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公开(公告)号：US06979807B2
公开(公告)日：2005-12-27
申请号：US10640188
申请日：2003-08-13
申请人： Donald A. Anderson , Ronald W. Brown , Brad L. Kirkwood , Marc R. Matsen , Douglas A. McCarville , Stephen G. Moore
发明人： Donald A. Anderson , Ronald W. Brown , Brad L. Kirkwood , Marc R. Matsen , Douglas A. McCarville , Stephen G. Moore
IPC分类号： B29C33/04 , B29C33/06 , B29C35/08 , B29C35/16 , B29C70/44 , B29C70/54 , H05B6/02 , H05B6/14 , H05B6/10
CPC分类号： B29C33/06 , B29C33/04 , B29C33/046 , B29C35/0805 , B29C70/44 , B29C70/54 , B29C2035/0811 , B29C2035/1616 , H05B6/105 , H05B2206/023
摘要： An apparatus and method for forming a composite workpiece are provided. An electromagnetic field generator induces a current in a susceptor, thereby heating the workpiece in a die cavity. An elastomeric bladder in the cavity is inflated and urges the workpiece against a contour surface corresponding to a desired configuration of the workpiece. Coolant fluid can also be circulated through the die cavity to cool the workpiece. Thus, the workpiece can be heated, formed, and cooled quickly and without substantial heating of other components, thereby reducing the time and energy relative to conventional forming methods.
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公开(公告)号：US07102112B2
公开(公告)日：2006-09-05
申请号：US11181071
申请日：2005-07-14
申请人： Donald A. Anderson , Ronald W. Brown , Brad L. Kirkwood , Marc R. Matsen , Douglas A. McCarville , Stephen G. Moore
发明人： Donald A. Anderson , Ronald W. Brown , Brad L. Kirkwood , Marc R. Matsen , Douglas A. McCarville , Stephen G. Moore
IPC分类号： H05B6/10
CPC分类号： B29C33/06 , B29C33/04 , B29C33/046 , B29C35/0805 , B29C70/44 , B29C70/54 , B29C2035/0811 , B29C2035/1616 , H05B6/105 , H05B2206/023
摘要： An apparatus and method for forming a composite workpiece are provided. An electromagnetic field generator induces a current in a susceptor, thereby heating the workpiece in a die cavity. An elastomeric bladder in the cavity is inflated and urges the workpiece against a contour surface corresponding to a desired configuration of the workpiece. Coolant fluid can also be circulated through the die cavity to cool the workpiece. Thus, the workpiece can be heated, formed, and cooled quickly and without substantial heating of other components, thereby reducing the time and energy relative to conventional forming methods.
摘要翻译： 提供一种用于形成复合工件的装置和方法。 电磁场发生器感应基座中的电流，从而在模腔中加热工件。 空腔中的弹性体囊被充气并且将工件推向对应于工件的期望构造的轮廓表面。 冷却液也可以通过模腔循环，以冷却工件。 因此，可以快速地加热，形成和冷却工件，并且不会对其它部件进行大量加热，从而相对于常规成形方法减少时间和能量。
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3.发明授权Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections 有权飞机机身和其他结构的复合部分，以及制造这些部分的方法和系统公开(公告)号：US08168023B2
公开(公告)日：2012-05-01
申请号：US12367479
申请日：2009-02-06
申请人： Michael R. Chapman , Robert M. Watson , Donald A. Anderson , Marc J. Piehl , Joseph L. Sweetin , Douglas L. Grose
发明人： Michael R. Chapman , Robert M. Watson , Donald A. Anderson , Marc J. Piehl , Joseph L. Sweetin , Douglas L. Grose
CPC分类号： B29C70/323 , B29C70/386 , B29D99/0014 , B29L2031/3082 , B64C1/068 , B64C1/12 , B64F5/10 , Y02T50/43 , Y10T156/1028 , Y10T156/1348 , Y10T156/1702 , Y10T156/1754 , Y10T156/1788 , Y10T156/1795
摘要： Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections, are disclosed herein. A method for manufacturing a shell structure in accordance with one embodiment of the invention includes applying composite material to an interior mold surface of a tool to form a skin extending 360 degrees around an axis. The method can further include positioning a plurality of stiffeners on an inner surface of the skin. After the stiffeners have been positioned, a vacuum bag can be installed over the stiffeners and evacuated to press the stiffeners and the skin outwardly against the interior mold surface of the tool. Next, the skin/stiffener combination can be cocured to bond the stiffeners to the skin and harden the shell structure.
摘要翻译： 本文公开了用于飞机机身和其他结构的复合部分，以及用于制造这种部分的方法和系统。 根据本发明的一个实施例的用于制造壳结构的方法包括将复合材料施加到工具的内部模具表面以形成围绕轴线360度延伸的皮肤。 该方法还可以包括将多个加强件定位在皮肤的内表面上。 在加强件已经定位之后，真空袋可以安装在加强件的上方并抽真空以将加强件和皮肤向外压靠在工具的内部模具表面上。 接下来，可以将皮肤/加强件组合物共固化以将加强件粘合到皮肤上并硬化壳体结构。
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公开(公告)号：US20080290208A1
公开(公告)日：2008-11-27
申请号：US11829536
申请日：2007-07-27
IPC分类号： B65H35/00
CPC分类号： B65H18/103 , B65H2301/5111 , B65H2301/5151 , B65H2301/5152 , B65H2301/543 , B65H2701/377 , Y10T156/1052 , Y10T156/108 , Y10T156/1174 , Y10T156/1195 , Y10T156/12 , Y10T156/195 , Y10T156/1956 , Y10T156/1978 , Y10T156/1983 , Y10T156/1994
摘要： In one embodiment, an apparatus is provided for preparing a cassette spool. The apparatus includes: a supply reel for supplying and unrolling tape material on original backing paper; at least one cutting member for cutting unrolled tape material while on original backing paper; a cutting surface defined in a plane; a pivoting path member adapted to move from a first position aligned in the plane to a second position aligned at least partially out of the plane; at least one removing member for removing uncut unrolled tape material from original backing paper; and a cassette spool for rolling up unrolled cut tape material on original backing paper. In further embodiments, methods are provided for preparing a cassette spool with cut tape material on original backing paper.
摘要翻译： 在一个实施例中，提供了一种用于准备盒式卷轴的装置。 该设备包括：用于在原始背纸上提供和展开胶带材料的供带盘; 至少一个用于在原始背纸上切割展开的带材的切割构件; 在平面中限定的切割表面; 枢转路径构件，其适于从在所述平面中对准的第一位置移动到至少部分地离开所述平面的第二位置; 至少一个去除构件，用于从原始背衬纸去除未切割的未卷曲的带材料; 以及用于在原始背纸上卷起展开的切割胶带材料的盒式卷轴。 在另外的实施例中，提供了用于在原始背衬纸上制备具有切割带材料的盒式卷轴的方法。
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公开(公告)号：US5077106A
公开(公告)日：1991-12-31
申请号：US416650
申请日：1989-10-03
CPC分类号： B29C31/002 , B29C53/42 , B29C63/0047 , B29C63/14 , B29C63/30 , B29C65/78 , B29C66/4322 , B29C66/45 , B29C66/49 , B29C66/71 , B29C66/7212 , B29C66/7394 , F16L57/06 , Y10T428/1359
摘要： Methods are provided for lining and wrapping both interior and exterior surfaces of tubular structures with materials that protect the underlying structures from adverse environmental conditions, provide a thermal control coating and prevent exchanging moisture with the surrounding environments. The methods use adhesives to securely position the lining or wrapping material inside or around the exterior of the tubular structure. The adhesives prevent the formation of discontinuities in the protective layer provided by the lining or wrapping material by holding the protective materials in place during the fabrication process. The wrapping materials are sealed by an ultrasonically welded seam to prevent environmental attack through the seam to the underlying tubular structure.
摘要翻译： 提供了用于将管状结构的内表面和外表面衬里和包裹的材料与保护下面的结构免受恶劣环境条件的材料，提供热控制涂层并防止与周围环境交换湿气的方法。 该方法使用粘合剂将衬里或包裹材料牢固地定位在管状结构的外部或周围。 粘合剂通过在制造过程中将保护材料保持在适当位置，防止在由衬里或包裹材料提供的保护层中形成不连续性。 包裹材料通过超声波焊缝密封，以防止通过接缝到下面的管状结构的环境侵蚀。
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公开(公告)号：US5024437A
公开(公告)日：1991-06-18
申请号：US492973
申请日：1990-03-13
申请人： Donald A. Anderson
发明人： Donald A. Anderson
CPC分类号： A63B53/04 , A63B53/0466 , A63B53/047 , A63B2053/0416 , A63B2053/0458
摘要： A golf club head has a main body portion formed by investment casting of material such as stainless steel, beryllium copper, titanium, or aluminum. The face plate of the head is formed of a forged metal such as forged carbon steel, this plate being welded to the face portion of the casting to form an integral assembly therewith. The forged metal faceplate affords a more solid impact and feel to the club which provides better control.
摘要翻译： 高尔夫球杆头具有通过不锈钢，铍铜，钛或铝等材料的熔模铸造而形成的主体部。 头部的面板由诸如锻造碳钢的锻造金属形成，该板被焊接到铸件的面部以形成与其一体的组件。 锻造的金属面板为俱乐部提供了更加坚实的冲击和感觉，从而提供更好的控制。
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公开(公告)号：US4900383A
公开(公告)日：1990-02-13
申请号：US183680
申请日：1988-04-19
CPC分类号： F16L57/06 , B29C31/002 , B29C53/42 , B29C63/0047 , B29C63/14 , B29C63/30 , B29C65/78 , B29C66/4322 , B29C66/49 , B29C66/71 , B29C66/7212 , B29C66/7394 , Y10S138/10 , Y10T156/1038 , Y10T428/1359
摘要： Methods are provided for lining and wrapping both interior and exterior surfaces of tubular structures with materials that protect the underlying structures from adverse environmental conditions, provide a thermal control coating and prevent exchanging moisture with the surrounding environments. The methods use adhesives to securely position the lining or wrapping material inside or around the exterior of the tubular structure. The adhesives prevent the formation of discontinuities in the protective layer provided by the lining or wrapping material by holding the protective materials in place during the fabrication process. The wrapping materials are sealed by an ultrasonically welded seam to prevent environmental attack through the seam to the underlying tubular structure.
摘要翻译： 提供了用于将管状结构的内表面和外表面衬里和包裹的材料与保护下面的结构免受恶劣环境条件的材料，提供热控制涂层并防止与周围环境交换湿气的方法。 该方法使用粘合剂将衬里或包裹材料牢固地定位在管状结构的外部或周围。 粘合剂通过在制造过程中将保护材料保持在适当位置，防止在由衬里或包裹材料提供的保护层中形成不连续性。 包裹材料通过超声波焊缝密封，以防止通过接缝到下面的管状结构的环境侵蚀。
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公开(公告)号：US08663026B2
公开(公告)日：2014-03-04
申请号：US12027156
申请日：2008-02-06
IPC分类号： A63B53/04
CPC分类号： A63B53/0466 , A63B53/0475 , A63B53/08 , A63B60/00 , A63B60/42 , A63B2053/0433 , A63B2053/0491 , A63B2209/00 , Y10T29/49986
摘要： A golf club having a hollow golf club head which is filled with a gas under pressure. The interior surface of the golf club head is coated with a solidified layer of plastic material. The pressurized gas permits the use of thinner face plates by compensating for forces generated when the face plate strikes a golf ball. The plastic layer is preferably applied through the process of rotational molding using a thermoplastic material.
摘要翻译： 一种具有中空高尔夫球杆头的高尔夫球杆，其在压力下充满气体。 高尔夫球杆头的内表面涂覆有塑料材料的凝固层。 加压气体允许通过补偿当面板撞击高尔夫球时产生的力而使用较薄的面板。 塑料层优选通过使用热塑性材料的旋转成型的方法来施加。
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公开(公告)号：US20120276351A1
公开(公告)日：2012-11-01
申请号：US13543656
申请日：2012-07-06
CPC分类号： C09J5/06 , B29C35/02 , B29C65/4815 , B29C65/4835 , B29C65/5021 , B29C65/5057 , B29C66/721 , B29C66/73122 , B29C66/8227 , B29C66/8242 , B29C66/8322 , B29C66/9141 , B29C66/919 , B29C66/929 , B29C66/949 , B29L2031/3076 , C09J2463/00 , Y10T428/2495 , Y10T428/26 , Y10T428/2817 , Y10T428/31511 , Y10T428/31678
摘要： The invention relates to a method of bonding two members together utilizing a stack of solid film adhesive and a layer of solid film adhesive, both disposed between the members. A pressure-applying device may be utilized to apply low pressure to force the members together. The pressure may force the stack to compress and expand in varying directions in order to substantially remove air-bubbles between the layer and one of the members. A heating device may be utilized to change the layer and the stack into liquid states in order to bond the members together with a void-free bond-line.
摘要翻译： 本发明涉及一种利用固体膜粘合剂和一层固体膜粘合剂将两个构件结合在一起的方法，两者均设置在构件之间。 压力施加装置可以用于施加低压力以迫使构件在一起。 压力可以迫使堆叠件在不同的方向上压缩和膨胀，以便基本上去除层和其中一个构件之间的气泡。 可以使用加热装置来将层和堆叠改变成液态，以便将这些构件与无空隙的粘合线结合在一起。
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公开(公告)号：US07935289B2
公开(公告)日：2011-05-03
申请号：US11695561
申请日：2007-04-02
IPC分类号： B32B37/00
CPC分类号： B29C70/543 , B29C33/68 , B29C37/0003 , B29C53/60 , B29C53/68 , B29C70/30 , B29C70/446 , Y02T50/43 , Y10T29/49867 , Y10T29/49879 , Y10T29/49895 , Y10T29/49998
摘要： A method is provided for making a composite laminate aircraft skin for a fuselage in multiple composite panels. A resin-impregnated composite tape is placed on a lay-up surface of a mandrel tool to form the composite laminate aircraft skin as a barrel that is substantially the shape of a fuselage section. The barrel is cut into a plurality of panels on the mandrel tool, and at least one panel of the plurality of panels is transferred, individually and independently of all other of the plurality of panels, from the lay-up surface of the mandrel tool to a first cure tool of a plurality of cure tools having an aero surface tooled to an outer mold line. The at least one of the panels is cured on the first cure tool to form a cured composite panel. The first cure tool defines and controls the outer mold line of the at least one panel. The cured composite panel is removed from the first cure tool.
摘要翻译： 提供了一种用于制造用于多个复合板中的机身的复合层压飞机皮肤的方法。 将树脂浸渍的复合带放置在心轴工具的叠置表面上，以形成基本上为机身部分形状的复合层压飞机皮肤。 将筒体切割成心轴工具上的多个面板，并且多个面板中的至少一个面板独立地且独立于多个面板中的所有其他面板从芯棒工具的叠置表面传递到 多个固化工具的第一固化工具，其具有加工到外模线的航空表面。 所述至少一个所述面板在所述第一固化工具上固化以形成固化的复合板。 第一固化工具定义和控制至少一个面板的外模线。 固化的复合板从第一固化工具移除。
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