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    • 2. 发明授权
    • Ducting for a fuel pipeline of aircraft or spacecraft, method for producing same and aircraft wing incorporating same
    • 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
    • US08248748B2
    • 2012-08-21
    • US12578153
    • 2009-10-13
    • Jean-Pierre CiolczykJulien BouletiMarc Dolez
    • Jean-Pierre CiolczykJulien BouletiMarc Dolez
    • H01H47/00
    • F16L9/125B64D37/005
    • 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.
    • 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。
    • 3. 发明授权
    • Method for manufacturing a door upper module for a window panel of a vehicle
    • 一种用于制造车辆的窗板的门上模块的方法
    • US08192671B2
    • 2012-06-05
    • US12196448
    • 2008-08-22
    • Laurent ColdreOlivier LaudeJean-Pierre Ciolczyk
    • Laurent ColdreOlivier LaudeJean-Pierre Ciolczyk
    • B29B7/00B29C45/00
    • B29C45/1676B29C45/1704B29L2012/00B29L2031/26B29L2031/30B60J5/0406B60J5/0481B60J10/45B60J10/80Y10T29/49
    • The present invention relates to a method of manufacturing an opening leaf upper module intended to be mounted at the periphery of a glass panel of a vehicle, and to an opening leaf upper module of this type particularly comprising a rigid frame and a flexible weather strip.The method of manufacturing an opening leaf upper module (1) according to the invention, comprising a molded frame (3) based on at least one thermoplastic polymer and a molded weather strip (4) secured to the frame and based on at least one elastomer, comprises a step whereby a moving-platen mold or alternatively transfer molding is used to perform multiple-shot injection molding of materials that are intended to form the frame and the strip which are injected in succession, the elastomer being a thermoplastic elastomer compatible with this thermoplastic polymer, so as to obtain the module formed as a single piece.For preference, the strip comprises a continuous wiping lip (8) for wiping the glass panel and an interface lip (9) for interfacing with the bodywork (10) of the vehicle, and the frame has a longitudinal hollow (3b).
    • 本发明涉及一种制造安装在车辆玻璃面板周边的开口叶片上部模块的方法以及一种特别包括刚性框架和柔性防风条的开口叶片上模块。 根据本发明的开式叶片上模块(1)的制造方法,包括基于至少一种热塑性聚合物的模制框架(3)和固定到框架并基于至少一种弹性体的模制耐候条带(4) 包括一个步骤,由此使用移动压板模具或交替传送模塑来进行多次注射成型用于连续注入的用于形成框架和条的材料,该弹性体是与该材料兼容的热塑性弹性体 热塑性聚合物,以获得形成为单件的模块。 优选地,条带包括用于擦拭玻璃面板的连续擦拭唇缘(8)和用于与车辆的车身(10)对接的接口唇缘(9),并且框架具有纵向中空部(3b)。
    • 5. 发明授权
    • Flexible joint with bellows
    • 带波纹管的柔性接头
    • US07506896B2
    • 2009-03-24
    • US11948183
    • 2007-11-30
    • Hervé Richer De ForgesJean-Pierre Ciolczyk
    • Hervé Richer De ForgesJean-Pierre Ciolczyk
    • F16L27/04
    • F16L27/103E21B17/085F16L27/11
    • A flexible joint with bellows for coupling two tubular elements together for passing fluid in a flow space and presenting a main axis that is constituted by the axis common to the tubular elements when they are in their aligned position, and including at least one flexible joint element functionally connected to a first tubular element and to a casing, together with a coupling bellows coupling together the two tubular elements, the coupling bellows, the flexible joint element, and the casing defining walls of a fluid-filled cavity. The joint including a flexible pressure-compensation device spaced apart from the bellows and having a first face forming at least part of a wall of said cavity and a second face that is in communication with the flow space.
    • 一种具有波纹管的柔性接头,用于将两个管状元件联接在一起,用于使流体流动,并且当主管轴线处于对准位置时,呈现由与管状元件共同的轴线构成的主轴线,并且包括至少一个柔性接头元件 功能上连接到第一管状元件和壳体,以及将两个管状元件,联接波纹管,柔性关节元件和限定流体填充腔的壁的壳体联接在一起的联接波纹管。 所述接头包括与所述波纹管间隔开的柔性压力补偿装置,并且具有形成所述空腔的壁的至少一部分的第一面和与所述流动空间连通的第二面。
    • 7. 发明授权
    • Ducting for a fluid transfer pipeline for an aircraft or spacecraft, method for producing same and aeronautical structure incorporating same
    • 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
    • US08920704B2
    • 2014-12-30
    • US12577980
    • 2009-10-13
    • Jean-Pierre CiolczykMarc DolezBertrand Florentz
    • Jean-Pierre CiolczykMarc DolezBertrand Florentz
    • B29C49/22F16L9/133
    • F16L9/133B29C49/04B29C49/26B29C49/44B29C53/083B29C65/08B29C65/66B29C70/30B29C70/443B29C70/446B29D23/001B29K2077/00B29K2275/00B29K2307/04B29K2995/0058B29K2995/0069B29L2023/004B29L2023/22B64D37/005Y10T428/1393
    • 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.
    • 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。
    • 8. 发明申请
    • Ducting for a fluid transfer pipeline for an aircraft or spacecraft, method for producing same and aeronautical structure incorporating same
    • 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
    • US20100147446A1
    • 2010-06-17
    • US12577980
    • 2009-10-13
    • Jean-Pierre CiolczykMarc DolezBertrand Florentz
    • Jean-Pierre CiolczykMarc DolezBertrand Florentz
    • B29C47/00B29C65/00F16L11/00
    • F16L9/133B29C49/04B29C49/26B29C49/44B29C53/083B29C65/08B29C65/66B29C70/30B29C70/443B29C70/446B29D23/001B29K2077/00B29K2275/00B29K2307/04B29K2995/0058B29K2995/0069B29L2023/004B29L2023/22B64D37/005Y10T428/1393
    • 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.
    • 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。
    • 9. 发明申请
    • METHOD FOR MANUFACTURING A DOOR UPPER MODULE FOR A WINDOW PANEL OF A VEHICLE, AND SUCH A MODULE
    • 用于制造车辆窗户的门上模块的方法,以及这样的模块
    • US20090051191A1
    • 2009-02-26
    • US12196448
    • 2008-08-22
    • Laurent ColdreOlivier LaudeJean-Pierre Ciolczyk
    • Laurent ColdreOlivier LaudeJean-Pierre Ciolczyk
    • B60J1/20
    • B29C45/1676B29C45/1704B29L2012/00B29L2031/26B29L2031/30B60J5/0406B60J5/0481B60J10/45B60J10/80Y10T29/49
    • The present invention relates to a method of manufacturing an opening leaf upper module intended to be mounted at the periphery of a glass panel of a vehicle, and to an opening leaf upper module of this type particularly comprising a rigid frame and a flexible weather strip.The method of manufacturing an opening leaf upper module (1) according to the invention, comprising a molded frame (3) based on at least one thermoplastic polymer and a molded weather strip (4) secured to the frame and based on at least one elastomer, comprises a step whereby a moving-platen mold or alternatively transfer molding is used to perform multiple-shot injection molding of materials that are intended to form the frame and the strip which are injected in succession, the elastomer being a thermoplastic elastomer compatible with this thermoplastic polymer, so as to obtain the module formed as a single piece.For preference, the strip comprises a continuous wiping lip (8) for wiping the glass panel and an interface lip (9) for interfacing with the bodywork (10) of the vehicle, and the frame has a longitudinal hollow (3b).
    • 本发明涉及一种制造安装在车辆玻璃面板周边的开口叶片上部模块的方法以及一种特别包括刚性框架和柔性防风条的开口叶片上模块。 根据本发明的开式叶片上模块(1)的制造方法,包括基于至少一种热塑性聚合物的模制框架(3)和固定到框架并基于至少一种弹性体的模制耐候条带(4) 包括一个步骤,由此使用移动压板模具或交替传送模塑来进行多次注射成型用于连续注入的用于形成框架和条的材料,该弹性体是与该材料兼容的热塑性弹性体 热塑性聚合物,以获得形成为单件的模块。 优选地,条带包括用于擦拭玻璃面板的连续擦拭唇缘(8)和用于与车辆的车身(10)对接的接口唇缘(9),并且框架具有纵向中空部(3b)。
    • 10. 发明授权
    • Device for filtering vibration, and a fixing system comprising a
plurality of such devices for fixing a load on a support
    • 用于过滤振动的装置,以及包括用于将负载固定在支撑件上的多个这种装置的固定系统
    • US5358210A
    • 1994-10-25
    • US39857
    • 1993-03-30
    • Jean-Michel SimonJean-Pierre Ciolczyk
    • Jean-Michel SimonJean-Pierre Ciolczyk
    • F16F1/40F16F1/42F16F3/12F16M13/00
    • F16F3/12F16F1/40F16F1/426F16F2236/025
    • The invention relates to a vibration-filtering device and to a system for fixing a load on a support by means of a plurality of such devices.The device of the invention for fixing a load on a support comprises:a first fastening zone including fastening means for fastening the device to a support;an arcuate zone;a beam substantially parallel to the first fastening zone;a second fastening zone including fastening means for fastening a load to the device; andat least two spring blades interconnected by an elastomer layer extending through the first fastening zone and the arcuate zone; wherein:the device is a vibration-filtering device;the spring blades interconnected by an elastomer layer pass through the beam to terminate in the second fastening zone close to the fastening means but separated therefrom by respective elastomer layers, in that the spring blades are separated from one another in the first fastening zone for fastening the fastening means on a support by an elastomer layer; andthe layer interconnecting the spring blades includes an elastomer having a high damping coefficient, in particular butyl rubber, in particular in the arcuate zone.
    • 本发明涉及一种振动过滤装置和一种借助于多个这样的装置将负载固定在支撑件上的系统。 用于将负载固定在支撑件上的本发明的装置包括:第一紧固区域,包括用于将装置紧固到支撑件的紧固装置; 弧形区 基本上平行于所述第一紧固区的梁; 第二紧固区域,包括用于将负载紧固到所述装置的紧固装置; 以及至少两个由通过所述第一紧固区和所述弓形区延伸的弹性体层相互连接的弹簧片; 其中:所述装置是振动过滤装置; 通过弹性体层相互连接的弹簧片穿过梁终止在靠近紧固装置的第二紧固区域中,但是由相应的弹性体层分离,因为弹簧片在第一紧固区域中彼此分开,以便紧固 通过弹性体层在支撑体上的紧固装置; 并且互连弹簧叶片的层包括具有高阻尼系数的弹性体,特别是丁基橡胶,特别是在弓形区域中。