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1. 发明申请

US20070163682A1 Ni-based superalloy having high oxidation resistance and gas turbine part 审中-公开
标题翻译：具有高抗氧化性的Ni基超级合金和燃气轮机部件
公开(公告)号：US20070163682A1
公开(公告)日：2007-07-19
申请号：US11591561
申请日：2006-11-02
申请人： Hideki Tamaki , Akira Yoshinari , Akira Okayama , Tsuyoshi Takano , Hiroyuki Doi
发明人： Hideki Tamaki , Akira Yoshinari , Akira Okayama , Tsuyoshi Takano , Hiroyuki Doi
IPC分类号： C22C19/05
CPC分类号： C22C19/056 , C22C19/057
摘要： A Ni-based alloy hardened with the γ phase, which is able to exhibit not only superior strength at high temperatures, but also excellent hot corrosion resistance and oxidation resistance at high temperatures in spite of containing no Re or reducing the amount of Re. The Ni-based superalloy contains, by weight, C: 0.01 to 0.5%, B: 0.01 to 0.04%, Hf: 0.1 to 2.5%, Co: 0.8 to 15%, Ta: more than 0% but less than 8.5%, Cr: 1.5 to 16%, Mo: more than 0% but less than 1.0%, W: 5 to 14%, Ti: 0.1 to 4.75%, Al: 2.5 to 7%, Nb: more than 0 % but less than 4%, V: 0 to less than 1.0%, Zr: 0 to less than 0.1%, Re: 0 to less than 9%, at least one of platinum group elements: 0 to less than 0.5% in total, at least one of rare earth elements: 0 to less than 0.1% in total, and the rest being Ni except for unavoidable impurities.
摘要翻译：使用γ相硬化的Ni基合金，不仅在高温下不仅表现出优异的强度，而且在高温下也能表现出优异的耐热腐蚀性和耐氧化性，尽管不含Re或减少Re的量。 Ni基超合金含有C：0.01〜0.5％，B：0.01〜0.04％，Hf：0.1〜2.5％，Co：0.8〜15％，Ta：0％以上且小于8.5％ Cr：1.5〜16％，Mo：大于0％但小于1.0％，W：5〜14％，Ti：0.1〜4.75％，Al：2.5〜7％，Nb：大于0％％，V：0〜小于1.0％，Zr：0〜小于0.1％，Re：0〜小于9％，铂族元素中的至少一种：0〜小于0.5％稀土元素总计为0〜小于0.1％，其余为Ni，不含不可避免的杂质。

2. 发明授权

US07169241B2 Ni-based superalloy having high oxidation resistance and gas turbine part 有权
标题翻译：具有高抗氧化性的Ni基超级合金和燃气轮机部件
公开(公告)号：US07169241B2
公开(公告)日：2007-01-30
申请号：US10804065
申请日：2004-03-19
申请人： Hideki Tamaki , Akira Yoshinari , Akira Okayama , Tsuyoshi Takano , Hiroyuki Doi
发明人： Hideki Tamaki , Akira Yoshinari , Akira Okayama , Tsuyoshi Takano , Hiroyuki Doi
IPC分类号： C22C19/05
CPC分类号： C22C19/056 , C22C19/057
摘要： A Ni-based alloy hardened with the γ′ phase, which is able to exhibit not only superior strength at high temperatures, but also excellent hot corrosion resistance and oxidation resistance at high temperatures in spite of containing no Re or reducing the amount of Re. The Ni-based superalloy contains, by weight, C: 0.01 to 0.5%, B: 0.01 to 0.04%, Hf: 0.1 to 2.5%, Co: 0.8 to 15%, Ta: more than 0% but less than 8.5%, Cr: 1.5 to 16%, Mo: more than 0% but less than 1.0%, W: 5 to 14%, Ti: 0.1 to 4.75%, Al: 2.5 to 7%, Nb: more than 0% but less than 4%, V: 0 to less than 1.0%, Zr: 0 to less than 0.1%, Re: 0 to less than 9%, at least one of platinum group elements: 0 to less than 0.5% in total, at least one of rare earth elements: 0 to less than 0.1% in total, and the rest being Ni except for unavoidable impurities.
摘要翻译：用γ-相硬化的Ni基合金，不仅在高温下不仅表现出优异的强度，而且在高温下也表现出优异的耐热腐蚀性和抗氧化性，尽管不含Re或减少Re的量。 Ni基超合金含有C：0.01〜0.5％，B：0.01〜0.04％，Hf：0.1〜2.5％，Co：0.8〜15％，Ta：0％以上且小于8.5％ Cr：1.5〜16％，Mo：大于0％但小于1.0％，W：5〜14％，Ti：0.1〜4.75％，Al：2.5〜7％，Nb：大于0％％，V：0〜小于1.0％，Zr：0〜小于0.1％，Re：0〜小于9％，铂族元素中的至少一种：0〜小于0.5％稀土元素总计为0〜小于0.1％，其余为Ni，不含不可避免的杂质。

3. 发明授权

US6051083A High strength Ni-base superalloy for directionally solidified castings 失效
标题翻译：用于定向凝固铸件的高强度Ni基超级合金
公开(公告)号：US6051083A
公开(公告)日：2000-04-18
申请号：US799017
申请日：1997-02-07
申请人： Hideki Tamaki , Akira Yoshinari , Akira Okayama , Mitsuru Kobayashi , Kagehiro Kageyama , Takehiro Ohno
发明人： Hideki Tamaki , Akira Yoshinari , Akira Okayama , Mitsuru Kobayashi , Kagehiro Kageyama , Takehiro Ohno
IPC分类号： B22D27/04 , C22C19/05 , C22C19/00
CPC分类号： B22D27/045 , C22C19/056 , C22C19/057
摘要： In order to provide a high strength Ni-base superalloy for directionally solidified castings, which is prevented from solidification cracking at the casting, having a sufficient grain boundary strength for ensuring reliability during its operation and a superior high temperature concurrently, a high strength Ni-base superalloy for directionally solidified castings having a superior grain boundary strength, which contains C: 0.05% to less than 0.1%, B: 0.015% to 0.04%, Hf: 0.01.about.less than 0.5%, Zr: less than 0.01%, Cr: 1.5%.about.16%, Mo: utmost 6%, W: 2.about.12%, Re: 0.1.about.9%, Ta: 2.about.12%, Nb: utmost 4%, Al: 4.5.about.6.5%, Ti: less than 0.5%, Co: less than 9%, and Ni: at least 60% in weight, is disclosed.
摘要翻译：为了提供用于定向凝固铸件的高强度Ni基超合金，其在铸造时防止固化裂纹，具有足够的晶界强度以确保其操作期间的可靠性和高的高温同时，高强度的Ni- 具有优异的晶界强度的定向凝固铸件用基体超合金，其含有C：0.05〜小于0.1％，B：0.015％〜0.04％，Hf：0.01分散度小于0.5％，Zr：小于0.01％，Cr ：1.5％差异16％，Mo：最大6％，W：2差异12％，Re：0.1差异9％，Ta：2差异12％，Nb：最大4％，Al：4.5差异6.5％，Ti：较小不超过0.5％，Co：小于9％，Ni：至少为60重量％。

4. 发明授权

US06818077B2 High-strength Ni-base superalloy and gas turbine blades 有权
标题翻译：高强度镍基超级合金和燃气轮机叶片
公开(公告)号：US06818077B2
公开(公告)日：2004-11-16
申请号：US10429801
申请日：2003-05-06
申请人： Akira Yoshinari , Hideki Tamaki , Hiroyuki Doi
发明人： Akira Yoshinari , Hideki Tamaki , Hiroyuki Doi
IPC分类号： C22C1905
CPC分类号： C22C19/058 , C22C19/056
摘要： A nickel-based superalloy containing 12.0 to 16.0% by weight of Cr, 4.0 to 9.0% by weight of Co, 3.4 to 4.6% by weight of Al, 0.5 to 1.6% by weight of Nb, 0.05 to 0.16% by weight of C, 0.005 to 0.025% by weight of B, and at least one of Ti, Ta and Mo. Amounts of Ti, Ta and Mo are ones calculated by the equations (1) and (2), wherein TiEq is 4.0 to 6.0 and MoEq is 5.0 to 8.0. TiEq=Ti % by weight+0.5153×Nb % by weight+0.2647×Ta % by weight (1) MoEq−Mo % by weight+0.5217×W % by weight+0.5303×Ta % by weight+1.0326×Nb % by weight (2)
摘要翻译：含有12.0〜16.0重量％的Cr，4.0〜9.0重量％的Co，3.4〜4.6重量％的Al，0.5〜1.6重量％的Nb，0.05〜0.16重量％的C的镍系超合金，0.005〜0.025重量％的B，以及Ti，Ta和Mo中的至少一种，Ti，Ta和Mo中的至少一个是通过式（1）和（2）计算的，TiEq为4.0〜6.0，MoEq 为5.0〜8.0。

5. 发明申请

US20090214379A1 NI-BASED SINGLE CRYSTAL ALLOY 审中-公开
标题翻译：基于NI的单晶合金
公开(公告)号：US20090214379A1
公开(公告)日：2009-08-27
申请号：US12389633
申请日：2009-02-20
申请人： Akira Yoshinari , Hideki Tamaki
发明人： Akira Yoshinari , Hideki Tamaki
IPC分类号： C22C19/05
CPC分类号： C22C19/057 , F01D5/28 , F05C2201/025 , F05C2201/0466 , F05D2300/11 , F05D2300/121 , F05D2300/131 , F05D2300/132 , F05D2300/134 , F05D2300/607 , Y02T50/671
摘要： Disclosed is a single crystal alloy consisting essentially of, by weight, 0.06-0.09% carbon, 0.016-0.035% B, 0.2-0.4% Hf, 0-0.02% Zr, 6.5-8.5% Cr, 0.4-1.0% Mo, 5.5-9.5% W, 1.2-3.1% Re, 8-10% Ta, 0.3-1.0% Nb, 0-0.4% Ti, 4.7-5.4% Al, 0.5-5.0% Co, 0.1-5% Fe, and the balance of Ni and unavoidable impurities. The alloy is free from solidification cracks during casting a large-sized blade of gas turbines, has grain boundary strength sufficient for assuring the reliability during operation, and further has excellent oxidation resistance to a high combustion gas temperature while having excellent high-temperature strength comparable to that of a conventional single crystal alloy.
摘要翻译：公开了基本上由0.06-0.09％的碳，0.016-0.035％的B，0.2-0.4％的Hf，0-0.02％的Zr，6.5-8.5％的Cr，0.4-1.0％的Mo，5.5 -9.5％W，1.2-3.1％Re，8-10％Ta，0.3-1.0％Nb，0-0.4％Ti，4.7-5.4％Al，0.5-5.0％Co，0.1-5％Fe，余量的Ni和不可避免的杂质。该合金在铸造大型燃气轮机叶片期间没有固化裂纹，具有足够的晶界强度以确保运行时的可靠性，并且还具有优异的耐高温燃烧气体温度的抗氧化性，同时具有优异的高温强度可比性与传统的单晶合金相比。

6. 发明授权

US5611670A Blade for gas turbine 失效
标题翻译：燃气轮机叶片
公开(公告)号：US5611670A
公开(公告)日：1997-03-18
申请号：US280992
申请日：1994-07-27
申请人： Akira Yoshinari , Hideki Tamaki , Tosiaki Saito , Mitsuru Kobayashi , Katsumi Iijima , Katsuo Wada , Kimio Kano , Hiroyuki Matsuzaki
发明人： Akira Yoshinari , Hideki Tamaki , Tosiaki Saito , Mitsuru Kobayashi , Katsumi Iijima , Katsuo Wada , Kimio Kano , Hiroyuki Matsuzaki
IPC分类号： B22D27/04 , C22C19/05 , C30B11/00 , F01D5/28 , F01D5/14
CPC分类号： F01D5/28 , B22D27/045 , C22C19/056 , C22C19/057 , C30B11/00 , C30B29/52 , Y02T50/671 , Y10S148/902
摘要： A gas-turbine moving blade made of a Ni-base superalloy containing less grain boundary strengthening elements, in which a blade portion is formed of a single crystal and the rest is formed of columnar crystals, and a gas turbine including the moving blade. A thermal efficiency of the gas turbine can be improved to 35% or more, and a thermal efficiency of complex power generation with a steam turbine can be improved to 45% or more.
摘要翻译：一种由含有较少晶界强化元素的Ni基超级合金制成的燃气轮机动叶片，其中叶片部分由单晶形成，其余部分由柱状晶体形成，以及包括该动叶片的燃气轮机。燃气轮机的热效率可以提高到35％以上，并且能够将蒸汽轮机的发电效率提高到45％以上。

7. 发明授权

US5916382A High corrosion resistant high strength superalloy and gas turbine utilizing the alloy 失效
标题翻译：高耐蚀高强度超合金和燃气轮机利用该合金
公开(公告)号：US5916382A
公开(公告)日：1999-06-29
申请号：US331155
申请日：1994-10-28
申请人： Koji Sato , Takehiro Ohno , Ken Yasuda , Hideki Tamaki , Akira Yoshinari
发明人： Koji Sato , Takehiro Ohno , Ken Yasuda , Hideki Tamaki , Akira Yoshinari
IPC分类号： C22C19/05 , C30B11/00
CPC分类号： C22C19/057 , C22C19/056 , C30B11/00 , C30B29/52
摘要： A superalloy having more excellent hot corrosion resistance than conventional single crystal alloys, oxidation resistance levels as high as that of conventional single crystal alloys, high strength, and creep rupture strength; single crystal members used for a blade or a nozzle produced by utilizing such an alloy; and a combined cycle power generation system produced by utilizing such members. A highly hot corrosion resistant and high-strength superalloy consisting essentially of, by weight, 6-12% Cr, 4.5-6.5% Al, 2-12% W, 2.5-10% Ta, not more than 5.8% Mo, 0.1-3% Co, 0.2-3% Nb, 0.1-4% Re, not more than 0.3% Hf, and the balance being Ni and unavoidable impurities; single crystal members used for a blade or a nozzle produced utilizing such an alloy; and a combined cycle power generation system produced by utilizing such members.
摘要翻译：具有比常规单晶合金更优异的耐热腐蚀性的超耐热合金，与常规单晶合金相同的抗氧化性水平，高强度和蠕变断裂强度; 用于通过利用这种合金制造的叶片或喷嘴的单晶构件; 以及通过利用这些构件制造的联合循环发电系统。高度耐热的高强度超合金，主要由重量比为6-12％的Cr，4.5-6.5％的Al，2-12％的W，2.5-10％的Ta，不超过5.8％的Mo，0.1- 3％Co，0.2-3％Nb，0.1-4％Re，不超过0.3％Hf，余量为Ni和不可避免的杂质; 用于使用这种合金制造的叶片或喷嘴的单晶构件; 以及通过利用这些构件制造的联合循环发电系统。

8. 发明授权

US08656723B2 Operation control method for gas turbine and operation controller for gas turbine 有权
标题翻译：燃气轮机运行控制方法及燃气轮机运行控制器
公开(公告)号：US08656723B2
公开(公告)日：2014-02-25
申请号：US13382162
申请日：2009-07-07
申请人： Hiroshi Haruyama , Hideki Tamaki , Yoshitaka Kojima , Hironori Kamoshida
发明人： Hiroshi Haruyama , Hideki Tamaki , Yoshitaka Kojima , Hironori Kamoshida
IPC分类号： F02C1/00
CPC分类号： F02C9/28 , F02C3/24 , F02C9/40 , F05D2260/95 , F05D2270/00 , F05D2270/083 , F05D2270/44
摘要： An operation control method for a gas turbine includes making a molten salt map of molten salt for causing high-temperature corrosion on high-temperature components of the turbine due to impurities using a thermodynamic equilibrium calculation on the basis of the impurities contained in low-quality fuel and operation data of the gas turbine, indicating a surface temperature and a pressure of the high-temperature components of the turbine on the molten salt map , predicting a lifetime of the high-temperature components of the gas turbine by estimating a corrosion rate thereof, and controlling the flow rate of the low-quality fuel supplied to a combustor so that an area of surface temperature and pressure regions of the high-temperature components superposing on the region of molten salt in the liquid phase on the molten salt map is reduced.
摘要翻译：燃气轮机的操作控制方法包括：利用基于低品质的杂质的热力学平衡计算，由于杂质而使得对于涡轮机的高温部件造成高温腐蚀的熔融盐的熔盐图燃气轮机的燃料和运转数据，表示熔融盐图上的涡轮机的高温部件的表面温度和压力，通过估计燃气轮机的高温部件的寿命来估计其腐蚀速度并且控制供给到燃烧器的低质量燃料的流量，使得在熔融盐图上液相中的熔融盐区域上叠加的高温部件的表面温度和压力区域的面积减小。

9. 发明授权

US5625153A Method of non-destructively estimating life of ceramic member 失效
标题翻译：无损估计陶瓷构件寿命的方法
公开(公告)号：US5625153A
公开(公告)日：1997-04-29
申请号：US572891
申请日：1995-12-18
申请人： Yuichi Sawai , Yoshiyuki Yasutomi , Motoyuki Miyata , Hideki Tamaki , Katsuo Wada
发明人： Yuichi Sawai , Yoshiyuki Yasutomi , Motoyuki Miyata , Hideki Tamaki , Katsuo Wada
IPC分类号： G01N33/38 , G01N3/00
CPC分类号： G01N33/388
摘要： A method of estimating non-destructively the life expectancy of ceramic members, at least a surface layer of which is made of ceramics, is disclosed. The method comprises measuring a variation in at least one of physical characteristics of said ceramic members including color, grain size, electroconductivity and Young's modulus and estimating the life expectancy of the ceramic members on the basis of the predetermined relationship between the life of said ceramics and the physical characteristics. The method is excellent in estimation of the life expectancy of ceramic members of gas turbines or nuclear fusion reactor since the life expectancy of the members to be inspected can easily be estimated in a short time without fracturing the members.
摘要翻译：公开了一种非破坏性地估计陶瓷构件的寿命的方法，陶瓷构件的至少表面层由陶瓷制成。该方法包括测量所述陶瓷构件的物理特性中的至少一个的变化，包括颜色，晶粒尺寸，导电性和杨氏模量，并且基于陶瓷构件的寿命和陶瓷构件的寿命之间的预定关系来估计陶瓷构件的预期寿命身体特征。该方法在估计燃气轮机或核聚变反应堆的陶瓷构件的预期寿命方面是非常好的，因为待检查构件的预期寿命可以很容易地在短时间内被估计而不破坏构件。

10. 发明申请

US20120102966A1 OPERATION CONTROL METHOD FOR GAS TURBINE AND OPERATION CONTROLLER FOR GAS TURBINE 有权
标题翻译：用于气体涡轮机的操作控制方法和用于气体涡轮的操作控制器
公开(公告)号：US20120102966A1
公开(公告)日：2012-05-03
申请号：US13382162
申请日：2009-07-07
申请人： Hiroshi Haruyama , Hideki Tamaki , Yoshitaka Kojima , Hironori Kamoshida
发明人： Hiroshi Haruyama , Hideki Tamaki , Yoshitaka Kojima , Hironori Kamoshida
IPC分类号： F02C9/00
CPC分类号： F02C9/28 , F02C3/24 , F02C9/40 , F05D2260/95 , F05D2270/00 , F05D2270/083 , F05D2270/44
摘要： An operation control method for a gas turbine comprising the steps of: making a molten salt map in a liquid phase state by calculating a dew point and a solidus temperature of molten salt for causing high-temperature corrosion on high-temperature components of the turbine due to impurities using a thermodynamic equilibrium calculation on the basis of the impurities contained in low-quality fuel and operation data of the gas turbine, indicating a surface temperature and a pressure of the high-temperature components of the turbine on the molten salt map to determine a superposition state thereof on a region of molten salt in a liquid phase, predicting a lifetime of the high-temperature components of the gas turbine by estimating a corrosion rate thereof, and controlling the flow rate of the low-quality fuel supplied to a combustor on the basis of the prediction of the lifetime of the high-temperature components so that an area of surface temperature and pressure regions of the high-temperature components superposing on the region of molten salt in the liquid phase on the molten salt map is reduced.
摘要翻译：一种用于燃气轮机的操作控制方法，包括以下步骤：通过计算用于对涡轮机的高温部件造成高温腐蚀的熔融盐的露点和固相线温度，使熔融盐图形成液相状态使用基于低质量燃料中包含的杂质和燃气轮机的操作数据的热力学平衡计算的杂质，表示在熔融盐图上的涡轮的高温组分的表面温度和压力，以确定其在液相中的熔融盐区域上的叠加状态，通过估计燃气轮机的腐蚀速率来预测燃气轮机的高温部件的寿命，以及控制供给到燃烧器的低质量燃料的流量在预测高温部件的寿命的基础上，使得高温部件的表面温度和压力区域的面积在熔盐图上液相中的熔融盐区域上叠加的成分分量降低。

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