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31. 发明授权

US5847375A Fastenerless bonder wingbox 失效
标题翻译：紧固件粘接机翼箱
公开(公告)号：US5847375A
公开(公告)日：1998-12-08
申请号：US685059
申请日：1996-07-19
申请人： Marc R. Matsen , Douglas A. McCarville , Michael M. Stepan
发明人： Marc R. Matsen , Douglas A. McCarville , Michael M. Stepan
IPC分类号： B21D26/055 , B22F3/105 , B29C33/06 , B29C35/08 , B29C65/00 , B29C65/34 , B29C65/36 , B29C70/44 , B29C70/54 , B64C3/18 , H05B6/02 , H05B6/14 , H05B6/36 , H05B6/10
CPC分类号： C22C47/068 , B21D26/055 , B22F3/105 , B29C33/06 , B29C65/34 , B29C65/364 , B29C65/3644 , B29C66/634 , B29C66/721 , B29C66/7392 , B29C66/91411 , B29C66/91443 , B29C66/91645 , B29C66/91655 , B29C66/91951 , B29C70/44 , B29C70/542 , B64C3/18 , H05B6/365 , B22F2003/1046 , B22F2003/1053 , B22F2998/00 , B29C2035/0811 , B29C65/3476 , B29C65/3492 , B29C65/3676 , B32B2309/62 , Y02P10/253 , Y02T50/433
摘要： Rib and spar webs are joined in a composite wingbox to eliminate fasteners by welding the webs along bond lines defined by overlapping sections of the webs. Heat to produce the weld is generally achieved resistively by connecting a multistrip susceptor positioned along the bond line to a current source, since the geometry makes it difficult to heat these web joints inductively. The wingbox is completed without fasteners by welding skins to the rib-spar wingbox.
摘要翻译：肋和翼梁腹板连接在复合翼箱中，以通过沿腹板的重叠部分限定的接合线焊接腹板来消除紧固件。通常通过将沿着接合线定位的多脚架基座连接到电流源来实现焊接的热量，因为几何形状使得难以感应地加热这些纤维网接头。翼形框架通过将表皮焊接到肋翼翼箱而完成无紧固件。

32. 发明授权

US4913910A Apparatus for forming laminate into a predetermined configuration 失效
标题翻译：用于将层压制成预定构型的装置
公开(公告)号：US4913910A
公开(公告)日：1990-04-03
申请号：US209986
申请日：1988-06-22
申请人： Douglas A. McCarville , Dennis C. Rocheleau
发明人： Douglas A. McCarville , Dennis C. Rocheleau
IPC分类号： B29C53/04
CPC分类号： B32B38/00 , B29C53/04 , B29C53/043
摘要： Apparatus for forming elongate laminate into a predetermined configuration having a substantially uniform cross-sectional shape in the axial direction, including a plurality of roller pairs having complementary transverse peripheral profiles, plate members disposed between the roller pairs and the laminate and having a transverse configuration corresponding to the peripheral profiles of the rollers.
摘要翻译：用于将细长层压体形成为在轴向上具有基本上均匀横截面形状的预定构造的装置，包括具有互补的横向周边轮廓的多个辊对，设置在辊对之间的板构件和层压板，并且具有相应的横向构型到辊子的周边轮廓。

33. 发明授权

US08446330B1 Antenna fabrication 有权
标题翻译：天线制造
公开(公告)号：US08446330B1
公开(公告)日：2013-05-21
申请号：US12693672
申请日：2010-01-26
申请人： Douglas A. McCarville , Joseph A. Marshall , Manny S. Urcia , Otis F. Layton
发明人： Douglas A. McCarville , Joseph A. Marshall , Manny S. Urcia , Otis F. Layton
IPC分类号： H01Q21/26
CPC分类号： H01Q21/26 , H01Q21/0087 , H01Q21/064 , Y10T29/49002 , Y10T29/49016
摘要： In one embodiment a method to form a load bearing antenna aperture comprises forming a honeycomb core structure having a plurality of wall sections, the wall sections including electromagnetic radiating elements, and wherein lower surfaces of the wall sections defines a first surface and upper surfaces of the wall sections define a second surface, positioning a back skin to the first surface of the honeycomb core structure with an adhesive layer which comprises a layer of adhesive film and a paste adhesive disposed on the layer of adhesive film. Other embodiments are disclosed.
摘要翻译：在一个实施例中，形成承载天线孔的方法包括形成具有多个壁部的蜂窝芯结构，所述壁部包括电磁辐射元件，并且其中所述壁部的下表面限定所述第一表面和壁部分限定第二表面，将背部皮肤定位在蜂窝芯结构的第一表面上，其中粘合剂层包括一层粘合剂膜和设置在粘合剂膜层上的糊状粘合剂。公开了其他实施例。

34. 发明申请

US20110097554A1 CURVED COMPOSITE FRAMES AND METHOD OF MAKING THE SAME 有权
标题翻译：弯曲复合框架及其制造方法
公开(公告)号：US20110097554A1
公开(公告)日：2011-04-28
申请号：US12776781
申请日：2010-05-10
申请人： David J. Kehrl , Kent E. Johnson , Douglas A. McCarville
发明人： David J. Kehrl , Kent E. Johnson , Douglas A. McCarville
IPC分类号： B32B1/00 , B23P17/00 , B23P11/00
CPC分类号： B64C1/061 , B29C70/207 , B29C70/30 , B29C70/38 , B29D99/0003 , B29L2031/3082 , B64C1/064 , B64C2001/0072 , Y02T50/43 , Y10T29/49622 , Y10T29/49801 , Y10T29/49826 , Y10T428/24628
摘要： A curved composite aircraft frame comprises a multi-ply composite laminate having a generally Z-shaped cross section. At least certain of the laminate plies include unidirectional reinforcing fibers that are substantially tangent at substantially all points along the curvature of the frame.
摘要翻译：弯曲的复合飞机框架包括具有大致Z形横截面的多层复合层压板。至少某些层压板包括在沿着框架的曲率的基本上所有点处基本上切线的单向增强纤维。

35. 发明授权

US06284089B1 Thermoplastic seam welds 失效
标题翻译：热塑性焊缝
公开(公告)号：US06284089B1
公开(公告)日：2001-09-04
申请号：US09120500
申请日：1998-07-21
申请人： David M. Anderson , Steven E. Hahn , Douglas A. McCarville
发明人： David M. Anderson , Steven E. Hahn , Douglas A. McCarville
IPC分类号： B29C6502
CPC分类号： B29C65/5014 , B29C65/3644 , B29C65/368 , B29C65/4815 , B29C65/483 , B29C65/5021 , B29C65/5042 , B29C66/0344 , B29C66/1142 , B29C66/12443 , B29C66/139 , B29C66/301 , B29C66/3472 , B29C66/43 , B29C66/438 , B29C66/524 , B29C66/5326 , B29C66/54 , B29C66/71 , B29C66/721 , B29C66/7212 , B29C66/72141 , B29C66/72525 , B29C66/73116 , B29C66/73921 , B29C66/7394 , B29C66/81423 , B29C66/81821 , B29C66/8242 , B29C66/83221 , B29C66/836 , B29K2101/12 , B29L2031/608 , B29L2031/7156 , B64F5/10 , F17C1/16 , F17C2201/0109 , F17C2203/0629 , F17C2203/0631 , F17C2203/0636 , F17C2203/0646 , F17C2203/0651 , F17C2203/066 , F17C2203/0663 , F17C2209/221 , F17C2209/232 , Y10T428/236 , Y10T428/24149 , Y10T428/24157 , B29K2309/08 , B29K2307/04 , B29K2277/00 , B29K2071/00 , B29K2079/085 , B29K2081/06 , B29K2063/00 , B29K2081/04
摘要： The present invention is a method for joining thermoplastic composite sandwich panels with thermoplastic welds (fusion bonds) made without autoclave processing of the joint. The preferred joint is a double interleaf staggered joint with supporting titanium doublers providing a tensile strength of at least 12,000 lb/in. The joint is particularly suited for joining sections of a cryogenic tank for spacecraft.
摘要翻译：本发明是一种将热塑性复合夹层板与不用接头高压灭菌处理制成的热塑性焊接（熔接）接合的方法。优选的接头是具有支撑钛倍增器的双层交错交错接头，其提供至少12,000lb / in的拉伸强度。接头特别适用于连接用于航天器的低温储罐的部分。

36. 发明授权

US6040563A Bonded assemblies 失效
标题翻译：保固组件
公开(公告)号：US6040563A
公开(公告)日：2000-03-21
申请号：US995387
申请日：1997-12-22
申请人： Marc R. Matsen , Douglas A. McCarville
发明人： Marc R. Matsen , Douglas A. McCarville
IPC分类号： B21D26/02 , B22F3/105 , B22F3/18 , B23K1/002 , B23K20/02 , B29C33/06 , B29C33/60 , B29C35/08 , B29C43/36 , B29C65/00 , B29C65/32 , B29C65/34 , B29C65/36 , B29C65/48 , B29C70/44 , B29C70/50 , B29C70/54 , B64C3/18 , C22C47/00 , C22C47/20 , H05B6/02 , H05B6/14 , H05B6/36 , H05B6/10
CPC分类号： B22F3/105 , B21D26/02 , B21D26/021 , B21D26/025 , B21D26/029 , B21D26/053 , B21D26/055 , B22F3/18 , B23K1/002 , B23K20/023 , B29C33/06 , B29C33/60 , B29C35/08 , B29C43/3642 , B29C43/52 , B29C65/14 , B29C65/18 , B29C65/32 , B29C65/34 , B29C65/3644 , B29C65/3676 , B29C65/4815 , B29C65/4835 , B29C66/0342 , B29C66/5346 , B29C66/54 , B29C66/634 , B29C66/721 , B29C66/7254 , B29C66/73921 , B29C66/73941 , B29C66/8122 , B29C66/81261 , B29C66/81811 , B29C66/81821 , B29C66/8322 , B29C70/44 , B29C70/506 , B29C70/542 , B32B37/06 , B64C3/18 , B64C3/185 , C22C47/00 , C22C47/068 , C22C47/20 , H05B6/365 , B22F2003/1046 , B22F2003/1053 , B22F2998/00 , B23K2201/18 , B29C2035/0811 , B29C2043/3233 , B29C2043/3655 , B29C33/08 , B29C65/3476 , B29C65/3668 , B29C65/368 , B29C66/53462 , B29C66/71 , B29C66/7212 , B29K2105/0854 , B32B2305/024 , B32B2309/62 , B32B2310/0812 , C09K2205/12 , Y02P10/253 , Y02P20/124 , Y02T50/433
摘要： The processing time and energy efficiency of metal or composite bonding operations is improved by heating the lay-up preform of the structure in an induction heating press where energy goes primarily to heating the workpieces rather than to heating the tooling or being lost to the environment. The bonding process is especially beneficial for joining thermoplastic composites, but it also can be used with metals or thermosets. Preferential heating at the bondline is achieved by using shims to define the bondline and to define bead regions that have relief from contact with the susceptor envelope because of the thickness of the shims in the bondline regions.
摘要翻译：通过在感应加热压机中加热结构的叠层预制件来改善金属或复合粘合操作的处理时间和能量效率，其中能量主要用于加热工件，而不是加热工具或丢失到环境中。接合方法对于接合热塑性复合材料是特别有益的，但也可以与金属或热固性材料一起使用。通过使用垫片来限定粘合线并且限定由于粘合线区域中的垫片的厚度而能够缓解与基座包层接触的胎圈区域，从而实现了粘合线上的优先加热。

37. 发明授权

US5968445A Method and apparatus for curing large composite panels 失效
标题翻译：固化大型复合板的方法和装置
公开(公告)号：US5968445A
公开(公告)日：1999-10-19
申请号：US2685
申请日：1998-01-05
申请人： Douglas A. McCarville , David F. Taylor
发明人： Douglas A. McCarville , David F. Taylor
IPC分类号： B29C70/44
CPC分类号： B29C70/44 , B29C2043/3657
摘要： A method and apparatus for curing large composite parts. The method utilizes a fiber metal mesh sheet (40) situated against a composite material(34) during a curing process. The fiber metal mesh sheet (40) provides a porous network for flow of the reaction by-products during a curing and vacuuming process, yet gives adequate structure to prevent both mark-off by vacuum ports (52, 70) and crushing of the porous network as a result of autoclave and vacuum pressure. External vacuum ports (52) are located in a bagging film (50) surrounding the composite material (34). Alternatively, vacuum ports (70) are located below the composite material (34). The use of the external vacuum ports (52), vacuum ports (70) located beneath the composite material (34), or both, shortens by-product flow path and provides adequate vacuum pressure over all areas of the composite material (34) to remove reaction by-products.
摘要翻译：一种固化大型复合材料零件的方法和装置。该方法利用在固化过程中位于复合材料（34）上的纤维金属网片（40）。纤维金属网片（40）为固化和抽真空过程中的反应副产物流提供了一个多孔网络，但提供了足够的结构，以防止真空口（52,70）的两个标记和多孔由于高压灭菌和真空压力，网络化。外部真空端口（52）位于围绕复合材料（34）的袋装薄膜（50）中。或者，真空端口（70）位于复合材料（34）的下方。使用位于复合材料（34）下方的外部真空端口（52），真空端口（70）或两者，缩短副产物流动路径并且在复合材料（34）的所有区域上提供足够的真空压力至去除反应副产物。

38. 发明授权

US5793024A Bonding using induction heating 失效
标题翻译：使用感应加热接合
公开(公告)号：US5793024A
公开(公告)日：1998-08-11
申请号：US468116
申请日：1995-06-06
申请人： Marc R. Matsen , Douglas A. McCarville
发明人： Marc R. Matsen , Douglas A. McCarville
IPC分类号： B21D26/02 , B22F3/105 , B22F3/18 , B23K1/002 , B23K20/02 , B29C33/06 , B29C33/60 , B29C35/08 , B29C43/36 , B29C65/00 , B29C65/32 , B29C65/34 , B29C65/36 , B29C65/48 , B29C70/44 , B29C70/50 , B29C70/54 , B64C3/18 , C22C47/00 , C22C47/20 , H05B6/02 , H05B6/14 , H05B6/36 , H05B6/10
CPC分类号： B22F3/105 , B21D26/02 , B21D26/021 , B21D26/025 , B21D26/029 , B21D26/053 , B21D26/055 , B22F3/18 , B23K1/002 , B23K20/023 , B29C33/06 , B29C33/60 , B29C35/08 , B29C43/3642 , B29C43/52 , B29C65/14 , B29C65/18 , B29C65/32 , B29C65/34 , B29C65/3644 , B29C65/3676 , B29C65/4815 , B29C65/4835 , B29C66/0342 , B29C66/5346 , B29C66/54 , B29C66/634 , B29C66/721 , B29C66/7254 , B29C66/73921 , B29C66/73941 , B29C66/8122 , B29C66/81261 , B29C66/81811 , B29C66/81821 , B29C66/8322 , B29C70/44 , B29C70/506 , B29C70/542 , B32B37/06 , B64C3/18 , B64C3/185 , C22C47/00 , C22C47/068 , C22C47/20 , H05B6/365 , B22F2003/1046 , B22F2003/1053 , B22F2998/00 , B23K2201/18 , B29C2035/0811 , B29C2043/3233 , B29C2043/3655 , B29C33/08 , B29C65/3476 , B29C65/3668 , B29C65/368 , B29C66/53462 , B29C66/71 , B29C66/7212 , B29K2105/0854 , B32B2305/024 , B32B2309/62 , B32B2310/0812 , C09K2205/12 , Y02P10/253 , Y02P20/124 , Y02T50/433
摘要： The processing time and energy efficiency of metal or composite bonding operations is improved by heating the lay-up preform of the structure in an induction heating press where energy goes primarily to heating the workpieces rather than to heating the tooling or being lost to the environment. The bonding process is especially beneficial for joining thermoplastic composites, but it also can be used with metals or thermosets. Preferential heating at the bondline is achieved by using shims to define the bondline and to define bead regions that have relief from contact with the susceptor envelope because of the thickness of the shims in the bondline regions.
摘要翻译：通过在感应加热压机中加热结构的叠层预制件来改善金属或复合粘合操作的处理时间和能量效率，其中能量主要用于加热工件，而不是加热工具或丢失到环境中。接合方法对于接合热塑性复合材料是特别有益的，但也可以与金属或热固性材料一起使用。通过使用垫片来限定粘合线并且限定由于粘合线区域中的垫片的厚度而能够缓解与基座包层接触的胎圈区域，从而实现了粘合线上的优先加热。

39. 发明授权

US5268055A Method for making perforated composite laminates 失效
标题翻译：穿孔复合层压板的制造方法
公开(公告)号：US5268055A
公开(公告)日：1993-12-07
申请号：US786157
申请日：1991-10-31
申请人： John L. Bales , Daniel A. Buchacher , Clint A. Luttgeharm , Douglas A. McCarville
发明人： John L. Bales , Daniel A. Buchacher , Clint A. Luttgeharm , Douglas A. McCarville
IPC分类号： B29C33/00 , B29C35/02 , B29C43/32 , B29C70/34 , B29C43/02
CPC分类号： B29C70/545 , B29C33/0033 , B29C35/0222 , B29C43/32 , B29C70/34 , B29C2791/008 , B29C2793/0045 , Y10T156/1056 , Y10T156/1057 , Y10T156/1304
摘要： A novel method and apparatus are provided for consolidating and perforating multilayer laminates by a combination of vibratory motion and impacting pressure applied by a special compacting tool preparatory to final cure.
摘要翻译：提供了一种新颖的方法和装置，用于通过振动运动和通过专门的压实工具施加的冲击压力的组合来整合和穿孔多层层压材料，以准备最终固化。

40. 发明授权

US08784596B2 Method for making and joining composite sandwich shell edge joint 有权
标题翻译：复合夹心壳边缘接头的制作与连接方法
公开(公告)号：US08784596B2
公开(公告)日：2014-07-22
申请号：US12950191
申请日：2010-11-19
申请人： Michael Leslie Hand , Douglas A. McCarville , Juan Carlos Guzman
发明人： Michael Leslie Hand , Douglas A. McCarville , Juan Carlos Guzman
IPC分类号： B28B7/20
CPC分类号： B32B38/1866 , B29C66/5221 , B29C66/5241 , B29C66/721 , B29C66/72523 , B29C70/46 , Y10T403/553
摘要： A method for joining fittings to a composite sandwich shell edge includes laying up an inner facesheet and positioning a wrapped flute mandrel on top; applying a layer of adhesive on the inner facesheet and positioning spacer-supported fittings on top; applying adhesive over the co-bonded fittings and laying up an outer facesheet forming an assembly; curing the assembly under heat and pressure; removing the fittings by first collapsing the spacers and removing the flute mandrel; placing an adhesive layer on the fittings with collapsible spacers inserted therein; reinserting the fittings between the inner and outer facesheets and effecting bonding and curing; and removing the spacers from the fittings by collapsing the spacers.
摘要翻译：将配件连接到复合夹层壳边缘的方法包括铺设内面板并将包裹的长槽心轴定位在顶部; 在内面板上施加一层粘合剂并将间隔件支撑的配件定位在顶部; 将粘合剂涂覆在共接合配件上并铺设形成组件的外面板; 在热和压力下固化组件; 通过首先塌缩间隔件并移除槽纹心轴来移除配件; 将粘合剂层放置在具有插入其中的可折叠间隔件的配件上; 将接头重新插入内外面板之间，实现粘结和固化; 以及通过使间隔件折叠从配件中移除间隔件。

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