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公开(公告)号：US4933239A
公开(公告)日：1990-06-12
申请号：US319593
申请日：1989-03-06
申请人： Walter E. Olson , Dinesh K. Gupta
发明人： Walter E. Olson , Dinesh K. Gupta
CPC分类号： C23C10/02 , C23C10/48 , Y10T428/1209 , Y10T428/12493 , Y10T428/1275 , Y10T428/12806 , Y10T428/12826 , Y10T428/12931 , Y10T428/31678
摘要： A protective coating system for superalloys is described. The coating is an active element enriched aluminide, and can be formed by aluminizing an overlay coated superalloy, wherein during the aluminizing process, aluminum diffuses completely through the overlay coating and into the substrate. The coating system exhibits desirable oxidation resistance and resistance to thermal fatigue cracking, due to the presence of oxygen active elements in the overlay.
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2.发明申请Apparatus and Method for Coating Internal Surfaces of a Turbine Engine Component 审中-公开用于涂覆涡轮发动机部件的内表面的装置和方法公开(公告)号：US20110293826A1
公开(公告)日：2011-12-01
申请号：US13193764
申请日：2011-07-29
申请人： Mark A. Livings , Walter E. Olson
发明人： Mark A. Livings , Walter E. Olson
CPC分类号： C23C16/045 , C23C10/06 , C23C16/4488
摘要： A coating apparatus for coating interior surfaces of internal passages of a workpiece, such as a turbine engine component is provided. The coating apparatus comprises a vessel defining an internal space, a plate dividing the internal space into a first chamber and a second chamber, a divider supporting the plate, and the plate having at least one cut-out for receiving a portion of the workpiece having the internal passages to be coated.
摘要翻译： 提供一种用于涂覆诸如涡轮发动机部件的工件的内部通道的内表面的涂覆装置。 涂覆装置包括限定内部空间的容器，将内部空间分成第一室和第二室的板，支撑板的分隔板，以及具有至少一个切口的板，用于接收工件的一部分， 要涂层的内部通道。
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公开(公告)号：US07700154B2
公开(公告)日：2010-04-20
申请号：US11284611
申请日：2005-11-22
申请人： Walter E. Olson
发明人： Walter E. Olson
CPC分类号： C23C8/04 , C23C10/04 , C23C10/06 , F01D5/18 , F01D5/28 , F05D2230/313 , F05D2300/121
摘要： A method for coating internal surfaces of a turbine engine component comprises flowing an aluminide containing gas into passages in the turbine engine component so as to coat the internal surfaces formed by the passages, allowing the aluminide containing gas to flow through the passages and out openings in external surfaces of the turbine engine component, and flowing a volume of a gas selected from the group consisting of argon, hydrogen, and mixtures thereof over the external surfaces to minimize any build-up of an aluminide coating on the external surfaces.
摘要翻译： 一种用于涂覆涡轮发动机部件的内表面的方法包括将含铝化物的气体流入涡轮发动机部件中的通道，以便涂覆由通道形成的内表面，允许含铝化物的气体流过通道，并将出口 涡轮发动机部件的外表面，并且将一批体积的选自氩，氢及其混合物的气体流过外表面，以最小化铝表面在外表面上的积聚。
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4.发明申请Apparatus and method for coating internal surfaces of a turbine engine component 有权用于涂覆涡轮发动机部件的内表面的装置和方法公开(公告)号：US20090017205A1
公开(公告)日：2009-01-15
申请号：US11825782
申请日：2007-07-09
申请人： Mark A. Livings , Walter E. Olson
发明人： Mark A. Livings , Walter E. Olson
IPC分类号： B05D7/22
CPC分类号： C23C16/045 , C23C10/06 , C23C16/4488
摘要： A coating apparatus for coating interior surfaces of internal passages of a workpiece, such as a turbine engine component is provided. The coating apparatus comprises a vessel defining an internal space, a plate dividing the internal space into a first chamber and a second chamber, a divider supporting the plate, and the plate having at least one cut-out for receiving a portion of the workpiece having the internal passages to be coated.
摘要翻译： 提供一种用于涂覆诸如涡轮发动机部件的工件的内部通道的内表面的涂覆装置。 涂覆装置包括限定内部空间的容器，将内部空间分成第一室和第二室的板，支撑板的分隔板，以及具有至少一个切口的板，用于接收工件的一部分， 要涂层的内部通道。
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公开(公告)号：US06435835B1
公开(公告)日：2002-08-20
申请号：US09467517
申请日：1999-12-20
IPC分类号： F01D514
CPC分类号： C23C30/00 , C23C4/00 , F01D5/288 , F05D2300/132 , F05D2300/143 , F05D2300/15 , F05D2300/21 , Y02T50/67 , Y02T50/671
摘要： According to the invention, an article that is exposed to high temperatures, e.g., over 1000° C. during operation is disclosed. In one embodiment, a turbine blade for a gas turbine engine includes a directionally solidified metallic substrate, e.g., a superalloy, which defines an airfoil, a root and a platform located between the blade and root. The platform has an underside adjacent the root, and a corrosion resistant noble metal-containing aluminide coating is located on portions of the blade susceptible to corrosion and/or stress corrosion cracking, such as the underside of the platform and the neck. The applied coating prevents corrosion and stress corrosion cracking of blade in these regions.
摘要翻译： 根据本发明，公开了在操作期间暴露于高温例如超过1000℃的制品。 在一个实施例中，用于燃气涡轮发动机的涡轮机叶片包括定向凝固的金属基底，例如超合金，其定义了叶片，根部和位于叶片和根部之间的平台。 该平台具有邻近根部的下侧，并且耐腐蚀的含贵金属的铝化物涂层位于易受腐蚀和/或应力腐蚀开裂的刀片的部分上，例如平台和颈部的下侧。 涂覆的涂层防止了这些区域中刀片的腐蚀和应力腐蚀开裂
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6.发明授权Apparatus and method for coating internal surfaces of a turbine engine component 有权一种用于涂覆涡轮发动机部件的内表面的装置和方法公开(公告)号：US08025730B2
公开(公告)日：2011-09-27
申请号：US11825782
申请日：2007-07-09
申请人： Mark A. Livings , Walter E. Olson
发明人： Mark A. Livings , Walter E. Olson
IPC分类号： C23C16/52
CPC分类号： C23C16/045 , C23C10/06 , C23C16/4488
摘要： A coating apparatus for coating interior surfaces of internal passages of a workpiece, such as a turbine engine component is provided. The coating apparatus comprises a vessel defining an internal space, a plate dividing the internal space into a first chamber and a second chamber, a divider supporting the plate, and the plate having at least one cut-out for receiving a portion of the workpiece having the internal passages to be coated.
摘要翻译： 提供一种用于涂覆诸如涡轮发动机部件的工件的内部通道的内表面的涂覆装置。 涂覆装置包括限定内部空间的容器，将内部空间分成第一室和第二室的板，支撑板的分隔板，以及具有至少一个切口的板，用于接收工件的一部分， 要涂层的内部通道。
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公开(公告)号：US06403157B2
公开(公告)日：2002-06-11
申请号：US09907301
申请日：2001-07-17
IPC分类号： C23C1600
CPC分类号： B05B12/20
摘要： A fixture for selectively masking a turbine blade 60 includes a locator 10 with a separable receptacle 40 having portals 50. Guide bars 18 extend from the locator for guiding a pair of shield carriers 20 between deployed and retracted positions. Each shield carrier has a shield 26 projecting therefrom. In use, a turbine blade 60, whose root 70 includes a fir tree attachment 72 and a damper pocket 74, is mounted on the fixture so that the receptacle embraces the blade root. The shield carriers are translated along the guide bars until the shields penetrate through the portals and into the receptacle thus segregating the attachment 72 from the damper pocket 74. Masking powder 84 is then compressed into the receptacle to envelop the attachment while leaving the damper pocket unmasked. The fixture facilitates selective masking of the blade root so that when the receptacle and masked blade are subsequently exposed to a metal bearing vapor at an elevated temperature, the vapor coats the damper pocket but not the highly stressed attachment. In one variant of the invention, the shields are independent, consumable shields dimensioned and shaped to substantially conform to the size and shape of the damper pocket. The shields are made of a thermally decomposable material. In use, the shields are wedged into the damper pockets prior to blade masking. During the coating cycle, the shields decompose at a temperature lower than the temperature at which coating vapors are produced to expose the damper pocket to the vapors.
摘要翻译： 用于选择性地掩蔽涡轮机叶片60的固定器包括定位器10，定位器10具有具有入口50的可分离的容器40.导杆18从定位器延伸，用于在展开位置和缩回位置之间引导一对屏蔽架20。 每个屏蔽载体具有从其突出的屏蔽26。 在使用中，其根部70包括枞树附件72和阻尼器袋74的涡轮机叶片60安装在固定装置上，使得容器包围叶片根部。 屏蔽载体沿着导杆平移，直到屏蔽件穿过入口并进入插座，从而将附件72与阻尼器袋74分离。然后将掩蔽粉末84压缩到容器中以封闭附件，同时使阻尼袋未被遮蔽 。 夹具有助于叶片根部的选择性掩蔽，使得当容器和掩蔽的叶片随后在升高的温度下暴露于含金属的蒸气时，蒸气涂覆阻尼器袋而不是高应力附件。 在本发明的一个变型中，屏蔽件是独立的，可消耗的屏蔽件的尺寸和形状以基本上符合阻尼器袋的尺寸和形状。 护罩由热分解材料制成。 在使用中，在刀片遮蔽之前，屏蔽件楔入阻尼口袋中。 在涂覆循环期间，屏蔽层在低于制备涂层蒸汽的温度的温度下分解，以将阻尼器袋暴露于蒸气。
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公开(公告)号：US06296705B1
公开(公告)日：2001-10-02
申请号：US09461579
申请日：1999-12-15
IPC分类号： C23C1600
CPC分类号： B05B12/20
摘要： A fixture for selectively masking a turbine blade 60 includes a locator 10 with a separable receptacle 40 having portals 50. Guide bars 18 extend from the locator for guiding a pair of shield carriers 20 between deployed and retracted positions. Each shield carrier has a shield 26 projecting therefrom. In use, a turbine blade 60, whose root 70 includes a fir tree attachment 72 and a damper pocket 74, is mounted on the fixture so that the receptacle embraces the blade root. The shield carriers are translated along the guide bars until the shields penetrate through the portals and into the receptacle thus segregating the attachment 72 from the damper pocket 74. Masking powder 84 is then compressed into the receptacle to envelop the attachment while leaving the damper pocket unmasked. The fixture facilitates selective masking of the blade root so that when the receptacle and masked blade are subsequently exposed to a metal bearing vapor at an elevated temperature, the vapor coats the damper pocket but not the highly stressed attachment. In one variant of the invention, the shields are independent, consumable shields dimensioned and shaped to substantially conform to the size and shape of the damper pocket. The shields are made of a thermally decomposable material. In use, the shields are wedged into the damper pockets prior to blade masking. During the coating cycle, the shields decompose at a temperature lower than the temperature at which coating vapors are produced to expose the damper pocket to the vapors.
摘要翻译： 用于选择性地掩蔽涡轮机叶片60的固定器包括定位器10，定位器10具有具有入口50的可分离的容器40.导杆18从定位器延伸，用于在展开位置和缩回位置之间引导一对屏蔽架20。 每个屏蔽载体具有从其突出的屏蔽26。 在使用中，其根部70包括枞树附件72和阻尼器袋74的涡轮机叶片60安装在固定装置上，使得容器包围叶片根部。 屏蔽载体沿着导杆平移，直到屏蔽件穿过入口并进入插座，从而将附件72与阻尼器袋74分离。然后将掩蔽粉末84压缩到容器中以封闭附件，同时使阻尼袋未被遮蔽 。 夹具有助于叶片根部的选择性掩蔽，使得当容器和掩蔽的叶片随后在升高的温度下暴露于含金属的蒸气时，蒸气涂覆阻尼器袋而不是高应力附件。 在本发明的一个变型中，屏蔽件是独立的，可消耗的屏蔽件的尺寸和形状以基本上符合阻尼器袋的尺寸和形状。 护罩由热分解材料制成。 在使用中，在刀片遮蔽之前，屏蔽件楔入阻尼口袋中。 在涂覆循环期间，屏蔽层在低于制备涂层蒸汽的温度的温度下分解，以将阻尼器袋暴露于蒸气。
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公开(公告)号：US6022632A
公开(公告)日：2000-02-08
申请号：US733590
申请日：1996-10-18
CPC分类号： C23C10/48 , C23C10/04 , C23C26/00 , Y10T428/12736 , Y10T428/1275 , Y10T428/12757
摘要： The invention includes a low activity localized aluminide coating for a metallic article made by positioning a coating material, preferably in the form of a tape, on a portion of the article. The coating material comprises a binder, a halide activator, an aluminum source, and an inert ceramic material. The coating material and the article are heated in an inert atmosphere between about 1800.degree. F. (982.degree. C.) and about 2050.degree. F. (1121.degree. C.) for between about four and about seven hours thereby producing a low activity localized aluminide coating having an outward diffusion aluminide coating microstructure characterized by two distinct zones, an inner diffusion zone and an outer zone including between about 20-28 percent, by weight, aluminum.
摘要翻译： 本发明包括用于金属制品的低活性局部铝化物涂层，其通过将优选为带状的涂层材料定位在制品的一部分上而制成。 涂层材料包括粘合剂，卤化物活化剂，铝源和惰性陶瓷材料。 将涂层材料和制品在约1800°F（982℃）至约2050°F（1121℃）的惰性气氛中加热约4小时至约7小时，从而产生局部 铝化物涂层具有向外扩散的铝化物涂层微结构，其特征在于两个不同的区域，内扩散区和包含约20-28重量％的铝的外区。
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公开(公告)号：US5277936A
公开(公告)日：1994-01-11
申请号：US122868
申请日：1987-11-19
申请人： Walter E. Olson , Dinesh K. Gupta
发明人： Walter E. Olson , Dinesh K. Gupta
摘要： The oxidation resistance of MCrAlY-type overlay coatings is improved by incorporating small discrete oxide particles into the coating. The particles are preferably yttrium oxide, and the coating is applied by simultaneously plasma spraying MCrAlY-type powder particles and oxide particles onto a substrate in a nonoxidizing atmosphere. Improvements in resistance to rumpling has also been observed in coatings applied according to this invention.
摘要翻译： 通过将小的离散的氧化物颗粒结合到涂层中来改善MCrAlY型覆盖层的抗氧化性。 颗粒优选为氧化钇，并且通过在非氧化气氛中同时将MCrAlY型粉末颗粒和氧化物颗粒等离子体喷涂到基材上来施加涂层。 在根据本发明应用的涂料中也观察到抗皱性的改善。
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