首页> 外国专利> Blanks for Forging of powder compact rotor and forged, pressed from powder ROTOR TURBINE AND ITS MANUFACTURING METHODS

Blanks for Forging of powder compact rotor and forged, pressed from powder ROTOR TURBINE AND ITS MANUFACTURING METHODS

机译:粉末压坯转子的锻造毛坯,由粉末压制的压制毛坯汽轮机及其制造方法

摘要

1. The preform (200) for forging a rotor disk (10) of the turbine, comprising: a body (202) of material (8) of special alloy, having a weight of about 2268 kg (5,000 pounds) or more, the material (8) has a special alloy a substantially uniform morphology of the grains and the average grain size of ASTM 10 or menee.2. Forged rotor disk (10), the turbine comprising: a substantially cylindrical disk of material (8) of special alloy, having a weight of about 2268 kg (5,000 pounds) or more, the material (8) special alloy has a substantially uniform morphology of the grains and the average the grain size of approximately ASTM 10 or menee.3. the rotor disk (10) of the turbine according to claim 2, wherein the material (8) comprises a special alloy special alloy based on Fe, Fe-Ni, Ni or Co.4. the rotor disk (10) of the turbine according to claim 2, wherein the average ASTM grain size of from about 10 to about 16.5. The disc (10) The turbine rotor of claim 2, wherein the disc has a central bore (9) and an outer edge (11) and the material (8) has a special alloy elongation and yield strength, the elongation and the yield strength are of substantially identical to the central channel (9) to the outer edge (11) .6. A method of manufacturing a rotor (100) of a turbine comprising: providing a particulate material (110), special alloy, and pressing (120) the special alloy powder material to form a sintered powder compact - forging preform for turbiny.7 rotor disk. Method of manufacture (100) of the turbine rotor according to claim 6, further comprising forging the preform (130) to obtain turbiny.8 rotor disk. The method (100) of the turbine rotor manufacturing according to claim 6, wherein providing a powder material (110) including a special alloy
机译:1.一种用于锻造涡轮机转子盘(10)的预成型件(200),其包括:重量为约2268kg(5,000磅)或更大的特殊合金材料(8)的主体(202),材料(8)具有一种特殊的合金,其晶粒形态基本均一,平均晶粒尺寸为ASTM 10或Menee.2。锻造转子盘(10),涡轮机包括:重量约为2268千克(5,000磅)或更高的特殊合金材料(8)的基本上圆柱形的盘,该特殊合金材料(8)具有基本均匀的形态晶粒的平均粒径约为ASTM 10或3。 3.根据权利要求2所述的涡轮的转子盘(10),其中,所述材料(8)包括基于Fe,Fe-Ni,Ni或Co.4的特殊合金特殊合金。 3.根据权利要求2所述的涡轮机的转子盘(10),其中,所述平均ASTM晶粒尺寸为约10至约16.5。 3.根据权利要求2所述的盘片(10),其特征在于,所述盘片具有中心孔(9)和外边缘(11),并且所述材料(8)具有特殊的合金伸长率和屈服强度,所述伸长率和屈服强度与中央通道(9)至外边缘(11).6基本相同。一种制造涡轮机转子(100)的方法,该方法包括:提供颗粒材料(110),特殊合金,以及对特殊合金粉末材料进行压制(120)以形成用于涡轮机的烧结粉末压坯-锻造预成型坯.7转子盘。 7.根据权利要求6所述的涡轮转子的制造方法(100),其特征在于,还包括锻造所述预成型件(130)以获得涡轮8转子盘。 7.根据权利要求6所述的涡轮转子的制造方法(100),其中,提供包括特殊合金的粉末材料(110)。

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