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公开(公告)号：US20120189778A1
公开(公告)日：2012-07-26
申请号：US13014104
申请日：2011-01-26
摘要： A coating method includes depositing a coating material onto a turbine engine component using an ionic liquid that is a melt of the salt. The coating material includes aluminum. The turbine engine component is then heat treated to react with at least one element of the coating material with at least one other element to form a protective coating on the component.
摘要翻译： 涂覆方法包括使用作为盐的熔体的离子液体将涂料沉积到涡轮发动机部件上。 涂层材料包括铝。 涡轮发动机部件然后被热处理以与涂覆材料的至少一个元件与至少一个其它元件反应，以在部件上形成保护涂层。
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公开(公告)号：US20120052200A1
公开(公告)日：2012-03-01
申请号：US12871028
申请日：2010-08-30
CPC分类号： C23C4/12 , C23C4/01 , C23C4/02 , C23C4/137 , C23C14/042 , F01D5/186 , F01D5/288 , F05D2230/312 , F05D2250/70 , F05D2300/13 , F05D2300/21
摘要： An airfoil for use in a gas turbine engine is provided, the airfoil having a hole therein. A ceramic plug is inserted in the hole so that the plug extends above a depth of a thermal barrier coating, such as a ceramic, to be placed on the airfoil. The airfoil is then coated by non-line of sight vapor deposition and the plugs are then removed.
摘要翻译： 提供了一种用于燃气涡轮发动机的翼型件，其中具有孔的翼型件。 将陶瓷塞插入孔中，使得插头延伸到诸如陶瓷的热障涂层的深度之上，以放置在翼型上。 然后通过非视线气相沉积涂覆翼型件，然后将塞子移除。
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公开(公告)号：US20130299453A1
公开(公告)日：2013-11-14
申请号：US13470676
申请日：2012-05-14
摘要： A method for making a component for a gas turbine engine comprises forming a non-metal substrate having at least one metal receiving surface. A cathode is formed corresponding to a shape of the at least one metal receiving surface. The cathode is submerged into an ionic liquid plating solution. The solution comprises a source of metal cations and a first ionic liquid solvent. An electrical current is applied through the plating solution to the cathode, thereby depositing metal cations onto the cathode and forming an outer metal element The outer metal element is secured to the at least one metal receiving surface of the non-metal substrate.
摘要翻译： 一种用于制造燃气涡轮发动机的部件的方法包括形成具有至少一个金属接收表面的非金属基板。 形成对应于至少一个金属接收表面的形状的阴极。 将阴极浸没在离子液体电镀溶液中。 溶液包含金属阳离子源和第一离子液体溶剂。 通过电镀液将电流施加到阴极，从而将金属阳离子沉积到阴极上并形成外部金属元件。外部金属元件固定到非金属基底的至少一个金属接收表面。
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公开(公告)号：US20140220324A1
公开(公告)日：2014-08-07
申请号：US13586099
申请日：2012-08-15
申请人： Christopher W. Strock , Michael Maloney , David A. Litton , Benjamin Joseph Zimmerman , Brian T. Hazel
发明人： Christopher W. Strock , Michael Maloney , David A. Litton , Benjamin Joseph Zimmerman , Brian T. Hazel
IPC分类号： F02C7/24
CPC分类号： F02C7/24 , C23C28/321 , C23C28/3215 , C23C28/3455 , C23C28/36 , F01D5/286 , F01D5/288 , F05D2230/90 , F05D2300/501 , F05D2300/514 , Y10T428/24942 , Y10T428/249981
摘要： A component according to an exemplary aspect of the present disclosure includes, among other things, a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer includes a material that absorbs energy in response to an impact event along at least a portion of the outer layer.
摘要翻译： 根据本公开的示例性方面的部件包括沉积在基底的至少一部分上的基底，热障涂层以及沉积在热障涂层的至少一部分上的外层。 外层包括响应于沿着外层的至少一部分的冲击事件吸收能量的材料。
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公开(公告)号：US20140065408A1
公开(公告)日：2014-03-06
申请号：US13603891
申请日：2012-09-05
申请人： Christopher W. Strock , Michael Maloney , David A. Litton , Benjamin Joseph Zimmerman , Brian T. Hazel
发明人： Christopher W. Strock , Michael Maloney , David A. Litton , Benjamin Joseph Zimmerman , Brian T. Hazel
CPC分类号： C23C4/02 , C23C4/11 , C23C4/134 , C23C28/321 , C23C28/3215 , C23C28/3455 , C23C28/347 , F01D5/288 , F05D2300/13 , F05D2300/514 , Y10T428/249981 , Y10T428/31678
摘要： A component for a gas turbine engine according to an exemplary embodiment of the present disclosure can include a substrate, a thermal barrier coating deposited on at least a portion of the substrate, and an outer layer deposited on at least a portion of the thermal barrier coating. The outer layer can include a material that is reactive with an environmental contaminant that comes into contact with the outer layer to alter a microstructure of the outer layer.
摘要翻译： 根据本公开的示例性实施例的用于燃气涡轮发动机的部件可以包括基板，沉积在基板的至少一部分上的热障涂层以及沉积在热障涂层的至少一部分上的外层 。 外层可以包括与环境污染物反应的材料，其与外层接触以改变外层的微观结构。
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公开(公告)号：US20130118643A1
公开(公告)日：2013-05-16
申请号：US13735329
申请日：2013-01-07
IPC分类号： C23C10/60
CPC分类号： C23C10/60 , C23C10/20 , C23C10/26 , C23C30/00 , C25D3/665 , C25D5/10 , C25D5/50 , F01D5/288 , F05D2230/30 , F05D2230/90
摘要： A coating method includes depositing substantially pure hafnium metal, that is free of other elements that are present in more than trace amounts as inadvertent impurities, onto a metallic substrate, and heat treating the metallic substrate to react the hafnium metal with at least one other element to form a protective coating on the metallic substrate.
摘要翻译： 一种涂覆方法包括将基本上纯的铪金属沉积在金属基底上，将不存在超过痕量的其它元素作为无意杂质沉积，并且对金属基底进行热处理以使铪金属与至少一种其它元素反应 以在金属基底上形成保护涂层。
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公开(公告)号：US20120114862A1
公开(公告)日：2012-05-10
申请号：US12940171
申请日：2010-11-05
IPC分类号： B05D3/02
CPC分类号： C23C10/60 , C23C10/20 , C23C10/26 , C23C30/00 , C25D3/665 , C25D5/10 , C25D5/50 , F01D5/288 , F05D2230/30 , F05D2230/90
摘要： A coating method includes depositing a reactive material onto a turbine engine component using an ionic liquid that is a melt of a salt, and heat treating the turbine engine component to react the reactive material with at least one other element to form a protective coating on the turbine engine component.
摘要翻译： 涂覆方法包括使用作为盐的熔体的离子液体将反应性材料沉积到涡轮发动机部件上，以及热处理涡轮发动机部件以使反应性材料与至少一种其它元件反应以在其上形成保护涂层 涡轮发动机部件。
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公开(公告)号：US09206499B2
公开(公告)日：2015-12-08
申请号：US12871028
申请日：2010-08-30
CPC分类号： C23C4/12 , C23C4/01 , C23C4/02 , C23C4/137 , C23C14/042 , F01D5/186 , F01D5/288 , F05D2230/312 , F05D2250/70 , F05D2300/13 , F05D2300/21
摘要： An airfoil for use in a gas turbine engine is provided, the airfoil having a hole therein. A ceramic plug is inserted in the hole so that the plug extends above a depth of a thermal barrier coating, such as a ceramic, to be placed on the airfoil. The airfoil is then coated by non-line of sight vapor deposition and the plugs are then removed.
摘要翻译： 提供了一种用于燃气涡轮发动机的翼型件，其中具有孔的翼型件。 将陶瓷塞插入孔中，使得插头延伸到诸如陶瓷的热障涂层的深度之上，以放置在翼型上。 然后通过非视线气相沉积涂覆翼型件，然后将塞子移除。
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公开(公告)号：US20130164558A1
公开(公告)日：2013-06-27
申请号：US13337542
申请日：2011-12-27
CPC分类号： C23C30/00 , C22C19/05 , C22C19/058 , C23C4/073 , C23C14/16 , Y10T428/12931
摘要： An oxidation resistant coating has a composition which comprises from 11 to 14 wt % chromium, from 11 to 14 wt % cobalt, from 7.5 to 9.5 wt % aluminum, from 0.20 to 0.60 wt % yttrium, from 0.10 to 0.50 wt % hafnium, from 0.10 to 0.30 wt % silicon, from 0.10 to 0.20 wt % zirconium, and the balance nickel.
摘要翻译： 耐氧化涂层具有包含11至14重量％的铬，11至14重量％的钴，7.5至9.5重量％的铝，0.20至0.60重量％的钇，0.10至0.50重量％的铪， 0.10〜0.30重量％的硅，0.10〜0.20重量％的锆，余量为镍。
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公开(公告)号：US08367160B2
公开(公告)日：2013-02-05
申请号：US12940171
申请日：2010-11-05
IPC分类号： B05D3/02
CPC分类号： C23C10/60 , C23C10/20 , C23C10/26 , C23C30/00 , C25D3/665 , C25D5/10 , C25D5/50 , F01D5/288 , F05D2230/30 , F05D2230/90
摘要： A coating method includes depositing a reactive material onto a turbine engine component using an ionic liquid that is a melt of a salt, and heat treating the turbine engine component to react the reactive material with at least one other element to form a protective coating on the turbine engine component.
摘要翻译： 涂覆方法包括使用作为盐的熔体的离子液体将反应性材料沉积到涡轮发动机部件上，以及热处理涡轮发动机部件以使反应性材料与至少一种其它元件反应以在其上形成保护涂层 涡轮发动机部件。
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