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91. 发明申请

WO1987001069A1 COMPOSITE TUBULAR ELEMENT INTENDED TO FORM A STRUCTURE PART, FABRICATION METHOD THEREOF AND DEVICE FOR IMPLEMENTING SUCH METHOD 审中-公开
标题翻译：构成结构部件的复合材料元件及其制造方法及其实施方法
公开(公告)号：WO1987001069A1
公开(公告)日：1987-02-26
申请号：PCT/FR1986000287
申请日：1986-08-18
申请人： AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE , COUTANT, Hervé , JUMEL, Jean-Pierre
发明人： AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE
IPC分类号： B29C53/44
CPC分类号： E04B1/5837 , B29C43/027 , B29C43/36 , B29C53/44 , B29C70/347 , B29D23/00 , B29K2105/06 , B29L2031/601 , B64G9/00 , E04C3/28 , Y02T50/43 , Y10T156/1038
摘要： Structural tubular element (1) made of curable resin-coated resistant fibres and intended to form a part of a structure. According to the invention, said tubular element is characterized in that it comprises an internal axial wall (4) which is also made of curable resin-coated resistant fibres which are integrally part of said element and which extend throughout the length thereof and in that, at the extremities (3) of said element (1), portions (4a) of said axial wall (4) are accessible to form areas for the fixing of said element to other parts of said structure. Construction of structure parts, particularly in the aircraft and spatial fields.
摘要翻译：结构管状元件（1）由可固化树脂涂覆的耐磨纤维制成并且旨在形成结构的一部分。根据本发明，所述管状元件的特征在于，其包括内部轴向壁（4），该内部轴向壁（4）也由可固化的树脂涂覆的耐磨纤维制成，所述可固化的树脂涂覆的耐磨纤维是所述元件的整体部分并且在整个长度上延伸，在所述元件（1）的末端（3）处，所述轴向壁（4）的部分（4a）可接近以形成用于将所述元件固定到所述结构的其它部分的区域。结构部件的构造，特别是在飞机和空间领域。

92. 发明申请

WO1980002008A1 METHOD FOR MAKING LIP TYPE SHAFT SEAL 审中-公开
标题翻译：用于制造LIP型轴封的方法
公开(公告)号：WO1980002008A1
公开(公告)日：1980-10-02
申请号：PCT/US1980000274
申请日：1980-03-12
申请人： GARLOCK INC
发明人： GARLOCK INC , ONEAL R , BAINARD D
IPC分类号： B29H09/10
CPC分类号： B29C43/18 , B29C43/027 , B29D99/0053 , B29K2021/00 , B29L2031/26 , F16J15/328
摘要： A method for molding an annular lip type shaft seal (10) of the type having an annular elastomeric shaft seal element (12) and a resin liner (14) (preferably polytetrafluoroethylene) integrally molded therewith and bonded thereto, including providing a step or shoulder (36) on the mold core (26) to prevent the resin liner (14) from flowing axially beyond a predetermined location during molding. The method includes providing a certain range of acute angles "//c" between the shoulder surface (42) and the liner forming surface (38) of the mold core surface (34), and a certain range of shoulder heights "d" relative to the liner thickness "t", for various values of the initial viscosity of the elastomeric preform (18). The percentage of rejects due to undesired flow of the resin liner (14) during molding has been greatly reduced.
摘要翻译：一种用于模制具有环形弹性体轴密封元件（12）的环形唇形轴封（10）和与其一体模制并与其结合的树脂衬套（14）（优选聚四氟乙烯）的方法，包括提供台阶或肩部（36）在模芯（26）上，以防止树脂衬套（14）在模制期间轴向地超过预定位置。该方法包括在模芯表面（34）的肩部表面（42）和衬垫形成表面（38）之间提供一定范围的锐角“// c”，并且一定范围的肩部高度“d”相对对于弹性体预成型件（18）的初始粘度的各种值，到衬里厚度“t”。在模制期间由于树脂衬垫（14）的不期望的流动导致的废品的百分比已经大大降低。

93. 发明申请

WO2016077427A1 METHOD OF SHAPING A TAMPON FOR FEMININE HYGIENE 审中-公开
标题翻译：形成有限元素卫生用TAMPON的方法
公开(公告)号：WO2016077427A1
公开(公告)日：2016-05-19
申请号：PCT/US2015/060098
申请日：2015-11-11
申请人： JOHNSON & JOHNSON GMBH , PELLEY, Kenneth A.
发明人： PELLEY, Kenneth A.
IPC分类号： A61F13/551 , A61F13/20
CPC分类号： A61F13/2088 , A61F13/15747 , A61F13/202 , A61F13/2022 , A61F13/2037 , A61F13/2085 , A61F13/55175 , A61F2013/15715 , B29C43/027 , B29C43/183 , B29C43/184 , B29C2043/029 , B29C2043/3405 , B29L2031/769 , B65B5/04 , B65B63/02
摘要： A process of forming a shaped, dimensionally stable tampon includes the steps of: radially compressing a tampon blank to form a dimensionally stable intermediate pledget having an intermediate pledget diameter and a longitudinal axis; placing the intermediate pledget into a hollow carrier and inserting the intermediate pledget and hollow carrier into a mold; urging the intermediate pledget into the mold via a ram bearing on an end of the intermediate pledget contained within the hollow carrier and withdrawing the hollow carrier from the mold to permit the exposed end of the intermediate pledget to substantially fill the mold and to form the shaped, dimensionally stable tampon; removing the shaped, dimensionally stable tampon from the mold; and enclosing the shaped, dimensionally stable tampon in a primary package that conforms to the shape thereof. The mold has an access opening through which the hollow carrier can be withdrawn.
摘要翻译：形成成形尺寸稳定的棉条的方法包括以下步骤：径向压缩棉塞坯料以形成具有中间毛细管直径和纵向轴线的尺寸稳定的中间填料; 将中间填料放入中空载体并将中间填料和中空载体插入模具中; 通过中空托盘的一端的压头轴承将中间填料推入模具中，将中空载体从模具中取出，使中间填料的露出端基本上填充模具并形成成形，尺寸稳定的棉塞; 从模具中取出成形的尺寸稳定的棉条; 并将成形的尺寸稳定的棉条封装在符合其形状的初级包装中。模具具有进入开口，中空托架可通过该开口取出。

94. 发明申请

WO2015118401A1 GAINE TUBULAIRE ANNELÉE COMPORTANT UN MOYEN INTÉRIEUR DE SERRAGE 审中-公开
标题翻译：包括内部夹紧手段的环形管
公开(公告)号：WO2015118401A1
公开(公告)日：2015-08-13
申请号：PCT/IB2015/000117
申请日：2015-02-06
申请人： DELFINGEN FR-ANTEUIL S.A.
发明人： ROUX, Sébastien , GUIHOT, Michael , VOIDEY, Patrick , BERNICOT, Matthieu
IPC分类号： H02G3/04
CPC分类号： H02G3/0468 , B29C43/021 , B29C43/027 , B29C43/36 , B29C2043/023 , B29C2043/3602 , B29K2101/12 , B29K2105/258 , B29L2023/18
摘要： L'invention concerne une gaine tubulaire annelée comprenant au moins un moyen intérieur de serrage (5) permettant notamment de serrer un tube (11), en particulier un tube lisse, se trouvant à l'intérieur de la gaine, cette gaine ayant ceci de particulier qu' au moins une zone souple (8) est associée au moyen intérieur de serrage (5). L'invention a également trait à un procédé de fabrication d'une telle gaine, ainsi qu'à un procédé de maintien d'une gaine tubulaire annelée sur un tube (11), dans lequel : on utilise une gaine tubulaire annelée selon l'invention; - on agit sur la ou les zone (s) souple (s) (8) pour déformer la gaine; - on introduit le tube (11) dans la gaine tubulaire annelée, puis - on relâche la ou les zone (s) souple (s) (8).
摘要翻译：本发明涉及一种环形管状护套，其包括至少一个内部装置（5），用于特别夹紧管（11），更具体地说是位于所述护套内的光滑管，所述护套是独特的，因为至少一个柔性区域（8）与内部夹紧装置（5）相关联。本发明还涉及一种用于制造这种护套的方法，以及用于在管（11）上保持环形管状护套的方法，其中：根据本发明使用环形管状护套; 控制柔性区域（8）以使护套变形; 管（11）插入环形管状护套中，然后释放柔性区域（8）。

95. 发明申请

WO2015108141A1 転がり軸受用保持器およびその製造方法、並びに転がり軸受审中-公开
标题翻译：滚动轴承保持器，其制造方法和滚动轴承
公开(公告)号：WO2015108141A1
公开(公告)日：2015-07-23
申请号：PCT/JP2015/051052
申请日：2015-01-16
申请人： NTN株式会社
发明人：姫野　芳英
IPC分类号： F16C33/44 , B29C43/18 , F16C19/06
CPC分类号： B29C43/36 , B29C43/027 , B29K2105/12 , B29L2031/04 , B29L2031/7096 , F16C19/163 , F16C33/3856 , F16C2208/82
摘要：　高強度・高弾率でありながら、ウエルド部のような強度が低い箇所や材料欠陥がなく、比較的安価に製造することができる転がり軸受用保持器およびその製造方法、並びに該保持器を組み込んだ転がり軸受を提供する。転がり軸受における転動体を保持する円環状の転がり軸受用保持器５であり、母材の熱硬化性樹脂を繊維材で強化してなる複合材を円環軸方向に圧縮成形した成形体の熱硬化物であり、特に繊維材が炭素繊維であり、上記複合材は該炭素繊維の不織布にフェノール樹脂などの熱硬化性樹脂を含浸または被覆してなる。
摘要翻译：提供具有高强度和高弹性的滚动轴承保持器，没有材料缺陷和低强度区域，例如焊接，并且可以以相对低的成本制造，所述保持器的制造方法和集成所述保持器的滚动轴承。用于滚动轴承的圆柱形保持器（5）将滚动元件保持在滚动轴承中，并且是通过在环形轴线方向上压缩复合材料形成的成型体的热固化产物，所述复合材料为通过用纤维材料增强热固性树脂基材而形成。特别地，纤维材料是碳纤维，复合材料是用酚醛树脂等热固性树脂浸渍或覆盖所述碳纤维的无纺布而形成的。

96. 发明申请

WO2015006146A1 METHOD OF FORMING A GOLF BALL OR A PART OF A GOLF BALL, AND GOLF BALLS OBTAINED THEREBY 审中-公开
标题翻译：形成高尔夫球或高尔夫球的一部分的方法及获得的高尔夫球
公开(公告)号：WO2015006146A1
公开(公告)日：2015-01-15
申请号：PCT/US2014/045334
申请日：2014-07-03
申请人： NIKE INNOVATE C.V. , NIKE, INC.
发明人： CHEN, John, C.
IPC分类号： A63B37/00 , B29C43/02 , B29D99/00 , C08K5/09
CPC分类号： A63B37/0003 , A63B37/0018 , A63B37/0024 , A63B37/0039 , A63B37/0051 , A63B37/0075 , A63B37/0076 , A63B37/0078 , A63B37/0096 , A63B45/00 , B29B9/06 , B29C43/003 , B29C43/02 , B29C43/027 , B29C43/18 , B29C43/52 , B29C45/0001 , B29C45/14819 , B29C45/72 , B29C2043/182 , B29D99/0042 , B29K2009/00 , B29K2105/0014 , B29K2105/243 , B29K2995/0046 , B29L2009/00 , B29L2031/546 , C08F136/04 , C08F136/06 , C08J3/24 , C08J3/243 , C08J3/244 , C08J3/247 , C08J2309/00 , C08J2323/22 , C08K5/09 , C08K5/098 , C08K5/14
摘要： A method of forming a golf ball includes forming a pair of thermoplastic hemispherical shells from an elastomer compound including an elastomer and first, second, and third free radical initiators, with the elastomer being pre-crosslinked to a first crosslinking density, then positioning a spherical component between the hemispherical shells and compression molding and curing the hemispherical shells to a second crosslinking density around the spherical component. The method uses three different crosslinking temperatures.
摘要翻译：形成高尔夫球的方法包括由包括弹性体的弹性体化合物和第一，第二和第三自由基引发剂形成一对热塑性半球形壳，弹性体预交联至第一交联密度，然后定位球形半球形壳体之间的部件和压缩成型，并将半球形壳体固化成球形部件周围的第二交联密度。该方法使用三种不同的交联温度。

97. 发明申请

WO2013084045A1 METHOD FOR COMPRESSION MOLDING A DUAL CORE FOR A GOLF BALL 审中-公开
标题翻译：压缩成型用于高尔夫球的双核心的方法
公开(公告)号：WO2013084045A1
公开(公告)日：2013-06-13
申请号：PCT/IB2012/002581
申请日：2012-12-03
申请人： NIKE INTERNATIONAL LTD. , CHOU, Chien-Hsien , KO, Chin-Shun , CHIANG, Chun-Ting , LIU, Chen-Tal , ONO, Takahisa
发明人： CHOU, Chien-Hsien , KO, Chin-Shun , CHIANG, Chun-Ting , LIU, Chen-Tal , ONO, Takahisa
IPC分类号： B29C43/02 , A63B37/00 , B29D99/00 , B29C43/14 , B29C43/18
CPC分类号： B29C43/146 , A63B37/005 , A63B37/0051 , A63B37/0069 , A63B37/0076 , A63B45/00 , B29C43/027 , B29C43/18 , B29C65/70 , B29C2043/182 , B29C2043/189 , B29D99/0042 , B29K2009/00 , B29L2031/546
摘要： A method and system for compression molding a dual core of a golf ball is disclosed. The method may include a first cycle in which a top mold plate, a middle mold plate, and a bottom mold plate may be used to compression mold concave shells. During the first cycle, the top mold plate and the bottom mold plate may be held at a first temperature T1 and the middle mold plate may be held at a second temperature T2. During the first cycle, the mold plates may be pressed together with a first pressure P1 for a first time t1. A second cycle may include compression molding the concave shells about a solid core. During the second cycle, the top mold plate and the bottom mold plate may be held at the first temperature T1 and pressed together with a second pressure P2 for a second time t2.
摘要翻译：公开了一种用于压缩成型高尔夫球双芯的方法和系统。该方法可以包括第一循环，其中可以使用顶模板，中模板和底模板来压缩模具凹形壳体。在第一周期期间，顶模板和底模板可以保持在第一温度T1，并且中模板可以保持在第二温度T2。在第一循环期间，模板可以以第一压力P1第一次被压在一起t1。第二循环可以包括围绕实心芯压缩模制凹形壳体。在第二周期期间，顶模板和底模板可以保持在第一温度T1并且用第二压力P2压在第二时间t2。

98. 发明申请

WO2011049634A1 ROTARY HIGH SPEED LOW COMPRESSION THERMOPLASTIC MOLDING METHOD AND APPARATUS 审中-公开
标题翻译：旋转高速低压缩热塑性成型方法和装置
公开(公告)号：WO2011049634A1
公开(公告)日：2011-04-28
申请号：PCT/US2010/002833
申请日：2010-10-25
申请人： FLEXTRONICS AP LLC , LOFGREN, Matt, James
发明人： LOFGREN, Matt, James
IPC分类号： B28B5/06
CPC分类号： B29C43/04 , B29C43/021 , B29C43/027 , B29C43/08 , B29C43/34 , B29C43/36 , B29C43/52 , B29C43/54 , B29C2043/029 , B29C2043/3433 , B29C2043/3444 , B29C2043/3689 , B29K2101/12 , B29L2031/7544
摘要： A molding apparatus includes a plurality of deep-draw compression molds. Each of the molds includes a mold cavity and an associated mold core. A rotating support structure operatively supports the mold cavities and the mold cores relative to each other. The molds open and close as they travel around a closed path defined by the support structure. A mold material discharge mechanism deposits a predetermined amount of mold material in each of the molds. A heat source superheats the molds, and a mold closing mechanism closes the superheated molds, compressing the mold material between the mold cavities and the mold cores to form a deep-draw component A coolant source rapidly and actively cools the molds, and a mold opening mechanism opens the cooled molds. An ejector is disposed to eject the deep draw components from the molds. A method of molding deep-draw components is also disclosed. The system and method of the present invention facilitate compression molding of deep-draw components.
摘要翻译：成型设备包括多个深拉压模。每个模具包括模腔和相关的模芯。旋转支撑结构相对于彼此可操作地支撑模腔和模芯。当模具围绕由支撑结构限定的封闭路径行进时，模具打开和关闭。模具材料排出机构在每个模具中沉积预定量的模具材料。热源使模具过热，并且模具关闭机构关闭过热模具，在模具腔和模具芯之间压缩模具材料，以形成深拉成分A冷却剂源快速且主动地冷却模具，并且模具开口机构打开冷却模具。喷射器被设置成从模具中喷出深拉伸部件。还公开了一种成型深拉成分的方法。本发明的系统和方法有利于深拉成分的压塑。

99. 发明申请

WO2010077595A2 PROCESS AND APPARATUS FOR PRODUCING COMPOSITE STRUCTURES 审中-公开
标题翻译：生产复合结构的方法和装置
公开(公告)号：WO2010077595A2
公开(公告)日：2010-07-08
申请号：PCT/US2009/066957
申请日：2009-12-07
申请人： MRA SYSTEMS, INC. , MAHESHWARI, Mahendra , VELTEN, James, J.
发明人： MAHESHWARI, Mahendra , VELTEN, James, J.
IPC分类号： B29C70/34 , B29C70/54
CPC分类号： B29C70/545 , B29C43/027 , B29C43/10 , B29C2043/3655 , B29K2995/0002 , B29L2031/3076 , B29L2031/737 , Y10S264/57 , Y10S264/70 , Y10S264/78 , Y10S425/037 , Y10T156/1028 , Y10T156/1056 , Y10T156/1057 , Y10T156/1062 , Y10T156/1304
摘要： A process and apparatus for producing perforated composite structures, such as acoustic skins suitable for aircraft engine nacelle and duct components. The process includes placing a mat member, a non-impregnated fabric member, and a resin film on a tool surface so that pins disposed on the mat member project through the fabric member and resin film to define holes therein. The fabric member is between the mat member and resin film, and the fabric member and resin film define a stack that conforms to the mat member and tool surface. A caul member is then placed on the stack so that apertures in the caul member are penetrated by the pins. The stack is heated to melt the resin film and cause molten resin to infuse the fabric member and yield a resin-infused fabric stack, after which the molten resin within the resin-infused fabric stack is at least partially cured.
摘要翻译：用于生产穿孔复合结构的方法和设备，例如适用于飞机发动机机舱和管道部件的声学皮肤。该方法包括将垫子，非浸渍的织物构件和树脂膜放置在工具表面上，使得设置在垫构件上的销突出穿过织物构件和树脂膜以在其中限定孔。织物构件在垫材和树脂膜之间，织物和树脂膜限定了与垫材和工具表面一致的叠层。然后将一个止动件放置在堆叠上，使得止动件中的孔被销钉穿透。将该叠层加热熔融树脂薄膜，使熔融树脂注入织物，并产生树脂注入的织物叠层，此后树脂注入的织物叠层内的熔融树脂至少部分固化。

100. 发明申请

WO2007092305A3 METHOD AND MOLD FOR MAKING NON-METALLIC FIBER REINFORCED PARTS 审中-公开
标题翻译：用于制造非金属纤维增强部件的方法和模具
公开(公告)号：WO2007092305A3
公开(公告)日：2008-09-12
申请号：PCT/US2007002887
申请日：2007-02-01
申请人： TIODIZE CO INC
发明人： ADAMS THOMAS R , WILTMAN GARY R
IPC分类号： B29C43/00 , B29C33/02
CPC分类号： B29C43/36 , B29C33/30 , B29C43/027 , B29C70/462 , B29K2105/08 , B29L2031/3076
摘要： A mold (30) and a method for molding high strength, non-metallic fiber reinforced composite parts having a variety of (e.g., cylindrical) shapes that are lighter in weight than similar parts manufactured from metal. An unmolded non-metallic pre-form (3) having long continuous fibers (9) is placed around a mandrel (1), and a segmented, adjustable diameter compression ring (40) is disposed in surrounding engagement with the pre-form (3) at an upper position within an inwardly tapered compression ring support (16). The compression ring (40) is formed from a plurality of loose compression ring segments (12) that are initially spaced circumferentially from one another at the upper position of the compression ring support. The mandrel (1) and the pre-form (3) are first heated and then located in a press. The press is closed to push the compression ring (40) and the heated mandrel (1) from the upper position of the compression ring support (16), at which the compression ring has an open configuration (FIG. 4) and a wide diameter, to a lower position, at which the compression ring has a closed configuration (FIG. 5) and a narrow diameter. As the compression ring (40) is pushed to the lower position, the compression ring segments (12) slide along the inwardly tapered compression ring support (16) so as to be moved end-to-end one another to apply a compressive force for consolidating and shaping the heated pre-form (3) into the molded part.
摘要翻译：一种模具（30）和用于模制具有多种（例如，圆柱形）形状的高强度非金属纤维增强复合材料部件的方法，其重量比由金属制成的类似部件重。具有长连续纤维（9）的未模塑的非金属预成型件（3）围绕心轴（1）放置，并且分段的可调直径的压缩环（40）被布置成与预成型件（3））在向内锥形的压缩环支撑件（16）内的上部位置。压缩环（40）由多个松散的压缩环段（12）形成，该压缩环段最初在压缩环支撑件的上部位置处彼此周向彼此间隔开。心轴（1）和预成型件（3）首先被加热然后位于压机中。压力机关闭以将压缩环（40）和加热的心轴（1）从压缩环支撑件（16）的上部位置推动，在该位置压缩环具有打开构型（图4）和宽直径压缩环具有闭合构型（图5）和较窄直径的较低位置。随着压缩环（40）被推到下部位置，压缩环段（12）沿着向内的锥形压缩环支撑件（16）滑动，以便彼此端对端地移动以对其施加压缩力将加热的预成型件（3）固结和成型成模制部件。

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