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21. 发明申请

US20120163979A1 PROCESSES FOR PRODUCING COMPONENTS CONTAINING CERAMIC-BASED AND METALLIC MATERIALS 有权
标题翻译：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
IPC分类号： F04D29/38 , B23P15/04
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。

22. 发明授权

US08141370B2 Methods and apparatus for radially compliant component mounting 有权
标题翻译：用于径向兼容部件安装的方法和装置
公开(公告)号：US08141370B2
公开(公告)日：2012-03-27
申请号：US11463142
申请日：2006-08-08
申请人： David Edward Bulman , Toby George Darkins, Jr. , James Anthony Stumpf , Mark S. Schroder , John Joseph Lipinski
发明人： David Edward Bulman , Toby George Darkins, Jr. , James Anthony Stumpf , Mark S. Schroder , John Joseph Lipinski
IPC分类号： F02C7/20
CPC分类号： F02C7/20 , F02C3/14 , F05D2230/642 , F05D2300/21 , F05D2300/50212 , F05D2300/603 , F23R3/007
摘要： Methods and apparatus for a mounting assembly for a liner of a gas turbine engine combustor are provided. The combustor includes a combustor liner and a radially outer annular flow sleeve. The mounting assembly includes an inner ring surrounding a radially outer surface of the liner and including a plurality of axially extending fingers. The mounting assembly also includes a radially outer ring coupled to the inner ring through a plurality of spacers that extend radially from a radially outer surface of the inner ring to the outer ring.
摘要翻译：提供了一种用于燃气涡轮发动机燃烧器的衬套的安装组件的方法和装置。燃烧器包括燃烧器衬套和径向外部环形流动套筒。安装组件包括围绕衬套的径向外表面的内环，并且包括多个轴向延伸的指状物。安装组件还包括通过多个间隔件联接到内环的径向外环，其从内环的径向外表面径向延伸到外环。

23. 发明授权

US06895761B2 Mounting assembly for the aft end of a ceramic matrix composite liner in a gas turbine engine combustor 有权
标题翻译：用于燃气轮机发动机燃烧器中的陶瓷基体复合衬套的后端的安装组件
公开(公告)号：US06895761B2
公开(公告)日：2005-05-24
申请号：US10326209
申请日：2002-12-20
申请人： Krista Anne Mitchell , David Edward Bulman , Mark Eugene Noe , Harold Ray Hansel , Thomas Allen Wells , Christopher Charles Glynn , John David Bibler , Toby George Darkins, Jr. , Joseph John Charneski , Craig Patrick Burns
发明人： Krista Anne Mitchell , David Edward Bulman , Mark Eugene Noe , Harold Ray Hansel , Thomas Allen Wells , Christopher Charles Glynn , John David Bibler , Toby George Darkins, Jr. , Joseph John Charneski , Craig Patrick Burns
IPC分类号： F23R3/00 , F23R3/60 , F02C7/20
CPC分类号： F23R3/60 , F05B2230/606 , F23R3/007
摘要： A mounting assembly for an aft end of a liner of a gas turbine engine combustor including a support member, wherein a longitudinal centerline axis extends through the gas turbine engine. The mounting assembly includes a pin member extending through each one of a plurality of circumferentially spaced openings in a portion of the support member for the combustor and into a plurality of partial openings formed in the aft end of the liner, with each pin member including a head portion at one end thereof, and a device positioned within each opening in the support member so as to retain the pin members therein. The pin members and the support member are able to slide radially and/or axially with respect to the liner aft end as the support member experiences thermal growth greater than the liner.
摘要翻译：包括支撑构件的燃气涡轮发动机燃烧器的衬套的后端的安装组件，其中纵向中心线轴线延伸穿过燃气涡轮发动机。安装组件包括销构件，其延伸穿过用于燃烧器的支撑构件的一部分中的多个周向间隔开的开口中的每一个并且形成在衬套的后端中的多个部分开口，每个销构件包括在其一端的头部，以及位于支撑构件中的每个开口内的装置，以便将销构件保持在其中。当支撑构件经历大于衬套的热生长时，销构件和支撑构件能够相对于衬垫后端部径向和/或轴向地滑动。

24. 发明授权

US06733235B2 Shroud segment and assembly for a turbine engine 有权
标题翻译：用于涡轮发动机的护罩段和组件
公开(公告)号：US06733235B2
公开(公告)日：2004-05-11
申请号：US10109014
申请日：2002-03-28
申请人： Mary Ellen Alford , Mark Eugene Noe , Toby George Darkins, Jr. , Madeleine Elise Fessler
发明人： Mary Ellen Alford , Mark Eugene Noe , Toby George Darkins, Jr. , Madeleine Elise Fessler
IPC分类号： F01D1108
CPC分类号： F01D25/246 , F01D11/08 , Y10T29/49323
摘要： A turbine engine shroud segment comprises a body including a radially outer surface having axially and circumferentially spaced apart edge surfaces. The segment includes a projection integral with and projecting generally radially outwardly from the body, and positioned at a generally midway surface portion between the axially spaced apart edge surfaces. The projection comprises a head and a transition portion with a cross section smaller than that of the head and integral with and between the head and the body. In a turbine engine shroud assembly, a plurality of such shroud segments are assembled circumferentially with a shroud hanger carrying the projection in a hanger cavity through end portions of radially inner opposed hook members that register with the projection at the transition portion.
摘要翻译：涡轮发动机护罩段包括主体，该主体包括具有轴向和周向间隔开的边缘表面的径向外表面。该段包括与主体一体并且大致径向向外突出并且位于轴向间隔开的边缘表面之间的大致中间表面部分处的突出部。突起包括头部和过渡部分，其横截面小于头部的横截面，并与头部和主体成一体。在涡轮发动机护罩组件中，多个这样的护罩区段与护罩悬挂器组装在一起，护罩悬挂器通过在过渡部分处与突起对准的径向内部相对的钩构件的端部将悬臂承载在衣架空腔中。

25. 发明授权

US06702550B2 Turbine shroud segment and shroud assembly 有权
标题翻译：涡轮护罩段和护罩组件
公开(公告)号：US06702550B2
公开(公告)日：2004-03-09
申请号：US10050451
申请日：2002-01-16
申请人： Toby George Darkins, Jr. , Mary Ellen Alford , Christopher Charles Glynn
发明人： Toby George Darkins, Jr. , Mary Ellen Alford , Christopher Charles Glynn
IPC分类号： F01D1108
CPC分类号： F01D11/08 , F01D9/04 , F01D11/24 , F01D25/12
摘要： A turbine engine shroud segment, preferably a low ductility material, for example a ceramic matrix composite, comprises a segment body extending between body circumferential ends. The body includes a body radially inner surface arcuate at least circumferentially, and a body radially outer surface from which a plurality of hooks extend generally radially outwardly. Each hook comprises a generally radially outwardly extending hook arm with a generally axially extending hook end having a generally radially inner surface in spaced apart juxtaposition with a portion of the body radially outer surface. Such body outer surface includes at least two body contact surfaces each matched in shape and in juxtaposition at least at body circumferential ends with a cooperating hanger contact surface. The radially inner surface of each hook end includes a hook end contact surface matched in shape with a cooperating hanger contact surface at least in a circumferential middle portion of such surface. In a turbine engine shroud assembly, a plurality of such shroud segments are assembled circumferentially with a shroud hanger including at least one hanger foot assembled within and between the segment hooks. The hanger foot includes a plurality of spaced apart hanger foot contact surfaces cooperating in juxtaposition with the contact surfaces of the shroud segment body radially outer surface and the hook end radially inner surfaces. The various contact surfaces cooperating in juxtaposition are matched in shape each to define a fluid choke therebetween.
摘要翻译：涡轮发动机护罩段，优选低延展性材料，例如陶瓷基质复合材料，包括在主体周向端部之间延伸的段体。主体包括至少周向弧形的主体径向内表面，以及主体径向外表面，多个钩从该径向外表面大致径向向外延伸。每个钩包括大致径向向外延伸的钩臂，具有大致轴向延伸的钩端，其具有与主体径向外表面的一部分间隔开并置的大致径向内表面。这种主体外表面包括至少两个身体接触表面，每个至少两个身体接触表面的形状和形状至少在身体周向端部处并置，并具有配合的衣架接触表面。每个钩端的径向内表面包括至少在该表面的周向中间部分中与配合的衣架接触面匹配的钩端接触表面。在涡轮发动机护罩组件中，多个这样的护罩段与护罩悬挂器圆周地组装，护罩悬挂器包括组装在段钩内部和之间的至少一个衣架脚。衣架脚包括多个间隔开的衣架脚接触表面，其与护罩段主体的径向外表面和钩端径向内表面的接触表面并置配合。并列配合的各个接触表面的形状各自在其间形成流体扼流圈。

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