公开(公告)号：US20130052474A1

公开(公告)日：2013-02-28

申请号：US13571492

申请日：2012-08-10

申请人： Shinya IMANO ,  Hironori Kamoshida ,  Satoshi Hirano ,  Park Seunghwan ,  Takehiko Yoshida

发明人： Shinya IMANO ,  Hironori Kamoshida ,  Satoshi Hirano ,  Park Seunghwan ,  Takehiko Yoshida

IPC分类号： B32B15/04 ,  B32B1/08 ,  F03B3/12 ,  B23K20/12

CPC分类号： F01D5/063 ,  B23K9/167 ,  B23K20/122 ,  B23K35/3033 ,  B23K2101/001 ,  C22C19/055 ,  C22F1/00 ,  F05D2220/31 ,  Y10T428/12292 ,  Y10T428/12944

摘要： A Ni-base alloy large-size member comprises a base material having strip-shaped carbide segregation, and a homogeneous modified layer formed on a welding groove surface by treatment using Friction stir processing and solution treatment. In addition, a Ni-base alloy welded structure is manufactured by welding the Ni-base alloy large-size member with other member constituting the Ni-base alloy welded structure, such as a member formed of ferrite steel or another Ni-base alloy large-size member under the condition that weld penetration depth is shallower than the thickness of the modified layer.

摘要翻译： 镍基合金大尺寸构件包括具有带状碳化物偏析的基材，以及通过使用摩擦搅拌处理和溶液处理的处理在焊接槽表面上形成的均匀改性层。 另外，通过将Ni基合金大尺寸构件与构成Ni基合金焊接结构的其他构件，例如由铁素体钢或其它Ni基合金构成的构件焊接，制造Ni基合金焊接结构 在焊缝穿透深度比改性层的厚度浅的条件下成形。

公开(公告)号：US20120183410A1

公开(公告)日：2012-07-19

申请号：US13337636

申请日：2011-12-27

申请人： Shinya IMANO ,  Hironori Kamoshida ,  Satoshi Hirano ,  Kenichi Murata ,  Seunghwan Park ,  Kunio Asai ,  Takehiko Yoshida

发明人： Shinya IMANO ,  Hironori Kamoshida ,  Satoshi Hirano ,  Kenichi Murata ,  Seunghwan Park ,  Kunio Asai ,  Takehiko Yoshida

IPC分类号： F04D29/38

CPC分类号： F01D5/14 ,  F01D5/28 ,  F01D5/286 ,  F05D2300/174 ,  F05D2300/506 ,  Y02T50/671

摘要： It is an objective of the present invention to provide an effective use of the friction stir processing (FSP) technology for Ti-alloy turbine blades with a long radial length, and provide a Ti-alloy turbine blade having both high erosion resistance and high long term reliability. There is provided a turbine blade made of an α-β titanium alloy having an average Vickers hardness of 320 Hv or less, the turbine blade having a leading edge, in which: the turbine blade includes, at the leading edge thereof, a first hardened surface region having a thickness of from 0.5 to 3.0 mm and having an average Vickers hardness of 340 Hv or more; and the first hardened surface region is formed by friction stir processing a surface region of the leading edge of the turbine blade.

摘要翻译： 本发明的一个目的是为了有效利用具有长径向长度的钛合金涡轮叶片的摩擦搅拌处理（FSP）技术，并且提供具有高抗侵蚀性和高长度的Ti合金涡轮叶片 长期可靠性。 提供由α-＆bgr制成的涡轮叶片; 具有320Hv或更小的维氏硬度的钛合金，所述涡轮叶片具有前缘，其中：所述涡轮叶片在其前缘处包括厚度为0.5至3.0mm的第一硬化表面区域和 平均维氏硬度为340Hv或更高; 并且通过摩擦搅拌处理涡轮叶片的前缘的表面区域来形成第一硬化表面区域。

公开(公告)号：US09457422B2

公开(公告)日：2016-10-04

申请号：US13529156

申请日：2012-06-21

申请人： Hironori Kamoshida ,  Shinya Imano ,  Takehiko Yoshida ,  Seunghwan Park

发明人： Hironori Kamoshida ,  Shinya Imano ,  Takehiko Yoshida ,  Seunghwan Park

IPC分类号： B23K20/12

CPC分类号： B23K20/1255 ,  B23K20/1275 ,  B23K2103/02 ,  B23K2103/04 ,  B23K2103/05 ,  B23K2103/08 ,  B23K2103/26

摘要： A heat resistant alloy member that maintains the creep strength and improves the fatigue characteristics is provided. The heat resistant alloy member according to the present invention includes a recrystallized structure layer including finer grains on the surface of the member than those inside of the member. The recrystallized structure layer is formed by forming a stirred layer by giving processing strain to the surface of the member using a friction stir processing, and applying recrystallization heat treatment to the stirred layer for recrystallization.

摘要翻译： 提供了保持蠕变强度并改善疲劳特性的耐热合金构件。 根据本发明的耐热合金构件包括在构件的表面上包括比构件内部更细的颗粒的再结晶结构层。 通过使用摩擦搅拌处理对构件表面施加加工应变，形成搅拌层而形成再结晶结构层，对搅拌层进行再结晶热处理。

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 。

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。