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1. 发明授权

US08703045B2 Method of manufacturing a multiple composition component 有权
标题翻译：多组分成分的制造方法
公开(公告)号：US08703045B2
公开(公告)日：2014-04-22
申请号：US12946168
申请日：2010-11-15
申请人： Robert J. Mitchell , Catherine M. F. Rae , Mark C. Hardy , Shaun R. Holmes
发明人： Robert J. Mitchell , Catherine M. F. Rae , Mark C. Hardy , Shaun R. Holmes
IPC分类号： B22F3/15 , B22F7/06 , B22F7/08
CPC分类号： B22F5/009 , B22F3/15 , B22F5/106 , B22F7/062 , B22F2999/00
摘要： The present invention relates to a method of manufacturing a multiple composition component 10, comprising: arranging first, second and third constituent parts 40, 30, 42 having first, second and third compositions respectively A, B, C so that the first constituent part 40 shares a first boundary with the second constituent part 30 and the second constituent part 30 shares a second boundary with the third constituent part 40. The first, second and third constituent parts 40, 30, 42 are each either a powder or a solid so that the first and second boundaries are each a solid adjacent to a powder. The arrangement is then processed so as to form a single solid component having first, second and third regions 16, 18, 20 having first, second and third compositions A, B, C respectively.
摘要翻译：本发明涉及一种多组分成分10的制造方法，其特征在于，包括：将分别具有A，B，C的第一，第二和第三组分的第一，第二和第三组分40,30,42分别排列成第一组成部分40 与第二构成部分30共享第一边界，并且第二构成部分30与第三构成部分40共享第二边界。第一，第二和第三组成部分40,30,42各自是粉末或固体，使得第一和第二边界各自是与粉末相邻的固体。然后处理该装置以形成具有分别具有第一，第二和第三组合物A，B，C的第一，第二和第三区域16,18,20的单个固体组分。

2. 发明申请

US20130052077A1 NICKEL ALLOY 有权
标题翻译：镍合金
公开(公告)号：US20130052077A1
公开(公告)日：2013-02-28
申请号：US13566490
申请日：2012-08-03
申请人： Mark C. HARDY
发明人： Mark C. HARDY
IPC分类号： C22C19/05
CPC分类号： F01D5/02 , B22F2998/10 , C22C1/0433 , C22C19/056 , C22F1/10 , F01D25/005 , B22F9/082 , B22F3/15 , B22F3/20
摘要： A nickel-base alloy having the following composition (in weight percent unless otherwise stated): Cr 13/-17.5; Co 2.5-5.6; Fe 8.0-9.3; Si 0-0.6; Mn 0-0.95; Mo 0.5-2.3; W 2.7-3.0; Al 2.2-3.5; Nb 2.7-7.2; Ti 0-0.85; Ta 0-3.25; Hf 0.0-0.5; C 0.01-0.05; B 0.02-0.04; Zr 0.04-0.06; Mg 0.015-0.025; S
摘要翻译：具有以下组成的镍基合金（除非另有说明，以重量百分比计）：Cr 13 / -17.5; Co 2.5-5.6; Fe 8.0-9.3; Si 0-0.6; Mn 0-0.95; Mo 0.5-2.3; W 2.7-3.0; Al 2.2-3.5; Nb 2.7-7.2; Ti 0-0.85; Ta 0-3.25; Hf 0.0-0.5; C 0.01-0.05; B 0.02-0.04; Zr 0.04-0.06; Mg 0.015-0.025; S <50ppm; P <50ppm; 余量为镍和杂质。与已知合金相比，该合金具有改进的性能组合（主要是表面环境损伤和停留疲劳裂纹扩展），并且旨在在700℃以上长时间运行，直到峰值温度为800° C。

3. 发明授权

US08323424B2 Alloy component including a fine grain structure, a coarse grain structure and a transitional structure 有权
标题翻译：合金成分包括细晶粒结构，粗晶结构和过渡结构
公开(公告)号：US08323424B2
公开(公告)日：2012-12-04
申请号：US13097567
申请日：2011-04-29
申请人： Robert J. Mitchell , David Ulrich Furrer , Joseph Andrew Lemsky , Mark C. Hardy
发明人： Robert J. Mitchell , David Ulrich Furrer , Joseph Andrew Lemsky , Mark C. Hardy
IPC分类号： C22C19/03 , C22C14/00
CPC分类号： C21D1/70 , C21D1/26 , C21D9/0068 , C21D2221/00
摘要： An alloy disc includes a hub portion, a rim portion and a web portion disposed between the hub portion and the rim portion. The disc includes a fine grain structure substantially in a first region of the disc and a coarse grain structure substantially in a second region of the disc. The fine grain structure may be in the hub portion of the disc, and the coarse grain structure may be in the rim portion of the disc. The coarse grain structure may extend a greater distance radially inwardly from the rim portion into the web portion on the first axial end of the disc than on the second axial end of the disc. The fine grain structure may extend a greater distance radially outwardly from the hub portion into the web portion on the second axial end of the disc than on the first axial end of the disc.
摘要翻译：合金盘包括轮毂部分，轮缘部分和布置在轮毂部分和轮缘部分之间的腹板部分。盘包括基本上在盘的第一区域中的细晶粒结构和基本上在盘的第二区域中的粗晶粒结构。细晶粒结构可以在盘的毂部分中，粗粒结构可以在盘的边缘部分中。粗颗粒结构可以从轮缘部分径向向内延伸到盘的第一轴向端部上的纤维网部分中比在盘的第二轴向端部更远的距离。细晶粒结构可以从轮毂部分径向向外延伸到盘的第二轴向端部上的腹板部分中比在盘的第一轴向端部上更远的距离。

4. 发明申请

US20110103961A1 METHOD OF PRODUCING AN OXIDE DISPERSION STRENGTHENED NICKEL-BASE SUPERALLOY 审中-公开
标题翻译：生产氧化物分散强化镍基超级合金的方法
公开(公告)号：US20110103961A1
公开(公告)日：2011-05-05
申请号：US12891188
申请日：2010-09-27
申请人： Neil E. GLOVER , Catherine M.F. RAE , Mark C. HARDY , Robert J. MITCHELL
发明人： Neil E. GLOVER , Catherine M.F. RAE , Mark C. HARDY , Robert J. MITCHELL
IPC分类号： B64C27/46 , C23C4/10 , B32B15/04 , B22F1/00
CPC分类号： C22C1/1031 , B22F3/115 , C22C19/056 , C22C32/0026
摘要： A method of producing an oxide dispersion strengthened nickel-base superalloy, comprising introducing an oxide dispersoid material into a plasma gun of a plasma spray apparatus, where it is sublimed and turned to vapour; and introducing a nickel-base superalloy material into the plasma spray apparatus at a cooler location, downstream of the plasma gun, such that the oxide dispersoid material condenses on the superalloy material to produce the oxide dispersion strengthened nickel-base superalloy.
摘要翻译：一种生产氧化物分散强化的镍基超级合金的方法，包括将氧化物分散质材料引入等离子喷涂装置的等离子体枪中，在其中升华并转向蒸气; 并在等离子体枪的下游的较冷的位置将镍基超合金材料引入等离子体喷涂装置中，使得氧化物分散质材料在超合金材料上冷凝以产生氧化物分散强化的镍基超级合金。

5. 发明申请

US20120269646A1 NICKEL BASE SUPERALLOY 审中-公开
标题翻译：镍基超级合金
公开(公告)号：US20120269646A1
公开(公告)日：2012-10-25
申请号：US13538184
申请日：2012-06-29
申请人： Robert J. MITCHELL , Mark C. HARDY
发明人： Robert J. MITCHELL , Mark C. HARDY
IPC分类号： C22C19/05 , C22C30/00 , F01D5/14 , B22F3/00
CPC分类号： C22C19/056 , C22C1/0433 , C22C1/0491 , C22C19/07 , C22C30/00
摘要： A nickel base superalloy consisting of 20 to 40 wt % cobalt, 10 to 15 wt % chromium, 3 to 6 wt % molybdenum, 0 to 5 wt % tungsten, 2.5 to 4 wt % aluminium, 3.4 to 5 wt % titanium, 1.35 to 2.5 wt % tantalum, 0 to 2 wt % niobium, 0.5 to 1 wt % hafnium, 0 to 0.1 wt % zirconium, 0.01 to 0.05 wt % carbon, 0.01 to 0.05 wt % boron, 0 to 2 wt % silicon and the balance nickel plus incidental impurities. The gamma prime phase comprises (Ni/Co)3 (Al/Ti/Ta).
摘要翻译：由20〜40重量％的钴，10〜15重量％的铬，3〜6重量％的钼，0〜5重量％的钨，2.5〜4重量％的铝，3.4〜5重量％的钛，1.35〜 2.5重量％的钽，0至2重量％的铌，0.5至1重量％的铪，0至0.1重量％的锆，0.01至0.05重量％的碳，0.01至0.05重量％的硼，0至2重量％的硅，加附加杂质。 γ'相包括（Ni / Co）3（Al / Ti / Ta）。

6. 发明申请

US20110198001A1 METHOD OF HEAT TREATING A SUPERALLOY COMPONENT AND AN ALLOY COMPONENT 有权
标题翻译：加热处理超级组件和合金部件的方法
公开(公告)号：US20110198001A1
公开(公告)日：2011-08-18
申请号：US13097567
申请日：2011-04-29
申请人： Robert J. MITCHELL , David U. FURRER , Joseph A. LEMSKY , Mark C. HARDY
发明人： Robert J. MITCHELL , David U. FURRER , Joseph A. LEMSKY , Mark C. HARDY
IPC分类号： C22C19/03 , C22C14/00
CPC分类号： C21D1/70 , C21D1/26 , C21D9/0068 , C21D2221/00
摘要： A method of heat treating a superalloy component includes solution heat treating the component at a temperature below the gamma prime solvus temperature to produce a fine grain structure. Insulation is placed over a first area to form an insulated assembly that is placed in a furnace at a temperature below the solvus temperature and maintained at that temperature for a predetermined time to achieve a uniform temperature. The temperature is increased at a predetermined rate to a temperature above the solvus temperature to maintain a fine grain structure in a first region, produce a coarse grain structure in a second region and produce a transitional structure in a third region between the first and second regions. The insulated assembly is removed from the furnace when the second region has been above the solvus temperature for a predetermined time and/or the first region has reached a predetermined temperature.
摘要翻译：热处理超合金部件的方法包括在低于γ'固溶温度的温度下对组分进行固溶热处理以产生细晶粒结构。将绝缘材料放置在第一区域上以形成绝缘组件，其被放置在低于固溶温度的温度下的炉中，并在该温度下保持预定时间以达到均匀的温度。将温度以预定的速率增加到高于溶剂温度的温度以保持第一区域中的细晶粒结构，在第二区域中产生粗晶粒结构，并在第一和第二区域之间的第三区域中产生过渡结构。当第二区域已经超过固溶温度达预定时间和/或第一区域已经达到预定温度时，将绝热组件从炉中移出。

7. 发明授权

US08083872B2 Method of heat treating a superalloy component and an alloy component 有权
标题翻译：高温合金部件和合金部件的热处理方法
公开(公告)号：US08083872B2
公开(公告)日：2011-12-27
申请号：US12155826
申请日：2008-06-10
申请人： Robert J Mitchell , David U Furrer , Joseph A Lemsky , Mark C Hardy
发明人： Robert J Mitchell , David U Furrer , Joseph A Lemsky , Mark C Hardy
IPC分类号： C21D9/00 , C22F1/10
CPC分类号： C21D1/70 , C21D1/26 , C21D9/0068 , C21D2221/00
摘要： A method of heat treating a superalloy component includes solution heat treating the component at a temperature below the gamma prime solvus temperature to produce a fine grain structure. Insulation is placed over a first area to form an insulated assembly that is placed in a furnace at a temperature below the solvus temperature and maintained at that temperature for a predetermined time to achieve a uniform temperature. The temperature is increased at a predetermined rate to a temperature above the solvus temperature to maintain a fine grain structure in a first region, produce a coarse grain structure in a second region and produce a transitional structure in a third region between the first and second regions. The insulated assembly is removed from the furnace when the second region has been above the solvus temperature for a predetermined time and/or the first region has reached a predetermined temperature.
摘要翻译：热处理超合金部件的方法包括在低于γ'固溶温度的温度下对组分进行固溶热处理以产生细晶粒结构。将绝缘材料放置在第一区域上以形成绝缘组件，其被放置在低于固溶温度的温度下的炉中，并在该温度下保持预定时间以达到均匀的温度。将温度以预定的速率增加到高于溶剂温度的温度以保持第一区域中的细晶粒结构，在第二区域中产生粗晶粒结构，并在第一和第二区域之间的第三区域中产生过渡结构。当第二区域已经超过固溶温度达预定时间和/或第一区域已经达到预定温度时，将绝热组件从炉中移出。

8. 发明申请

US20090071580A1 Method of heat treating a superalloy component and an alloy component 有权
标题翻译：高温合金部件和合金部件的热处理方法
公开(公告)号：US20090071580A1
公开(公告)日：2009-03-19
申请号：US12155826
申请日：2008-06-10
申请人： Robert J. Mitchell , David U. Furrer , Joseph A. Lemsky , Mark C. Hardy
发明人： Robert J. Mitchell , David U. Furrer , Joseph A. Lemsky , Mark C. Hardy
IPC分类号： C22F1/10 , C21D9/00
CPC分类号： C21D1/70 , C21D1/26 , C21D9/0068 , C21D2221/00
摘要： A method of heat treating a superalloy component comprises solution heat treating the component at a temperature below the gamma prime solvus temperature to produce a fine grain structure in the component. Insulation is placed over a first area of the component to form an insulated assembly. The insulated assembly is placed in a furnace at a temperature below the solvus temperature and maintained at that temperature for a predetermined time to achieve a uniform temperature in the component. The temperature is increased at a predetermined rate to a temperature above the solvus temperature to maintain a fine grain structure in a first region, to produce a coarse grain structure in a second region and to produce a transitional structure in a third region between the first and second regions of the component. The insulated assembly is removed from the furnace when the second region of the component has been above the solvus temperature for a predetermined time and/or the first region of the component has reached a predetermined temperature.
摘要翻译：热处理超合金部件的方法包括在低于伽马质子溶质温度的温度下对组分进行固溶热处理，以在组分中产生细晶粒结构。绝缘被放置在部件的第一区域上以形成绝缘组件。将绝缘组件放置在低于固溶温度的温度下的炉中，并在该温度下保持预定时间，以实现组分中均匀的温度。温度以预定速率增加到高于溶剂温度的温度，以在第一区域中保持细晶粒结构，以在第二区域中产生粗晶粒结构，并在第一区域和第二区域之间的第三区域产生过渡结构组件的第二个区域。当组件的第二区域已经高于固相温度达预定时间和/或部件的第一区域已经达到预定温度时，将绝热组件从炉中移除。

9. 发明申请

US20120006452A1 METHOD OF IMPROVING THE MECHANICAL PROPERTIES OF A COMPONENT 审中-公开
标题翻译：改善组分的机械性能的方法
公开(公告)号：US20120006452A1
公开(公告)日：2012-01-12
申请号：US13162205
申请日：2011-06-16
申请人： Robert J. MITCHELL , David U. FURRER , Mark C. HARDY
发明人： Robert J. MITCHELL , David U. FURRER , Mark C. HARDY
IPC分类号： C21D9/00 , C22F1/10 , C22F1/18
CPC分类号： C22F1/10 , C22C1/023 , C22C14/00 , C22C19/03 , C22C19/05 , C22C19/051 , C22C19/056 , C22C19/057 , C22F1/183 , F01D5/02 , F05D2230/10 , F05D2230/25 , F05D2230/40
摘要： A method (40) of improving the mechanical properties of a component, for example a gas turbine engine turbine disc, (24) comprises isothermally forging (42) a preform to produce a shaped preform with a predetermined shape at a first predetermined temperature, solution heat treating (44) the shaped preform, quenching (46) the shaped preform, forging (48) the shaped preform at a second predetermined temperature to impart a predetermined residual strain in the shaped preform, ageing (50) the shaped preform and finally machining (52) the shaped preform to a finished shape. The second predetermined temperature is less than the first predetermined temperature.
摘要翻译：改进组件（例如燃气涡轮发动机涡轮盘）的机械性能的方法（40）包括等温锻造（42）预制件，以在第一预定温度下产生具有预定形状的成形预制件，溶液对成形预成型件进行热处理（44），淬火（46）成形预成型件，在第二预定温度下锻造（48）成形预成型件，以在成形预制件中赋予预定的残余应变，使成形预成型件老化（50）（52）成形的预成型件成型成形。第二预定温度小于第一预定温度。

10. 发明申请

US20110123386A1 METHOD OF MANUFACTURING A MULTIPLE COMPOSITION COMPONENT 有权
标题翻译：制造多种组成成分的方法
公开(公告)号：US20110123386A1
公开(公告)日：2011-05-26
申请号：US12946168
申请日：2010-11-15
申请人： Robert J. MITCHELL , Catherine M.F. RAE , Mark C. HARDY , Shaun R. HOLMES
发明人： Robert J. MITCHELL , Catherine M.F. RAE , Mark C. HARDY , Shaun R. HOLMES
IPC分类号： B22F3/15
CPC分类号： B22F5/009 , B22F3/15 , B22F5/106 , B22F7/062 , B22F2999/00
摘要： The present invention relates to a method of manufacturing a multiple composition component 10, comprising: arranging first, second and third constituent parts 40, 30, 42 having first, second and third compositions respectively A, B, C so that the first constituent part 40 shares a first boundary with the second constituent part 30 and the second constituent part 30 shares a second boundary with the third constituent part 40. The first, second and third constituent parts 40, 30, 42 are each either a powder or a solid so that the first and second boundaries are each a solid adjacent to a powder. The arrangement is then processed so as to form a single solid component having first, second and third regions 16, 18, 20 having first, second and third compositions A, B, C respectively.
摘要翻译：本发明涉及一种多组分成分10的制造方法，其特征在于，包括：将分别具有A，B，C的第一，第二和第三组分的第一，第二和第三组分40,30,42分别排列成第一组成部分40 与第二构成部分30共享第一边界，并且第二构成部分30与第三构成部分40共享第二边界。第一，第二和第三组成部分40,30,42各自是粉末或固体，使得第一和第二边界各自是与粉末相邻的固体。然后处理该装置以形成具有分别具有第一，第二和第三组合物A，B，C的第一，第二和第三区域16,18,20的单个固体组分。

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