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1. 发明授权

US07799405B1 Three dimensional reinforced CMC articles by interlocking two dimensional structures 有权
标题翻译：三维增强CMC制品通过联锁二维结构
公开(公告)号：US07799405B1
公开(公告)日：2010-09-21
申请号：US11607345
申请日：2006-12-01
申请人： Steve James Vance , Gary B. Merrill , Alfred Paul Matheny , Jay A. Morrison
发明人： Steve James Vance , Gary B. Merrill , Alfred Paul Matheny , Jay A. Morrison
IPC分类号： B32B3/24 , C03B29/00
CPC分类号： B32B38/00 , B32B18/00 , B32B38/0012 , B32B38/10 , B32B2038/045 , B32B2315/02 , C04B2237/38 , C04B2237/62 , C04B2237/64 , Y10T428/24008 , Y10T428/24017 , Y10T428/24182 , Y10T428/24198 , Y10T428/24281 , Y10T428/24289 , Y10T428/24339
摘要： The interlocking of two or more sections via the insertion of one or more out-of-plane features in one section or combination of sections through a void in one or more a complementary sections can result in a reinforced ceramic matrix composite article upon securing of the sections. The sections can be secured by friction between two tightly matched sections or by the use of a pin, hook, or clamp. The sections can be constructed from one or more CMC laminate sheets. The out-of-plane feature can be a loop or a flange and the void can be an orifice or a matched loop in the complementary sheet. The securing of the sections can result in a CMC article where the delamination between sheets is inhibited.
摘要翻译：通过在一个部分中插入一个或多个平面外部特征或通过一个或多个互补部分中的空隙的部分组合来连接两个或多个部分可以导致加固的陶瓷基体复合制品，部分。这些部分可以通过两个紧密匹配的部分之间的摩擦或通过使用销，钩或夹具来固定。这些部分可以由一个或多个CMC层压板构成。平面外的特征可以是环或法兰，空隙可以是互补片中的孔或匹配环。这些部分的固定可导致CMC制品，其中片材之间的分层被抑制。

2. 发明申请

US20100221485A1 THREE DIMENSIONAL REINFORCED CMC ARTICLES BY INTERLOCKING TWO DIMENSIONAL STRUCTURES 有权
标题翻译：通过互连两维结构三维增强CMC文章
公开(公告)号：US20100221485A1
公开(公告)日：2010-09-02
申请号：US11607345
申请日：2006-12-01
申请人： Steve James Vance , Gary B. Merrill , Alfred Paul Matheny , Jay A. Morrison
发明人： Steve James Vance , Gary B. Merrill , Alfred Paul Matheny , Jay A. Morrison
IPC分类号： B32B7/04 , B32B3/24 , B32B7/08 , B32B18/00 , B32B37/14
CPC分类号： B32B38/00 , B32B18/00 , B32B38/0012 , B32B38/10 , B32B2038/045 , B32B2315/02 , C04B2237/38 , C04B2237/62 , C04B2237/64 , Y10T428/24008 , Y10T428/24017 , Y10T428/24182 , Y10T428/24198 , Y10T428/24281 , Y10T428/24289 , Y10T428/24339
摘要： The interlocking of two or more sections via the insertion of one or more out-of-plane features in one section or combination of sections through a void in one or more a complementary sections can result in a reinforced ceramic matrix composite article upon securing of the sections. The sections can be secured by friction between two tightly matched sections or by the use of a pin, hook, or clamp. The sections can be constructed from one or more CMC laminate sheets. The out-of-plane feature can be a loop or a flange and the void can be an orifice or a matched loop in the complementary sheet. The securing of the sections can result in a CMC article where the delamination between sheets is inhibited.
摘要翻译：通过在一个部分中插入一个或多个平面外部特征或通过一个或多个互补部分中的空隙的部分组合来连接两个或多个部分可以导致加固的陶瓷基体复合制品，部分。这些部分可以通过两个紧密匹配的部分之间的摩擦或通过使用销，钩或夹具来固定。这些部分可以由一个或多个CMC层压板构成。平面外的特征可以是环或法兰，空隙可以是互补片中的孔或匹配环。这些部分的固定可导致CMC制品，其中片材之间的分层被抑制。

3. 发明授权

US07871716B2 Damage tolerant gas turbine component 有权
标题翻译：耐损燃气轮机组件
公开(公告)号：US07871716B2
公开(公告)日：2011-01-18
申请号：US11642119
申请日：2006-12-20
申请人： Steve James Vance
发明人： Steve James Vance
IPC分类号： B32B18/00
CPC分类号： F23R3/007 , F23R2900/00019 , Y10T428/16
摘要： A damage tolerant component (90) for use in a high temperature combustion gas environment. The component includes a plurality of ceramic tiles (94) bonded to a substrate (92) for isolating any impact damage to the damaged tile(s). A grout (98) may fill gaps between adjacent tiles to blunt any crack tip extending from a damaged tile. Ceramic tile insulation may be applied in two layers (56, 58) with the material properties of the two layers being different, such as with a bottom layer selected for its thermal insulating properties and a top layer selected for its impact resistance properties. A layer of sealing material (100) may be applied over at least a portion of the ceramic tiles.
摘要翻译：用于高温燃烧气体环境的耐损伤部件（90）。该组件包括多个结合到基板（92）的瓷砖（94），用于隔离对损坏的瓦片的任何冲击损伤。灌浆（98）可以填充相邻瓦片之间的间隙以钝化从损坏的瓦片延伸的任何裂纹尖端。陶瓷砖绝缘体可以施加在两层（56,58）中，其中两层的材料性质是不同的，例如由于其绝热性质而选择的底层和由于其耐冲击性而选择的顶层。可以在陶瓷砖的至少一部分上施加一层密封材料（100）。

4. 发明申请

US20100260960A1 DAMAGE TOLERANT GAS TURBINE COMPONENT 有权
标题翻译：耐损燃气涡轮机组件
公开(公告)号：US20100260960A1
公开(公告)日：2010-10-14
申请号：US11642119
申请日：2006-12-20
申请人： Steve James Vance
发明人： Steve James Vance
IPC分类号： B32B3/22
CPC分类号： F23R3/007 , F23R2900/00019 , Y10T428/16
摘要： A damage tolerant component (90) for use in a high temperature combustion gas environment. The component includes a plurality of ceramic tiles (94) bonded to a substrate (92) for isolating any impact damage to the damaged tile(s). A grout (98) may fill gaps between adjacent tiles to blunt any crack tip extending from a damaged tile. Ceramic tile insulation may be applied in two layers (56, 58) with the material properties of the two layers being different, such as with a bottom layer selected for its thermal insulating properties and a top layer selected for its impact resistance properties. A layer of sealing material (100) may be applied over at least a portion of the ceramic tiles.
摘要翻译：用于高温燃烧气体环境的耐损伤部件（90）。该组件包括多个结合到基板（92）的瓷砖（94），用于隔离对损坏的瓦片的任何冲击损伤。灌浆（98）可以填充相邻瓦片之间的间隙以钝化从损坏的瓦片延伸的任何裂纹尖端。陶瓷砖绝缘体可以施加在两层（56,58）中，其中两层的材料性质是不同的，例如由于其绝热性质而选择的底层和由于其耐冲击性而选择的顶层。可以在陶瓷砖的至少一部分上施加一层密封材料（100）。

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