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公开(公告)号：US20130104567A1
公开(公告)日：2013-05-02
申请号：US13285946
申请日：2011-10-31
申请人： Douglas Gerard Konitzer , Mark Willard Marusko , James Herbert Deines , Brian David Przeslawski , MIchael William Bell , Andrew David William Thiel , Xi Yang
发明人： Douglas Gerard Konitzer , Mark Willard Marusko , James Herbert Deines , Brian David Przeslawski , MIchael William Bell , Andrew David William Thiel , Xi Yang
CPC分类号： F01D5/189 , F05D2260/201 , Y02T50/671 , Y02T50/676 , Y10T29/49341
摘要： An airfoil for a gas turbine engine is provided that includes a first sidewall and a second sidewall coupled together at a leading edge and a trailing edge, such that a cavity is defined therebetween. A central plenum and an impingement chamber are defined within the cavity. The central plenum channels cooling fluid to the impingement chamber where cooling fluid impinges on the sidewalls. Cooling fluid is discharged from the impingement chamber via film cooling holes.
摘要翻译： 提供了一种用于燃气涡轮发动机的翼型件，其包括在前缘和后缘处联接在一起的第一侧壁和第二侧壁，使得在其间限定空腔。 在腔内限定了中央气室和冲击腔。 中央集气室将冷却流体冷却到冲击室，其中冷却流体撞击在侧壁上。 冷却液通过膜冷却孔从冲击室排出。
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公开(公告)号：US20120163985A1
公开(公告)日：2012-06-28
申请号：US12978676
申请日：2010-12-27
申请人： Toby George Darkins, JR. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
发明人： Toby George Darkins, JR. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
CPC分类号： F01D5/147 , F01D5/282 , F01D5/284 , F01D5/288 , F05D2300/222 , F05D2300/2261 , F05D2300/603 , Y02T50/672
摘要： Hybrid components containing a ceramic material, in which detailed features of the components are formed of materials other than ceramic materials, yet result in a robust mechanical attachment of the ceramic and non-ceramic portions of the components. The components includes a first subcomponent formed of a ceramic-based material and a second subcomponent formed of a metallic material. The first subcomponent has a nub and the second subcomponent is separately formed and attached to the first subcomponent by casting the metallic material around the nub of the first subcomponent. The second subcomponent is attached to the first subcomponent by a compression fit and encapsulation of the second subcomponent on the nub of the first subcomponent. The nub has a compliant coating system that provides thermal expansion compliance between the metallic material of the second subcomponent and the ceramic-based material of the first subcomponent.
摘要翻译： 包含陶瓷材料的混合部件，其中部件的详细特征由除陶瓷材料之外的材料形成，但是导致部件的陶瓷和非陶瓷部分的坚固的机械连接。 这些部件包括由陶瓷基材料形成的第一副部件和由金属材料形成的第二副部件。 第一副部件具有凸块，并且第二副部件被分开地形成并且通过将金属材料铸造在第一副部件的凸块周围而附接到第一副部件。 第二子组件通过第二子组件的压缩拟合和封装附接到第一子组件，该第二子组件在第一子组件的组件上。 该微调具有柔性涂层系统，其提供第二次要组分的金属材料与第一次要组分的陶瓷基材料之间的热膨胀顺应性。
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3.发明授权Turbine airfoil components containing ceramic-based materials and processes therefor 有权含有陶瓷基材料的涡轮机翼部件及其工艺公开(公告)号：US09228445B2
公开(公告)日：2016-01-05
申请号：US12977299
申请日：2010-12-23
申请人： Toby George Darkins, Jr. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
发明人： Toby George Darkins, Jr. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
CPC分类号： F01D5/284 , F01D5/147 , F01D5/3084 , F05D2300/6033 , Y02T50/672
摘要： Hybrid turbine airfoil components containing a ceramic material, in which detailed features of the components are formed of materials other than ceramic materials. The components include a first component formed of a ceramic-based material and a second component formed of a metallic material. The first component comprises an airfoil portion and a nub, and the second component is separately formed and attached to the first component by casting the metallic material around the nub of the first component. The second component includes a platform portion between the airfoil portion and the nub of the first component and a dovetail portion on the nub of the first component. Each of the platform and dovetail portions has at least one off-axis geometric feature that results in the second component having a more complex geometry than the first component.
摘要翻译： 包含陶瓷材料的混合涡轮机翼型部件，其中部件的详细特征由不同于陶瓷材料的材料形成。 这些部件包括由陶瓷基材料形成的第一部件和由金属材料形成的第二部件。 第一部件包括翼型部分和凸缘，并且第二部件分开地形成并且通过将金属材料围绕第一部件的凸块浇铸而附接到第一部件。 第二部件包括位于第一部件的翼型部和凸缘之间的平台部分和第一部件的凸点上的燕尾部分。 平台和燕尾部分中的每一个具有至少一个离轴几何特征，其导致第二部件具有比第一部件更复杂的几何形状。
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公开(公告)号：US08777582B2
公开(公告)日：2014-07-15
申请号：US12978676
申请日：2010-12-27
申请人： Toby George Darkins, Jr. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
发明人： Toby George Darkins, Jr. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
IPC分类号： F01D5/28
CPC分类号： F01D5/147 , F01D5/282 , F01D5/284 , F01D5/288 , F05D2300/222 , F05D2300/2261 , F05D2300/603 , Y02T50/672
摘要： Hybrid components containing a ceramic material, in which detailed features of the components are formed of materials other than ceramic materials, yet result in a robust mechanical attachment of the ceramic and non-ceramic portions of the components. The components includes a first subcomponent formed of a ceramic-based material and a second subcomponent formed of a metallic material. The first subcomponent has a nub and the second subcomponent is separately formed and attached to the first subcomponent by casting the metallic material around the nub of the first subcomponent. The second subcomponent is attached to the first subcomponent by a compression fit and encapsulation of the second subcomponent on the nub of the first subcomponent. The nub has a compliant coating system that provides thermal expansion compliance between the metallic material of the second subcomponent and the ceramic-based material of the first subcomponent.
摘要翻译： 包含陶瓷材料的混合部件，其中部件的详细特征由除陶瓷材料之外的材料形成，但是导致部件的陶瓷和非陶瓷部分的坚固的机械连接。 这些部件包括由陶瓷基材料形成的第一副部件和由金属材料形成的第二副部件。 第一副部件具有凸块，并且第二副部件被分开地形成并且通过将金属材料铸造在第一副部件的凸块周围而附接到第一副部件。 第二子组件通过第二子组件的压缩拟合和封装附接到第一子组件，该第二子组件在第一子组件的组件上。 该微调具有柔性涂层系统，其提供第二次要组分的金属材料与第一次要组分的陶瓷基材料之间的热膨胀顺应性。
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5.发明申请公开(公告)号：US20120163978A1
公开(公告)日：2012-06-28
申请号：US12977299
申请日：2010-12-23
申请人： Toby George Darkins, JR. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
发明人： Toby George Darkins, JR. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
CPC分类号： F01D5/284 , F01D5/147 , F01D5/3084 , F05D2300/6033 , Y02T50/672
摘要： Hybrid turbine airfoil components containing a ceramic material, in which detailed features of the components are formed of materials other than ceramic materials. The components include a first component formed of a ceramic-based material and a second component formed of a metallic material. The first component comprises an airfoil portion and a nub, and the second component is separately formed and attached to the first component by casting the metallic material around the nub of the first component. The second component includes a platform portion between the airfoil portion and the nub of the first component and a dovetail portion on the nub of the first component. Each of the platform and dovetail portions has at least one off-axis geometric feature that results in the second component having a more complex geometry than the first component.
摘要翻译： 包含陶瓷材料的混合涡轮机翼型部件，其中部件的详细特征由不同于陶瓷材料的材料形成。 这些部件包括由陶瓷基材料形成的第一部件和由金属材料形成的第二部件。 第一部件包括翼型部分和凸缘，并且第二部件分开地形成并且通过将金属材料围绕第一部件的凸块浇铸而附接到第一部件。 第二部件包括位于第一部件的翼型部和凸缘之间的平台部分和第一部件的凸点上的燕尾部分。 平台和燕尾部分中的每一个具有至少一个离轴几何特征，其导致第二部件具有比第一部件更复杂的几何形状。
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6.发明授权Processes for producing components containing ceramic-based and metallic materials 有权用于生产含有陶瓷基和金属材料的组分的方法公开(公告)号：US08721290B2
公开(公告)日：2014-05-13
申请号：US12977364
申请日：2010-12-23
申请人： Toby George Darkins, Jr. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
发明人： Toby George Darkins, Jr. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
IPC分类号： F01D5/28
CPC分类号： B22D19/0054 , B22D19/04 , F01D5/225 , F01D5/284 , F01D5/3007 , F01D5/3092 , F01D9/041 , F01D9/042 , Y02T50/672
摘要： Processes for producing a component containing a ceramic-based material and having detailed features formed from materials other than ceramic materials. Such a process entails producing the component to include a first subcomponent and at least a second subcomponent having at least one off-axis geometric feature that results in the second subcomponent having a more complex geometry than the first subcomponent. The first subcomponent is formed of a ceramic-based material, and the second subcomponent and its off-axis geometric feature are separately formed of a metallic material and attached to the first subcomponent to yield a robust mechanical attachment. The component may be, for example, a gas turbine airfoil component.
摘要翻译： 用于生产含有陶瓷基材料并具有由陶瓷材料以外的材料形成的详细特征的组分的方法。 这样的过程需要生成组件以包括第一子组件和具有至少一个离轴几何特征的至少第二子组件，该第二子组件导致第二子组件具有比第一子组件更复杂的几何。 第一副部件由陶瓷基材料形成，并且第二副部件及其离轴几何特征分别由金属材料形成并附接到第一副部件以产生坚固的机械连接。 该部件可以是例如燃气轮机翼型件。
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7.发明申请PROCESSES FOR PRODUCING COMPONENTS CONTAINING CERAMIC-BASED AND METALLIC MATERIALS 有权生产含有陶瓷和金属材料的组件的方法公开(公告)号：US20120163979A1
公开(公告)日：2012-06-28
申请号：US12977364
申请日：2010-12-23
申请人： Toby George Darkins, JR. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
发明人： Toby George Darkins, JR. , John Peter Heyward , Eric Alan Estill , Joshua Brian Jamison , James Herbert Deines , Mark Willard Marusko , James Thomas Hawkins
CPC分类号： B22D19/0054 , B22D19/04 , F01D5/225 , F01D5/284 , F01D5/3007 , F01D5/3092 , F01D9/041 , F01D9/042 , Y02T50/672
摘要： Processes for producing a component containing a ceramic-based material and having detailed features formed from materials other than ceramic materials. Such a process entails producing the component to include a first subcomponent and at least a second subcomponent having at least one off-axis geometric feature that results in the second subcomponent having a more complex geometry than the first subcomponent. The first subcomponent is formed of a ceramic-based material, and the second subcomponent and its off-axis geometric feature are separately formed of a metallic material and attached to the first subcomponent to yield a robust mechanical attachment. The component may be, for example, a gas turbine airfoil component.
摘要翻译： 用于生产含有陶瓷基材料并具有由陶瓷材料以外的材料形成的详细特征的组分的方法。 这样的过程需要生成组件以包括第一子组件和具有至少一个离轴几何特征的至少第二子组件，该第二子组件导致第二子组件具有比第一子组件更复杂的几何。 第一副部件由陶瓷基材料形成，并且第二副部件及其离轴几何特征分别由金属材料形成并附接到第一副部件以产生坚固的机械连接。 该部件可以是例如燃气轮机翼型件。
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公开(公告)号：US08834105B2
公开(公告)日：2014-09-16
申请号：US12982082
申请日：2010-12-30
申请人： Joseph Charles Albers , Mark Willard Marusko , Barry Allan Wilson , Aaron Michael Dziech , Christopher Ryan Johnson
发明人： Joseph Charles Albers , Mark Willard Marusko , Barry Allan Wilson , Aaron Michael Dziech , Christopher Ryan Johnson
CPC分类号： F01D11/005 , F01D25/12 , F01D25/246 , F05D2260/202 , F05D2260/31 , F05D2300/6033
摘要： A turbine shroud apparatus for a gas turbine engine having a central axis includes: an arcuate shroud segment comprising low-ductility material and having a cross-sectional shape defined by opposed forward and aft walls, and opposed inner and outer walls, the walls extending between opposed first and second end faces and collectively defining a shroud cavity; and an annular stationary structure surrounding the shroud segment, where the shroud segment is mechanically coupled to the stationary structure. The stationary structure includes at least one axially-facing bearing surface which is in direct contact with the shroud segment, and the shroud segment is disposed so as to absorb at least one axially-aligned force and transfer the axially-aligned force to the bearing surface.
摘要翻译： 一种用于具有中心轴线的燃气涡轮发动机的涡轮机护罩装置包括：弓形护罩段，其包括低延展性材料并且具有由相对的前壁和后壁限定的横截面形状，以及相对的内壁和外壁， 相对的第一和第二端面并且共同地限定护罩腔; 以及围绕所述护罩段的环形固定结构，其中所述护罩段机械地联接到所述固定结构。 固定结构包括与护罩段直接接触的至少一个面向轴向的轴承表面，并且护罩段设置成吸收至少一个轴向对齐的力并将轴向对准的力传递到支承表面 。
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公开(公告)号：US08753073B2
公开(公告)日：2014-06-17
申请号：US12821599
申请日：2010-06-23
CPC分类号： F01D11/125 , F01D25/246 , F05D2240/11 , F05D2240/55 , F05D2260/20 , F05D2300/603 , Y02T50/672 , Y02T50/676
摘要： A turbine shroud sealing apparatus for a gas turbine engine includes: (a) an arcuate shroud segment comprising a low-ductility material and having a cross-sectional shape defined by opposed forward and aft walls, and opposed inner and outer walls, the walls extending between opposed first and second end faces of the segment; and (b) a first seal assembly received in at least one slot formed in the first end face, the first seal assembly comprising one or more spline seals which protrude from the first end face and which are arranged to define a continuous sealing surface around the perimeter of the first end face.
摘要翻译： 一种用于燃气涡轮发动机的涡轮机护罩密封装置包括：（a）弓形护罩段，其包括低延展性材料并具有由相对的前壁和后壁限定的横截面形状，以及相对的内壁和外壁，所述壁延伸 在所述段的相对的第一和第二端面之间; 和（b）第一密封组件，其容纳在形成在所述第一端面中的至少一个槽中，所述第一密封组件包括一个或多个花键密封件，所述花键密封件从所述第一端面突出并且被布置成限定围绕所述第一端面的连续密封表面 第一端面的周长。
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公开(公告)号：US08740552B2
公开(公告)日：2014-06-03
申请号：US12790209
申请日：2010-05-28
IPC分类号： F01D11/08
CPC分类号： F01D11/08 , F01D9/04 , F01D11/122 , F05D2250/70 , F05D2300/2261 , F05D2300/228 , F05D2300/603 , Y02T50/672
摘要： A turbine shroud apparatus for a gas turbine engine includes an arcuate turbine shroud segment of low-ductility material and having a cross-sectional shape defined by opposed forward and aft walls, and opposed inner and outer walls, the walls extending between opposed first and second end faces. At least a portion of each of the forward and aft walls is oriented at an acute angle to the outer wall. Radially inner ends of the forward and aft walls are substantially closer together than radially outer ends thereof.
摘要翻译： 用于燃气涡轮发动机的涡轮机护罩装置包括低延性材料的弓形涡轮机护罩部分，并且具有由相对的前壁和后壁限定的横截面形状，以及相对的内壁和外壁，所述壁在相对的第一和第二相对之间延伸 端面。 前壁和后壁中的每一个的至少一部分被定向成与外壁呈锐角。 前壁和后壁的径向内端比其径向外端大致更靠近在一起。
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