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1. 发明授权

US08632115B2 Hatch system for a motor craft, in particular for an automobile vehicle 有权
标题翻译：用于汽车的舱口系统，特别是用于汽车的
公开(公告)号：US08632115B2
公开(公告)日：2014-01-21
申请号：US13397939
申请日：2012-02-16
申请人： Laurent Coldre , Bertrand Florentz
发明人： Laurent Coldre , Bertrand Florentz
IPC分类号： B60J5/00
CPC分类号： B60J5/0473
摘要： Hatch system (1) for a motor craft, in particular for an automobile vehicle, for example, the hatch (1) being mounted articulated about a substantially horizontal fixed main rotation axis (A) supported by the chassis of the motor craft, and being movable about the main rotation axis (A) manually or automatically by drive means (5) between a closed position and an open position, characterized in that, during a phase of movement of the hatch (1), the drive means (5) driving rotation of the hatch (1) about the main rotation axis (A) actuate means (7) for maneuvering the hatch (1) in rotation in the opposite direction about a secondary rotation axis (B), the combination of these two movements in rotation causing the hatch (1) to move in a substantially vertical plane without necessarily causing lateral movement of the hatch during this phase of movement of the hatch (1).
摘要翻译：用于汽车的舱口系统（1），特别是用于汽车的汽车，例如，舱口（1）围绕由电动机的底盘支撑的基本上水平的固定主旋转轴线（A）安装，并且是驱动装置（5）在关闭位置和打开位置之间通过手动或自动地围绕主旋转轴线（A）移动，其特征在于，在舱口（1）的移动阶段期间，驱动装置（5）驱动所述舱口（1）围绕所述主旋转轴线（A）旋转，用于使所述舱口（1）沿相反方向围绕次级旋转轴线（B）旋转来操作所述舱口（1），所述两个运动的组合旋转使得舱口（1）在基本上垂直的平面中移动，而不必在舱口（1）的这个移动阶段期间引起舱口的横向移动。

2. 发明授权

US07121046B2 Sealing gasket for mounting around a motor vehicle door that presents at least one corner having a small radius of curvature 有权
标题翻译：用于安装在机动车门周围的密封垫圈，其具有至少一个具有小曲率半径的角部
公开(公告)号：US07121046B2
公开(公告)日：2006-10-17
申请号：US10820041
申请日：2004-04-08
申请人： Sylvain Baratin , Bertrand Florentz
发明人： Sylvain Baratin , Bertrand Florentz
IPC分类号： E06B7/16 , B60J10/08
CPC分类号： B60J10/24 , B60J10/16 , B60J10/21 , B60J10/248 , B60J10/277 , B60J10/35 , B60J10/80 , Y10S277/921
摘要： A sealing gasket for mounting around a motor vehicle door presenting at least one corner of small radius of curvature, the gasket being mounted directly on its support without being subjected to any specific localized treatment operation in a support corner of small radius of curvature, and comprising at least a flexible or semi-rigid fixing portion fixed by adhesive to its support and an elastically-deformable tubular portion for providing sealing, wherein the elastically-deformable portion of the gasket is given a shape extending from its fixing portion that is generally triangular, being defined by two lateral pillars which between them form an angle of about 10° to 80°, and which are united by an arch, said angle being defined using two straight lines passing substantially through the middles of the two lateral pillars at ⅖ths and at ⅘ths of the total height of the gasket measured from its fixing portion.
摘要翻译：一种用于安装在车辆门周围的至少一个具有小曲率半径的拐角的密封垫片，所述垫片直接安装在其支撑件上，而不会在小曲率半径的支撑角中受到任何特定的局部处理操作，并且包括至少一个柔性或半刚性的固定部分通过粘合剂固定到其支撑件上，以及一个用于提供密封的可弹性变形的管状部分，其中该垫片的可弹性变形部分具有从其大致三角形的固定部分延伸的形状，由两个横向支柱限定，它们之间形成约10°至80°的角度，并且由拱形结合，所述角度使用两条直线穿过两条横向柱的中间线，其中两条直线在2 / 5s处并且在从其固定部分测量的垫圈的总高度的4 / 5s处。

3. 发明申请

US20120212006A1 Hatch System for a Motor Craft, in Particular for an Automobile Vehicle 有权
标题翻译：一种汽车工具的舱口系统，特别是汽车
公开(公告)号：US20120212006A1
公开(公告)日：2012-08-23
申请号：US13397939
申请日：2012-02-16
申请人： Laurent Coldre , Bertrand Florentz
发明人： Laurent Coldre , Bertrand Florentz
IPC分类号： B60J5/00
CPC分类号： B60J5/0473
摘要： Hatch system (1) for a motor craft, in particular for an automobile vehicle, for example, the hatch (1) being mounted articulated about a substantially horizontal fixed main rotation axis (A) supported by the chassis of the motor craft, and being movable about the main rotation axis (A) manually or automatically by drive means (5) between a closed position and an open position, characterized in that, during a phase of movement of the hatch (1), the drive means (5) driving rotation of the hatch (1) about the main rotation axis (A) actuate means (7) for maneuvering the hatch (1) in rotation in the opposite direction about a secondary rotation axis (B), the combination of these two movements in rotation causing the hatch (1) to move in a substantially vertical plane without necessarily causing lateral movement of the hatch during this phase of movement of the hatch (1).
摘要翻译：用于汽车的舱口系统（1），特别是用于汽车的汽车，例如，舱口（1）围绕由电动机的底盘支撑的基本上水平的固定主旋转轴线（A）安装，并且是驱动装置（5）在关闭位置和打开位置之间通过手动或自动地围绕主旋转轴线（A）移动，其特征在于，在舱口（1）的移动阶段期间，驱动装置（5）驱动所述舱口（1）围绕所述主旋转轴线（A）旋转，用于使所述舱口（1）沿相反方向围绕次级旋转轴线（B）旋转来操作所述舱口（1），所述两个运动的组合旋转使得舱口（1）在基本上垂直的平面中移动，而不必在舱口（1）的这个移动阶段期间引起舱口的横向移动。

4. 发明申请

US20050120634A1 Method of manufacturing a sealing gasket, in particular a window run for a motor vehicle, and to a gasket manufactured in this way 审中-公开
标题翻译：制造密封垫圈的方法，特别是用于机动车辆的车窗，以及以这种方式制造的垫圈
公开(公告)号：US20050120634A1
公开(公告)日：2005-06-09
申请号：US11008497
申请日：2004-12-09
申请人： Stephane Drivon , Emmanuelle Moisy , Bertrand Florentz
发明人： Stephane Drivon , Emmanuelle Moisy , Bertrand Florentz
IPC分类号： B29C47/04 , B60J10/00 , B60J10/04 , B60J10/06 , C09K3/10 , B32B31/00 , E06B7/00
CPC分类号： B60J10/88 , B60J10/16 , B60J10/17 , B60J10/265 , B60J10/30 , B60J10/74 , B60J10/79 , Y10T428/24198
摘要： The invention relates to a method of manufacturing a sealing gasket, in particular a hidden frame type window run for a motor vehicle, the method consisting in placing in the gasket that is made from thermoplastic materials, at least one anti-shrinkage element that is placed in a position that is determined so as to obtain automatically and naturally a gasket that is curved after it has been extruded and has cooled down, and the method further consisting in acting on the shrinkage ability of the materials constituting the gasket in order to obtain varying amounts of curvature.
摘要翻译：本发明涉及一种制造密封垫圈的方法，特别是一种用于机动车辆的隐形框架式跑道的方法，该方法包括放置由热塑性材料制成的垫圈，至少一个抗收缩元件被放置在确定为自动且自然地获得在挤压后被弯曲并被冷却的垫圈的位置，并且该方法还包括作用于构成垫圈的材料的收缩能力以获得变化的位置曲率大小

5. 发明授权

US08920704B2 Ducting for a fluid transfer pipeline for an aircraft or spacecraft, method for producing same and aeronautical structure incorporating same 有权
标题翻译：用于航空器或航天器的流体输送管道的管道，其制造方法和结合其的航空结构
公开(公告)号：US08920704B2
公开(公告)日：2014-12-30
申请号：US12577980
申请日：2009-10-13
申请人： Jean-Pierre Ciolczyk , Marc Dolez , Bertrand Florentz
发明人： Jean-Pierre Ciolczyk , Marc Dolez , Bertrand Florentz
IPC分类号： B29C49/22 , F16L9/133
CPC分类号： F16L9/133 , B29C49/04 , B29C49/26 , B29C49/44 , B29C53/083 , B29C65/08 , B29C65/66 , B29C70/30 , B29C70/443 , B29C70/446 , B29D23/001 , B29K2077/00 , B29K2275/00 , B29K2307/04 , B29K2995/0058 , B29K2995/0069 , B29L2023/004 , B29L2023/22 , B64D37/005 , Y10T428/1393
摘要： The present invention relates to a ducting for a fluid transfer pipeline for an aircraft or spacecraft, an aeronautical structure incorporating it and a method for producing this ducting.The ducting (1) comprises a pipe (2) with a thermoplastic or thermoplastic elastomeric layer (4) and a reinforcing layer (5) surmounting it. The pipe has a curved and/or bent geometry and the reinforcing layer is made of a composite material based on reinforcing means (6) that are in intimate and direct contact with the subjacent layer, such as the inner layer, said geometry being obtained by one or other of the following two methods (a) and (b): a) the inner layer is previously hot formed to give it this geometry, the reinforcing means being of choice: (i) impregnated with a thermosetting matrix, the reinforcing layer forming thermosetting composite, or (ii) either reinforcing fibers intermixed with thermoplastic fibers or powders, or impregnated with a plastic polymeric coating that is curable chemically, the reinforcing layer forming a thermoplastic composite; or b) the inner layer, in its initial rectilinear geometry, is first of all covered with the reinforcing layer in which said reinforcing means are reinforcing fibers intermixed with a thermoplastic material in the form of fibers, film or powder, and this inner layer covered in this way is then blow-molded in order to give the pipe its final geometry, the reinforcing layer obtained forming a thermoplastic composite.
摘要翻译：本发明涉及一种用于飞行器或航天器的流体输送管道，其结合的航空结构和用于生产该管道的方法。管道（1）包括具有热塑性或热塑性弹性体层（4）的管（2）和超过其的增强层（5）。管道具有弯曲和/或弯曲的几何形状，并且加强层由基于与下层（例如内层）紧密且直接接触的加强装置（6）的复合材料制成，所述几何形状由以下两种方法（a）和（b）中的一种或另一种：a）预先热成型内层以赋予其几何形状，加强装置可以选择：（i）用热固性基体浸渍，加强层或（ii）与热塑性纤维或粉末混合的增强纤维，或用可化学固化的塑料聚合物涂层浸渍，所述加强层形成热塑性复合材料; 或者b）在其初始直线几何形状中的内层首先被加强层覆盖，其中所述加强装置是与纤维，薄膜或粉末形式的热塑性材料混合的增强纤维，并且该内层被覆盖然后以这种方式吹塑以便给出管的最终几何形状，获得的增强层形成热塑复合材料。

6. 发明申请

US20100147446A1 Ducting for a fluid transfer pipeline for an aircraft or spacecraft, method for producing same and aeronautical structure incorporating same 有权
标题翻译：用于航空器或航天器的流体输送管道的管道，其制造方法和结合其的航空结构
公开(公告)号：US20100147446A1
公开(公告)日：2010-06-17
申请号：US12577980
申请日：2009-10-13
申请人： Jean-Pierre Ciolczyk , Marc Dolez , Bertrand Florentz
发明人： Jean-Pierre Ciolczyk , Marc Dolez , Bertrand Florentz
IPC分类号： B29C47/00 , B29C65/00 , F16L11/00
CPC分类号： F16L9/133 , B29C49/04 , B29C49/26 , B29C49/44 , B29C53/083 , B29C65/08 , B29C65/66 , B29C70/30 , B29C70/443 , B29C70/446 , B29D23/001 , B29K2077/00 , B29K2275/00 , B29K2307/04 , B29K2995/0058 , B29K2995/0069 , B29L2023/004 , B29L2023/22 , B64D37/005 , Y10T428/1393
摘要： The present invention relates to a ducting for a fluid transfer pipeline for an aircraft or spacecraft, an aeronautical structure incorporating it and a method for producing this ducting.The ducting (1) comprises a pipe (2) with a thermoplastic or thermoplastic elastomeric layer (4) and a reinforcing layer (5) surmounting it. The pipe has a curved and/or bent geometry and the reinforcing layer is made of a composite material based on reinforcing means (6) that are in intimate and direct contact with the subjacent layer, such as the inner layer, said geometry being obtained by one or other of the following two methods (a) and (b): a) the inner layer is previously hot formed to give it this geometry, the reinforcing means being of choice: (i) impregnated with a thermosetting matrix, the reinforcing layer forming thermosetting composite, or (ii) either reinforcing fibers intermixed with thermoplastic fibers or powders, or impregnated with a plastic polymeric coating that is curable chemically, the reinforcing layer forming a thermoplastic composite; or b) the inner layer, in its initial rectilinear geometry, is first of all covered with the reinforcing layer in which said reinforcing means are reinforcing fibers intermixed with a thermoplastic material in the form of fibers, film or powder, and this inner layer covered in this way is then blow-molded in order to give the pipe its final geometry, the reinforcing layer obtained forming a thermoplastic composite.
摘要翻译：本发明涉及一种用于飞行器或航天器的流体输送管道，其结合的航空结构和用于生产该管道的方法。管道（1）包括具有热塑性或热塑性弹性体层（4）的管（2）和超过其的增强层（5）。管道具有弯曲和/或弯曲的几何形状，并且加强层由基于与下层（例如内层）紧密且直接接触的加强装置（6）的复合材料制成，所述几何形状由以下两种方法（a）和（b）中的一种或另一种：a）预先热成型内层以赋予其几何形状，加强装置可以选择：（i）用热固性基体浸渍，加强层或（ii）与热塑性纤维或粉末混合的增强纤维，或用可化学固化的塑料聚合物涂层浸渍，所述加强层形成热塑性复合材料; 或者b）在其初始直线几何形状中的内层首先被加强层覆盖，其中所述加强装置是与纤维，薄膜或粉末形式的热塑性材料混合的增强纤维，并且该内层被覆盖然后以这种方式吹塑以便给出管的最终几何形状，获得的增强层形成热塑复合材料。

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