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    • 3. 发明授权
    • Heat-resisting steel, method for thermally treating heat-resisting steel, and components made of heat-resisting steel
    • 耐热钢,耐热钢热处理方法以及由耐热钢制成的部件
    • US06821360B2
    • 2004-11-23
    • US09725234
    • 2000-11-29
    • Ryuichi IshiiYoichi TsudaMasayuki Yamada
    • Ryuichi IshiiYoichi TsudaMasayuki Yamada
    • C22C3818
    • C22C38/32C21D1/28C21D9/38C22C38/001C22C38/22C22C38/24C22C38/26C22C38/28
    • A heat-resisting steel comprising 0.15-0.30 wt. % C, 0.05-0.3 wt. % Si, 0.01-0.7 wt. % Mn, 1.8-2.5 wt. % Cr, 0.15-0.23 wt. % V, 1.5-2.5 wt. % W, 0.01-0.02 wt. % Ti, 0.01-0.08 wt. % Nb, 0.005-0.03 wt. % N, 0.001-0.015 wt. % B, and Fe and unavoidable impurities as the remainder; a heat-resisting steel comprising 0.15-0.30 wt. % C, 0.05-0.3 wt. % Si, 0.01-0.7 wt. % Mn, 1.8-2.5 wt. % Cr, 0.15-0.23 wt. % V, 1.5-2.5 wt. % W, 0.3-0.8 wt. % Mo, 0.01-0.02 wt. % Ti, 0.01-0.08 wt. % Nb, 0.005-0.03 wt. % N, 0.001-0.015 wt. % B, and Fe and unavoidable impurities as the remainder; and a heat-resisting steel that is obtained by subjecting one of the above heat-resisting steels to a heat treatment comprising the step of oil-cooling the heat-resisting steel to a temperature of 300° C. or lower. These heat-resisting steels are excellent in both high-temperature strength and impact properties.
    • 一种耐热钢,其含有0.15-0.30wt。 %C,0.05-0.3重量% %Si,0.01-0.7wt。 %Mn,1.8-2.5重量% %Cr,0.15-0.23wt。 %V,1.5-2.5wt。 %W,0.01-0.02wt。 %Ti,0.01-0.08wt。 %Nb,0.005-0.03wt。 %N,0.001-0.015wt。 %B,Fe和其余的不可避免的杂质; 包含0.15-0.30重量%的耐热钢。 %C,0.05-0.3重量% %Si,0.01-0.7wt。 %Mn,1.8-2.5重量% %Cr,0.15-0.23wt。 %V,1.5-2.5wt。 %W,0.3-0.8wt。 %Mo,0.01-0.02wt。 %Ti,0.01-0.08wt。 %Nb,0.005-0.03wt。 %N,0.001-0.015wt。 %B,Fe和其余的不可避免的杂质; 以及耐热钢,其通过使上述耐热钢中的一种进行热处理而获得,所述热处理包括将耐热钢的油冷却步骤至300℃或更低的温度。 这些耐热钢在高温强度和冲击性方面均优异。
    • 6. 发明授权
    • High pressure-low pressure single cylinder turbine rotor and method of
making
    • 高压低压单缸汽轮机转子及其制造方法
    • US5611873A
    • 1997-03-18
    • US413156
    • 1995-03-29
    • Masayuki YamadaYoichi Tsuda
    • Masayuki YamadaYoichi Tsuda
    • G11B5/86C21D9/38C22C38/46C21D8/10C22C38/44
    • C22C38/46C21D9/38
    • A high pressure-low pressure single cylinder turbine rotor is disclosed which is characterized by being formed of a steel of a composition having, by weight, a C content of from 0.10 to 0.35%, a Si (silicon) content of not more than 0.3% (not including 0%), a Mn (manganese) content of not more than 1.0% (not including 0%), a Ni content of from 1.0 to 2.0%, a Cr (chromium) content of from 1.5 to 3.0%, a Mo content of from 0.9 to 1.3%, a V (vanadium) content of from 0.10 to 0.35%, a Nb (niobium) content of from 0.01 to 0.15%, a W content of from 0.1 to 1.5%, and the balance of Fe (iron) and inevitable impurities, the inevitable impurities having a P content of not more than 0.005%, a S content of not more than 0.001%, an As content of not more than 0.008%, a Sb content of not more than 0.004%, and a Sn content of not more than 0.008%.
    • 公开了一种高压低压单缸汽轮机转子,其特征在于由具有0.10至0.35重量%的C含量,不大于0.3的Si(硅)含量的组合物的钢形成 %(不包括0%),Mn(锰)含量不大于1.0%(不包括0%),Ni含量为1.0至2.0%,Cr(铬)含量为1.5至3.0% Mo含量为0.9〜1.3%,V(钒)含量为0.10〜0.35%,Nb(铌)含量为0.01〜0.15%,W含量为0.1〜1.5%,余量为 Fe(铁)和不可避免的杂质,P含量不大于0.005%,S含量不大于0.001%,As含量不大于0.008%,Sb含量不大于0.004的不可避免的杂质 %,Sn含量不大于0.008%。
    • 8. 发明授权
    • Heat resistant steel casting and method of manufacturing the same
    • 耐热铸钢及其制造方法
    • US06494970B1
    • 2002-12-17
    • US09721977
    • 2000-11-27
    • Ryuichi IshiiYoichi TsudaMasayuki Yamada
    • Ryuichi IshiiYoichi TsudaMasayuki Yamada
    • C22C3822
    • C22C38/46C21D1/18C21D6/002C21D6/02C21D2211/003C21D2211/004C22C38/001C22C38/44C22C38/54
    • Disclosed is a heat resistant steel casting, comprising C, 0.15-0.3%, Si, 0.1-0.30%, Mn, 0.01-0.1%, Cr, 2.0-2.5%, Mo, 0.3-0.8%, V, 0.23-0.3%, W, 1.6-2.6%, N, 0.005-0.03%, B, 0.001-0.004%, impurity elements including Ni not larger than 0.2%, P not larger than 0.03% and S not larger than 0.01%, B equivalent determined by B+0.5N given below being not larger than 0.02%, Mo equivalent determined by Mo+0.5W given below falling within a range of between 1.4% and 2.0%, and C equivalent determined by C+Mn/6+Si/24+Ni/40+Cr/5+Mo/14+V/14 given below being not smaller than 0.65%, and balance of iron wherein a precipitated phase consisting of a M23C6 carbide, a M7C3 carbide, and MX carbonitride is a texture finely precipitated in a matrix phase, and a ratio of the precipitated phase to the matrix phase falls within a range of between 0.6% and 1.0%.
    • 公开了一种耐热钢铸件,包括C:0.15-0.3%,Si,0.1-0.30%,Mn,0.01-0.1%,Cr,2.0-2.5%,Mo,0.3-0.8%,V,0.23-0.3% ,W为1.6-2.6%,N为0.005-0.03%,B为0.001-0.004%,包含Ni不大于0.2%的杂质元素,P不大于0.03%,S不大于0.01%,B等价物由 以下给出的B + 0.5N不大于0.02%,由Mo + 0.5W确定的Mo当量在1.4%至2.0%之间的范围内,C等于由C + Mn / 6 + Si / 24 + 下面给出的Ni / 40 + Cr / 5 + Mo / 14 + V / 14不小于0.65%,其中由M23C6碳化物,M7C3碳化物和MX碳氮化物组成的沉淀相的余量为精细沉淀的织构 在基质相中,析出相与基体相的比例在0.6%〜1.0%的范围内。
    • 9. 发明授权
    • Steam turbine
    • 汽轮机
    • US06368057B1
    • 2002-04-09
    • US09494347
    • 2000-01-31
    • Toru TakahashiKenichi ImaiRyou OdaYoichi Tsuda
    • Toru TakahashiKenichi ImaiRyou OdaYoichi Tsuda
    • F01D102
    • F01D1/04F05D2260/231
    • A steam turbine includes a turbine high pressure section, a turbine intermediate pressure section and a turbine low pressure section, in which at least two or more of these pressure sections are combined together, and a turbine rotor which is subjected to a gradient thermal treatment at different thermal treating temperatures at respective pressure sections is rotatably supported by bearings and accommodated in a turbine casing, and in a case where an axial distance from a setting position of a turbine movable blade of a final stage of the turbine low pressure section to a setting position of a partition plate disposed at a time when the gradient thermal treatment is performed to each of the pressure sections at different thermal treating temperature is defined as A, a blade length of the turbine movable blade is defined as B, and an axial distance from a prior stage of the final stage of the turbine low pressure section to the setting position of the partition plate is defined as C, the setting position of the partition plate is set in a range of (A/B)≧0.9 and C≧300 mm.
    • 蒸汽涡轮机包括涡轮机高压部分,涡轮中间压力部分和涡轮机低压部分,其中这些压力部分中的至少两个或更多个组合在一起,以及涡轮转子,其经受梯度热处理 各个压力部分的不同的热处理温度由轴承可旋转地支撑并容纳在涡轮机壳体中,并且在从涡轮机低压部分的最后级的涡轮可动叶片的设定位置到轴向距离的设置 将在不同的热处理温度下对每个压力部进行梯度热处理时设置的隔板的位置定义为A,将涡轮机动叶片的叶片长度定义为B,将轴距离 涡轮机低压部分的最后阶段到分隔板的设定位置的前一阶段被定义为C,t 分隔板的设定位置设定在(A / B)> 0.9,C> = 300mm的范围内。