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1. 发明授权

US08366983B2 Method of manufacturing a thermal insulation article 有权
标题翻译：隔热制品的制造方法
公开(公告)号：US08366983B2
公开(公告)日：2013-02-05
申请号：US12177623
申请日：2008-07-22
申请人： Jay E. Lane , Gary B. Merrill
发明人： Jay E. Lane , Gary B. Merrill
IPC分类号： B28B7/30
CPC分类号： B28B21/20 , B28B23/00 , F23R3/007 , F23R2900/00018
摘要： A method of manufacturing a thermal insulation article may include positioning, between opposing mold walls, a first layer comprising a ceramic matrix composite (CMC) material and a second layer comprising a plurality of tiles. The method may further include moving the opposing mold walls together to compress together the first and second layers, and curing the compressed together first and second layers to produce the thermal insulation article.
摘要翻译：制造隔热制品的方法可以包括在相对的模具壁之间定位包括陶瓷基质复合材料（CMC）材料的第一层和包括多个瓷砖的第二层。该方法还可以包括将相对的模具壁移动到一起以将第一和第二层压缩在一起，以及将压缩在一起的第一和第二层固化以产生绝热制品。

2. 发明申请

US20120125585A1 CMC WALL STRUCTURE WITH INTEGRAL COOLING CHANNELS 有权
标题翻译：具有集成冷却通道的CMC壁结构
公开(公告)号：US20120125585A1
公开(公告)日：2012-05-24
申请号：US11715678
申请日：2007-03-08
申请人： Jay A. Morrison , Douglas A. Keller , Malberto F. Gonzalez , Jay E. Lane
发明人： Jay A. Morrison , Douglas A. Keller , Malberto F. Gonzalez , Jay E. Lane
IPC分类号： F28F1/10
CPC分类号： F28F21/04 , B32B18/00 , C04B35/803 , C04B37/001 , C04B2237/34 , C04B2237/38 , C04B2237/62 , C04B2237/64 , F01D5/187 , F01D5/282 , F05D2260/201 , F28F7/02 , Y10T428/131 , Y10T428/1314 , Y10T428/1317 , Y10T428/1362 , Y10T428/139 , Y10T428/1393 , Y10T428/24521 , Y10T428/24612 , Y10T428/24744 , Y10T442/3195 , Y10T442/3203 , Y10T442/3211
摘要： A ceramic matrix composite wall structure (20A) constructed of interlocking layers (22A, 24A) of woven material with integral cooling channels (28A, 32A). The CMC layer closest to the hot gas path (41) contains internal cooling tubes (26A, 30A) protruding into a ceramic insulating layer (40A). This construction provides a cooled CMC lamellate wall structure with an interlocking truss core.
摘要翻译：一种由具有整体式冷却通道（28A，32A）的编织材料的互锁层（22A，24A）构成的陶瓷基体复合壁结构（20A）。最靠近热气体路径（41）的CMC层包含突出到陶瓷绝缘层（40A）中的内部冷却管（26A，30A）。这种结构提供了具有互锁桁架芯的冷却的CMC层状壁结构。

3. 发明授权

US07874059B2 Attachment for ceramic matrix composite component 有权
标题翻译：陶瓷基复合材料附件
公开(公告)号：US07874059B2
公开(公告)日：2011-01-25
申请号：US11330559
申请日：2006-01-12
申请人： Jay A. Morrison , Jay E. Lane
发明人： Jay A. Morrison , Jay E. Lane
IPC分类号： B23P11/00 , F01D5/14
CPC分类号： F16B5/0266 , Y10T29/49316 , Y10T29/49323 , Y10T29/49863 , Y10T29/49948 , Y10T29/49952 , Y10T29/49966 , Y10T29/53
摘要： A bushing (30, 31) in a hole (26) through a ceramic matrix composite structure (20) with a flange (34, 38) on each end of the bushing (30, 31) extending beyond and around the hole and pressing against opposed surfaces (22,24) of the CMC structure (20) with a preload that resists buckling of the composite structure fibers and resists internal CMC fiber separation. A connecting element (40), such as a bolt or pin, passes through the bushing (30, 31) for engagement with a supporting element (50). The bushing (31) may be formed in place as a single piece of ceramic, and cured along with the CMC structure (20), or it may be formed as two ceramic or metal parts (32, 36) that are joined together and preloaded by threads (33). The connecting element (40) may be a pin, or it may be a bolt with a shaft threaded into one part (32) of the bushing and a head (42) that pushes the second flange (38) toward the first flange (34).
摘要翻译：穿过陶瓷基体复合结构（20）的孔（26）中的衬套（30,31），其在衬套（30,31）的每个端部上具有凸缘（34,38），其延伸超过并围绕孔并压靠 CMC结构（20）的相对表面（22,24）具有防止复合结构纤维弯曲并抵抗内部CMC纤维分离的预载荷。诸如螺栓或销的连接元件（40）穿过衬套（30,31）以与支撑元件（50）接合。衬套（31）可以作为单块陶瓷形成就位，并与CMC结构（20）一起固化，或者可以形成为两个连接在一起并预加载的陶瓷或金属部件（32,36）通过螺纹（33）。连接元件（40）可以是销，或者其可以是具有螺纹连接到衬套的一个部分（32）中的轴的螺栓和将第二凸缘（38）朝着第一凸缘（34）推动的头部（42））。

4. 发明授权

US07745022B2 CMC with multiple matrix phases separated by diffusion barrier 有权
标题翻译：具有通过扩散阻挡层分离的多个矩阵相的CMC
公开(公告)号：US07745022B2
公开(公告)日：2010-06-29
申请号：US11489855
申请日：2006-07-20
申请人： Jay E. Lane , Jay A. Morrison , Steven C. Butner , Andrew Szweda
发明人： Jay E. Lane , Jay A. Morrison , Steven C. Butner , Andrew Szweda
IPC分类号： B32B9/00
CPC分类号： C04B35/185 , C04B35/803 , C04B38/0038 , C04B2111/00612 , C04B2235/3217 , C04B2235/3224 , C04B2235/3227 , C04B2235/3239 , C04B2235/3244 , C04B2235/326 , C04B2235/3287 , C04B2235/3463 , C04B2235/447 , C04B2235/522 , C04B2235/5228 , C04B2235/5256 , Y10T428/249957
摘要： A ceramic matrix composite (CMC) material (10) with increased interlaminar strength is obtained without a corresponding debit in other mechanical properties. This is achieved by infusing a diffusion barrier layer (20) into an existing porous matrix CMC to coat the exposed first matrix phase (19) and fibers (12), and then densifying the matrix with repeated infiltration cycles of a second matrix phase (22). The diffusion barrier prevents undesirable sintering between the matrix phases and between the second matrix phase and the fibers during subsequent final firing and use of the resulting component (30) in a high temperature environment.
摘要翻译：获得具有增加的层间强度的陶瓷基复合材料（CMC）材料（10），而在其它机械性能中没有相应的借方。这通过将扩散阻挡层（20）注入到现有的多孔基质CMC中以涂覆暴露的第一基质相（19）和纤维（12），然后用第二基质相（22）的重复渗透循环来致密化基质来实现）。扩散阻挡层在随后的最后焙烧和使用所得组分（30）在高温环境中，防止基质相之间和第二基质相与纤维之间的不期望的烧结。

5. 发明申请

US20100015394A1 CERAMIC MATRIX COMPOSITE WALL WITH POST LAMINATE STITCHING 有权
标题翻译：陶瓷矩阵复合墙与后层压缝合
公开(公告)号：US20100015394A1
公开(公告)日：2010-01-21
申请号：US12174243
申请日：2008-07-16
申请人： Jay A. Morrison , Jay E. Lane
发明人： Jay A. Morrison , Jay E. Lane
IPC分类号： B32B5/26 , B32B3/10
CPC分类号： C04B35/80 , B28B1/002 , B28B23/0006 , B32B18/00 , C04B35/6269 , C04B2235/5224 , C04B2235/616 , C04B2237/38 , C04B2237/62 , F01D5/282 , F05D2300/702 , Y10T428/24322
摘要： A stitching geometry and method for selective interlaminar reinforcement of a CMC wall (20A). The CMC wall is formed of ceramic fiber layers (22) individually infused with a ceramic matrix, stacked, and at least partially cured. A row of holes is formed in the wall, and a ceramic fiber thread (25) is infused with a wet ceramic matrix and passed through the holes to form stitches (28, 30, 31). The stitches are then cured, causing them to shrink more than any remaining wall shrinkage, thus tensioning the stitches and compressing the wall laminae together. The stitches may have through-wall portions (30, 31) that are angled differently in different wall areas as a function of interlaminar shear over interlaminar tension, optimizing wall reinforcement locally depending on magnitude and direction of shear. Alternate rows of stitches (54, 56) may have offsets in a stitch direction (34) and/or different through-wall angles (A1, A2).
摘要翻译：用于CMC壁（20A）的选择性层间增强的缝合几何和方法。 CMC壁由独立地注入陶瓷基体的陶瓷纤维层（22）形成，层叠并且至少部分固化。在壁中形成一排孔，陶瓷纤维线（25）注入湿陶瓷基体并通过孔形成线圈（28,30,31）。然后使线圈固化，导致它们比任何剩余的壁收缩更多地收缩，从而拉紧线圈并将壁板压在一起。线迹可以具有在不同壁面上不同角度的贯穿壁部分（30,31），作为层间张力之间的层间剪切的函数，根据剪切的大小和方向局部优化壁加固。线圈（54,56）的交替排可以在缝合方向（34）和/或不同的穿墙角（A1，A2）上具有偏移。

6. 发明申请

US20090183850A1 Method of Making a Combustion Turbine Component from Metallic Combustion Turbine Subcomponent Greenbodies 审中-公开
标题翻译：制造来自金属燃烧涡轮机组件燃烧涡轮机部件的方法
公开(公告)号：US20090183850A1
公开(公告)日：2009-07-23
申请号：US12238774
申请日：2008-09-26
申请人： Jay A. Morrison , Jay E. Lane , Allister W. James
发明人： Jay A. Morrison , Jay E. Lane , Allister W. James
IPC分类号： B22D17/00
CPC分类号： B22F7/062 , B22F3/1055 , B22F5/009 , B22F2005/005 , B22F2998/00 , B22F2998/10 , F05B2230/22 , Y02P10/295 , Y10T156/10 , B22F3/008 , B22F3/225 , B22F3/10
摘要： A method of making a combustion turbine component includes assembling a plurality of metallic combustion turbine subcomponent greenbodies together to form a metallic greenbody assembly and sintering the metallic greenbody assembly to thereby form the combustion turbine component. Each of the plurality of metallic combustion turbine subcomponent greenbodies may be formed by direct metal fabrication (DMF). In addition, each of plurality of metallic combustion turbine subcomponent greenbodies may include an activatable binder and the activatable binder may be activated prior to sintering.
摘要翻译：制造燃气轮机部件的方法包括将多个金属燃料涡轮机副部件生物体组装在一起以形成金属生坯体组件并烧结金属生坯体组件，从而形成燃气轮机部件。多个金属燃料涡轮机副部件生态体中的每一个可以通过直接金属制造（DMF）形成。此外，多个金属燃料涡轮机副部件生物体中的每一个可以包括可活化的粘合剂，并且可活化的粘合剂可以在烧结之前被活化。

7. 发明授权

US07413700B2 Methods of manufacturing insulated ceramic matrix composite 有权
标题翻译：绝缘陶瓷基复合材料的制造方法
公开(公告)号：US07413700B2
公开(公告)日：2008-08-19
申请号：US11649061
申请日：2007-01-03
申请人： Gary B. Merrill , Jay E. Lane , Steven C. Butner , Robert Kreutzer , Jay A. Morrison
发明人： Gary B. Merrill , Jay E. Lane , Steven C. Butner , Robert Kreutzer , Jay A. Morrison
IPC分类号： B28B11/04
CPC分类号： C04B38/085 , B28B11/041 , C04B28/00 , C04B28/18 , C04B28/34 , C04B35/117 , C04B35/18 , C04B35/803 , C04B41/009 , C04B41/5092 , C04B41/85 , C04B2235/3217 , C04B2235/3463 , C04B2235/5228 , C04B2235/528 , C04B2235/5436 , C04B2235/5445 , C04B2235/5472 , C04B2235/616 , Y10T428/249973 , C04B20/0036 , C04B20/004 , C04B14/303 , C04B14/306 , C04B14/324 , C04B14/328 , C04B20/0048 , C04B20/0076 , C04B38/0061 , C04B38/08
摘要： A composite material (10) formed of a ceramic matrix composite (CMC) material (12) protected by a ceramic insulating material (14). The constituent parts of the insulating material are selected to avoid degradation of the CMC material when the two layers are co-processed. The CMC material is processed to a predetermined state of shrinkage before wet insulating material is applied against the CMC material. The two materials are then co-fired together, with the relative amount of shrinkage between the two materials during the firing step being affected by the amount of pre-shrinkage of the CMC material during the bisque firing step. The shrinkage of the two materials during the co-firing step may be matched to minimize shrinkage stresses, or a predetermined amount of prestress between the materials may be achieved. An aluminum hydroxyl chloride binder material (24) may be used in the insulating material in order to avoid degradation of the fabric (28) of the CMC material during the co-firing step.
摘要翻译：由陶瓷绝缘材料（14）保护的陶瓷基复合材料（CMC）材料（12）形成的复合材料（10）。选择绝缘材料的组成部分以避免当两层被共同处理时CMC材料的劣化。在向CMC材料施加湿绝缘材料之前，将CMC材料加工成预定的收缩状态。然后将两种材料共烧，在焙烧步骤期间两种材料之间的相对收缩量受到在坯料烧结步骤期间CMC材料的预收缩量的影响。可以在共烧步骤期间两种材料的收缩率相匹配，以最小化收缩应力，或者可以实现材料之间的预定量的预应力。可以在绝缘材料中使用铝羟基氯化物粘合剂材料（24），以避免在共烧烧步骤期间CMC材料的织物（28）的降解。

8. 发明申请

US20080116614A1 Method of Forming Cmc Component 失效
标题翻译：形成Cmc组分的方法
公开(公告)号：US20080116614A1
公开(公告)日：2008-05-22
申请号：US10549024
申请日：2005-07-25
申请人： Jay A. Morrison , Jay E. Lane
发明人： Jay A. Morrison , Jay E. Lane
IPC分类号： C04B35/645
CPC分类号： C04B35/803 , C04B35/117 , C04B35/645 , C04B38/00 , C04B2235/5228 , C04B2235/5252 , C04B2235/77 , C04B2235/96 , C04B38/0074 , C04B40/0259
摘要： A method of forming a ceramic matrix composite (CMC) article (30) or a composite article (60) that minimizes the risk of delaminations while simultaneously maintaining a desired degree of porosity in the material. A pressure P applied against a surface of the article during a sintering process is controlled to be high enough to resist a separation force between the plies (66) of the CMC material (62) caused by anisotropic shrinkage of the material and/or to resist a separation force caused by differential shrinkage between the CMC material and an adjoined monolithic ceramic material (64). The pressure is also controlled to be low enough to avoid undue consolidation of the materials and to provide a desired degree of porosity in the sintered article. The pressure may be applied by delta-alpha tooling, and it may be varied verses the time of the sintering heating and/or across the article surface.
摘要翻译：一种形成陶瓷基质复合材料（CMC）制品（30）或复合制品（60）的方法，其最小化分层的风险，同时保持材料中期望的孔隙度。在烧结过程中施加到制品表面的压力P被控制到足够高以抵抗由材料的各向异性收缩和/或抵抗引起的CMC材料（62）的层（66）之间的分离力由CMC材料和邻接的整体陶瓷材料（64）之间的不均匀收缩引起的分离力。压力也被控制到足够低以避免材料的不适当的固结并且在烧结制品中提供期望的孔隙度。压力可以通过Δ-α加工来施加，并且可以随烧结加热时间和/或穿过制品表面而变化。

9. 发明授权

US06514046B1 Ceramic composite vane with metallic substructure 有权
标题翻译：陶瓷复合叶片与金属子结构
公开(公告)号：US06514046B1
公开(公告)日：2003-02-04
申请号：US09677044
申请日：2000-09-29
申请人： Jay A. Morrison , Gary B. Merrill , Jay E. Lane , Christian X. Campbell , Daniel G. Thompson , Eric V. Carelli , Christine Taut
发明人： Jay A. Morrison , Gary B. Merrill , Jay E. Lane , Christian X. Campbell , Daniel G. Thompson , Eric V. Carelli , Christine Taut
IPC分类号： F01D518
CPC分类号： F01D5/187 , F01D5/282 , F01D5/284 , F01D9/02 , F05D2260/201 , F05D2300/603 , F05D2300/611 , F05D2300/612
摘要： A vane assembly for a turbine assembly includes an inner endcap, an outer endcap, and a body. The body includes a metallic core assembly, a ceramic shell assembly and a support assembly. The metallic core assembly is coupled to the inner and outer endcaps and bears most of the mechanical loads, including aerodynamic loads. The ceramic shell bears substantially all of the thermal stress placed on the vane assembly. The support assembly is disposed between the metallic core assembly and said ceramic shell assembly and is coupled to the metallic core assembly.
摘要翻译：用于涡轮组件的叶片组件包括内端盖，外端盖和主体。主体包括金属芯组件，陶瓷壳组件和支撑组件。金属芯组件联接到内外端盖和承载大部分机械负载，包括空气动力学负载。陶瓷壳承受放置在叶片组件上的基本上所有的热应力。支撑组件设置在金属芯组件和所述陶瓷壳组件之间并且联接到金属芯组件。

10. 发明申请

US20110151239A1 HIGH TEMPERATURE INSULATION AND INSULATED ARTICLE 有权
标题翻译：高温绝缘和绝缘文章
公开(公告)号：US20110151239A1
公开(公告)日：2011-06-23
申请号：US11516324
申请日：2006-09-06
申请人： Jay E. Lane , Christian X. Campbell
发明人： Jay E. Lane , Christian X. Campbell
IPC分类号： B32B3/26
CPC分类号： C04B35/185 , C04B35/62655 , C04B35/6303 , C04B35/6306 , C04B35/632 , C04B35/634 , C04B41/009 , C04B41/52 , C04B41/89 , C04B2111/2084 , C04B2235/3217 , C04B2235/3244 , C04B2235/5436 , C04B2235/80 , C04B2235/96 , F05C2253/12 , Y10T428/24997 , C04B20/004 , C04B41/5037 , C04B41/5092 , C04B41/5031 , C04B41/508 , C04B41/522 , C04B41/5042 , C04B41/5044 , C04B41/53 , C04B35/01 , C04B35/18 , C04B35/481
摘要： An insulation (10, 100) and an insulated article (40, 56, 62, 82) having improved properties for use in a high temperature combustion environment. The improved insulation may include composite particles (18) of alumina and zirconia-hafnia exhibiting micro-cracks that remain contained within the particles and do not extend into a surrounding binder material. The improved insulation may be a vapor resistance layer (VRL) top coat (80) disposed over a layer of mullite-based ceramic thermal insulation (72) and may be anchored to the thermal insulation by extending into pits (79) formed in the surface (S′) of the mullite-based insulation. Porosity and thickness of the top coat may be controlled to provide compatibility between the elastic modulus of the zirconia hafnia top coat and that of the underlying mullite-based insulation.
摘要翻译：具有改进的用于高温燃烧环境的性能的绝缘体（10,100）和绝缘制品（40,56,62,82）。改进的绝缘体可以包括氧化铝和氧化锆 - 铪的复合颗粒（18），其表现出微小的裂缝，其仍然包含在颗粒内并且不延伸到周围的粘合剂材料中。改进的绝缘体可以是设置在莫来石基陶瓷绝热层（72）上的蒸汽电阻层（VRL）顶涂层（80），并且可以通过延伸到形成在表面中的凹坑（79）而被锚固到热绝缘体（S'）的莫来石基绝缘。可以控制顶涂层的孔隙率和厚度，以提供氧化锆瓦墩顶涂层的弹性模量与下面的莫来石基绝缘材料的弹性模量之间的相容性。

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