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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:US06653608B1
公开(公告)日:2003-11-25
申请号:US10032625
申请日:2001-10-24
IPC分类号: H05B606
CPC分类号: H05B6/105
摘要: A single or multilayer smart susceptor for temperature control of part fabrication in an induction processing system generally consists of single layer or laminated layers of ferromagnetic material susceptible to heating by induction. The use of the susceptors in fabrication at elevated temperatures causes oxidation damage to the surface. The susceptor may be coated with a nickel aluminide surface coating to minimize oxidation of the susceptor outer surface.
摘要翻译: 用于感应加工系统中部件制造的温度控制的单层或多层智能基座通常由容易受感应加热的铁磁材料的单层或层压层组成。 在高温制造中使用感受体会对表面造成氧化损伤。 基座可以涂覆有镍铝表面涂层,以使基座外表面的氧化最小化。
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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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公开(公告)号:US06855917B2
公开(公告)日:2005-02-15
申请号:US10011090
申请日:2001-12-06
CPC分类号: B29C33/02 , B29C33/3842 , B29C45/37 , B29C45/73
摘要: A die liner for use in a die having a die body wherein the die body is configured to form a workpiece. The die liner is a discrete structure that is configured to be used in conjunction with the die body. The die liner defines a forming surface for forming the workpiece and is configured to have at least one characteristic that is different than a corresponding characteristic of the die body such that the die liner increases the durability of the die.
摘要翻译: 一种用于具有模具主体的模具中的模具衬垫,其中模具主体构造成形成工件。 模具衬垫是被配置为与模具本体结合使用的分立结构。 模具衬套限定了用于形成工件的成形表面,并且构造成具有与模具主体的相应特性不同的至少一个特征,使得模具衬垫增加了模具的耐久性。
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公开(公告)号:US20100200123A1
公开(公告)日:2010-08-12
申请号:US12369157
申请日:2009-02-11
申请人: Brad L. Kirkwood , Marc R. Matsen , Tony Shen , Wesley B. Crow
发明人: Brad L. Kirkwood , Marc R. Matsen , Tony Shen , Wesley B. Crow
CPC分类号: C21D1/42 , B21K29/00 , B23F17/006 , C21D1/10 , C21D1/60 , C21D1/613 , C21D1/62 , C21D1/74 , C21D6/00 , C21D6/02 , C21D9/32 , C21D10/005 , C21D2211/004 , C22F1/10 , C22F1/183 , C23C14/06 , Y02P10/253 , Y10T29/4948
摘要: A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.
摘要翻译: 存在用于制造零件的方法和装置。 该部件由金属合金构成,并且定位成形成定位部件。 产生加热定位部件的电磁场。 定位部件的表面暴露于惰性气体中,同时产生电磁场以在定位部件的外部和定位部件的内部部分之间产生反向热梯度,以形成热处理部分。
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公开(公告)号:US09187818B2
公开(公告)日:2015-11-17
申请号:US12369157
申请日:2009-02-11
申请人: Brad L. Kirkwood , Marc R. Matsen , Tony Shen , Wesley B. Crow
发明人: Brad L. Kirkwood , Marc R. Matsen , Tony Shen , Wesley B. Crow
CPC分类号: C21D1/42 , B21K29/00 , B23F17/006 , C21D1/10 , C21D1/60 , C21D1/613 , C21D1/62 , C21D1/74 , C21D6/00 , C21D6/02 , C21D9/32 , C21D10/005 , C21D2211/004 , C22F1/10 , C22F1/183 , C23C14/06 , Y02P10/253 , Y10T29/4948
摘要: A method and apparatus are present for manufacturing a part. The part is comprised of a metal alloy and is positioned to form a positioned part. An electromagnetic field is generated that heats the positioned part. A surface of the positioned part is exposed to an inert gas, while the electromagnetic field is generated to create an inverse thermal gradient between an exterior of the positioned part and an interior section of the positioned part to form a heat treated part.
摘要翻译: 存在用于制造零件的方法和装置。 该部件由金属合金构成,并且定位成形成定位部件。 产生加热定位部件的电磁场。 定位部件的表面暴露于惰性气体中,同时产生电磁场以在定位部件的外部和定位部件的内部部分之间产生反向热梯度,以形成热处理部分。
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公开(公告)号:US08343402B1
公开(公告)日:2013-01-01
申请号:US12625354
申请日:2009-11-24
申请人: Marc R. Matsen , Wesley B. Crow , Brad L. Kirkwood
发明人: Marc R. Matsen , Wesley B. Crow , Brad L. Kirkwood
IPC分类号: B22F3/04
CPC分类号: B29C35/0805 , B22F3/02 , B22F2999/00 , B29C35/16 , B29C2035/0811 , B29C2035/1616 , B29C2035/1658 , B29C2035/1691 , C22C1/0491 , B22F2203/13
摘要: In one embodiment method to form a composite part from a metallic composite powder, comprises positioning a metallic composite powder preform in a mold cavity formed by a first susceptor and a second susceptor, heating the mold cavity to a first processing temperature, applying a pressure to the mold cavity, and applying a thermal oscillation cycle to the mold cavity, wherein the thermal oscillation cycle oscillates the temperature of the mold cavity between a first temperature in which the metallic composite powder is in a first phase and a second temperature in which the metallic composite powder is in a second phase, different from the first phase.
摘要翻译: 在一种实施方式中,从金属复合粉末形成复合部件,包括将金属复合粉末预制件定位在由第一基座和第二基座形成的模腔中,将模腔加热至第一加工温度,施加压力 模腔,并且向模腔施加热振荡循环,其中所述热振荡循环使所述模腔的温度在所述金属复合粉末处于第一相的第一温度和所述金属复合粉末处于第一温度的第二温度之间振荡,其中所述金属 复合粉末处于与第一相不同的第二相。
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公开(公告)号:US20090035632A1
公开(公告)日:2009-02-05
申请号:US11831776
申请日:2007-07-31
申请人: Brad L. Kirkwood
发明人: Brad L. Kirkwood
CPC分类号: H01M8/1246 , B21C1/003 , B22F2003/241 , B22F2003/248 , B22F2998/10 , B22F2999/00 , C22C47/20 , C22C49/14 , C22F1/08 , H01M8/0206 , H01M8/0208 , H01M8/0226 , H01M8/0228 , H01M2008/1293 , Y10T29/49 , C22C9/00 , B21C1/02 , B22F3/1258 , B22F3/18 , B22F3/10 , B22F3/24 , B22F3/15
摘要: A solid oxide fuel cell (SOFC) interconnect comprises a metal sheet with an air side and a fuel side in accordance with an embodiment of the present invention. The metal sheet comprises a metallic composite having a matrix. The matrix comprises a first metal. The metal sheet also comprises a plurality of discontinuous, elongated, directional reinforcement wires. The reinforcement wires comprise a second metal that is immiscible in the first metal. An oxidation protection layer is disposed on the air side of the metal sheet.
摘要翻译: 固体氧化物燃料电池(SOFC)互连件包括根据本发明实施例的具有空气侧和燃料侧的金属片。 金属片包括具有基体的金属复合物。 该基质包括第一金属。 金属片还包括多个不连续的,细长的定向加强线。 加强线包括在第一金属中不混溶的第二金属。 氧化保护层设置在金属板的空气侧。
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公开(公告)号:US20110135418A1
公开(公告)日:2011-06-09
申请号:US12632604
申请日:2009-12-07
CPC分类号: F16B13/04 , F16B1/0014 , F16B3/00 , Y10T29/49865 , Y10T29/49954
摘要: In one embodiment a method to join a first structure to a second structure, comprises aligning a first hole in the first structure with a second hole in the second structure and inserting a fastener into the first hole and the second hole. The fastener comprises a shape memory alloy which was formed into a first shape having a diameter slightly larger than a diameter of the first hole and the second hole when the shape memory alloy was in an austenite state and reduced to a second shape having a diameter less than the diameter of the first hole and the second hole when the shape memory alloy was in a martensite state. The method further comprises heating the fastener above an austenite start transition temperature, such that the fastener initiates free expansion from the second shape back to the first shape and establishes physical contact with the surface of the first hole and the second hole and continuing to heat the fastener such that first structure and the second structure proximate the holes and the fastener undergo plastic deformation.
摘要翻译: 在一个实施例中,将第一结构连接到第二结构的方法包括将第一结构中的第一孔与第二结构中的第二孔对准,并将紧固件插入第一孔和第二孔中。 紧固件包括形状记忆合金,其形状为第一形状,其形状记忆合金处于奥氏体状态时,直径略大于第一孔的直径,第二孔缩小至直径较小的第二形状 比形状记忆合金处于马氏体状态时的第一孔和第二孔的直径大。 该方法还包括将紧固件加热到高于奥氏体起始转变温度,使得紧固件开始从第二形状到第一形状的自由膨胀,并且与第一孔和第二孔的表面建立物理接触,并且继续加热 紧固件使得第一结构和靠近孔和紧固件的第二结构经历塑性变形。
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10.
公开(公告)号:US5556565A
公开(公告)日:1996-09-17
申请号:US483407
申请日:1995-06-07
CPC分类号: B64C1/065 , B29C65/3644 , B29C65/3676 , B29C66/524 , B29C66/532 , B29C66/5326 , B29C66/721 , B29C66/7392 , B29C66/742 , B29C66/8122 , B29C66/81457 , B29C66/81811 , B29C66/81821 , B29C66/8322 , E04C3/29 , H05B6/42 , B29C65/3668 , B29C65/368 , B29C66/71 , B29C66/7212 , B29C66/73711 , B29C66/73712 , B29C66/7394 , B29C66/81261 , B64C2001/0072 , B64C2001/0081 , Y02T50/433
摘要: A hybrid metal webbed composite beam includes a metal I or T web section and a composite cap formed over and adhered to the I or T web. The beam incorporates the advantages of metals and composites in modern aerospace construction allowing thermoplastic welding of the beam to skins while having the strength of metal.
摘要翻译: 混合金属网板复合梁包括形成在I或T网上并粘附到I或T网上的金属I或T腹板部分和复合帽。 该梁结合了金属和复合材料在现代航空航天结构中的优点,允许将热束焊接到外壳上,同时具有金属的强度。
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