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    • 11. 发明授权
    • Damping device and aircraft rotor system incorporating it
    • 阻尼装置和包括它的飞机转子系统
    • US08177202B2
    • 2012-05-15
    • US12398445
    • 2009-03-05
    • Hervé Richer De ForgesJean-Pierre Ciolczyk
    • Hervé Richer De ForgesJean-Pierre Ciolczyk
    • B60G13/00
    • B64C27/51F16F13/1463F16F13/16F16F13/18
    • The damping device is intended to form a drag-mode damper for a helicopter blade, and is incorporated in an aircraft rotor system. This damping device comprises: an external frame intended to be coupled to a first rotating element, and a radially internal element mounted coaxially to the frame and intended to be coupled to a second rotating element; at least one elastomer damper of annular cross section mounted fixedly to the frame and to the internal element; and a working chamber bounded by the frame and by the damper and communicating with a compensation chamber bounded by a highly deformable flexible member mounted coaxially to the internal element. The working chamber is formed at a first end of the device and communicates with the compensation chamber via a porous structure surmounting an end opening of the flexible member, which member is mounted in the internal element.
    • 阻尼装置旨在形成用于直升机叶片的牵引模式阻尼器,并且被结合在飞行器转子系统中。 该阻尼装置包括:用于联接到第一旋转元件的外框,以及与框架同轴安装且旨在联接到第二旋转元件的径向内部元件; 环形截面的至少一个弹性体阻尼器固定地安装在框架和内部元件上; 以及由框架和阻尼器限定的工作室,并且与由与内部元件同轴安装的高度可变形的柔性构件限定的补偿室连通。 所述工作室形成在所述装置的第一端,并且经由多孔结构与所述补偿室连通,所述多孔结构覆盖所述柔性构件的端部开口,所述构件安装在所述内部元件中。
    • 14. 发明申请
    • Opening Leaf Upper Module for a Vehicle Glass Panel
    • 车辆玻璃面板的开启叶上模块
    • US20120216461A1
    • 2012-08-30
    • US13466761
    • 2012-05-08
    • Laurent ColdreOlivier LaudeJean-Pierre Ciolczyk
    • Laurent ColdreOlivier LaudeJean-Pierre Ciolczyk
    • E06B7/23E05D15/28E05D15/16
    • B29C45/1676B29C45/1704B29L2012/00B29L2031/26B29L2031/30B60J5/0406B60J5/0481B60J10/45B60J10/80Y10T29/49
    • The present invention relates 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 according to the invention, comprising a molded frame based on at least one thermoplastic polymer and a molded weather strip 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 for wiping the glass panel and an interface lip for interfacing with the bodywork of the vehicle, and the frame has a longitudinal hollow.
    • 本发明涉及一种特别包括刚性框架和柔性防风条的这种类型的开口叶上模块。 根据本发明的制造开口叶片上模块的方法包括:基于至少一种热塑性聚合物的模制框架和固定到框架并基于至少一种弹性体的模制耐候条带,包括一个步骤,由此移动压板 模具或替代地传递模塑用于对旨在形成框架和连续注入的条带的材料进行多次注射成型,弹性体是与该热塑性聚合物相容的热塑性弹性体,以便获得模块 形成为单件。 优选地,条带包括用于擦拭玻璃面板的连续擦拭唇缘和用于与车辆的车身接合的接口唇缘,并且框架具有纵向中空部。
    • 15. 发明申请
    • DAMPING DEVICE AND AIRCRAFT ROTOR SYSTEM INCORPORATING IT
    • 阻尼装置和飞机转子系统
    • US20090224449A1
    • 2009-09-10
    • US12398445
    • 2009-03-05
    • Herve Richer De ForgesJean-Pierre Ciolczyk
    • Herve Richer De ForgesJean-Pierre Ciolczyk
    • F16F13/00
    • B64C27/51F16F13/1463F16F13/16F16F13/18
    • The damping is device intended to form a drag-mode damper for a helicopter blade, and is incorporated in an aircraft rotor system. This damping device comprises: an external frame intended to be coupled to a first rotating element, and a radially internal element mounted coaxially to the frame and intended to be coupled to a second rotating element; at least one elastomer damper of annular cross section mounted fixedly to the frame and to the internal element; and a working chamber bounded by the frame and by the damper and communicating with a compensation chamber bounded by a highly deformable flexible member mounted coaxially to the internal element. The working chamber is formed at a first end of the device and communicates with the compensation chamber via a porous structure surmounting an end opening of the flexible member, which member is mounted in the internal element.
    • 阻尼是旨在形成用于直升机叶片的牵引模式阻尼器的装置,并且被结合在飞行器转子系统中。 该阻尼装置包括:用于联接到第一旋转元件的外框,以及与框架同轴安装且旨在联接到第二旋转元件的径向内部元件; 环形截面的至少一个弹性体阻尼器固定地安装在框架和内部元件上; 以及由框架和阻尼器限定的工作室,并且与由与内部元件同轴安装的高度可变形的柔性构件限定的补偿室连通。 所述工作室形成在所述装置的第一端,并且经由多孔结构与所述补偿室连通,所述多孔结构覆盖所述柔性构件的端部开口,所述构件安装在所述内部元件中。
    • 16. 发明申请
    • FLEXIBLE JOINT WITH BELLOWS
    • 柔软的接头与BELLOWS
    • US20080139322A1
    • 2008-06-12
    • US11948183
    • 2007-11-30
    • Herve Richer De ForgesJean-Pierre Ciolczyk
    • Herve Richer De ForgesJean-Pierre Ciolczyk
    • F16D3/00
    • F16L27/103E21B17/085F16L27/11
    • The invention relates to 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.
    • 本发明涉及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,用于使流体在空间中流动,并且当主管轴处于对准位置时呈现由管状元件共用的轴线构成的主轴线,并且至少包括 一个与第一管状元件和壳体功能性连接的柔性关节元件,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空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。