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    • 2. 发明申请
    • TECHNIQUES FOR CONTROLLING PRECIPITATE PHASE DOMAIN SIZE IN AN ALLOY
    • 用于控制合金中的相位相位尺寸的技术
    • US20100252151A1
    • 2010-10-07
    • US12755170
    • 2010-04-06
    • David U. FurrerRandolph C. Helmink
    • David U. FurrerRandolph C. Helmink
    • C21D1/00C22F1/00
    • C21D1/00C21D2221/00C22F1/00C22F1/10C22F1/183
    • A heat treatment technique may include heating an alloy component to a temperature above a transition temperature of the alloy or heating an alloy component to a temperature below the transition temperature of the alloy. The heat treatment technique further may include cooling a first portion of the alloy component at a first cooling rate, and cooling a second portion of the alloy component at a second cooling rate different than the first rate. The first cooling rate may result in formation of a plurality of first precipitate phase domains comprising a first average size in the first portion, and the second cooling rate may result in formation of a plurality of second precipitate phase domains comprising a second average size in the second portion. The average size of the first precipitate phase domains may be different than the average size of the second precipitate phase domains.
    • 热处理技术可以包括将合金组分加热至高于合金转变温度的温度或将合金组分加热至低于合金转变温度的温度。 热处理技术还可以包括以第一冷却速度冷却合金部件的第一部分,并以不同于第一速率的第二冷却速率冷却合金部件的第二部分。 第一冷却速率可能导致在第一部分中形成包含第一平均尺寸的多个第一沉淀相结构域,第二冷却速率可导致形成多个第二沉淀相结构域 第二部分。 第一沉淀相结构域的平均尺寸可以不同于第二沉淀相结构域的平均尺寸。
    • 3. 发明申请
    • Method of heat treating a superalloy component and an alloy component
    • 高温合金部件和合金部件的热处理方法
    • US20090071580A1
    • 2009-03-19
    • US12155826
    • 2008-06-10
    • Robert J. MitchellDavid U. FurrerJoseph A. LemskyMark C. Hardy
    • Robert J. MitchellDavid U. FurrerJoseph A. LemskyMark C. Hardy
    • C22F1/10C21D9/00
    • C21D1/70C21D1/26C21D9/0068C21D2221/00
    • 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.
    • 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。
    • 4. 发明授权
    • Techniques for controlling precipitate phase domain size in an alloy
    • 控制合金中沉淀相域尺寸的技术
    • US08721812B2
    • 2014-05-13
    • US12755170
    • 2010-04-06
    • David U. FurrerRandolph C. Helmink
    • David U. FurrerRandolph C. Helmink
    • C21D1/00C21D9/00C22F1/10
    • C21D1/00C21D2221/00C22F1/00C22F1/10C22F1/183
    • A heat treatment technique may include heating an alloy component to a temperature above a transition temperature of the alloy or heating an alloy component to a temperature below the transition temperature of the alloy. The heat treatment technique further may include cooling a first portion of the alloy component at a first cooling rate, and cooling a second portion of the alloy component at a second cooling rate different than the first rate. The first cooling rate may result in formation of a plurality of first precipitate phase domains comprising a first average size in the first portion, and the second cooling rate may result in formation of a plurality of second precipitate phase domains comprising a second average size in the second portion. The average size of the first precipitate phase domains may be different than the average size of the second precipitate phase domains.
    • 热处理技术可以包括将合金组分加热至高于合金转变温度的温度或将合金组分加热至低于合金转变温度的温度。 热处理技术还可以包括以第一冷却速度冷却合金部件的第一部分,并以不同于第一速率的第二冷却速率冷却合金部件的第二部分。 第一冷却速率可能导致在第一部分中形成包含第一平均尺寸的多个第一沉淀相结构域,第二冷却速率可导致形成多个第二沉淀相结构域 第二部分。 第一沉淀相结构域的平均尺寸可以不同于第二沉淀相结构域的平均尺寸。
    • 5. 发明授权
    • Integrally stiffened rings
    • 整体加硬环
    • US5115655A
    • 1992-05-26
    • US649596
    • 1991-02-01
    • James R. MartinJames P. KuchmaDavid U. Furrer
    • James R. MartinJames P. KuchmaDavid U. Furrer
    • B21H1/06B21H7/00B23P15/24
    • B21H8/005B21H1/06B23P15/24
    • A method for preparing rings having an integral stiffening geometric pattern on its outer surface is disclosed. The method employs a variation of the drum rolling process, but it incorporates unique tooling for providing the pattern, preferably comprising a plurality of segments which fit together to define a ring, the inner surface of which presents the desired pattern toward the center of the ring. A unique drum arrangement includes inner and outer components for locking the segments in place and for providing the structural integrity required for the final drum rolling operation. A cylinder, for example an aluminum or aluminum alloy cylinder, is placed in the drum, the cylinder being preformed and presized to fit concentrically within the segment defining ring. Following heating of the assembly to forming temperature, the cylinder is radially expanded using a sizing tool, and the assembly is then placed over a mandrel in preparation for drum rolling. In the illustrated embodiment, an isogrid pattern of recesses is formed in the segments, so that upon completion of drum rolling and disassembly of the drum and segments, a raised, integral isogrid stiffening pattern is provided on the outer ring cylinder surface.
    • 公开了一种在其外表面上制备具有整体硬化几何图案的环的方法。 该方法采用滚筒轧制过程的变型,但是它包含用于提供图案的独特的工具,优选地包括多个段,所述多个段组合在一起以限定环,其内表面朝向环的中心呈现期望的图案 。 独特的鼓装置包括内部和外部部件,用于将节段锁定在适当位置并提供终轧滚筒操作所需的结构完整性。 将圆筒(例如铝或铝合金圆筒)放置在滚筒中,该圆柱体被预成型并且被预定为同心地配合在该段限定环内。 在将组件加热到成形温度之后,使用定径工具将圆筒径向膨胀,然后将组件放置在心轴上以准备滚筒滚动。 在所示的实施例中,在段中形成凹槽的等间距图案,使得在滚筒滚动和滚筒和分段的拆卸完成之后,在外圈滚筒表面上设置有凸起的整体式同格栅加强图案。