-
公开(公告)号：US09902116B2
公开(公告)日：2018-02-27
申请号：US14896326
申请日：2014-06-03
申请人： HUTCHINSON
IPC分类号： B29C70/46 , F16C7/02 , B29C70/32 , B29C70/52 , B29C57/00 , B29C67/00 , B29C70/06 , B29C70/50 , B29D23/00 , B64C1/18 , B29L31/06 , B29K101/12 , B29C53/60 , B29K23/00 , B29K71/00 , B29K77/00 , B29K81/00 , B29K105/08 , B29K105/10 , B29K307/04 , B29L31/30
CPC分类号： B29C70/462 , B29C53/60 , B29C57/00 , B29C67/0044 , B29C70/06 , B29C70/32 , B29C70/50 , B29C70/521 , B29D23/00 , B29K2023/00 , B29K2071/00 , B29K2077/00 , B29K2081/04 , B29K2081/06 , B29K2101/12 , B29K2105/0881 , B29K2105/089 , B29K2105/10 , B29K2307/04 , B29L2031/06 , B29L2031/3076 , B64C1/18 , F16C7/026 , F16C2326/43 , Y02T50/43
摘要： A connecting rod comprises a convex elongated body around a longitudinal axis of symmetry and two connecting ends for connecting to adjacent structures. The connecting rod includes two shells with two longitudinal edges that are assembled in these edges and that each have a base of at least one shell web including continuous shell fibers primarily parallel to this axis of symmetry and impregnated with a thermoplastic shell matrix. The connecting rod incorporates at least one assembly web wound around and along the shells, and assembly fibers primarily inclined relative to the axis and impregnated with a thermoplastic assembly matrix remelted in contact with the shell matrix.
-
2.发明申请Ducting For A Fluid Transfer Pipeline For An Aircraft Or Spacecraft, Method For Producing Same And Aeronautical Structure Incorporating Same 有权用于航空器或航天器的流体输送管线的管道，产生与其相同的航空结构的方法公开(公告)号：US20140338816A1
公开(公告)日：2014-11-20
申请号：US14448144
申请日：2014-07-31
申请人： Hutchinson
IPC分类号： B29D23/00 , B29C65/08 , B29C49/04 , B29C70/44 , B29C49/44 , B29C53/08 , B29C70/30 , B29C65/66 , B29C49/26
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： A ducting and associated method is provide in which the ducting includes a pipe with a thermoplastic or thermoplastic elastomeric layer and a reinforcing layer. The pipe has a curved or bent geometry and the reinforcing layer is made of a composite material based on reinforcement in intimate and direct contact with the subjacent layer. The geometry is obtained by hot forming the inner layer to give the geometry, and the reinforcement is either impregnated with a thermosetting matrix to form a thermosetting composite, or reinforcing fibers are intermixed with thermoplastic fibers or powders, or impregnated with a plastic polymeric coating that is curable chemically. Alternatively, the inner layer is first covered with the reinforcing layer in which the reinforcement includes reinforcing fibers intermixed with a thermoplastic material in the form of fibers, film or powder is blow-molded to give the pipe its final geometry.
摘要翻译： 提供了一种管道和相关联的方法，其中管道包括具有热塑性或热塑性弹性体层和加强层的管。 管道具有弯曲或弯曲的几何形状，并且加强层由基于加强物的复合材料制成，与邻近层紧密且直接接触。 几何形状通过热成型内层得到几何形状，并且增强物浸渍有热固性基质以形成热固性复合材料，或者增强纤维与热塑性纤维或粉末混合，或用塑料聚合物涂层浸渍， 是化学固化的。 或者，内层首先用增强层覆盖，其中增强件包括与纤维形式的热塑性材料混合的增强纤维，薄膜或粉末被吹塑成型，以使管成为其最终几何形状。
-
3.发明申请COMPOSITE CONNECTING ROD, METHOD FOR MANUFACTURING SUCH A ROD AND AERONAUTIC CEILING OR FLOOR STRUCTURE INCORPORATING SAME 有权复合连接杆，制造这种类型的方法和与其共同使用的气象天花板或地板结构公开(公告)号：US20160121561A1
公开(公告)日：2016-05-05
申请号：US14896326
申请日：2014-06-03
申请人： HUTCHINSON
CPC分类号： B29C70/462 , B29C53/60 , B29C57/00 , B29C67/0044 , B29C70/06 , B29C70/32 , B29C70/50 , B29C70/521 , B29D23/00 , B29K2023/00 , B29K2071/00 , B29K2077/00 , B29K2081/04 , B29K2081/06 , B29K2101/12 , B29K2105/0881 , B29K2105/089 , B29K2105/10 , B29K2307/04 , B29L2031/06 , B29L2031/3076 , B64C1/18 , F16C7/026 , F16C2326/43 , Y02T50/43
摘要： The present invention relates to a composite connecting rod, an aeronautic ceiling or floor structure incorporating it, and a method for manufacturing this connecting rod. The invention applies to reacting primarily axial forces, in particular in the aeronautics field.The connecting rod comprises a convex elongated body around a longitudinal axis of symmetry and two connecting ends for connecting to adjacent structures, and it includes two shells with two longitudinal edges that are assembled in these edges and that each have a base of at least one shell web including continuous shell fibers primarily parallel to this axis of symmetry and impregnated with a thermoplastic shell matrix.According to the invention, the connecting rod incorporates means for assembling shells comprising at least one assembly web wound around and along shells at said body, and assembly fibers primarily inclined relative to said axis and impregnated with a thermoplastic assembly matrix remelted in contact with the shell matrix.
摘要翻译： 本发明涉及一种复合连杆，包括它的航空天花板或地板结构，以及一种用于制造该连杆的方法。 本发明适用于主要的轴向力，特别是在航空领域。 连接杆包括围绕纵向对称轴线的凸形细长体和用于连接到相邻结构的两个连接端，并且其包括两个壳体，两个壳体具有组装在这些边缘中的两个纵向边缘，并且每个具有至少一个壳体 纤维网包括主要平行于该对称轴并且用热塑性壳基体浸渍的连续壳纤维。 根据本发明，连杆包括用于组装壳体的装置，包括沿着壳体围绕和围绕所述主体卷绕的至少一个组装腹板，以及主要相对于所述轴线倾斜的组装纤维，并浸渍有与壳体接触的热塑性组合体 矩阵。
-
4.发明申请CONNECTING ROD, METHOD FOR MANUFACTURING SUCH A ROD AND AERONAUTIC FLOOR STRUCTURE INCORPORATING SAME 审中-公开连接方法，制造这种类型的方法和包含其的气动地板结构公开(公告)号：US20160123380A1
公开(公告)日：2016-05-05
申请号：US14895898
申请日：2014-06-03
申请人： HUTCHINSON
CPC分类号： F16C7/02 , B29C65/4835 , B29C65/542 , B29C65/544 , B29C66/12441 , B29C66/12469 , B29C66/534 , B29C66/71 , B29C66/721 , B29C66/7392 , B29C66/7394 , B29C66/7422 , B29L2031/06 , B64C1/18 , F16B11/008 , F16C7/026 , F16C7/06 , F16C11/04 , Y02T50/43 , B29K2023/00 , B29K2063/00 , B29K2071/00 , B29K2077/00 , B29K2079/085 , B29K2081/04 , B29K2081/06
摘要： The present invention relates to a connecting rod, an aeronautic floor structure incorporating it, and a method for manufacturing this connecting rod. The invention applies to a connecting rod suitable for reacting primarily axial forces, in particular in the aeronautics field.This connecting rod comprises a tubular body with two ends and two heads for connecting those ends to adjacent structures and that is suitable for reacting primarily axial forces, each head comprising an end-piece flared toward the body and glued on the latter in a gluing interface.According to the invention, the connecting rod comprises at least one first sealing gasket mounted radially between and against the body and the end-piece of each head, axially toward the inside of the gluing interface. The connecting rod can be manufactured by assembling the first seal in contact with each end-piece and a first inner or outer face of an end zone opposite the body, then gluing each end-piece on the body, by injection and suction of a glue radially between the body and each end-piece and axially toward the outside of this first sealing gasket.
摘要翻译： 本发明涉及一种连杆，包括其的航空地板结构以及该连杆的制造方法。 本发明适用于适用于主要轴向力的连杆，特别是在航空领域。 该连杆包括具有两端的管状体和用于将这些端部连接到相邻结构的两个头部，并且其适于主要反作用于轴向力的作用，每个头部包括朝向身体向外延伸并以胶合界面 。 根据本发明，连杆包括至少一个第一密封垫片，其径向地安装在主体之间并且抵靠主体和每个头部的端部件，轴向地朝向胶合界面的内部。 连杆可以通过将第一密封件与每个端件接触并且与主体相对的端部区域的第一内表面或外表面组装，然后通过注射和吸取胶将每个端件粘合在主体上来制造 径向地位于主体和每个端部件之间并且轴向地朝向该第一密封垫圈的外侧。
-
5.发明申请Profile With U-Shaped Portion(S), Load-Bearing Structural Element Of A Vehicle Incorporating Same, And Method For Manufacturing The Profile 审中-公开具有U形部分（S）的轮廓，包含相同的车辆的承载结构元件以及制造方法公开(公告)号：US20150336621A1
公开(公告)日：2015-11-26
申请号：US14650650
申请日：2013-12-10
申请人： HUTCHINSON
摘要： A profile with one or more portion(s) whose cross-sections are substantially U-shaped, locally provided with capabilities of increasing torsional rigidity and potentially flexural rigidity, a load-bearing structural element of a vehicle such as a support grille of an electrical and/or hydraulic system incorporating that profile, and a method of manufacturing that profile are provided. The profile includes at least one U-shaped portion having a slot bounded by two wings and a core and that is locally provided and capable for increasing torsional rigidity, the profile being formed of a fibre-reinforced plastic composite, having at least one cross brace formed in the slot from a single part with the wings and the core. The wings and the core are reinforced by fibres mostly oriented in the longitudinal direction of the profile, with more than 60% of the fibres oriented in a −30° to +30° angle with that direction.
摘要翻译： 具有一个或多个部分的轮廓，其横截面基本上为U形，局部地具有提高扭转刚度和潜在弯曲刚度的能力，车辆的承载结构元件，例如电气的支撑格栅 和/或包含该轮廓的液压系统，以及制造该轮廓的方法。 该轮廓包括至少一个U形部分，其具有由两个翼部和芯部限定的狭槽，其局部地设置并能够增加扭转刚度，该轮廓由纤维增强塑料复合材料形成，该纤维增强塑料复合材料具有至少一个横支 从具有翼和芯的单个部分形成在狭槽中。 翼和芯通过主要沿纵向方向定向的纤维来增强，超过60％的纤维与该方向取向成-30°至+ 30°的角度。
-
6.发明授权公开(公告)号：US10427482B2
公开(公告)日：2019-10-01
申请号：US15569858
申请日：2015-04-28
申请人： HUTCHINSON
摘要： A link arm for connecting a first unsuspended mass to a second suspended mass, and its manufacturing method are provided. In some embodiment the arm applies in particular to a suspension system for a motor vehicle, wherein the arm is able to equip a wheel suspension by having triangular housings to receive a stub axle of the wheel and two connecting links to the chassis of the vehicle. In some embodiments, the arm comprises housings to receive a first linkage joint to the first mass, and at least a second linkage joint to the second mass, and comprises: a stiffening portion which comprises a first thermoplastic or thermosetting matrix composite material reinforced with fibers and which comprises a peripheral rim of the arm, and an anti-buckling portion interposed in the stiffening portion and extending from the rim over substantially the entire arm.
-
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 有权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：US09222605B2
公开(公告)日：2015-12-29
申请号：US14448144
申请日：2014-07-31
申请人： Hutchinson
IPC分类号： B29D23/00 , F16L9/133 , B29C49/04 , B29C49/26 , B29C49/44 , B29C53/08 , B29C65/08 , B29C65/66 , B29C70/30 , B29C70/44 , B64D37/00 , B29K77/00 , B29K275/00 , B29K307/04 , B29L23/00
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： A ducting and associated method is provide in which the ducting includes a pipe with a thermoplastic or thermoplastic elastomeric layer and a reinforcing layer. The pipe has a curved or bent geometry and the reinforcing layer is made of a composite material based on reinforcement in intimate and direct contact with the subjacent layer. The geometry is obtained by hot forming the inner layer to give the geometry, and the reinforcement is either impregnated with a thermosetting matrix to form a thermosetting composite, or reinforcing fibers are intermixed with thermoplastic fibers or powders, or impregnated with a plastic polymeric coating that is curable chemically. Alternatively, the inner layer is first covered with the reinforcing layer in which the reinforcement includes reinforcing fibers intermixed with a thermoplastic material in the form of fibers, film or powder is blow-molded to give the pipe its final geometry.
摘要翻译： 提供了一种管道和相关联的方法，其中管道包括具有热塑性或热塑性弹性体层和加强层的管。 管道具有弯曲或弯曲的几何形状，并且加强层由基于加强物的复合材料制成，与邻近层紧密且直接接触。 几何形状通过热成型内层得到几何形状，并且增强物浸渍有热固性基质以形成热固性复合材料，或者增强纤维与热塑性纤维或粉末混合，或用塑料聚合物涂层浸渍， 可化学固化。 或者，内层首先用增强层覆盖，其中增强件包括与纤维形式的热塑性材料混合的增强纤维，薄膜或粉末被吹塑成型，以使管成为其最终几何形状。
-
-
-
-
-
-
搜索结果
7 条记录 (耗时 0.026 秒)