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1. 发明授权

US08248748B2 Ducting for a fuel pipeline of aircraft or spacecraft, method for producing same and aircraft wing incorporating same 有权
标题翻译：用于航空器或航天器的燃料管道的管道，其制造方法和包含其的飞机机翼
公开(公告)号：US08248748B2
公开(公告)日：2012-08-21
申请号：US12578153
申请日：2009-10-13
申请人： Jean-Pierre Ciolczyk , Julien Bouleti , Marc Dolez
发明人： Jean-Pierre Ciolczyk , Julien Bouleti , Marc Dolez
IPC分类号： H01H47/00
CPC分类号： F16L9/125 , B64D37/005
摘要： The invention relates to a ducting for a fuel pipeline of an aircraft or spacecraft designed to be mounted in each of the wings of an aircraft, an aircraft wing incorporating this ducting and a method for producing same. This ducting comprises at least one multilayer pipe having two respectively inner and outer layers made of a composite plastic material that is leakproof and chemically resistant to the fuel and that is reinforced by electrically conductive reinforcing means, these layers being separated by an intermediate layer, notably capable of stiffening the pipe when flexed and/or to insulate it electrically. Each of the inner and outer layers has at least one winding with contiguous turns of a continuous element made of a composite thermoplastic incorporating these reinforcing means.
摘要翻译：本发明涉及一种设计成安装在飞行器的每个翼中的飞行器或航天器的燃料管道的管道，包括该管道的飞机机翼及其制造方法。该管道包括至少一个多层管，其具有由复合塑料材料制成的两层分别内层和外层，该复合塑料材料是防漏的并对燃料具有化学耐受性，并且由导电增强装置增强，这些层被中间层分隔，特别是能够在挠曲时加强管道和/或使其电绝缘。内层和外层中的每一层具有至少一个具有连续元件的连续匝组成的绕组，所述连续元件由包含这些增强装置的复合热塑性材料制成。

2. 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。

3. 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。

4. 发明申请

US20100116941A1 Ducting for a fuel pipeline of aircraft or spacecraft, method for producing same and aircraft wing incorporating same 有权
标题翻译：用于航空器或航天器的燃料管道的管道，其制造方法和包含其的飞机机翼
公开(公告)号：US20100116941A1
公开(公告)日：2010-05-13
申请号：US12578153
申请日：2009-10-13
申请人： Jean-Pierre Ciolcyzk , Julien Bouleti , Marc Dolez
发明人： Jean-Pierre Ciolcyzk , Julien Bouleti , Marc Dolez
IPC分类号： B64D37/00 , F16L9/14 , B29C63/08
CPC分类号： F16L9/125 , B64D37/005
摘要： The present invention relates to a ducting for a fuel pipeline of an aircraft or spacecraft, in particular designed to be mounted in each of the wings of an aircraft, an aircraft wing incorporating this ducting and a method for producing same.This ducting comprises at least one multilayer pipe (1) having two respectively inner (2) and outer (3) layers made of a composite plastic material that is leakproof and chemically resistant to the fuel and that is reinforced by electrically conductive reinforcing means, these layers being separated by an intermediate layer (4), notably capable of stiffening the pipe when flexed and/or to insulate it electrically.According to the invention, each of the inner and outer layers has at least one winding with contiguous turns of a continuous element made of a composite thermoplastic incorporating these reinforcing means, so that this pipe enables electrostatic charges to be eliminated through its inner layer and electrical charges due to lightning to be deflected through its outer layer while having a high modulus of inertia and reduced mass.
摘要翻译：本发明涉及一种用于航空器或航天器的燃料管道的管道，特别是设计成安装在飞行器的每个翼中，并入该管道的飞行器机翼及其制造方法。该管道包括至少一个多层管（1），其具有由复合塑料材料制成的两个分别为内部（2）和外部（3）的层，该层是防漏的并对燃料具有化学耐受性并且由导电加强装置加强，层被中间层（4）隔开，特别是当挠曲时能够加强管道和/或使其电绝缘。根据本发明，内层和外层中的每一个具有至少一个具有连续元件的连续匝组成的绕组，所述连续元件由包含这些加强装置的复合热塑性材料制成，使得该管能够通过其内层和电气来消除静电荷由于闪电引起的电荷通过其外层偏转，同时具有高的惯性模量和减小的质量。

5. 发明申请

US20070261781A1 FLEXIBLE FLUID-TRANSPORT DUCT PRESENTING REINFORCEMENT 审中-公开
标题翻译：柔性流体输送导管加固
公开(公告)号：US20070261781A1
公开(公告)日：2007-11-15
申请号：US11745578
申请日：2007-05-08
申请人： Daniel Mahin , Marc Dolez , Pascal Oesterle
发明人： Daniel Mahin , Marc Dolez , Pascal Oesterle
IPC分类号： B31C13/00
CPC分类号： F16L11/081 , B60H1/00564 , F16L11/112 , Y10T428/1362
摘要： The invention relates to a flexible duct of elastomer for transferring fluid and presenting a reinforcing element, wherein said reinforcing element comprises at least one laid-in web. The invention also relates to a method of using elastomer to fabricate a flexible duct for transferring fluid, the duct presenting a reinforcing element, and wherein it implements laying at least one laid-in web on a forming cylinder that is optionally coated in elastomer material, and then covering the laid-in web(s) with an elastomer coating, and finally performing vulcanization.
摘要翻译：本发明涉及一种用于传送流体和呈现加强元件的弹性体柔性管道，其中所述加强元件包括至少一个铺设的网。本发明还涉及一种使用弹性体来制造用于输送流体的柔性管道的方法，所述管道呈现增强元件，并且其中其实施了将至少一个铺设的网放置在可选地涂覆在弹性体材料上的成形滚筒上，然后用弹性体涂层覆盖铺设的网，最后进行硫化。

6. 发明授权

US06554321B1 Decoupling sleeve for mounting in a motor vehicle exaust pipe 有权
标题翻译：用于安装在汽车排气管中的去耦套筒
公开(公告)号：US06554321B1
公开(公告)日：2003-04-29
申请号：US09614498
申请日：2000-07-11
申请人： Vincent Boisseau , Jean-Michel Simon , Marc Dolez , Daniel Mahin
发明人： Vincent Boisseau , Jean-Michel Simon , Marc Dolez , Daniel Mahin
IPC分类号： F16L1114
CPC分类号： F16L59/21 , F01N13/14 , F01N13/1816 , F16L27/1004 , F16L27/111
摘要： A decoupling sleeve for mounting in a motor vehicle exhaust pipe (LE), the sleeve (5) comprising in particular a mechanical portion (10) having two rigid end zones (15) for connection to the exhaust pipe (LE), and a sealing portion (11) that is thermally insulated from the inside by an insulation portion (12) and that extends over substantially the entire length of the mechanical portion (10) of the sleeve, the sleeve being characterized in that the sealing portion (11) comprises a central zone (22) formed by a layer or wall (24) made of a material that is flexible and that withstands temperature, and two rigid end zones (23) respectively connected to two end zones (15) of the mechanical portion (10), the sealing portion (11) forming a covering that is continuous, closed, and leakproof.
摘要翻译：一种用于安装在机动车辆排气管（LE）中的分离套筒，套筒（5）特别包括具有用于连接到排气管（LE）的两个刚性端部区域（15）的机械部分（10）部分（11），其通过绝缘部分（12）与内部隔热并且在套筒的机械部分（10）的基本上整个长度上延伸，其特征在于，密封部分（11）包括由由柔性且耐受温度的材料制成的层或壁（24）形成的中心区（22）和分别连接到机械部分（10）的两个端部区域（15）的两个刚性端部区域（23）），所述密封部（11）形成连续，封闭和防漏的覆盖物。

7. 发明授权

US06508442B1 Mounting clamp for a tubular part 失效
标题翻译：用于管状部件的安装夹具
公开(公告)号：US06508442B1
公开(公告)日：2003-01-21
申请号：US09532126
申请日：2000-03-21
申请人： Marc Dolez
发明人： Marc Dolez
IPC分类号： F16L312
CPC分类号： F16L3/1233
摘要： The invention relates to a mounting clamp for a tubular part such as a cable, a hose, a coupling, or a tube, the clamp having a loop region for surrounding the tubular part, said loop region being open and terminating in fixing tabs, each provided with at least one fixing hole, wherein at least one of said fixing holes presents at least one claw enabling a fixing element of a fixing device to be tightened in preliminary manner by being moved in translation.
摘要翻译：本发明涉及一种用于诸如电缆，软管，联接器或管子的管状部件的安装夹具，夹具具有用于围绕管状部件的环形区域，所述环形区域是打开的并且终止于固定突出部，每个设置有至少一个固定孔，其中至少一个所述固定孔具有至少一个爪，所述至少一个爪使得定影装置的固定元件能够以平移方式被初步地紧固。

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