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131. 发明授权

US5690880A Process for the production of plastic material parts by controlled molding-thermoforming 失效
标题翻译：通过控制成型 - 热成型生产塑料材料零件的工艺
公开(公告)号：US5690880A
公开(公告)日：1997-11-25
申请号：US392891
申请日：1995-03-01
申请人： Fernand Le Coent
发明人： Fernand Le Coent
IPC分类号： B29C70/06 , A61F2/00 , A61F2/30 , A61F2/34 , A61F2/38 , B29C43/18 , B29C43/36 , B29C45/14 , B29C45/56 , B29C45/78 , B29C51/00 , B29C70/78 , B29C51/02 , B29C51/12
CPC分类号： A61F2/30965 , A61F2/30 , B29C43/184 , B29C43/361 , B29C45/1418 , B29C45/14778 , B29C45/561 , B29C70/78 , A61F2/3094 , A61F2/34 , A61F2/389 , A61F2002/30085 , A61F2002/30929 , B29C2043/3615 , B29C2043/3618 , B29C2045/14286 , B29C51/00 , B29K2105/0809 , B29K2995/0088 , B29L2031/7532
摘要： A process for the production of a plastic material part with a wear-resistant surface, having a predetermined nonplanar shape, comprising heating a blank of plastic material on a first side thereof opposite a second side on which it is desired to produce the wear-resistant surface, to adjacent the melting temperature of the plastic material, such that the temperature of the second side is substantially lower than the temperature of the first side. The blank thus heated on only the first side is introduced into a mold cavity, and is subjected to elevated pressure in the mold cavity with a surface of the mold cavity in contact with the second surface of the blank having a nonplanar shape complementary to the desired predetermined nonplanar shape of the second surface, thereby to impart to the second surface that predetermined shape while the second surface is at that substantially lower temperature. The surface of the mold cavity is produced either by extending a punch into the mold cavity in contact with the blank, or else the surface of the mold cavity is stationary and the blank is pressed into contact with the stationary surface of the mold cavity by pressure of a liquid, or both. The blank is of high molecular weight polyethylene having molecular chains oriented parallel to the second surface at least adjacent the second surface. The formed blank is for example an osteo implant such as a cotyle.
摘要翻译： PCT No.PCT / FR93 / 00844 Sec。 371 1995年3月1日 102（e）1995年3月1日PCT PCT 1993年3月9日PCT公布。公开号WO94 / 05481 日期1994年3月17日一种用于生产具有预定非平面形状的耐磨表面的塑料材料部件的方法，包括在其所期望的第二侧相对的第一侧上加热塑料材料坯料，产生相邻于塑料材料的熔化温度的耐磨表面，使得第二面的温度基本上低于第一面的温度。仅在第一侧上加热的坯料被引入模腔中，并且在模腔中承受升高的压力，模腔的表面与坯料的第二表面接触，其具有与期望的互补的非平面形状第二表面的预定非平面形状，从而在第二表面处于基本上较低的温度的同时赋予预定形状的第二表面。模腔的表面通过将冲头延伸到与坯料接触的模腔中来产生，或者模腔的表面是静止的，并且坯料通过压力被压在与模腔的固定表面接触的液体，或两者。空白是具有至少相邻于第二表面的分子链平行于第二表面定向的高分子量聚乙烯。所形成的坯料例如是骨盆植入物，例如cot骨。

132. 发明授权

US5688461A Method of molding a composite plastic article 失效
标题翻译：复合塑料制品的成型方法
公开(公告)号：US5688461A
公开(公告)日：1997-11-18
申请号：US542313
申请日：1995-10-12
申请人： Robert K. Howie, Jr.
发明人： Robert K. Howie, Jr.
IPC分类号： B29C45/16 , G05G1/10 , B29C45/14 , B29C70/78
CPC分类号： B29C45/1676 , G05G1/10 , Y10S16/19 , Y10T16/487 , Y10T74/2084
摘要： A method of molding a composite plastic article having a cylindrical transverse cross section. The method includes the steps of forming an inner core of a cylindrical transverse cross section having a longitudinally extending hub, an outer wall surrounding the hub and ribs extending between the hub and the outer wall. A plurality of openings are formed extending through the outer wall with the openings accessible between the hub and the outer wall. A soft, resilient plastic is injection molded through only one of the plurality of openings to form an outer covering on the outer wall and to fill the other openings which extend through the outer wall.
摘要翻译：一种模制具有圆柱形横截面的复合塑料制品的方法。该方法包括以下步骤：形成具有纵向延伸的毂的圆柱形横截面的内芯，围绕毂的外壁和在毂与外壁之间延伸的肋。多个开口形成为延伸穿过外壁，开口可在轮毂和外壁之间接近。柔软的弹性塑料仅通过多个开口中的一个开口注塑成型，以在外壁上形成外覆盖物并填充延伸穿过外壁的其它开口。

133. 发明授权

US5645670A Method for applying a skin layer to an airfoil structure 失效
标题翻译：将表皮层施加到翼型结构的方法
公开(公告)号：US5645670A
公开(公告)日：1997-07-08
申请号：US541669
申请日：1995-10-10
申请人： William C. Reinfelder , David A. Kovalsky , Corey D. Jones
发明人： William C. Reinfelder , David A. Kovalsky , Corey D. Jones
IPC分类号： B64C27/46 , B29C33/40 , B29C43/10 , B29C65/02 , B29C65/48 , B29C70/44 , B29C70/78 , B29C70/86 , B29D99/00 , B64C27/473 , B32B31/04
CPC分类号： B29D99/0025 , B29C70/44 , B29L2031/08 , Y10S425/044 , Y10T156/1028 , Y10T156/103
摘要： A fiberglass or other material skin is applied to a composite airfoil structure in a mold assembly having a partially compliant caul plate component which defines the shape of the lower surface of the airfoil. The caul plate component includes a first portion which is essentially rigid and which covers the leading edge of the airfoil. The rigid portion of the caul plate component provides improved conformation of the airfoil skin to the leading edge of the airfoil. The caul plate component also includes a compliant portion which covers and defines the shape of the trailing edge of the lower surface of the airfoil. The stiffness of the caul plate component also has a variable stiffness zone which interconnects the rigid and compliant portions thereof. The use of rigid and compliant portions on the caul plate provides for a controlled conformance of the skin to the leading edge of the airfoil, while allowing the skin to accurately conform to the remainder of the airfoil in spite of variations in the dimensions of internal operating components of the airfoil.
摘要翻译：将玻璃纤维或其它材料表皮施加到具有限定翼型件的下表面的形状的部分柔性挡板部件的模具组件中的复合翼型结构。刮板部件包括基本上刚性并且覆盖翼型件前缘的第一部分。挡板部件的刚性部分提供了翼型皮肤到翼型的前缘的改进构造。刮板部件还包括柔性部分，其覆盖并限定翼型件的下表面的后缘的形状。挡板部件的刚度还具有将刚性部分和柔性部分互连的可变刚度区域。在挡板上使用刚性和柔顺部分提供了皮肤对翼型前缘的受控一致性，同时允许皮肤准确地符合翼型的其余部分，尽管内部操作的尺寸有变化机翼的部件。

134. 发明授权

US5643504A Method of making a composite glass and resin optical element with an aspheric surface 失效
标题翻译：制造具有非球面的复合玻璃和树脂光学元件的方法
公开(公告)号：US5643504A
公开(公告)日：1997-07-01
申请号：US355006
申请日：1994-12-13
申请人： Toru Chiba
发明人： Toru Chiba
IPC分类号： G02B1/04 , B29C35/08 , B29C37/00 , B29C70/68 , B29C70/78 , B29D11/00 , B32B17/10 , G02B3/00 , G02B3/04 , G02B13/18
CPC分类号： B29C35/0888 , B29C37/0078 , B29C70/683 , B29C70/78 , B29D11/00019 , B29D11/0073 , B32B17/10018 , B32B17/10688 , G02B13/18 , B29C2035/0827 , B29L2011/0016
摘要： In order to provide an optical element with an aspheric surface, as well as a process by which the optical element can be mass-produced with high efficiency and consistent precision, the improved optical element with an aspheric surface includes a glass substrate and an overlying light-transmissive resin layer worked to have an aspheric surface. This optical element can be produced by molding a light-transmissive resin composition as it is cured between a glass substrate and a mold having an aspheric surfaced shape. The preferred light-transmissive resin has a Rockwell hardness of 40-80 on the M scale at -40.degree. C. to 60.degree. C.
摘要翻译：为了提供具有非球面的光学元件，以及可以以高效率和一致的精度大量生产光学元件的方法，具有非球面的改进的光学元件包括玻璃基板和上覆光 - 透明树脂层加工成具有非球面。该光学元件可以通过在透明树脂组合物在玻璃基板和具有非球面表面形状的模具之间固化的情况下模制来制造。优选的透光树脂在-40℃至60℃的M标度上具有40-80的洛氏硬度。

135. 发明授权

US5626704A Composite article of an automotive vehicle and method of making the same 失效
标题翻译：汽车的复合制品及其制造方法
公开(公告)号：US5626704A
公开(公告)日：1997-05-06
申请号：US540697
申请日：1995-10-11
申请人： Holton D. Bowers, Jr. , Stephen F. Lange
发明人： Holton D. Bowers, Jr. , Stephen F. Lange
IPC分类号： B29C45/00 , B29C45/14 , B29C51/00 , B29C65/02 , B29C69/02 , B29C70/78 , B60R13/04 , B29C43/18 , B29C43/20
CPC分类号： B60R13/04 , B29C45/14467 , B29C65/028 , B29C66/4724 , B29C66/7392 , B29C69/02 , B29C70/78 , B29C45/00 , B29C51/00 , B29C66/71 , B29L2031/302 , B29L2031/722 , Y10T428/14 , Y10T428/22 , Y10T428/24736
摘要： A composite article such as an automotive trim strip comprising a thermoplastic shell secured to the front of a supporting member. An icon is embedded in a recess in the front of the shell so that the front of the icon is substantially flush with the front of the shell. The icon is secured in the recess of the shell by an adhesive. The supporting member is made of a hot melt material and is bonded to the shell in an injection mold. The heat of the molding operation softens the thermoplastic shell sufficiently to cause the icon to form a recess in the shell and become embedded therein. The heat of the molding operation also cures the adhesive bonding the icon to the shell.
摘要翻译：一种复合制品，例如汽车装饰条，其包括固定到支撑构件前部的热塑性外壳。图标被嵌入在壳体前部的凹槽中，使得图标的前部与壳体的前部基本齐平。该图标通过粘合剂固定在壳体的凹槽中。支撑构件由热熔材料制成，并且在注射模具中结合到壳体。模制操作的热量使热塑性壳充分软化以使图标在壳体中形成凹陷并嵌入其中。模制操作的热量也固化粘合图标到外壳的粘合剂。

136. 发明授权

US5580621A Polyester backed acrylic composite molded structure and method of manufacturing thereof 失效
标题翻译：聚酯背衬丙烯酸复合成型结构体及其制造方法
公开(公告)号：US5580621A
公开(公告)日：1996-12-03
申请号：US164646
申请日：1993-12-08
申请人： Karl T. Kuszaj , Ronald D. Barndt , Jeffrey E. Willis
发明人： Karl T. Kuszaj , Ronald D. Barndt , Jeffrey E. Willis
IPC分类号： A47K3/04 , B29C70/02 , B29C70/48 , B29C70/60 , B29C70/78 , B29C70/86 , B29C39/12
CPC分类号： B29C70/025 , A47K3/04 , B29C70/026 , B29C70/48 , B29C70/603 , B29C70/78 , B29C70/86 , Y10T428/13 , Y10T428/1352 , Y10T428/31794 , Y10T428/31797
摘要： A polymeric composite structure having a polymeric shell layer with a finish-side and a non-finish side and a cross-linked thermosetting polymeric backing layer and method of manufacturing thereof is provided. The cross-linked thermosetting polymeric backing layer is simultaneously molded to conform to the shape of and bonded directly to essentially the entire non-finish side of the polymeric shell layer. The method includes forming the polymeric shell having a finish-side and non-finish side into a suitable shape, placing the shell into a mold, and introducing an uncured blended mixture of unsaturated thermosetting polymeric backing material and cross-linking promoter into the mold to force the backing material to directly coat the non-finish side of the shell. Curing the molded thermosetting polymeric backing material at a suitable temperature and sufficient time allows hardening and cross-linking of the thermosetting polymeric material and bonding directly to the non-finish side of the polymeric shell to permit demolding of the composite structure without damage.
摘要翻译：提供了一种聚合物复合结构，其具有具有精加工侧和非精加工侧的聚合物壳层和交联的热固性聚合物背衬层及其制造方法。交联的热固性聚合物背衬层同时模制成符合聚合物壳层的基本整个非整理面的形状并直接粘合到基体上。该方法包括将具有精加工侧和非精加工侧的聚合物壳体形成合适的形状，将壳体放置在模具中，以及将未固化的不饱和热固性聚合物背衬材料和交联促进剂的混合物引入模具中迫使背衬材料直接涂覆在外壳的未完成侧。在合适的温度和足够的时间固化模制的热固性聚合物背衬材料允许热固性聚合材料的硬化和交联并直接粘合到聚合物壳体的非终端侧，以允许复合结构的脱模而不损坏。

137. 发明授权

US5574623A Device panel with in-molded applique 失效
标题翻译：带嵌入式贴花的装置面板
公开(公告)号：US5574623A
公开(公告)日：1996-11-12
申请号：US395966
申请日：1995-02-28
申请人： Leland K. Girard
发明人： Leland K. Girard
IPC分类号： B29C33/00 , B29C70/78 , F24C7/08 , H01H13/702 , H02B15/00 , H02B1/04
CPC分类号： F24C7/082 , B29C33/0077 , B29C70/78 , H01H13/702 , H02B15/00 , H01H2223/002 , H01H2223/014 , H01H2229/048
摘要： A method of producing a molded assembly for at least partially encapsulating a touch panel structure. The method includes providing a touch panel structure which has a front side, a reverse side and an edge extending therebetween. A circuit is attached to the panel structure and includes at least one device. The panel is positioned in a cavity of a plastic injection mold which includes a hollow shutoff positioned relative to the device on the touch panel. When the mold is closed, a rim portion of the hollow shutoff is positioned against the reverse side of the panel spaced away from the device so as to at least partially shield the portion of the panel containing the device from the injection molding environment. The present invention also envisions a product produced by this method. The present invention further envisions a molded assembly which includes a touch panel in which the touch panel is retained in a molded portion and the devices associated with the touch panel are not degraded during the molding process. A window is provided on the reverse side of the touch panel. Additionally, a barrier material may be applied to the reverse side of the panel prior to molding so as to form a seal between the molded portion and the touch panel in the area of the window positioned relative to the device.
摘要翻译：一种生产用于至少部分地封装触摸面板结构的模制组件的方法。该方法包括提供具有正面，反面和在其之间延伸的边缘的触摸面板结构。电路附接到面板结构并且包括至少一个设备。该面板位于塑料注射模具的空腔中，其包括相对于触摸面板上的装置定位的空心截止。当模具关闭时，空心关闭的边缘部分被定位成抵靠与该装置间隔开的面板的相反侧，以至少部分地将包含该装置的面板的部分与注射成型环境屏蔽。本发明还设想通过该方法生产的产品。本发明还设想一种模制组件，其包括触摸面板，触摸面板保持在模制部分中，并且与模制部件相关联的装置在模制过程中不会降级。在触摸面板的背面设有一个窗口。此外，阻挡材料可以在模制之前施加到面板的相反侧，以便在相对于装置定位的窗口的区域中在模制部分和触摸面板之间形成密封。

138. 发明授权

US5543094A Method of forming a multilayer molded article 失效
标题翻译：形成多层成型体的方法
公开(公告)号：US5543094A
公开(公告)日：1996-08-06
申请号：US395190
申请日：1995-02-27
申请人： Takahisa Hara , Masahito Matsumoto , Nobuhiro Usui , Shigeyoshi Matubara
发明人： Takahisa Hara , Masahito Matsumoto , Nobuhiro Usui , Shigeyoshi Matubara
IPC分类号： B29C43/00 , B29C43/18 , B29C43/20 , B29C51/08 , B29C51/14 , B29C51/26 , B29C70/68 , B29C70/78 , B29L9/00 , B29L31/58 , B32B5/02 , B32B27/12 , B32B37/10 , B29C44/14 , B29C45/14 , B29C70/48
CPC分类号： B29C70/682 , B29C43/184 , B29C70/78 , B29C43/00 , B29C51/08 , B29C51/145 , B29C51/262 , B29L2009/00 , B29L2031/3005 , Y10T428/23979 , Y10T428/249958 , Y10T428/249987 , Y10T428/249991 , Y10T428/249992 , Y10T442/3325 , Y10T442/335 , Y10T442/3358
摘要： A method of forming a multilayer molded article with improved appearance having a core of a thermoplastic resin and a skin material laminated on the resin core, in which the skin material is made of a fabric which is lined with a nonwoven fabric having a weight of at least 50 g/m.sup.2 and an elongation at break of 20% to 80% and optionally has an intermediate foam layer between the fabric and the nonwoven fabric.
摘要翻译：一种形成具有改进外观的多层成型体的方法，其具有层压在树脂芯上的热塑性树脂和表层材料的芯，其中表层材料由衬里为织物的织物制成，该织物内衬有重量为至少50g / m 2，断裂伸长率为20％至80％，并且任选地在织物和非织造织物之间具有中间泡沫层。

139. 发明授权

US5528828A Methods for fabricating a helicopter main rotor blade 失效
标题翻译：制造直升机主转子叶片的方法
公开(公告)号：US5528828A
公开(公告)日：1996-06-25
申请号：US445627
申请日：1995-05-22
申请人： Kevin P. Leahy , Corey D. Jones
发明人： Kevin P. Leahy , Corey D. Jones
IPC分类号： B64C27/46 , B29C70/44 , B29C70/78 , B29C70/86 , B29D99/00 , B64C27/473 , B64F5/00 , B23P15/00
CPC分类号： B29D99/0028 , B29C70/446 , B29C70/78 , B29C70/86 , B64C27/473 , B29L2031/082 , B64C2027/4736 , Y10T29/37 , Y10T29/49332 , Y10T29/53026 , Y10T29/53539 , Y10T29/5397
摘要： A method for fabricating a helicopter main rotor blade includes a compaction fixture for assembling and compacting blade subassembly components and a sheath spreading/insertion apparatus for spreading and inserting a leading-edge sheath onto the blade subassembly during the compaction process. The compaction fixture includes a lower assembly having a contoured upper airfoil nest mounted in combination with a support structure and an upper assembly having a pressure bag affixed in sealed combination to a contoured backplate affixed in combination to a structural support truss. The contoured upper airfoil nest includes a plurality of tooling pins for locating an upper composite skin in aligned combination on the contoured upper airfoil nest and a plurality of pusher pins for chordwise alignment of a spar assembly in the contoured upper airfoil nest. Spar stanchions affixed to the support structure provide spanwise alignment of the spar assembly in the contoured upper airfoil nest. With the upper and lower assemblies in locked combination, the pressure bag is pressurized to compact the assembled blade subassembly components.
摘要翻译：一种用于制造直升机主转子叶片的方法包括用于组装和压实叶片组件部件的压实夹具和用于在压实过程中将前缘护套分散并插入到叶片子组件上的护套扩展/插入装置。压实夹具包括下部组件，其具有与支撑结构组合安装的轮廓上部翼型嵌套，以及具有与密封组合固定到与结构支撑桁架组合的轮廓背板的压力袋的上部组件。成型的上翼型嵌套包括多个工具销，用于将上复合材料表层以对准的组合定位在成型的上翼型嵌套上，以及多个推杆，用于在轮廓上的翼型嵌套中翼弦对准。固定到支撑结构的翼梁支柱提供了翼型组件在成型的上翼型嵌套中的翼展对准。通过将上部和下部组件锁定组合，压力袋被加压以压缩组装的叶片子组件部件。

140. 发明授权

US5525283A Method for producing flat, laminated moldings by back-embossing according to the preform method 失效
标题翻译：根据预成型方法通过背压印制造平面层压模制品的方法
公开(公告)号：US5525283A
公开(公告)日：1996-06-11
申请号：US334691
申请日：1994-11-04
申请人： Albert Nicolay
发明人： Albert Nicolay
IPC分类号： B29C45/14 , B29C43/14 , B29C43/18 , B29C45/00 , B29C59/00 , B29C69/00 , B29C70/78 , B29C45/16
CPC分类号： B29C45/0416 , B29C43/145 , B29C43/184 , B29C45/0053 , B29C45/14221 , B29C69/004 , B29C70/78 , B29C2043/525 , B29C2045/0079 , B29C2045/14237
摘要： A method for the production of laminated moldings, such as internal linings or panellings of motor vehicles and the like, and dimensionally stable parts in which a support part is provided with a surface lamination and in which initially a preform having the same volume as the support part, but not having the same surface area with respect to the final shaping, is produced. Utilizing the inherent production heat, the preform is then connected by pressure action to the lamination by back-embossing with the thermoplastic material of the support part and is given its final shape by material flow processes. The invention improves back-embossing in the production of laminated moldings in such a way that with reduced embossing forces the surface-unitary adhesion of the lamination to the support part is improved and the risk of bubble formation is eliminated. This is achieved in that preforms identical in volume to that of the support part and having the same contour shapes as the finished laminated molding and with a lattice-like structure at least in partial areas are subject to the material flow process so that the initially open lattice meshes of the preform are closed by local flow with the pressure application for the back-embossing process.
摘要翻译：用于制造层压模制品的方法，例如机动车辆的内衬或拼板等，以及尺寸稳定的部件，其中支撑部分设置有表面层压，并且其中最初具有与支撑件相同的体积的预成型件产生相对于最终成型而没有相同表面积的部分。利用固有的生产热量，然后通过用支撑部件的热塑性材料进行背压印，通过压力作用将预成型件连接到层压件上，并通过材料流动方法给予其最终形状。本发明改进了层压模制品生产中的背压纹，使得通过减小的压印力，层压体与支撑部分的表面一体粘合得到改善，并且消除了气泡形成的风险。这是通过以下方式实现的：预成型件的体积与支撑部件的体积相同，并且具有与成品层压成型相同的轮廓形状，并且至少在部分区域中的格子状结构受到材料流动过程的影响，使得初始打开通过用于背压花加工的压力施加的局部流动将预成型件的格子网格闭合。

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