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1. 发明授权

US4153485A Process for heating steel powder compacts 失效
标题翻译：钢粉末压块加工工艺
公开(公告)号：US4153485A
公开(公告)日：1979-05-08
申请号：US825470
申请日：1977-08-17
申请人： Kazuo Ogata , Seiya Furuta
发明人： Kazuo Ogata , Seiya Furuta
IPC分类号： B22F1/00 , B22F3/02 , B22F3/10 , B22F3/17 , C21D1/76 , C21D3/00 , C21D3/02 , C21D3/04 , C22C33/02 , C21D1/00
CPC分类号： C21D1/76 , B22F3/1007 , C21D3/02 , C22C33/0235
摘要： A process is provided for heating steel powder compacts in a controlled atmosphere consisting of a primary gas containing at least 80% by volume of an inert gas, and a secondary gas comprising 0.1 to 5% by volume, based on the volume of said primary gas, of a paraffinic hydrocarbon. The process makes it possible to reduce the residual oxygen concentration in the steel powder compacts, while maintaining accurate control of the carbon content.
摘要翻译：提供了一种在受控气氛中加热含有至少80体积％惰性气体的主要气体的钢粉末压块和基于所述主气体体积的0.1至5体积％的二次气体的方法的链烷烃。该方法可以在保持碳含量的精确控制的同时降低钢粉末成形体中的残留氧浓度。

2. 发明申请

US20080196796A1 Zn-Al Alloy Having Excellent High-Speed Deformation Properties and Process For Producing the Same 审中-公开
标题翻译：具有优异的高速变形性能的Zn-Al合金及其制造方法
公开(公告)号：US20080196796A1
公开(公告)日：2008-08-21
申请号：US11916293
申请日：2005-06-01
申请人： Koichi Makii , Seiya Furuta , Toshiaki Takagi
发明人： Koichi Makii , Seiya Furuta , Toshiaki Takagi
IPC分类号： C22F1/053 , C22C21/10 , C22C18/04
CPC分类号： C22C18/04 , B22D21/007 , B22D21/027 , C22C21/10 , C22C30/06 , C22F1/053 , C22F1/165
摘要： A Zn—Al alloy excellent in static deformability as well as dynamic deformability and applicable to large-sized structures, and a method for production thereof. The alloy contains 30-99% Zn, with the remainder being Al and inevitable impurities, and has a metallographic structure in which the α phase or α′ phase having an average grain size no larger than 5 μm contains the β phase finely dispersed therein, the Al inclusions have a maximum equivalent circle diameter no larger than 50 μm and are free of pores no smaller than 0.5 mm in terms of equivalent circle diameter, and the macrosegregation of Al is less than 3.0% and the microsegregation of Al is less than 2.0%. (% means mass %.)
摘要翻译：具有优异的静态变形性以及动态变形性且适用于大型结构的Zn-Al合金及其制造方法。该合金含有30-99％的Zn，其余为Al和不可避免的杂质，并且具有金相组织，其中平均粒径不大于5μm的α相或α'相含有微细分散于其中的β相， Al夹杂物的最大当量圆直径不大于50μm，并且不具有等于当量圆直径不小于0.5mm的孔，并且Al的宏观偏析小于3.0％，并且Al的微观偏析小于2.0 ％。（％表示质量％）

3. 发明申请

US20070107813A1 Zn-Al alloy excellent in elongation and method for producing the same 审中-公开
标题翻译：伸长率优良的Zn-Al系合金及其制造方法
公开(公告)号：US20070107813A1
公开(公告)日：2007-05-17
申请号：US11581032
申请日：2006-10-16
申请人： Toshiaki Takagi , Koichi Makii , Seiya Furuta
发明人： Toshiaki Takagi , Koichi Makii , Seiya Furuta
IPC分类号： C22C18/04
CPC分类号： C22C18/04 , C22F1/165
摘要： A Zn—Al alloy excellent in elongation, and a method for producing the same are provided. The Zn—Al alloy comprises Zn in a range of 68 to 88% by mass and the remainder including Al and unavoidable impurities, and has a structure with β phases finely dispersed in respective α phases or respective α′ phases, not more than 5 μm in average grain size, a macrosegregation value of Al in the structure being less than 3%, wherein lamellar structures at a central part of the structure is at not higher than 30% by volume, and a difference in average hardness between the central part and a surface layer zone of the structure is not more than 15%, so that the Zn—Al alloy is improved in respect of elongation and uniformity.
摘要翻译：提供伸长率优异的Zn-Al合金及其制造方法。 Zn-Al合金含有68〜88质量％的Zn，余量包括Al和不可避免的杂质，β相的结构在各自的α相或相应的α相中分散，不超过5μm 在平均晶粒尺寸中，结构中Al的宏观偏析值小于3％，其中在结构的中心部分的层状结构不高于30体积％，并且中心部分和该结构的表层区域不超过15％，从而在伸长率和均匀性方面提高了Zn-Al合金。

4. 发明授权

US5850590A Method for making a porous sintered material 失效
标题翻译：制造多孔烧结材料的方法
公开(公告)号：US5850590A
公开(公告)日：1998-12-15
申请号：US634920
申请日：1996-04-19
申请人： Seiya Furuta , Kenichi Aota , Kohro Takatsuka , Shigeki Saka , Masahiro Chiji , Masaru Saito
发明人： Seiya Furuta , Kenichi Aota , Kohro Takatsuka , Shigeki Saka , Masahiro Chiji , Masaru Saito
IPC分类号： B22F3/15 , B22F5/00 , B22F1/04
CPC分类号： B22F5/007 , B22F3/15 , B22F2998/00 , B22F2999/00
摘要： The invention provides a method for making a novel porous sintered material according to an HIP (Hot Isostatic Press) molding technique usually used for the purpose of obtaining defect-free and highly dense powder products. In the method of the invention, a capsule containing a starting powder in a hermetically sealed condition is heated according to a predetermined temperature pattern and is also subjected to hot isostatic pressing while a pressure is arrived at a maximum pressure level substantially in coincidence with commencement of a sintering temperature-applying period in the temperature pattern and is gradually lowered from the maximum pressure level during the sintering temperature-applying period. By the method, excessive densification is suppressed and the resulting sintered material has a required porosity and is provided with pores open to outside in the inside thereof, along with good strength and surface processability.
摘要翻译：本发明提供一种根据通常用于获得无缺陷和高密度粉末产品的HIP（热等静压）成型技术制造新型多孔烧结材料的方法。在本发明的方法中，将含有气密密封状态的起始粉末的胶囊根据预定的温度模式加热，并且在压力达到最大压力水平的同时进行热等静压，其基本上与烧结温度施加期间，在烧结温度施加期间从最高压力水平逐渐降低。通过该方法，抑制了过度的致密化，并且所得到的烧结材料具有所需的孔隙率，并且在其内部设置有向外部开口的孔以及良好的强度和表面加工性。

5. 发明授权

US4825522A Method of making heat resistant heavy-duty components of a turbine by superplasticity forging wherein different alloys are junctioned 失效
标题翻译：通过超塑性锻造制造涡轮机的耐热重型部件的方法，其中不同的合金结合
公开(公告)号：US4825522A
公开(公告)日：1989-05-02
申请号：US102402
申请日：1987-09-29
申请人： Kenji Iwai , Seiya Furuta , Hiroshi Takigawa , Nobuyasu Kawai
发明人： Kenji Iwai , Seiya Furuta , Hiroshi Takigawa , Nobuyasu Kawai
IPC分类号： C22C19/03 , B21K1/36 , B22F5/04 , B22F7/06 , C22C1/04 , C22C19/05 , C22F1/10 , F01D5/28 , B21K3/00
CPC分类号： C22F1/10 , B21K1/36 , B22F7/06 , C22C1/0433 , C22C19/056 , C22C19/057 , F01D5/28 , Y10T29/4932 , Y10T29/4998
摘要： The method concerns fabricating heat-resistant heavy-duty components of a rbine, e.g. disk, wheel, etc. wherein two or more different kinds of alloys are junctioned, which comprises solidifying the one alloy powder by hot isostatic pressing or extrusion, junctioning and solidifying the solidified alloy with the other alloy powder by hot isostatic pressing or extrusion, and subjecting the alloys thus obtained to superplasticity forging thereby to secure the junction boundary. Ni-base superalloys having different complete solid solution temperatures of gamma prime phase are selected for use in the hub and rim of a turbine disk or the like, the one alloy which is higher in the temperature being disposed for the hub and the other alloy for the rim. The difference in the temperature between both alloys is at least 8.degree. C. Further solution heat treatment is performed at a temperature between the complete solid solution temperatures to adjust crystal grain size. Heat-resistant heavy-duty components of a turbine, e.g. disk, etc. are thus fabricated by superplasticity forging from Ni-base superalloys.
摘要翻译：该方法涉及制造涡轮机的耐热重载部件，例如，盘，轮等，其中两种或多种不同种类的合金结合，其包括通过热等静压或挤出固化一种合金粉末，通过热等静压或挤压与其它合金粉末接合和固化固化的合金，以及对由此获得的合金进行超塑性锻造，从而确保接合界面。选择具有不同完整固溶温度的γ相的Ni基超级合金用于涡轮盘等的轮毂和轮辋，其中一个合金的温度高于轮毂，另一个合金用于边缘两种合金之间的温度差别至少为8℃。在完全固溶温度之间的温度下进行进一步的固溶热处理以调节晶粒尺寸。涡轮机的耐热重载部件，例如，因此通过从Ni基超级合金的超塑性锻造制造圆盘等。

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