公开(公告)号：US06575702B2

公开(公告)日：2003-06-10

申请号：US09682814

申请日：2001-10-22

申请人： Melvin Robert Jackson ,  Aaron Todd Frost ,  Shyh-Chin Huang ,  Charles Gitah Mukira ,  Thomas Robert Raber ,  Raymond Alan White ,  Paul Leonard Dupree ,  Canan Uslu Hardwicke

发明人： Melvin Robert Jackson ,  Aaron Todd Frost ,  Shyh-Chin Huang ,  Charles Gitah Mukira ,  Thomas Robert Raber ,  Raymond Alan White ,  Paul Leonard Dupree ,  Canan Uslu Hardwicke

IPC分类号： F01D528

CPC分类号： B23P6/005 ,  B23P15/04 ,  F01D5/005 ,  F01D5/28 ,  F05C2201/0463 ,  F05C2201/0466 ,  F05D2230/21 ,  F05D2230/23 ,  F05D2230/80 ,  F05D2300/11 ,  F05D2300/502 ,  F05D2300/606 ,  F05D2300/607 ,  Y02T50/67 ,  Y02T50/672 ,  Y10T29/49318 ,  Y10T29/49737

摘要： Methods for repairing and manufacturing a gas turbine airfoil, and the airfoil repaired and manufactured with such methods are presented with, for example, the repair method comprising providing an airfoil having specified nominal dimensions, the airfoil comprising a first material, the first material having a creep life and a fatigue life, the airfoil further comprising a leading edge section and a trailing edge section; removing at least one portion of at least one section of the airfoil to create at least one deficit of material for the airfoil relative to the specified nominal dimensions, the at least one section selected from the group consisting of the leading edge section and the trailing edge section; providing at least one insert comprising a second material, the second material having a creep life that is at least substantially equal to the creep life of the first material, and a fatigue life that is at least substantially equal to the fatigue life of the first material; and disposing the at least one insert onto the airfoil such that the at least one deficit of material is substantially eliminated.

摘要翻译： 提供了用于修理和制造燃气涡轮机翼型的方法以及用这种方法修理和制造的翼型，例如，提供了修复方法，该修复方法包括提供具有特定标称尺寸的翼型件，该翼型件包括第一材料，第一材料具有 蠕变寿命和疲劳寿命，翼型件还包括前缘部分和后缘部分; 去除所述翼型件的至少一个部分的至少一部分以产生相对于所述特定公称尺寸的所述翼型件的至少一个缺口，所述至少一个部分选自由所述前缘部分和所述后缘 部分; 提供包括第二材料的至少一个插入件，所述第二材料具有至少基本上等于所述第一材料的蠕变寿命的蠕变寿命，以及至少基本等于所述第一材料的疲劳寿命的疲劳寿命 ; 以及将所述至少一个插入件设置在所述翼型件上，使得所述至少一个材料缺陷基本上被消除。

公开(公告)号：US06908288B2

公开(公告)日：2005-06-21

申请号：US09682899

申请日：2001-10-31

申请人： Melvin Robert Jackson ,  Aaron Todd Frost ,  Shyh-Chin Huang ,  Charles Gitahi Mukira ,  Thomas Robert Raber ,  Raymond Alan White

发明人： Melvin Robert Jackson ,  Aaron Todd Frost ,  Shyh-Chin Huang ,  Charles Gitahi Mukira ,  Thomas Robert Raber ,  Raymond Alan White

IPC分类号： F01D5/00 ,  F01D5/14

CPC分类号： F01D5/005 ,  Y02T50/67 ,  Y02T50/672 ,  Y10T29/49318 ,  Y10T428/12944

摘要： Methods for repairing and manufacturing a gas turbine blade, and the gas turbine blade repaired and manufactured with such methods are presented with, for example, the repair method comprising providing a gas turbine blade, the blade comprising a blade tip and a blade body; removing at least one portion of the blade tip; providing at least one freestanding tip insert; and disposing the at least one tip insert onto the gas turbine blade body such that the at least one tip insert replaces the at least one removed portion of the blade tip.

摘要翻译： 提供了用于修理和制造燃气轮机叶片的方法以及用这种方法修理和制造的燃气轮机叶片，例如，包括提供燃气轮机叶片的修复方法，该叶片包括叶片尖端和叶片体; 去除所述叶片尖端的至少一部分; 提供至少一个独立的尖端插入物; 以及将所述至少一个尖端插入物设置在所述燃气轮机叶片体上，使得所述至少一个尖端插入物替换所述刀片尖端的所述至少一个移除部分。

公开(公告)号：US06615470B2

公开(公告)日：2003-09-09

申请号：US09725738

申请日：2000-11-29

申请人： Reed Roeder Corderman ,  Shyh-Chin Huang ,  Thomas Robert Raber ,  Don Mark Lipkin ,  Raymond Alan White ,  Sidney Perham Young ,  Melvin Robert Jackson ,  Peter William Schilke

发明人： Reed Roeder Corderman ,  Shyh-Chin Huang ,  Thomas Robert Raber ,  Don Mark Lipkin ,  Raymond Alan White ,  Sidney Perham Young ,  Melvin Robert Jackson ,  Peter William Schilke

IPC分类号： B23P600

CPC分类号： B23P6/005 ,  B22D19/10 ,  B23P6/007 ,  Y10T29/49318 ,  Y10T29/49726 ,  Y10T29/49728 ,  Y10T29/49734 ,  Y10T29/49737 ,  Y10T29/49742

摘要： A system and method for repairing defects such as bumper holes, cracks, freckles and inclusions, in a cast article, such as a turbine component. The system comprises a device for locating a defect in a cast article, a repair material that is disposable at a defect site, at least one heat source capable of heating the repair material and a portion of the cast article to a molten state. The method of using the system comprises locating a defect in the cast article, providing a repair material to the defect site, melting the repair material and cast article at the defect site, and cooling the molten repair material and portion of the casting article such that they resolidify and fuse together. The method may further comprise removing a portion of the cast article at the defect site, removal of excess repair material and inspecting the cast article following repair of the defect.

摘要翻译： 用于在诸如涡轮机部件的铸造制品中修复诸如保险杠孔，裂缝，雀斑和夹杂物之类的缺陷的系统和方法。 该系统包括用于定位铸造制品中的缺陷的装置，在缺陷部位是一次性的修复材料，至少一个能够将修复材料和一部分铸造制品加热至熔融状态的热源。 使用该系统的方法包括将缺陷定位在铸造制品中，向缺陷部位提供修复材料，在缺陷部位熔化修复材料和铸造制品，以及冷却熔融修复材料和铸件的部分，使得 他们重组并融合在一起。 该方法还可以包括在缺陷部位移除一部分铸造制品，去除多余的修复材料并在修复缺陷后检查铸造件。

公开(公告)号：US07651023B2

公开(公告)日：2010-01-26

申请号：US11751944

申请日：2007-05-22

申请人： Shyh-Chin Huang ,  Liang Jiang ,  Melvin Robert Jackson ,  Laurent Cretegny ,  Charles Gitahi Mukira

发明人： Shyh-Chin Huang ,  Liang Jiang ,  Melvin Robert Jackson ,  Laurent Cretegny ,  Charles Gitahi Mukira

IPC分类号： B23K31/02

CPC分类号： B23K35/3033 ,  Y10T428/12

摘要： A nickel-based braze composition is described, containing nickel, palladium, and restricted amounts of boron and silicon. The composition can also contain tantalum, titanium, and zirconium, as well as aluminum, chromium, and cobalt. A method for joining two metal components, using the braze composition, is also described. The braze composition can also be used to fill cracks or other cavities in a component, e.g., a gas turbine part formed from a nickel-based superalloy. Articles of manufacture which contain the braze composition are also described.

摘要翻译： 描述了镍基钎焊组合物，其含有镍，钯和限制量的硼和硅。 组合物还可以含有钽，钛和锆，以及铝，铬和钴。 还描述了使用钎焊组合物接合两种金属组分的方法。 钎焊组合物还可以用于填充部件中的裂纹或其它空腔，例如由镍基超级合金形成的燃气涡轮部分。 还描述了含有钎焊组合物的制品。

公开(公告)号：US20080128475A1

公开(公告)日：2008-06-05

申请号：US11751944

申请日：2007-05-22

申请人： Shyh-Chin Huang ,  Liang Jiang ,  Melvin Robert Jackson ,  Laurent Cretegny ,  Charles Gitahi Mukira

发明人： Shyh-Chin Huang ,  Liang Jiang ,  Melvin Robert Jackson ,  Laurent Cretegny ,  Charles Gitahi Mukira

IPC分类号： B23K28/00 ,  C22C19/03

CPC分类号： B23K35/3033 ,  Y10T428/12

摘要： A nickel-based braze composition is described, containing nickel, palladium, and restricted amounts of boron and silicon. The composition can also contain tantalum, titanium, and zirconium, as well as aluminum, chromium, and cobalt. A method for joining two metal components, using the braze composition, is also described. The braze composition can also be used to fill cracks or other cavities in a component, e.g., a gas turbine part formed from a nickel-based superalloy. Articles of manufacture which contain the braze composition are also described.

摘要翻译： 描述了镍基钎焊组合物，其含有镍，钯和限制量的硼和硅。 组合物还可以含有钽，钛和锆，以及铝，铬和钴。 还描述了使用钎焊组合物接合两种金属组分的方法。 钎焊组合物还可以用于填充部件中的裂纹或其它空腔，例如由镍基超级合金形成的燃气涡轮部分。 还描述了含有钎焊组合物的制品。

公开(公告)号：US08876481B2

公开(公告)日：2014-11-04

申请号：US12984836

申请日：2011-01-05

申请人： Shyh-Chin Huang ,  Frederic Joseph Klug ,  Robert John Zabala ,  Andrea Jeanne Howard ,  Toby George Darkins, Jr.

发明人： Shyh-Chin Huang ,  Frederic Joseph Klug ,  Robert John Zabala ,  Andrea Jeanne Howard ,  Toby George Darkins, Jr.

IPC分类号： F01D5/30 ,  F01D5/28

CPC分类号： F01D5/3007 ,  C04B41/009 ,  C04B41/52 ,  C04B41/89 ,  F01D5/282 ,  F01D5/288 ,  F01D5/30 ,  F01D5/3092 ,  F05D2300/6033 ,  Y02T50/672 ,  Y10T29/49229 ,  Y10T29/49337 ,  Y10T29/49885 ,  C04B35/565 ,  C04B35/806 ,  C04B41/5096 ,  C04B41/5071 ,  C04B41/522 ,  C04B41/5059 ,  C04B41/5024 ,  C04B41/5031 ,  C04B41/5042 ,  C04B41/5044 ,  C04B41/5064 ,  C04B41/5068 ,  C04B41/5045 ,  C04B41/5032

摘要： A turbine airfoil component assembly for use with a turbine engine including a attachment assembly having an inner surface defining a cavity. The attachment assembly includes a metal alloy substrate. An airfoil assembly is at least partially positioned within the attachment assembly and extends outwardly from the attachment assembly. The airfoil assembly includes a ceramic matrix composite (CMC) substrate. A reaction barrier coating is disposed over at least a portion of the airfoil assembly. The reaction barrier coating is positioned between the attachment assembly and the airfoil assembly.

摘要翻译： 一种与涡轮发动机一起使用的涡轮机翼部件组件，其包括具有限定腔的内表面的附接组件。 附接组件包括金属合金基板。 翼型组件至少部分地定位在附接组件内并从附接组件向外延伸。 翼型组件包括陶瓷基复合材料（CMC）基材。 反应阻挡涂层设置在翼型组件的至少一部分上。 反应阻挡涂层定位在附接组件和翼型组件之间。

公开(公告)号：US08307881B2

公开(公告)日：2012-11-13

申请号：US12348937

申请日：2009-01-06

申请人： Shyh-Chin Huang ,  Andrew John Elliott ,  Michael Francis Xavier Gigliotti, Jr. ,  Roger John Petterson ,  Stephen Francis Rutkowski

发明人： Shyh-Chin Huang ,  Andrew John Elliott ,  Michael Francis Xavier Gigliotti, Jr. ,  Roger John Petterson ,  Stephen Francis Rutkowski

IPC分类号： B22D27/04 ,  B22C9/00 ,  B22C1/02

CPC分类号： B22D27/045 ,  B22C9/04 ,  C30B11/002

摘要： Casting molds suitable for directional solidification processes using a liquid cooling bath include a graded facecoat structure on a mold body. The graded facecoat structure includes an innermost layer and a delamination layer, wherein the delamination layer fractures upon cooling of the molten metal so as to separate the mold body from the innermost layer, which remains in contact with or in close proximity to the metal being cast. Also disclosed are directional solidification processes.

摘要翻译： 适用于使用液体冷却浴的定向凝固方法的铸模包括在模体上的分级面涂层结构。 分级面涂层结构包括最内层和分层，其中分层在熔融金属冷却时破裂，从而将模具体与最内层分开，其保持与正在铸造的金属接触或非常接近 。 还公开了定向凝固方法。

公开(公告)号：US20110076182A1

公开(公告)日：2011-03-31

申请号：US12571013

申请日：2009-09-30

申请人： Akane Suzuki ,  Michael Francis Xavier Gigliotti, JR. ,  Shyh-Chin Huang ,  Pazhayannur Ramanathan Subramanian

发明人： Akane Suzuki ,  Michael Francis Xavier Gigliotti, JR. ,  Shyh-Chin Huang ,  Pazhayannur Ramanathan Subramanian

IPC分类号： C22C19/05 ,  B22D27/04

CPC分类号： C22C19/057

摘要： Rhenium-free nickel based alloys are provided. More particularly, the alloys comprise preferred levels and ratios of elements so as to achieve good high temperature strength of both gamma matrix phase and gamma prime precipitates, as well as good environmental resistance, without using rhenium. When cast and directionally solidified into single crystal form, the alloys exhibit creep resistance substantially equivalent to rhenium-bearing single-crystal alloys. Further, the alloys can be processed by directional solidification into articles in single crystal form or columnar structure comprising fine dendrite arm spacing, e.g., less than 400 μm, if need be, so that further improvements in mechanical properties in the articles can be seen.

摘要翻译： 提供无铼镍基合金。 更具体地，合金包括优选的含量和元素比例，以便在不使用铼的情况下实现γ基质相和γ初始沉淀物的良好的高温强度以及良好的耐环境性。 当铸造和定向凝固成单晶形式时，合金具有基本上等同于含铼单晶合金的抗蠕变性。 此外，如果需要，合金可以通过定向固化加工成单晶形状或柱状结构的制品，包括细小的枝晶臂间距，例如小于400μm，从而可以看到制品中机械性能的进一步改善。

公开(公告)号：US20110076181A1

公开(公告)日：2011-03-31

申请号：US12570861

申请日：2009-09-30

申请人： Akane Suzuki ,  Michael Francis Xavier Gigliotti, Jr. ,  Shyh-Chin Huang ,  Pazhayannur Ramanathan Subramanian

发明人： Akane Suzuki ,  Michael Francis Xavier Gigliotti, Jr. ,  Shyh-Chin Huang ,  Pazhayannur Ramanathan Subramanian

IPC分类号： C22C19/05 ,  B22D27/04

CPC分类号： C22C19/057 ,  C30B11/00 ,  C30B28/06 ,  C30B29/52 ,  C30B29/605

摘要： Rhenium-free nickel based alloys are provided. More particularly, the alloys comprise preferred levels and ratios of elements so as to achieve good high temperature strength of both gamma matrix phase and gamma prime precipitates, as well as good environmental resistance, without using rhenium. When cast and directionally solidified into single crystal form, the alloys exhibit oxidation resistance better than or comparable to rhenium-bearing single-crystal alloys, and creep rupture life comparable to rhenium-bearing single-crystal alloys. Further, the alloys can be processed by directional solidification into articles in single crystal form or columnar structure comprising fine dendrite arm spacing, e.g., less than 400 μm, if need be, so that further improvements in mechanical properties in the articles can be seen.

摘要翻译： 提供无铼镍基合金。 更具体地，合金包括优选的含量和元素比例，以便在不使用铼的情况下实现γ基质相和γ初始沉淀物的良好的高温强度以及良好的耐环境性。 当铸造和定向凝固成单晶形式时，合金表现出比具有铼承载单晶合金更好或可媲美的抗氧化性，以及与含铼单晶合金相当的蠕变断裂寿命。 此外，如果需要，合金可以通过定向固化加工成单晶形状或柱状结构的制品，包括细小的枝晶臂间距，例如小于400μm，从而可以看到制品中机械性能的进一步改善。

公开(公告)号：US20100170654A1

公开(公告)日：2010-07-08

申请号：US12348937

申请日：2009-01-06

申请人： Shyh-Chin Huang ,  Andrew John Elliott ,  Michael Francis Xavier Gigliotti, JR. ,  Roger John Petterson ,  Stephen Francis Rutkowski

发明人： Shyh-Chin Huang ,  Andrew John Elliott ,  Michael Francis Xavier Gigliotti, JR. ,  Roger John Petterson ,  Stephen Francis Rutkowski

IPC分类号： B22D27/04 ,  B29C33/60

CPC分类号： B22D27/045 ,  B22C9/04 ,  C30B11/002

摘要： Casting molds suitable for directional solidification processes using a liquid cooling bath include a graded facecoat structure on a mold body. The graded facecoat structure includes an innermost layer and a delamination layer, wherein the delamination layer fractures upon cooling of the molten metal so as to separate the mold body from the innermost layer, which remains in contact with or in close proximity to the metal being cast. Also disclosed are directional solidification processes.

摘要翻译： 适用于使用液体冷却浴的定向凝固方法的铸模包括在模体上的分级面涂层结构。 分级面涂层结构包括最内层和分层，其中分层在熔融金属冷却时破裂，从而将模具体与最内层分开，其保持与正在铸造的金属接触或非常接近 。 还公开了定向凝固方法。