公开(公告)号：US20090169750A1

公开(公告)日：2009-07-02

申请号：US11964977

申请日：2007-12-27

申请人： Melvin Howard Wilkins ,  Lawrence Bernard Kool ,  Warren Davis Grossklaus, JR. ,  Brent Ross Tholke

发明人： Melvin Howard Wilkins ,  Lawrence Bernard Kool ,  Warren Davis Grossklaus, JR. ,  Brent Ross Tholke

IPC分类号： B05D5/00

CPC分类号： C23C10/30 ,  C23C10/02 ,  C23C10/52 ,  C23C10/60 ,  Y02T50/67

摘要： Formation of a silicon-modified aluminide coating on the under platform region of a superalloy gas turbine engine blade for improved corrosion and oxidation resistance. The coating is formed from a slurry composition including colloidal silica and aluminum-based powder and is substantially free of hexavalent chromium. The coating provides aluminum and silicon content in the outer 25% of a coating thickness of at least about 20% by weight aluminum and about 3% by weight silicon.

摘要翻译： 在超合金燃气涡轮发动机叶片的平台下面形成硅改性的铝化物涂层，以改善耐腐蚀和抗氧化性。 涂层由包括胶体二氧化硅和铝基粉末的浆料组合物形成，并且基本上不含六价铬。 该涂层在涂层厚度的外部25％中提供铝和硅含量，其为至少约20重量％的铝和约3重量％的硅。

公开(公告)号：US20130230406A1

公开(公告)日：2013-09-05

申请号：US11964970

申请日：2007-12-27

申请人： Melvin Howard Wilkins ,  Brent Ross Tholke ,  Lawrence Bernard Kool ,  Warren Davis Grossklaus, JR.

发明人： Melvin Howard Wilkins ,  Brent Ross Tholke ,  Lawrence Bernard Kool ,  Warren Davis Grossklaus, JR.

IPC分类号： F01D5/28

CPC分类号： F01D5/28 ,  F01D5/286 ,  F05D2230/40 ,  F05D2230/90 ,  F05D2300/222 ,  F05D2300/611

摘要： Gas turbine engine turbine blade includes a silicon-modified aluminide coating on at least an under platform region formed from a slurry composition being substantially free of hexavalent chromium. The silicon-modified aluminide coating provides oxidation resistance comparable to PtAl coatings without adding a weight penalty.

摘要翻译： 燃气涡轮发动机涡轮机叶片包括在基本上不含六价铬的浆料组合物形成的至少一个下平台区域上的硅改性的铝化物涂层。 硅改性的铝化物涂层提供与PtAl涂层相当的抗氧化性，而不增加重量损失。

公开(公告)号：US07749569B2

公开(公告)日：2010-07-06

申请号：US11964977

申请日：2007-12-27

申请人： Melvin Howard Wilkins ,  Lawrence Bernard Kool ,  Warren Davis Grossklaus, Jr. ,  Brent Ross Tholke

发明人： Melvin Howard Wilkins ,  Lawrence Bernard Kool ,  Warren Davis Grossklaus, Jr. ,  Brent Ross Tholke

IPC分类号： B05D3/02

CPC分类号： C23C10/30 ,  C23C10/02 ,  C23C10/52 ,  C23C10/60 ,  Y02T50/67

摘要： Formation of a silicon-modified aluminide coating on the under platform region of a superalloy gas turbine engine blade for improved corrosion and oxidation resistance. The coating is formed from a slurry composition including colloidal silica and aluminum-based powder and is substantially free of hexavalent chromium. The coating provides aluminum and silicon content in the outer 25% of a coating thickness of at least about 20% by weight aluminum and about 3% by weight silicon.

摘要翻译： 在超合金燃气涡轮发动机叶片的平台下面形成硅改性的铝化物涂层，以改善耐腐蚀和抗氧化性。 涂层由包括胶体二氧化硅和铝基粉末的浆料组合物形成，并且基本上不含六价铬。 该涂层在涂层厚度的外部25％中提供铝和硅含量，其为至少约20重量％的铝和约3重量％的硅。

公开(公告)号：US07811396B2

公开(公告)日：2010-10-12

申请号：US11845352

申请日：2007-08-27

申请人： David Edwin Budinger ,  Brent Ross Tholke ,  Matthew Nicklus Miller ,  Warren Davis Grossklaus, Jr. ,  Joshua Leigh Miller ,  Melvin Robert Jackson

发明人： David Edwin Budinger ,  Brent Ross Tholke ,  Matthew Nicklus Miller ,  Warren Davis Grossklaus, Jr. ,  Joshua Leigh Miller ,  Melvin Robert Jackson

IPC分类号： C23C10/28

CPC分类号： C23C4/18 ,  B23K10/027 ,  B23K2101/001 ,  B23K2103/26 ,  B23P6/007 ,  C23C4/129

摘要： A method for repairing a nickel-base superalloy article, such as a gas turbine stationary flowpath shroud having flowpath cooling holes therein that has previously been in service, includes the steps of providing the nickel-base superalloy article that has previously been in service; and applying a restoration to a surface of the article. The restoration is applied by the steps of providing a restoration nickel-base alloy, wherein the restoration nickel-base alloy preferably has no more than about 15 weight percent chromium and no more than about 0.01 percent yttrium, thereafter applying a restoration coating of the restoration nickel-base alloy to the surface of the article by a hyper-velocity oxyfuel metal spray process or a low-pressure plasma spray process, and thereafter heating the article with the restoration coating applied to the surface thereof to a sufficiently high temperature to diffusion bond the restoration coating to the surface of the article. The article is then returned to service.

摘要翻译： 镍基超级合金制品的修复方法，例如其中已经使用的具有流路冷却孔的燃气轮机固定流路护罩，包括提供先前已经使用的镍基超合金制品的步骤; 以及将修复物应用于所述制品的表面。 通过提供恢复镍基合金的步骤来应用恢复，其中恢复镍基合金优选具有不超过约15重量％的铬和不超过约0.01％的钇，然后应用恢复镍基合金的恢复涂层 镍基合金通过超速氧化物金属喷涂法或低压等离子体喷涂法制成制品的表面，然后将具有施加到其表面的恢复涂层的制品加热至足够高的温度以扩散粘结 将修复物涂覆到制品的表面。 该文章然后返回服务。

公开(公告)号：US20100136247A1

公开(公告)日：2010-06-03

申请号：US11845352

申请日：2007-08-27

申请人： David Edwin Budinger ,  Brent Ross Tholke ,  Matthew Nicklus Miller ,  Warren Davis Grossklaus, Jr. ,  Joshua Leigh Miller ,  Melvin Robert Jackson

发明人： David Edwin Budinger ,  Brent Ross Tholke ,  Matthew Nicklus Miller ,  Warren Davis Grossklaus, Jr. ,  Joshua Leigh Miller ,  Melvin Robert Jackson

IPC分类号： B05D1/08 ,  B05D1/32

CPC分类号： C23C4/18 ,  B23K10/027 ,  B23K2101/001 ,  B23K2103/26 ,  B23P6/007 ,  C23C4/129

摘要： A method for repairing a nickel-base superalloy article, such as a gas turbine stationary flowpath shroud having flowpath cooling holes therein that has previously been in service, includes the steps of providing the nickel-base superalloy article that has previously been in service; and applying a restoration to a surface of the article. The restoration is applied by the steps of providing a restoration nickel-base alloy, wherein the restoration nickel-base alloy preferably has no more than about 15 weight percent chromium and no more than about 0.01 percent yttrium, thereafter applying a restoration coating of the restoration nickel-base alloy to the surface of the article by a hyper-velocity oxyfuel metal spray process or a low-pressure plasma spray process, and thereafter heating the article with the restoration coating applied to the surface thereof to a sufficiently high temperature to diffusion bond the restoration coating to the surface of the article. The article is then returned to service.

摘要翻译： 镍基超级合金制品的修复方法，例如其中已经使用的具有流路冷却孔的燃气轮机固定流路护罩，包括提供先前已经使用的镍基超合金制品的步骤; 以及将修复物应用于所述制品的表面。 通过提供恢复镍基合金的步骤来应用恢复，其中恢复镍基合金优选具有不超过约15重量％的铬和不超过约0.01％的钇，然后应用恢复镍基合金的恢复涂层 镍基合金通过超速氧化物金属喷涂法或低压等离子体喷涂法制成制品的表面，然后将具有施加到其表面的恢复涂层的制品加热至足够高的温度以扩散粘结 将修复物涂覆到制品的表面。 该文章然后返回服务。

公开(公告)号：US06982123B2

公开(公告)日：2006-01-03

申请号：US10703010

申请日：2003-11-06

申请人： David Edwin Budinger ,  Brent Ross Tholke ,  Matthew Nicklus Miller ,  Warren Davis Grossklaus, Jr. ,  Joshua Leigh Miller ,  Melvin Robert Jackson

发明人： David Edwin Budinger ,  Brent Ross Tholke ,  Matthew Nicklus Miller ,  Warren Davis Grossklaus, Jr. ,  Joshua Leigh Miller ,  Melvin Robert Jackson

IPC分类号： B32B15/01 ,  B23K31/00

CPC分类号： C23C26/02 ,  C23C30/00 ,  Y10S428/926 ,  Y10T29/49318 ,  Y10T29/49718 ,  Y10T29/49732 ,  Y10T29/49737 ,  Y10T29/49742 ,  Y10T29/49746 ,  Y10T428/12 ,  Y10T428/12493 ,  Y10T428/12639 ,  Y10T428/12944

摘要： A nickel-base superalloy article, such as a gas turbine stationary flowpath shroud that has previously been in service, is repaired by applying a restoration coating to a surface of the article. The restoration coating is applied by providing a precursor mixture, wherein the precursor mixture has no more than about 15 weight percent chromium and no more than about 0.01 percent yttrium, and wherein the precursor mixture includes a higher-melting-point alloy component and a lower-melting-point alloy component. The precursor mixture is applied to the surface of the article, in a form such as a preform of the alloy components. The article with the precursor mixture applied to the surface thereof is heated to a sufficiently high temperature to melt the lower-melting-point alloy component, thereby forming the restoration coating on the surface of the article.

摘要翻译： 镍基超级合金制品，例如先前已经使用的燃气轮机固定流路护罩，通过将物品的表面施加恢复涂层来修复。 通过提供前体混合物来施加复原涂层，其中前体混合物具有不超过约15重量％的铬和不超过约0.01％的钇，并且其中前体混合物包括较高熔点的合金组分和较低的 熔点合金成分。 将前体混合物以诸如合金组分的预成型体的形式施加到制品的表面。 将其前体混合物施加在其表面上的制品被加热到足够高的温度以熔化低熔点合金成分，从而在制品的表面上形成复原涂层。

公开(公告)号：US06610416B2

公开(公告)日：2003-08-26

申请号：US09842576

申请日：2001-04-26

申请人： Thomas Tracy Wallace ,  Brent Ross Tholke

发明人： Thomas Tracy Wallace ,  Brent Ross Tholke

IPC分类号： B32B312

CPC分类号： C23C8/06 ,  C23C8/08 ,  C23C8/24 ,  C23C10/08 ,  F01D11/127 ,  F05D2250/283 ,  Y02T50/671 ,  Y10S428/925 ,  Y10S428/926 ,  Y10S428/938 ,  Y10S428/941 ,  Y10T428/1234 ,  Y10T428/12347 ,  Y10T428/12646 ,  Y10T428/12736 ,  Y10T428/1275 ,  Y10T428/12757 ,  Y10T428/12931 ,  Y10T428/236 ,  Y10T428/24149 ,  Y10T428/24165

摘要： The present invention provides for a method to reduce the strength of the honeycomb of a jet turbine stator, increasing its machinability, with a resultant reduction in measured peak tooth temperature, while maintaining or even improving its high temperature capability, so as not to limit its operating environment. The air seal functionality is unaffected, and even improved in some instances. The machinability of the honeycomb is increased by using a light element diffused into the honeycomb ribbon to produce the effect of reducing its strength and ductility while maintaining the environmental resistance needed. The present invention also includes the stator honeycomb produced by the foregoing method.