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1. 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。

2. 发明授权

US07001679B2 Protective overlayer for ceramics 有权
标题翻译：陶瓷保护层
公开(公告)号：US07001679B2
公开(公告)日：2006-02-21
申请号：US10214785
申请日：2002-08-08
申请人： Christian X. Campbell , Jay E. Lane
发明人： Christian X. Campbell , Jay E. Lane
IPC分类号： B32B9/00 , C04B35/51
CPC分类号： C04B41/009 , C04B41/5048 , C04B41/52 , C04B41/87 , C04B41/89 , F01D5/288 , Y10T428/249967 , Y10T428/24997 , C04B41/4582 , C04B41/5037 , C04B41/5042 , C04B41/522 , C04B41/5024 , C04B35/10 , C04B35/185 , C04B35/44 , C04B35/565 , C04B35/48 , C04B35/584 , C04B35/80 , C04B35/505
摘要： A xenotime phosphate protective overlayer (22) for protecting a ceramic material (24) from a high temperature, moisture-containing environment. Yttrium phosphate may be used as a protective overlayer to protect an underlying mullite layer to temperatures in excess of 1,500° C. The coating may have porosity of greater than 15% for improved thermal shock protection. To prevent the ingress of oxygen to an underlying ceramic non-oxide material, such as silicon carbide or silicon nitride, an oxygen barrier layer (34) is disposed between the xenotime phosphate coating and the non-oxide material. Such a protective overlayer may be used for an article having a ceramic matrix composite substrate.
摘要翻译：一种用于保护陶瓷材料（24）免受高温，含湿气体环境的磷酸脱氧磷酸盐保护覆层（22）。磷酸钇可以用作保护层，以保护下面的莫来石层达到超过1500℃的温度。涂层可具有大于15％的孔隙率，以改善热冲击保护。为了防止氧气进入诸如碳化硅或氮化硅的下面的陶瓷非氧化物材料，氧化阻挡层（34）被设置在磷酸铋磷酸盐涂层和非氧化物材料之间。这种保护性覆盖层可以用于具有陶瓷基复合基板的制品。

3. 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。

4. 发明授权

US07985493B2 High temperature insulation and insulated article 有权
标题翻译：高温绝缘和绝缘制品
公开(公告)号：US07985493B2
公开(公告)日：2011-07-26
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： B32B9/00
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 - 铪顶面涂层的弹性模量与下面的富铝红柱石基绝缘体的弹性模量之间的相容性。

5. 发明授权

US06528190B1 Fiber coating compounds for reinforced ceramic matrix composites 有权
标题翻译：用于增强陶瓷基复合材料的纤维涂层化合物
公开(公告)号：US06528190B1
公开(公告)日：2003-03-04
申请号：US09631097
申请日：2000-08-02
申请人： Christian X. Campbell , Jay E. Lane
发明人： Christian X. Campbell , Jay E. Lane
IPC分类号： B32B900
CPC分类号： C04B35/62847 , C04B35/117 , C04B35/185 , C04B35/44 , C04B35/803 , C04B2235/3225 , C04B2235/5224 , C04B2235/5264 , C04B2235/764 , C04B2235/77 , F23R3/007 , Y10T428/249928 , Y10T428/24993 , Y10T428/26
摘要： A composite (20) has a matrix (10), preferably of ceramic, interspersed with reinforcement structures (12), preferably ceramic fibers, coated with a material (14) selected from ZrGeO4, HfGeO4 and CeGeO4, where the composite can be used as a component in high temperature turbines.
摘要翻译：复合材料（20）具有优选陶瓷的基体（10），散布有加强结构（12），优选陶瓷纤维，涂覆有选自ZrGeO4，HfGeO4和CeGeO4的材料（14），其中复合材料可以用作高温涡轮机组件。

6. 发明申请

US20100263194A1 ATTACHMENT FOR CERAMIC MATRIX COMPOSITE COMPONENT 有权
标题翻译：陶瓷基质复合材料的附件
公开(公告)号：US20100263194A1
公开(公告)日：2010-10-21
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： B23P19/04
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））。

7. 发明授权

US07641440B2 Cooling arrangement for CMC components with thermally conductive layer 失效
标题翻译：具有导热层的CMC部件的冷却布置
公开(公告)号：US07641440B2
公开(公告)日：2010-01-05
申请号：US11514745
申请日：2006-08-31
申请人： Jay A. Morrison , Jay E. Lane
发明人： Jay A. Morrison , Jay E. Lane
IPC分类号： F01D5/18
CPC分类号： F01D5/187 , F01D5/288 , F01D25/12 , F05C2201/0466 , F05D2260/201 , F05D2300/122 , F05D2300/141 , F05D2300/172 , F05D2300/222 , F05D2300/224 , F05D2300/2262 , F05D2300/5024 , F05D2300/603 , F23R3/007 , F23R2900/03044
摘要： A CMC wall (22) with a front surface (21) heated (24) by a working fluid in a gas turbine. A back CMC surface (23) is coated with a layer (42) of a thermally conductive material to accelerate heat transfer in the plane of the CMC wall (22), reducing thermal gradients (32-40) on the back CMC surface (23) caused by cold spots (32) resulting from impingement cooling flows (26). The conductive material (42) may have a coefficient of thermal conductivity at least 10 times greater than that of the CMC material (22), to provide a minimal thickness conductive layer (42). This reduces thermal gradient stresses within the CMC material (22), and minimizes differential thermal expansion stresses between the CMC material (22) and the thin conductive layer (42).
摘要翻译：具有通过燃气轮机中的工作流体加热（24）的前表面（21）的CMC壁（22）。背部CMC表面（23）涂覆有导热材料层（42），以加速在CMC壁（22）的平面中的热传递，从而降低背面CMC表面（23）上的热梯度（32-40））由冲击冷却流产生的冷点（32）引起（26）。导电材料（42）的导热系数可以比CMC材料（22）的导热系数高至少10倍，以提供最小厚度的导电层（42）。这降低了CMC材料（22）内的热梯度应力，并且使CMC材料（22）和薄导电层（42）之间的差热膨胀应力最小化。

8. 发明授权

US07179524B2 Insulated ceramic matrix composite and method of manufacturing 有权
标题翻译：绝缘陶瓷基复合材料及其制造方法
公开(公告)号：US07179524B2
公开(公告)日：2007-02-20
申请号：US10667264
申请日：2003-09-19
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： B32B3/00
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。

9. 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。

10. 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。

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