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81. 发明授权

US07269986B2 Method of forming a tubular blank into a structural component and die therefor 有权
标题翻译：将管状坯料形成为结构部件并将其模具的方法
公开(公告)号：US07269986B2
公开(公告)日：2007-09-18
申请号：US11342943
申请日：2006-01-30
申请人： George D. Pfaffmann , William C. Dykstra , Marc R. Matsen
发明人： George D. Pfaffmann , William C. Dykstra , Marc R. Matsen
IPC分类号： B21D26/02
CPC分类号： B21D26/033 , B21D26/043 , B21D26/047 , B21D37/16 , Y10S72/709 , Y10T29/49805
摘要： A method of forming an elongated metal blank into a structural component having a predetermined outer configuration. The method includes providing a shape imparting cavity or shell section formed from a rigid material which includes an inner surface defining the predetermined shape, placing the metal blank into the cavity or shell section, and forming the metal blank into the component by heating axial portions of the metal blank and forcing a fluid at a high pressure into the metal blank until the metal blank at least partially conforms to at least a portion of the inner surface of the cavity or shell section to form the structural component.
摘要翻译：将细长金属坯料形成为具有预定外部构造的结构部件的方法。该方法包括提供由刚性材料形成的形状赋予空腔或壳体部分，该刚性材料包括限定预定形状的内表面，将金属坯料放入空腔或壳体部分中，并且通过加热金属坯料的轴向部分金属坯料并迫使高压的流体进入金属坯料，直到金属坯件至少部分地符合腔体或壳体部分的内表面的至少一部分以形成结构部件。

82. 发明授权

US07126096B1 Resistance welding of thermoplastics in aerospace structure 失效
标题翻译：热塑性塑料在航空航天结构中的电阻焊接
公开(公告)号：US07126096B1
公开(公告)日：2006-10-24
申请号：US08470168
申请日：1995-06-06
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： H05B6/10
CPC分类号： C22C47/068 , B21D26/055 , B22F3/105 , B22F2003/1046 , B22F2003/1053 , B22F2998/00 , B29C33/06 , B29C65/34 , B29C65/3476 , B29C65/3492 , B29C65/364 , B29C65/3644 , B29C65/3676 , B29C66/634 , B29C66/71 , B29C66/721 , B29C66/7392 , B29C66/91411 , B29C66/91443 , B29C66/91645 , B29C66/91655 , B29C66/91951 , B29C70/44 , B29C70/542 , B29C2035/0811 , B32B2309/62 , B64C3/18 , H05B6/365 , Y02P10/253 , Y02T50/43 , C22C47/20 , B29K2071/00
摘要： Rib and spar webs are joined in a composite wingbox to eliminate fasteners by welding the webs along bondlines 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粘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。

83. 发明授权

US07108290B2 Corrugated web hole reinforcement 有权
标题翻译：波纹网孔加固
公开(公告)号：US07108290B2
公开(公告)日：2006-09-19
申请号：US10610344
申请日：2003-06-30
申请人： David S. Nansen , Paul S. Gregg , Marc R. Matsen , John J. Gurbach , Soo Y. Oh
发明人： David S. Nansen , Paul S. Gregg , Marc R. Matsen , John J. Gurbach , Soo Y. Oh
IPC分类号： F16L5/00
CPC分类号： E04C3/083 , E04C3/06 , E04C3/28
摘要： A device is provided for reinforcing a penetration in corrugated material having a plurality of corrugations. The device includes a tube configured to be received within the penetration. A first holder is attached to the tube, and the first holder has at least one finger arranged to engage at least one corrugation in the corrugated material. If desired, a second holder may be arranged to also engage at least one corrugation.
摘要翻译：提供一种用于加强具有多个波纹的波纹材料中的穿透的装置。该装置包括配置成接收在穿透内的管。第一保持器附接到管，并且第一保持器具有布置成与波纹材料中的至少一个波纹接合的至少一个手指。如果需要，第二保持器可以布置成还接合至少一个波纹。

84. 发明授权

US06884975B2 Localized stress relief by induction heating 失效
标题翻译：感应加热局部应力消除
公开(公告)号：US06884975B2
公开(公告)日：2005-04-26
申请号：US10292038
申请日：2002-11-12
申请人： Marc R. Matsen , Terry L. Smith
发明人： Marc R. Matsen , Terry L. Smith
IPC分类号： H05B6/02 , H05B6/40
CPC分类号： H05B6/105 , C21D1/30 , C21D1/42 , C21D9/50 , H05B2206/023 , Y02P10/253
摘要： A system and method inductively heats and stress relieves a weld joint area having a stress induced zone. A susceptor assembly is positioned over the stress induced zone. The susceptor assembly includes susceptor sheets manufactured to operate at different, preselected Curie temperatures. A housing is mounted over the susceptor assembly including an induction coil positioned adjacent to the susceptor assembly. An alternating electric current is applied to the induction coil. The alternating electric current causes the induction coil to generate a plurality of magnetic flux lines. The invention provides the advantage that the magnetic flux lines passing through the susceptor assembly heat the susceptor assembly providing localized and controlled temperature heat to the weld joint area to stress relieve the stress induced zone.
摘要翻译：感应加热和应力的系统和方法消除了具有应力诱导区的焊缝接合区域。感应器组件位于应力诱导区域的上方。基座组件包括制造成在不同的预定居里温度下工作的基座片。壳体安装在基座组件上方，包括邻近基座组件定位的感应线圈。对感应线圈施加交流电流。交流电流使感应线圈产生多个磁通线。本发明提供的优点是，通过基座组件的磁通线加热基座组件，从而为焊接接头区域提供局部和受控的温度热量，以减轻应力诱发区域。

85. 发明授权

US06211497B1 Induction consolidation system 失效
标题翻译：感应整合系统
公开(公告)号：US06211497B1
公开(公告)日：2001-04-03
申请号：US08465289
申请日：1995-06-05
申请人： Marc R. Matsen , Paul S. Gregg , Howard Martinson , Robert Snyder
发明人： Marc R. Matsen , Paul S. Gregg , Howard Martinson , Robert Snyder
IPC分类号： H05B610
CPC分类号： B22F3/105 , B21D26/021 , B21D26/025 , B21D26/053 , B21D26/055 , B22F3/18 , B22F2003/1046 , B22F2003/1053 , B22F2998/00 , B23K20/023 , B23K2101/18 , B29C33/06 , B29C33/08 , B29C33/60 , B29C35/08 , B29C43/3642 , B29C43/52 , B29C65/18 , B29C65/32 , B29C65/34 , B29C65/3476 , B29C65/3644 , B29C65/3668 , B29C65/3676 , B29C65/4815 , B29C65/4875 , B29C65/489 , B29C66/0342 , B29C66/54 , B29C66/634 , B29C66/71 , B29C66/721 , B29C66/7392 , B29C66/7394 , B29C66/8122 , B29C66/81241 , B29C66/81261 , B29C66/8181 , B29C66/81811 , B29C66/81821 , B29C66/8322 , B29C66/949 , B29C70/44 , B29C70/506 , B29C70/542 , B29C2035/0811 , B29C2043/3233 , B29C2043/3655 , B29K2105/0854 , B32B37/06 , B32B2305/024 , B32B2309/62 , B32B2310/0812 , B64C3/185 , C09K2205/12 , C22C47/00 , C22C47/062 , C22C47/20 , H05B6/365 , Y02P10/253 , Y02T50/43 , Y10T29/49805 , Y10T428/12292 , Y10T428/12569 , Y10T428/12611 , Y10T428/12618 , B29K2071/00 , B29K2063/00 , B29K2909/02 , B29K2079/08
摘要： An apparatus for forming and consolidating organic matrix composites. An organic matrix composite panel comprising laid-up prepregs is placed between sheets of a susceptor material that is susceptible to inductive heating to form a workpiece. The resulting workpiece is placed within upper and lower dies formed of a material that is not susceptible to inductive heating. An induction coil embedded within the dies is energized and inductively heats the susceptor sheets surrounding the panel. The sheets in turn conductively heat the organic matrix composite panel. A pressure zone between the workpiece and one of the dies is pressurized to form the workpiece to the contour of a forming surface on one of the dies. The pressure in the pressure zone is maintained on the workpiece until the organic matrix composite panel is fully consolidated and formed.
摘要翻译：一种用于形成和固结有机基质复合材料的装置。将包含预浸料坯的有机基质复合板置于容易感应加热以形成工件的感受体材料的片材之间。将所得到的工件放置在由不受感应加热敏感的材料形成的上模和下模中。嵌入在模具内的感应线圈通电并感应加热围绕面板的基座片。片材依次导电地加热有机基质复合板。在工件和其中一个模具之间的压力区域被加压以将工件形成为其中一个模具上的成形表面的轮廓。压力区内的压力保持在工件上，直到有机基质复合板完全固结并形成为止。

86. 发明授权

US5914064A Combined cycle for forming and annealing 失效
标题翻译：用于成型和退火的组合循环
公开(公告)号：US5914064A
公开(公告)日：1999-06-22
申请号：US890529
申请日：1997-07-09
申请人： Franna S. P. Gillespie , Marc R. Matsen
发明人： Franna S. P. Gillespie , Marc R. Matsen
IPC分类号： B21D26/021 , B21D26/055 , B22F3/105 , B23K20/02 , B29C33/06 , B29C35/08 , B29C43/36 , B29C65/00 , B29C65/32 , B29C65/34 , B29C65/36 , B29C65/48 , B29C70/44 , B29C70/54 , B64C3/18 , H05B6/02 , H05B6/14 , H05B6/36 , B23K13/01
CPC分类号： B29C43/52 , B21D26/021 , B21D26/055 , B22F3/105 , B23K20/023 , B29C33/06 , B29C35/08 , B29C43/10 , B29C70/44 , B29C70/542 , B32B37/06 , B64C3/18 , H05B6/105 , H05B6/365 , B23K2201/18 , B29C2035/0811 , B29C2043/3222 , B32B2305/024 , B32B2310/0812 , C09K2205/12 , Y02T50/433
摘要： Capitalizing on the unique feature of our induction heating workcell that permits rapid and controlled heating and cooling of a workpiece within a wide temperature range allows us to combine manufacturing into a single heating cycle to save time, energy, capital, touch labor, and factory space. For example, we can combine superplastic forming (SPF) with annealing two operations that occur at temperatures that differ by about 150-200.degree. F. (85-105.degree. C.) or more, to produce quality parts. We mill parts flat to simplify their machining, form them to complex curvature, and anneal them.
摘要翻译：利用我们的感应加热工作单元的独特功能，允许在宽温度范围内快速和受控地加热和冷却工件，使我们将制造结合到单个加热循环中，以节省时间，能源，资金，触摸人工和工厂空间。例如，我们可以将超塑性成形（SPF）与退火温度相差约150-200°F（85-105℃）或更高的退火两种操作结合在一起，以产生优质部件。我们轧制零件平面以简化其加工，形成复杂的曲率并退火。

87. 发明授权

US5821506A Superplastically formed part 失效
标题翻译：超塑性部分
公开(公告)号：US5821506A
公开(公告)日：1998-10-13
申请号：US862114
申请日：1997-05-22
申请人： Marc R. Matsen
发明人： Marc R. Matsen
IPC分类号： B21D26/021 , B21D26/055 , B22F3/105 , B23K20/02 , B29C33/06 , B29C35/08 , B29C43/36 , B29C65/00 , B29C65/32 , B29C65/34 , B29C65/36 , B29C65/48 , B29C70/44 , B29C70/54 , B64C3/18 , H05B6/02 , H05B6/14 , H05B6/36 , B23K13/01
CPC分类号： B29C43/10 , B21D26/021 , B21D26/055 , B22F3/105 , B23K20/023 , B29C33/06 , B29C35/08 , B29C43/3642 , B29C43/52 , B29C70/44 , B29C70/542 , B32B37/06 , B64C3/18 , H05B6/365 , B23K2201/18 , B29C2035/0811 , B29C2043/3222 , B29C2043/3233 , B29C33/08 , B32B2305/024 , B32B2310/0812 , C09K2205/12 , Y02P20/124 , Y02T50/433 , Y10T428/1234
摘要： Multisheet SPF parts with braze joints at selected locations are produced with improved energy efficiency and at lower cost. The parts include a core defined with intermittent welds between two or more core sheets and aerodynamically smooth facing sheets brazed to the core. The manufacturing process includes heating the multisheet pack to its superplastic forming range below the melting point of the braze alloy, superplastically forming the pack to define braze joints having unmelted braze alloy; increasing the temperature to the braze temperature of the braze alloy, and cooling the pack below the superplastic range to freeze the braze alloy in the braze joint.
摘要翻译：在选定位置具有钎焊接头的多片SPF部件以更高的能量效率和更低的成本生产。这些部件包括在两个或更多个芯片之间间断焊接和钎焊到芯部的空气动力学平滑的板之间限定的芯。制造过程包括将多片材包装加热到其钎焊合金熔点以下的超塑性成形范围，超塑性地形成包装以限定具有未熔化的钎焊合金的钎焊接头; 将钎焊温度提高到钎焊合金的钎焊温度，并将组件冷却到超塑性范围以下，以使钎焊接头中的钎焊合金冷冻。

88. 发明授权

US5760379A Monitoring the bond line temperature in thermoplastic welds 失效
标题翻译：监测热塑性焊缝中的粘结线温度
公开(公告)号：US5760379A
公开(公告)日：1998-06-02
申请号：US548823
申请日：1995-10-26
申请人： Marc R. Matsen , Karl A. Hansen, deceased , John J. deJong, executor
发明人： Marc R. Matsen , Karl A. Hansen, deceased , John J. deJong, executor
IPC分类号： B29C65/00 , B29C65/36 , H05B6/06 , H05B6/10
CPC分类号： B29C65/3644 , B29C66/301 , B29C66/524 , B29C66/5326 , B29C66/721 , B29C66/7212 , B29C66/73116 , B29C66/7392 , B29C66/73921 , B29C66/836 , B29C66/91221 , B29C66/91411 , B29C66/91443 , B29C66/91641 , B29C66/91645 , B29C66/91651 , B29C66/91655 , B29C66/91921 , B29C66/91931 , B29C66/91951 , B29C66/9261 , B29C66/934 , B29C66/961 , B29C65/368 , B29C66/71 , B29C66/72141 , B29C66/72143 , B29C66/919 , B29C66/929 , B29C66/944 , B29C66/949 , B29C66/9592
摘要： Quality welds are highly dependent upon achieving appropriate temperatures everywhere along the bond line. The present invention uses multinode thermocouples to measure the bond line temperature in real time and to provide control signals for the moving coil (welding head).
摘要翻译：质量焊接高度依赖于沿着粘合线在各处达到适当的温度。本发明使用多节点热电偶实时测量接合线温度，并为动圈（焊头）提供控制信号。

89. 发明授权

US5641422A Thermoplastic welding of organic resin composites using a fixed coil induction heater 失效
标题翻译：使用固定线圈感应加热器的有机树脂复合材料的热塑性焊接
公开(公告)号：US5641422A
公开(公告)日：1997-06-24
申请号：US471503
申请日：1995-06-16
申请人： Marc R. Matsen , John A. Mittleider , Karl A. Hansen, deceased , John J. deJong, representative
发明人： Marc R. Matsen , John A. Mittleider , Karl A. Hansen, deceased , John J. deJong, representative
IPC分类号： B21D26/021 , B21D26/025 , B21D26/053 , B21D26/055 , B22F3/105 , B22F3/18 , 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： B29C43/52 , B21D26/021 , B21D26/025 , B21D26/053 , B21D26/055 , B22F3/105 , B22F3/18 , B23K20/023 , B29C33/06 , B29C33/60 , B29C35/08 , B29C43/3642 , B29C65/18 , B29C65/32 , B29C65/34 , B29C65/364 , B29C65/3644 , B29C65/3676 , B29C65/4815 , B29C65/4875 , B29C65/489 , B29C66/1122 , B29C66/524 , B29C66/54 , B29C66/634 , B29C66/721 , B29C66/8122 , B29C66/81457 , B29C66/8181 , B29C66/81811 , B29C66/81821 , B29C66/8322 , B29C70/44 , B29C70/506 , B29C70/542 , B32B37/06 , B64C3/18 , 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 , B29C65/3492 , B29C65/3668 , B29C65/368 , B29C66/71 , B29C66/7212 , B29C66/72141 , B29C66/72143 , B29C66/7392 , B29C66/7394 , B29C66/81261 , B29K2105/0854 , B32B2305/024 , B32B2309/62 , B32B2310/0812 , C09K2205/12 , Y02P10/253 , Y02T50/433
摘要： Quality thermoplastic fusion welds are formed in prefabricated resin composite parts by aligning a susceptor along a bondline between parts with the induction coil segments of a solenoid induction coil along the centerline of the coil. Energizing the coil heats the susceptor to form the weld at the bondline. For this operation, our induction heating workcell users complementary dies that define a central cavity with an oval pattern of induction cool segments surrounding all faces of the cavity where the preform composite parts and susceptor are positioned.
摘要翻译：通过沿着线圈的中心线沿电磁感应线圈的感应线圈段沿部件之间的接合线对准基座，在预制树脂复合部件中形成优质热塑性熔接焊缝。使线圈通电加热感受器以在接合线处形成焊缝。对于这种操作，我们的感应加热工作单元使用互补的模具，其定义了围绕腔体的所有面的感应冷段的椭圆形图案的中心空腔，其中预成型件复合部件和基座被定位。

90. 发明授权

US5591370A System for consolidating organic matrix composites using induction heating 失效
标题翻译：使用感应加热固结有机基质复合材料的系统
公开(公告)号：US5591370A
公开(公告)日：1997-01-07
申请号：US460786
申请日：1995-06-05
申请人： Marc R. Matsen , Paul S. Gregg , Howard Martinson , Robert Snyder
发明人： Marc R. Matsen , Paul S. Gregg , Howard Martinson , Robert Snyder
IPC分类号： B21D26/02 , B22F3/105 , B22F3/18 , 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 , B21D26/021 , B21D26/025 , B21D26/053 , B21D26/055 , B22F3/18 , B23K20/023 , B29C33/06 , B29C33/60 , B29C35/08 , B29C43/3642 , B29C43/52 , B29C65/18 , B29C65/32 , B29C65/34 , B29C65/3644 , B29C65/4815 , B29C65/4875 , B29C65/489 , B29C66/0342 , B29C66/54 , B29C66/634 , B29C66/721 , B29C66/8122 , B29C66/81261 , B29C66/8181 , B29C66/81811 , B29C66/81821 , B29C66/8322 , B29C70/44 , B29C70/506 , B29C70/542 , B32B37/06 , B64C3/185 , C22C47/00 , C22C47/062 , C22C47/20 , H05B6/365 , B22F2003/1046 , B22F2003/1053 , B22F2998/00 , B23K2201/18 , B29C2035/0811 , B29C2043/3233 , B29C2043/3655 , B29C33/08 , B29C65/3476 , B29C65/3668 , B29C65/3676 , B29C66/71 , B29C66/7392 , B29C66/7394 , B29C66/81241 , B29C66/949 , B29K2105/0854 , B32B2305/024 , B32B2309/62 , B32B2310/0812 , C09K2205/12 , Y02P10/253 , Y02T50/433 , Y10T29/49805 , Y10T428/12292 , Y10T428/12569 , Y10T428/12611 , Y10T428/12618
摘要： An apparatus for forming and consolidating organic matrix composites. An organic matrix composite panel comprising laid-up prepegs is placed between sheets of a susceptor material that is susceptible to inductive heating to form a workpiece. The resulting workpiece is placed within upper and lower dies formed of a material that is not susceptible to inductive heating. An induction coil embedded within the dies is energized and inductively heats the susceptor sheets surrounding the panel. The sheets in turn conductively heat the organic matrix composite panel. A pressure zone between the workpiece and one of the dies is pressurized to form the workpiece to the contour of a forming surface on one of the dies. The pressure in the pressure zone is maintained on the workpiece until the organic matrix composite panel is fully consolidated and formed.
摘要翻译：一种用于形成和固结有机基质复合材料的装置。包含铺设的预制物的有机基质复合板被放置在容易感应加热以形成工件的感受体材料的片材之间。将所得到的工件放置在由不受感应加热敏感的材料形成的上模和下模中。嵌入在模具内的感应线圈通电并感应加热围绕面板的基座片。片材依次导电地加热有机基质复合板。在工件和其中一个模具之间的压力区域被加压以将工件形成为其中一个模具上的成形表面的轮廓。压力区内的压力保持在工件上，直到有机基质复合板完全固结并形成为止。

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