being braided with braiding threads which are unwound by means of bobbins circling concentrically about the braiding core in different directions, characterized in that the bobbins of one circling direction are fitted with reinforcing threads and the bobbins of the opposite circling direction are at least partially fitted with supporting threads, the supporting threads at least partially consisting of thermoplastic threads.
摘要翻译：通过圆形编织技术制造纤维复合半成品的方法，编织芯由编织线编织，编织线通过绕不同方向的编织芯同心盘绕的绕线筒而展开，其特征在于，一个卷绕方向的线轴是装配有加强螺纹并且相对的盘旋方向的筒管至少部分地配有支撑螺纹，所述支撑螺纹至少部分地由热塑性螺纹组成。

3. 发明授权

US07942993B2 Method for producing multilayer tailored fiber placement (TFP) preforms using meltable fixing fibers 失效
标题翻译：使用可熔融固定纤维生产多层定制纤维布置（TFP）预成型件的方法
公开(公告)号：US07942993B2
公开(公告)日：2011-05-17
申请号：US10450187
申请日：2001-12-10
申请人： Andreas Gessler , Juergen Filsinger
发明人： Andreas Gessler , Juergen Filsinger
IPC分类号： B32B37/00
CPC分类号： B29C70/202 , B29C70/226
摘要： In a method, multilayer tailored fiber placement (TFP) preforms of any desired thickness may be easily produced without fixing threads or intermediate layers interfering. Reinforcing fibers are sewn onto a substrate using a chemically or thermally meltable fixing thread thus resulting in the formation of a reinforcing fiber structure. The fixing thread firstly serves to fix the reinforcing fibers on the substrate and is subsequently melted so that the fixing thread disintegrates while pre-fixing the reinforcing fibers and may not influence the mechanical properties of the reinforcing fiber structure.
摘要翻译：在一种方法中，可以容易地产生任何所需厚度的多层定制的纤维铺放（TFP）预制件，而不会固定螺纹或中间层干扰。使用化学或热可熔融的固定螺纹将增强纤维缝合到基底上，从而形成增强纤维结构。固定螺纹首先用于将增强纤维固定在基材上，随后熔化，使得固定螺纹在预固定增强纤维的同时分解，并且可能不影响增强纤维结构的机械性能。

4. 发明申请

US20090311487A1 METHOD FOR PRODUCTION OF SEVERAL FIBRE COMPOSITE COMPONENTS 有权
标题翻译：几种纤维复合材料的生产方法
公开(公告)号：US20090311487A1
公开(公告)日：2009-12-17
申请号：US12375828
申请日：2007-07-03
申请人： Juergen Filsinger , Franz Maidl , Andreas Gessler , Marinus Schouten
发明人： Juergen Filsinger , Franz Maidl , Andreas Gessler , Marinus Schouten
IPC分类号： B29C70/54 , B29C70/30 , B29D31/00 , E04C3/00
CPC分类号： B29C70/443 , B29C70/086 , B29C70/50 , B29C70/545 , B29C70/865 , B29C2793/009 , B29L2031/003 , Y02T50/43 , Y10T156/10 , Y10T428/24628
摘要： A method for production of fiber composite components, particularly suitable for the production of profiles of complicated shape with varying profile cross-section and/or with at least parts with curved lines, such as used for the production of aircraft, for example. The method (a) produces plural core components, (b) separates application of a first fiber material to each of the core components, (c) assembles the core components provided with the first fiber material to form a sequence of core components, (d) applies a second fiber material common to the core component sequence along at least one side of the core component sequence, provided with the first fiber material, (e) impregnates and hardens the first and second fiber materials to form a fiber-reinforced component body, and (f) separates the component body into plural sections as represented by the fiber composite components.
摘要翻译：一种生产纤维复合材料组件的方法，特别适用于生产具有不同轮廓横截面的复杂形状的轮廓和/或至少具有弯曲线的部件，例如用于生产飞行器的轮廓。方法（a）产生多个核心部件，（b）将第一纤维材料应用于每个核心部件，（c）组装具有第一纤维材料的芯部件以形成核心部件序列（d ）沿着核心部件序列的至少一侧施加第一纤维材料，所述第二纤维材料沿核芯部件序列的至少一侧施加第一纤维材料，（e）浸渍并硬化第一和第二纤维材料以形成纤维增强部件体，和（f）将组分体分成如纤维复合组分所表示的多个部分。

5. 发明授权

US08142583B2 Method for production of several fibre composite components 有权
标题翻译：多种纤维复合材料的生产方法
公开(公告)号：US08142583B2
公开(公告)日：2012-03-27
申请号：US12375828
申请日：2007-07-03
申请人： Juergen Filsinger , Franz Maidl , Andreas Gessler , Marinus Schouten
发明人： Juergen Filsinger , Franz Maidl , Andreas Gessler , Marinus Schouten
IPC分类号： B29C70/54 , B29C70/30
CPC分类号： B29C70/443 , B29C70/086 , B29C70/50 , B29C70/545 , B29C70/865 , B29C2793/009 , B29L2031/003 , Y02T50/43 , Y10T156/10 , Y10T428/24628
摘要： A method for production of fiber composite components, particularly suitable for the production of profiles of complicated shape with varying profile cross-section and/or with at least parts with curved lines, such as used for the production of aircraft, for example. The method (a) produces plural core components, (b) separates application of a first fiber material to each of the core components, (c) assembles the core components provided with the first fiber material to form a sequence of core components, (d) applies a second fiber material common to the core component sequence along at least one side of the core component sequence, provided with the first fiber material, (e) impregnates and hardens the first and second fiber materials to form a fiber-reinforced component body, and (f) separates the component body into plural sections as represented by the fiber composite components.
摘要翻译：一种生产纤维复合材料组件的方法，特别适用于生产具有不同轮廓横截面的复杂形状的轮廓和/或至少具有弯曲线的部件，例如用于生产飞行器的轮廓。方法（a）产生多个核心部件，（b）将第一纤维材料应用于每个核心部件，（c）组装具有第一纤维材料的芯部件以形成核心部件序列（d ）沿着核心部件序列的至少一侧施加第一纤维材料，所述第二纤维材料沿核芯部件序列的至少一侧施加第一纤维材料，（e）浸渍并硬化第一和第二纤维材料以形成纤维增强部件体，和（f）将组分体分成如纤维复合组分所表示的多个部分。

6. 发明授权

US07581479B2 Method for producing fiber composite semi-finished products by means of a round braiding technique 有权
标题翻译：通过圆形编织技术生产纤维复合半成品的方法
公开(公告)号：US07581479B2
公开(公告)日：2009-09-01
申请号：US10592678
申请日：2005-04-06
申请人： Andreas Gessler , Franz Maidl
发明人： Andreas Gessler , Franz Maidl
IPC分类号： D04C1/00
CPC分类号： D04C1/02 , D10B2505/02
摘要： Method of producing fiber composite semifinished products by means of a circular braiding technique, a braiding core being braided with braiding threads which are unwound by means of bobbins circling concentrically about the braiding core in different directions, characterized in that the bobbins of one circling direction are fitted with reinforcing threads and the bobbins of the opposite circling direction are at least partially fitted with supporting threads, the supporting threads at least partially consisting of thermoplastic threads.
摘要翻译：通过圆形编织技术制造纤维复合半成品的方法，编织芯由编织线编织，编织线通过绕不同方向的编织芯同心盘绕的绕线筒而展开，其特征在于，一个卷绕方向的线轴是装配有加强螺纹并且相对的盘旋方向的筒管至少部分地配有支撑螺纹，所述支撑螺纹至少部分地由热塑性螺纹组成。

7. 发明授权

US06890470B2 Method for producing a fiber composite structural component 有权
标题翻译：纤维复合结构部件的制造方法
公开(公告)号：US06890470B2
公开(公告)日：2005-05-10
申请号：US10385288
申请日：2003-03-10
申请人： Martin Staub , Tim Leeraar , Juergen Filsinger , Andreas Gessler
发明人： Martin Staub , Tim Leeraar , Juergen Filsinger , Andreas Gessler
IPC分类号： B64C1/00 , B29C39/10 , B29C70/34 , B29C70/48 , B29D99/00 , B29K105/08 , B29L31/30 , B64C9/02 , B29C57/04
CPC分类号： B29D99/0007 , B29C70/347 , B29C70/48 , B64C9/02 , Y02T50/43 , Y10T156/1005
摘要： A fiber composite structural component such as a fitting, bracket, mounting or the like is produced by applying fiber material such as fiber threads or fiber yarns in an automatic circular weaving operation to a core that has at least two sections, to form a fiber material body (6). One core section is removed from the fiber material body when the weaving is completed. The body is then deformed in a mold that has the contour of the finished structural component with at least one mold core section still in the fiber material body. The deformed configuration of the structural component is then impregnated in an RTM device with a resin and hardener followed by curing. Reinforcements may be inserted or secured to the fiber material body prior to the impregnated and curing step.
摘要翻译：纤维复合结构件如配件，支架，安装件等通过在自动循环织造操作中将诸如纤维线或纤维纱的纤维材料施加到具有至少两个部分的芯上，以形成纤维材料身体（6）。当编织完成时，一个芯部从纤维材料主体中取出。然后在具有至少一个模芯部分仍在纤维材料体中的成品结构部件的轮廓的模具中变形。然后将结构组分的变形构型用树脂和硬化剂浸渍在RTM装置中，然后固化。在浸渍和固化步骤之前，可以将纤维素材插入或固定到纤维材料体上。

8. 发明授权

US06863245B2 Aerodynamic profile with an adjustable flap 有权
标题翻译：具有可调节挡板的气动轮廓
公开(公告)号：US06863245B2
公开(公告)日：2005-03-08
申请号：US10291750
申请日：2002-11-12
申请人： Andreas Gessler , Heinz Hansen , Tamas Havar , Alexander Horoschenkoff
发明人： Andreas Gessler , Heinz Hansen , Tamas Havar , Alexander Horoschenkoff
IPC分类号： B64C3/50
CPC分类号： B64C3/50 , Y02T50/14
摘要： An aerodynamic profile has an adjustable flap, which has a forward profile area as well as a rearward profile area situated in the downward current, bounded by a pressure-side covering skin as well as a suction-side covering skin. The pressure-side and suction-side covering skins converge in the rearward profile area at a trailing profile edge. In the rearward profile area on the underside of the pressure-side covering skin, a flap is swivellably disposed such that, in the inoperative condition, the flap, pointing in the flow direction, rests against the contour of the pressure-side covering skin and, in the deflected condition, the flap encloses an angle with the pressure-side covering skin. An airtight hinge connection is integrated in the flap so that, on the side of the flap protected from the wind, a turbulence system which improves the flow conditions is formed.
摘要翻译：空气动力学轮廓具有可调节的翼片，其具有前向轮廓区域以及位于向下的电流中的向后轮廓区域，其由压力侧覆盖皮肤以及吸力侧覆盖皮肤限定。压力侧和吸力侧覆盖物在后轮廓边缘处会聚在后向轮廓区域中。在压力侧覆盖皮肤下侧的向后轮廓区域中，翼片可旋转地设置，使得在不工作状态下，指向流动方向的翼片抵靠压力侧覆盖皮肤的轮廓，并且在偏转状态下，翼片与压力侧覆盖皮肤包围一定角度。翼片上集成有密封的铰链连接，从而在挡风板的侧面防风，形成改善流动条件的湍流系统。

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