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1.发明授权Method and assembly for gas turbine engine airfoils with protective coating 有权具有保护涂层的燃气涡轮发动机翼型的方法和装配公开(公告)号：US08366386B2
公开(公告)日：2013-02-05
申请号：US12360312
申请日：2009-01-27
申请人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
IPC分类号： F04D29/44
CPC分类号： F01D9/02 , F01D5/288 , F05D2230/237 , F05D2230/90 , Y02T50/67 , Y10T29/49231 , Y10T29/49238
摘要： A method of processing turbine airfoils includes depositing a protective coating on first and second turbine airfoils, and bonding the first and second turbine airfoils together after the deposition such that there is an open throat between the first and second turbine airfoil and at least portions of surfaces in the open throat are coated with the protective coating.
摘要翻译： 一种处理涡轮机翼片的方法包括在第一和第二涡轮机翼型上沉积保护涂层，以及在沉积之后将第一和第二涡轮机翼型件结合在一起，使得在第一和第二涡轮机翼面之间存在开放的喉部和至少部分表面 在开放的喉咙里涂上保护涂层。
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2.发明申请METHOD AND ASSEMBLY FOR GAS TURBINE ENGINE AIRFOILS WITH PROTECTIVE COATING 有权具有保护涂层的气体涡轮发动机空气的方法和装配公开(公告)号：US20100189555A1
公开(公告)日：2010-07-29
申请号：US12360312
申请日：2009-01-27
申请人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Daniel E. Quinn , David J. Hiskes , Carl W. Mercier , Michael Minor , Paul M. Pellet , Michael L. Miller
CPC分类号： F01D9/02 , F01D5/288 , F05D2230/237 , F05D2230/90 , Y02T50/67 , Y10T29/49231 , Y10T29/49238
摘要： A method of processing turbine airfoils includes depositing a protective coating on first and second turbine airfoils, and bonding the first and second turbine airfoils together after the deposition such that there is an open throat between the first and second turbine airfoil and at least portions of surfaces in the open throat are coated with the protective coating.
摘要翻译： 一种处理涡轮机翼片的方法包括在第一和第二涡轮机翼型上沉积保护涂层，以及在沉积之后将第一和第二涡轮机翼型件结合在一起，使得在第一和第二涡轮机翼面之间存在开放的喉部和至少部分表面 在开放的喉咙里涂上保护涂层。
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公开(公告)号：US09687926B2
公开(公告)日：2017-06-27
申请号：US12417714
申请日：2009-04-03
CPC分类号： B23H9/10 , B23H11/003 , B23Q3/063 , B24B19/14 , B24B41/06
摘要： A method of securing an workpiece for machining the trailing edge. The workpiece has a platform from which extends an airfoil, the airfoil including a leading edge and a trailing edge, and a pressure side and a suction side. A fixture with at least one locating datum that relates to the platform and at least one locating datum that relates to the leading edge is provided. The fixture does not contact the trailing edge of the workpiece. The workpiece is positioned so that the platform is against the related locating datum and the leading edge is against the related locating datum. The workpiece is secured within the fixture, and the trailing edge of the workpiece is machined.
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公开(公告)号：US20100252533A1
公开(公告)日：2010-10-07
申请号：US12417714
申请日：2009-04-03
CPC分类号： B23H9/10 , B23H11/003 , B23Q3/063 , B24B19/14 , B24B41/06
摘要： A method of securing an workpiece for machining the trailing edge. The workpiece has a platform from which extends an airfoil, the airfoil including a leading edge and a trailing edge, and a pressure side and a suction side. A fixture with at least one locating datum that relates to the platform and at least one locating datum that relates to the leading edge is provided. The fixture does not contact the trailing edge of the workpiece. The workpiece is positioned so that the platform is against the related locating datum and the leading edge is against the related locating datum. The workpiece is secured within the fixture, and the trailing edge of the workpiece is machined.
摘要翻译： 一种固定用于加工后缘的工件的方法。 工件具有一个平台，从该平台延伸翼型件，该翼型件包括前缘和后缘，以及压力侧和吸力侧。 提供具有至少一个与平台相关的定位基准的固定装置和至少一个与前缘相关的定位基准。 夹具不接触工件的后缘。 工件被定位成使得平台抵靠相关的定位基准，并且前缘抵靠相关的定位基准。 工件被固定在固定装置内，并且加工工件的后缘。
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公开(公告)号：US20100297472A1
公开(公告)日：2010-11-25
申请号：US12470993
申请日：2009-05-22
CPC分类号： C23C30/00 , C23C4/073 , C23C14/16 , Y10T428/12778 , Y10T428/12944
摘要： A metallic coating for protecting a substrate from high temperature oxidation and hot corrosion environments comprising about 2.5 to about 13.5 wt. % cobalt, about 12 to about 27 wt. % chromium, about 5 to about 7 wt. % aluminum, about 0.0 to about 1.0 wt. % yttrium, about 0.0 to about 1.0 wt. % hafnium, about 1.0 to about 3.0 wt. % silicon, about 0.0 to about 4.5 wt. % tantalum, about 0.0 to about 6.5 wt. % tungsten, about 0.0 to about 2.0 wt. % rhenium, about 0.0 to about 1.0 wt. % molybdenum and the balance nickel.
摘要翻译： 用于保护基材免受高温氧化和热腐蚀环境的金属涂层，其包含约2.5至约13.5wt。 ％钴，约12至约27wt。 约5至约7wt。％的铬。 ％铝，约0.0至约1.0wt。 ％钇，约0.0至约1.0wt。 ％铪，约1.0至约3.0wt。 ％硅，约0.0-约4.5wt。 ％钽，约0.0-约6.5wt。 ％钨，约0.0至约2.0重量％ ％铼，约0.0至约1.0wt。 钼和余量为镍。
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公开(公告)号：US08354176B2
公开(公告)日：2013-01-15
申请号：US12470993
申请日：2009-05-22
CPC分类号： C23C30/00 , C23C4/073 , C23C14/16 , Y10T428/12778 , Y10T428/12944
摘要： A metallic coating for protecting a substrate from high temperature oxidation and hot corrosion environments comprising about 2.5 to about 13.5 wt. % cobalt, about 12 to about 27 wt. % chromium, about 5 to about 7 wt. % aluminum, about 0.0 to about 1.0 wt. % yttrium, about 0.0 to about 1.0 wt. % hafnium, about 1.0 to about 3.0 wt. % silicon, about 0.0 to about 4.5 wt. % tantalum, about 0.0 to about 6.5 wt. % tungsten, about 0.0 to about 2.0 wt. % rhenium, about 0.0 to about 1.0 wt. % molybdenum and the balance nickel.
摘要翻译： 用于保护基材免受高温氧化和热腐蚀环境的金属涂层，其包含约2.5至约13.5wt。 ％钴，约12至约27wt。 约5至约7wt。％的铬。 ％铝，约0.0至约1.0wt。 ％钇，约0.0至约1.0wt。 ％铪，约1.0至约3.0wt。 ％硅，约0.0-约4.5wt。 ％钽，约0.0-约6.5wt。 ％钨，约0.0至约2.0重量％ ％铼，约0.0至约1.0wt。 钼和余量为镍。
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公开(公告)号：US08075662B2
公开(公告)日：2011-12-13
申请号：US12109398
申请日：2008-04-25
申请人： Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Michael Minor , Paul M. Pellet , Michael L. Miller
IPC分类号： B22F1/00
CPC分类号： C22C19/057 , B23K35/304 , B23K2101/001 , C22C1/0433 , C22C19/055 , C22C19/056
摘要： A nickel braze alloy composition includes a blend of a first nickel alloy and a second nickel alloy. The first nickel alloy includes about 4.75 wt %-10.5 wt % of chromium, about 5.5 wt %-6.7 wt % of aluminum, up to about 13 wt % cobalt, about 3.75 wt %-9.0 wt % of tantalum, about 1.3 wt %-2.25 wt % of molybdenum, about 3.0 wt %-6.8 wt % of tungsten, about 2.6 wt %-3.25 wt % of rhenium, up to about 0.02 wt % of boron, about 0.05 wt %-2.0 wt % of hafnium, up to about 0.14 wt % of carbon, up to about 0.35 wt % of zirconium, and a balance of nickel. The second nickel alloy includes about 21.25 wt %-22.75 wt % of chromium, about 5.7 wt %-6.3 wt % of aluminum, about 11.5 wt %-12.5 wt % of cobalt, about 5.7 wt %-6.3 wt % of silicon, boron in an amount no greater than 1.0 wt %, and a balance of nickel.
摘要翻译： 镍钎焊合金组合物包括第一镍合金和第二镍合金的共混物。 第一种镍合金包括约4.75wt％-10.5wt％的铬，约5.5wt％-6.7wt％的铝，至多约13wt％的钴，约3.75wt％的-9.0wt％的钽，约1.3wt％ -2.25重量％的钼，约3.0重量％的-6.8重量％的钨，约2.6重量％的-3.25重量％的铼，至多约0.02重量％的硼，约0.05重量％〜2.0重量％的铪， 至约0.14重量％的碳，至多约0.35重量％的锆，余量为镍。 第二镍合金包括约21.25重量％-22.75重量％的铬，约5.7重量％-6.3重量％的铝，约11.5重量％-12.5重量％的钴，约5.7重量％-6.3重量％的硅，硼 不大于1.0重量％，余量为镍。
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公开(公告)号：US20090266446A1
公开(公告)日：2009-10-29
申请号：US12109398
申请日：2008-04-25
申请人： Michael Minor , Paul M. Pellet , Michael L. Miller
发明人： Michael Minor , Paul M. Pellet , Michael L. Miller
IPC分类号： B23K35/22
CPC分类号： C22C19/057 , B23K35/304 , B23K2101/001 , C22C1/0433 , C22C19/055 , C22C19/056
摘要： A nickel braze alloy composition includes a blend of a first nickel alloy and a second nickel alloy. The first nickel alloy includes about 4.75 wt %-10.5 wt % of chromium, about 5.5 wt %-6.7 wt % of aluminum, up to about 13 wt % cobalt, about 3.75 wt %-9.0 wt % of tantalum, about 1.3 wt %-2.25 wt % of molybdenum, about 3.0 wt %-6.8 wt % of tungsten, about 2.6 wt %-3.25 wt % of rhenium, up to about 0.02 wt % of boron, about 0.05 wt %-2.0 wt % of hafnium, up to about 0.14 wt % of carbon, up to about 0.35 wt % of zirconium, and a balance of nickel. The second nickel alloy includes about 21.25 wt %-22.75 wt % of chromium, about 5.7 wt %-6.3 wt % of aluminum, about 11.5 wt %-12.5 wt % of cobalt, about 5.7 wt %-6.3 wt % of silicon, boron in an amount no greater than 1.0 wt %, and a balance of nickel.
摘要翻译： 镍钎焊合金组合物包括第一镍合金和第二镍合金的共混物。 第一种镍合金包括约4.75wt％-10.5wt％的铬，约5.5wt％-6.7wt％的铝，至多约13wt％的钴，约3.75wt％的-9.0wt％的钽，约1.3wt％ -2.25重量％的钼，约3.0重量％的-6.8重量％的钨，约2.6重量％的-3.25重量％的铼，至多约0.02重量％的硼，约0.05重量％〜2.0重量％的铪， 至约0.14重量％的碳，至多约0.35重量％的锆，余量为镍。 第二镍合金包括约21.25重量％-22.75重量％的铬，约5.7重量％-6.3重量％的铝，约11.5重量％-12.5重量％的钴，约5.7重量％-6.3重量％的硅，硼 不大于1.0重量％，余量为镍。
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公开(公告)号：US20110116912A1
公开(公告)日：2011-05-19
申请号：US12617741
申请日：2009-11-13
CPC分类号： F01D5/288 , C23C4/01 , C23C14/042 , F01D5/186 , F01D9/041 , F05D2230/90
摘要： A turbine component has an airfoil extending between a leading edge and a trailing edge, and has an outer surface. A coating includes at least two discontinuous areas that are spaced from each other such that there is an area of uncoated surface between the discontinuous areas of coating. In addition, a method of providing such a coating is disclosed.
摘要翻译： 涡轮机部件具有在前缘和后缘之间延伸的翼型件，并且具有外表面。 涂层包括彼此间隔开的至少两个不连续区域，使得在不连续涂层区域之间存在未涂覆表面的区域。 此外，公开了一种提供这种涂层的方法。
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公开(公告)号：US20090274562A1
公开(公告)日：2009-11-05
申请号：US12151102
申请日：2008-05-02
CPC分类号： F01D9/04 , F01D5/288 , Y10T29/49746
摘要： A method for coating a nozzle segment, the method comprising separating an outer shroud and an inner platform of the nozzle segment along pathways that bisect a first stator vane and a second stator vane of the of the nozzle segment, coating the first stator vane and the second stator vane after separating the outer shroud and the inner platform, and rejoining the separated outer shroud and the separated inner platform after coating the first stator vane and the second stator vane.
摘要翻译： 一种用于涂覆喷嘴段的方法，所述方法包括沿着将所述喷嘴段的第一定子叶片和第二定子叶片平分的路径分离所述喷嘴段的外护罩和内平台，涂覆所述第一定子叶片和 第二定子叶片在分离外护罩和内平台之后，并且在涂覆第一定子叶片和第二定子叶片之后重新接合分离的外护罩和分离的内平台。
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