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1. 发明授权

US09200526B2 Transition piece between combustor liner and gas turbine 有权
标题翻译：燃烧器衬套与燃气轮机之间的过渡件
公开(公告)号：US09200526B2
公开(公告)日：2015-12-01
申请号：US13332106
申请日：2011-12-20
申请人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
发明人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
IPC分类号： F02C3/02 , F23R3/54 , F01D9/02
CPC分类号： F01D9/023
摘要： A transition piece 10 in an embodiment is provided with an inner duct 20 through which a combustion gas is led to a turbine part 130 and an outer duct 30 that is provided so as to cover an outer periphery of the inner duct 20 and has a plurality of ejection holes 31 to eject air onto an outer peripheral surface of the inner duct 20 formed therein. It is structured such that a channel cross-sectional area of a cooling air channel 50 that is formed between the inner duct 20 and the outer duct 30 and through which the air ejected from the ejection holes 31 flows gradually decreases at an air flow downstream side rather than the portion where the ejection holes 31 are formed, and gradually increases from a throat portion 60 having the minimized channel cross-sectional area to an air flow downstream side.
摘要翻译：在一个实施例中的过渡件10设置有内部管道20，燃烧气体通过该管道20被引导到涡轮机部分130和外部管道30，外部管道30设置成覆盖内部管道20的外周并且具有多个的喷射孔31以将空气喷射到形成在其中的内部管道20的外周表面上。其结构使得形成在内部管道20和外部管道30之间的冷却空气通道50的通道横截面积，并且从喷射孔31喷出的空气流过的通道横截面积在空气流下游侧逐渐减小而不是形成喷射孔31的部分，并且从具有最小的通道横截面积的喉部60逐渐增加到气流下游侧。

2. 发明申请

US20110088260A1 BRAZING REPAIR MATERIAL AND BRAZING REPAIRING METHOD USING THE MATERIAL 审中-公开
标题翻译：使用材料的修补修复材料和修补方法
公开(公告)号：US20110088260A1
公开(公告)日：2011-04-21
申请号：US12994396
申请日：2009-02-17
申请人： Yomei Yoshioka , Toshiaki Fuse , Daizo Saito , Reki Takaku , Kazuhiro Kitayama , Kazutoshi Ishibashi
发明人： Yomei Yoshioka , Toshiaki Fuse , Daizo Saito , Reki Takaku , Kazuhiro Kitayama , Kazutoshi Ishibashi
IPC分类号： B23P17/00 , B23K35/24 , B23K31/12 , B23K31/02 , B23K9/167
CPC分类号： B23P6/007 , B22F7/062 , B22F2998/00 , B22F2998/10 , B23K1/0018 , B23K35/0244 , B23K35/3033 , B23K35/3046 , B23K2101/001 , C22C19/05 , C22C19/07 , F01D5/005 , F05D2230/237 , F05D2230/80 , Y02T50/671 , Y02T50/6765 , Y10T29/49229 , B22F5/04 , B22F3/15 , B22F2003/248
摘要： In a brazing repair material 3 which is charged into a repairing portion of base material 1 in which a failure such as a crack 2 and corrosion is generated, diffusion heat treatment is carried out, the brazing repair material 3 is integrally bonded to the repairing portion to repair the repairing portion, the brazing repair material 3 comprises a mixture of non-molten alloy powder having a composition similar to that of the base material 1 and molten alloy powder which is melted at a temperature of the diffusion heat treatment, and the molten alloy powder is brazing repairing alloy consisting of 0.001 to 0.05 mass % of C, 2 to 5 mass % of Si, 10 to 25 mass % of Cr, 15 to 25 mass % of Co, 1 to 5 mass % of B, and balance of Ni, and excluding Al. With this configuration, a part having a failure such as a crack can restore original characteristics like the inherent base material.
摘要翻译：在将其装入其中产生裂纹2和腐蚀的故障的基材1的修复部分的钎焊修补材料3中，进行扩散热处理，钎焊修复材料3一体地结合到修复部分为了修复修补部分，钎焊修复材料3包括具有与基材1的组成相似的组成的非熔融合金粉末和在扩散热处理的温度下熔化的熔融合金粉末的混合物，并且熔融合金粉末是由C：0.001〜0.05质量％，Si：2〜5质量％，Cr：10〜25质量％，Co 15〜25质量％，B：1〜5质量％的Ni，不包括Al。利用这种构造，具有诸如裂纹的故障的部件可以恢复诸如固有基材的原始特性。

3. 发明授权

US07632363B2 Method for refurbishing a service-degraded component of a gas turbine 有权
标题翻译：一种用于翻新燃气轮机的服务劣化部件的方法
公开(公告)号：US07632363B2
公开(公告)日：2009-12-15
申请号：US11149231
申请日：2005-06-10
申请人： Yomei Yoshioka , Daizo Saito , Junji Ishii , Yoshihiro Aburatani
发明人： Yomei Yoshioka , Daizo Saito , Junji Ishii , Yoshihiro Aburatani
IPC分类号： C22F1/10
CPC分类号： B23P6/002 , C21D9/0068 , C22F1/02 , C22F1/10 , C23C4/02 , F01D5/286 , F05D2230/80 , F05D2230/90 , Y02T50/671 , Y10T29/49318
摘要： A method for refurbishing service-degraded gas turbine component can recover the microstructure of the alloy of the gas turbine component, whose material is deteriorated or damaged after its operation, to the extent that is equivalent or more than the characteristic at the time of its manufacture. The method comprises performing a recovery heat treatment, performing a solution heat treatment, and performing an aging heat treatment. The recovery heat treatment heat-treats the component under a predetermined pressure, which is higher than normal pressure, wherein the temperature of the component is increased to a predetermined temperature under the predetermined pressure. The solution heat treatment is processed under reduced pressure or inert gas atmosphere after the recovery heat treatment. The aging heat treatment is processed under reduced pressure or inert gas atmosphere after the recovery heat treatment.
摘要翻译：一种用于翻新服务降级的燃气轮机部件的方法可以恢复燃料轮机部件的合金的微结构，该组合物的材料在其操作之后被劣化或损坏到相当于或大于其制造时的特性的程度。该方法包括进行回收热处理，进行固溶热处理，进行时效热处理。回收热处理在高于常压的预定压力下对组分进行热处理，其中组分的温度在预定压力下增加到预定温度。在回收热处理后，在减压或惰性气体气氛下处理固溶热处理。老化热处理在回收热处理后在减压或惰性气体气氛下进行处理。

4. 发明授权

US09149881B2 Damage-repairing method of transition piece and transition piece 有权
标题翻译：过渡件和过渡件的损伤修复方法
公开(公告)号：US09149881B2
公开(公告)日：2015-10-06
申请号：US13355105
申请日：2012-01-20
申请人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
发明人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
IPC分类号： B23K1/00 , F01D5/00 , F01D9/02
CPC分类号： B23K1/0018 , B23K2101/001 , F01D5/005 , F01D9/023 , F05D2230/80
摘要： A damage-repairing method of a transition piece in an embodiment includes; an oxide removing step of removing an oxide on an outer surface 20b of an inner duct 20 of a transition piece 10 having damage; a repair material placing step of placing a brazing repair material 80 on the outer surface 20b of the inner duct 20 so as to cover the damage; and a diffusion brazing step of diffusion heat treating the inner duct 20 to repair the damage formed in the outer surface 20b. The damage-repairing method of the transition piece includes: a pressurized heat treating step of, under high pressure, heat treating the inner duct 20; a surface finishing step of scraping off the brazing repair material 80 projecting from the outer surface 20b; and a non-pressurized heat treating step of solution heat treating and aging heat treating the inner duct 20 under non-pressure.
摘要翻译：实施例中的过渡件的损伤修复方法包括：去除损坏的过渡件10的内管20的外表面20b上的氧化物的氧化物去除步骤; 修补材料放置步骤，将钎焊修复材料80放置在内部管道20的外表面20b上以覆盖损坏; 以及对内管20进行扩散热处理以修复形成在外表面20b中的损伤的扩散钎焊步骤。过渡件的损伤修复方法包括：在高压下对内管20进行热处理的加压热处理步骤; 刮削从外表面20b突出的钎焊修复材料80的表面精加工步骤; 以及非压力热处理步骤，在非压力下对内管20进行固溶热处理和老化热处理。

5. 发明申请

US20060016527A1 Method for refurbishing a service-degraded component of a gas turbine 有权
公开(公告)号：US20060016527A1
公开(公告)日：2006-01-26
申请号：US11149231
申请日：2005-06-10
申请人： Yomei Yoshioka , Daizo Saito , Junji Ishii , Yoshihiro Aburatani
发明人： Yomei Yoshioka , Daizo Saito , Junji Ishii , Yoshihiro Aburatani
IPC分类号： C22F1/18 , C22F1/10
CPC分类号： B23P6/002 , C21D9/0068 , C22F1/02 , C22F1/10 , C23C4/02 , F01D5/286 , F05D2230/80 , F05D2230/90 , Y02T50/671 , Y10T29/49318
摘要： A method for refurbishing service-degraded gas turbine component can recover the microstructure of the alloy of the gas turbine component, whose material is deteriorated or damaged after its operation, to the extent that is equivalent or more than the characteristic at the time of its manufacture. The method comprises performing a recovery heat treatment, performing a solution heat treatment, and performing an aging heat treatment. The recovery heat treatment heat-treats the component under a predetermined pressure, which is higher than normal pressure, wherein the temperature of the component is increased to a predetermined temperature under the predetermined pressure. The solution heat treatment is processed under reduced pressure or inert gas atmosphere after the recovery heat treatment. The aging heat treatment is processed under reduced pressure or inert gas atmosphere after the recovery heat treatment.

6. 发明授权

US06938447B2 Apparatus and method of correcting deformation of gas turbine blade 有权
标题翻译：燃气轮机叶片变形校正装置及方法
公开(公告)号：US06938447B2
公开(公告)日：2005-09-06
申请号：US10603805
申请日：2003-06-26
申请人： Toshiaki Fuse , Daizo Saito , Yomei Yoshioka , Masahiro Hiragishi , Junji Ishii
发明人： Toshiaki Fuse , Daizo Saito , Yomei Yoshioka , Masahiro Hiragishi , Junji Ishii
IPC分类号： F01D25/00 , B21D3/10 , B21D3/16 , B21D53/78 , B23P6/00 , F01D5/12 , F02C7/00
CPC分类号： F01D25/285 , B21D3/16 , B21D53/78 , B23P6/002 , Y10T29/49318 , Y10T29/49325
摘要： An apparatus for correcting deformation of a gas turbine blade includes a stationary die fixed to a backside of a tip shroud of a gas turbine blade to hold a back surface thereof and a pressing die pressing a front surface of the tip shroud so as to press the tip shroud of the blade between the pressing die and the stationary. A hydraulic drive mechanism including pressure generator is arranged for pressing the pressing die against the tip shroud held by the stationary die and a control device is operatively connected to the hydraulic drive mechanism so as to set and indicate a driving condition on a basis of deformation correction data preliminarily stored in the control device.
摘要翻译：一种用于校正燃气轮机叶片的变形的装置，包括：固定在燃气轮机叶片的顶部护罩的后侧的固定模具，用于保持其后表面;以及按压模具，其按压尖端护罩的前表面，在压模和固定件之间的叶片的尖端护罩。包括压力发生器的液压驱动机构布置成用于将压模压靠在由固定模具保持的尖端护罩上，并且控制装置可操作地连接到液压驱动机构，以便基于变形校正来设定和指示驾驶状况预先存储在控制装置中的数据。

7. 发明申请

US20070039177A1 Method of regenerating stator vane of gas turbine and gas turbine 审中-公开
标题翻译：燃气轮机和燃气轮机定子叶片再生方法
公开(公告)号：US20070039177A1
公开(公告)日：2007-02-22
申请号：US11193639
申请日：2005-08-01
申请人： Yomei Yoshioka , Toshiaki Fuse , Masako Nakahashi , Daizo Saito , Hiroaki Okamoto , Kazutoshi Ishibashi
发明人： Yomei Yoshioka , Toshiaki Fuse , Masako Nakahashi , Daizo Saito , Hiroaki Okamoto , Kazutoshi Ishibashi
IPC分类号： B23P6/00 , B23P19/04
CPC分类号： B23P6/007 , B23K1/0018 , B23K20/021 , B23K2101/001 , Y10T29/49318 , Y10T29/49732 , Y10T29/49737
摘要： A method of regenerating gas-turbine stator vane comprising the steps of: grinding the oxidized layer and the cracks 2 formed at surface portion so that a part of the cracks 2 remains; filling an equivalent material and a brazing material 4 into the ground portion, the equivalent material 3 having an equality with the base material 1 for the stator vane, and the brazing material 4 having a melting point lower than that of the equivalent material 3; heat treating the filled portion under pressurized inert gas atmosphere so as to melt the brazing material; performing brazing treatment by diffusing the molten brazing material into the cracked portions. According to the above method, the stator vane occurred with material deterioration and damages or the like due to operation of a gas turbine can be efficiently regenerated to provide a high quality without requiring to completely grinding and removing the cracks including a closed crack formed at surface of the stator vane.
摘要翻译：一种再生燃气轮机定子叶片的方法，包括以下步骤：研磨形成在表面部分处的氧化层和裂缝2，使得部分裂纹2保留; 将等效材料和钎焊材料4填充到接地部分中，等效材料3与定子叶片的基材1相同，熔点低于等效材料3的熔点; 在加压惰性气体气氛下对填充部分进行热处理，以熔化钎料; 通过将熔融钎焊材料扩散到裂纹部分进行钎焊处理。根据上述方法，由于燃气轮机的运转引起的材料劣化和损伤等的定子叶片发生，可以有效地再生以提供高质量，而不需要完全研磨和去除包括在表面形成的封闭裂纹的裂纹的定子叶片。

8. 发明申请

US20120186254A1 DAMAGE-REPAIRING METHOD OF TRANSITION PIECE AND TRANSITION PIECE 有权
标题翻译：过渡片和过渡片的损伤修复方法
公开(公告)号：US20120186254A1
公开(公告)日：2012-07-26
申请号：US13355105
申请日：2012-01-20
申请人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
发明人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
IPC分类号： F02C7/00 , B23K31/02
CPC分类号： B23K1/0018 , B23K2101/001 , F01D5/005 , F01D9/023 , F05D2230/80
摘要： A damage-repairing method of a transition piece in an embodiment includes; an oxide removing step of removing an oxide on an outer surface 20b of an inner duct 20 of a transition piece 10 having damage; a repair material placing step of placing a brazing repair material 80 on the outer surface 20b of the inner duct 20 so as to cover the damage; and a diffusion brazing step of diffusion heat treating the inner duct 20 to repair the damage formed in the outer surface 20b. The damage-repairing method of the transition piece includes: a pressurized heat treating step of, under high pressure, heat treating the inner duct 20; a surface finishing step of scraping off the brazing repair material 80 projecting from the outer surface 20b; and a non-pressurized heat treating step of solution heat treating and aging heat treating the inner duct 20 under non-pressure.
摘要翻译：实施例中的过渡件的损伤修复方法包括：去除损坏的过渡件10的内管20的外表面20b上的氧化物的氧化物去除步骤; 修补材料放置步骤，将钎焊修复材料80放置在内部管道20的外表面20b上以覆盖损坏; 以及对内管20进行扩散热处理以修复在外表面20b中形成的损伤的扩散钎焊步骤。过渡件的损坏修复方法包括：在高压下对内管20进行热处理的加压热处理步骤; 刮削从外表面20b突出的钎焊修复材料80的表面精加工步骤; 以及非压力热处理步骤，在非压力下对内管20进行固溶热处理和老化热处理。

9. 发明申请

US20120159954A1 TRANSITION PIECE AND GAS TURBINE 有权
标题翻译：过渡件和气体涡轮
公开(公告)号：US20120159954A1
公开(公告)日：2012-06-28
申请号：US13332106
申请日：2011-12-20
申请人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
发明人： Shoko Ito , Daizo Saito , Yoshiaki Sakai
IPC分类号： F23R3/16 , F02C7/00
CPC分类号： F01D9/023
摘要： A transition piece 10 in an embodiment is provided with an inner duct 20 through which a combustion gas is led to a turbine part 130 and an outer duct 30 that is provided so as to cover an outer periphery of the inner duct 20 and has a plurality of ejection holes 31 to eject air onto an outer peripheral surface of the inner duct 20 formed therein. It is structured such that a channel cross-sectional area of a cooling air channel 50 that is formed between the inner duct 20 and the outer duct 30 and through which the air ejected from the ejection holes 31 flows gradually decreases at an air flow downstream side rather than the portion where the ejection holes 31 are formed, and gradually increases from a throat portion 60 having the minimized channel cross-sectional area to an air flow downstream side.
摘要翻译：在一个实施例中的过渡件10设置有内部管道20，燃烧气体通过该管道20被引导到涡轮机部分130和外部管道30，外部管道30设置成覆盖内部管道20的外周并且具有多个的喷射孔31以将空气喷射到形成在其中的内部管道20的外周表面上。其结构使得形成在内部管道20和外部管道30之间的冷却空气通道50的通道横截面积，并且从喷射孔31喷出的空气流过的通道横截面积在空气流下游侧逐渐减小而不是形成喷射孔31的部分，并且从具有最小的通道横截面积的喉部60逐渐增加到气流下游侧。

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