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131 条记录 (耗时 0.021 秒)

    Stacked laminate bolted ring segment
    2.
    发明授权
    Stacked laminate bolted ring segment 有权
    堆叠层压螺栓环段

    公开(公告)号：US07753643B2

    公开(公告)日：2010-07-13

    申请号：US11526256

    申请日：2006-09-22

    申请人： Malberto F. Gonzalez ,  David C. Radonovich ,  Anthony L. Schiavo ,  Jay A. Morrison ,  Steven J. Vance

    发明人： Malberto F. Gonzalez ,  David C. Radonovich ,  Anthony L. Schiavo ,  Jay A. Morrison ,  Steven J. Vance

    IPC分类号： F01D11/08

    CPC分类号： F01D9/04 ,  F01D11/08 ,  F01D25/246 ,  F05D2300/21 ,  Y10T29/49236

    摘要： A ceramic ring segment for a turbine engine that may be used as a replacement for one or more metal components. The ceramic ring segment may be formed from a plurality of ceramic plates, such as ceramic matrix composite plates, that are joined together using a strengthening mechanism to reinforce the ceramic plates while permitting the resulting ceramic article to be used as a replacement for components for turbine systems that are typically metal, thereby taking advantage of the properties provided by ceramic materials. The strengthening mechanism may include a bolt or a plurality of bolts designed to prevent delamination of the ceramic plates when in use by keeping the ceramic plates in compression.

    摘要翻译： 用于涡轮发动机的陶瓷环段，其可用作一种或多种金属组分的替代物。 陶瓷环段可以由多个陶瓷板形成，例如陶瓷基复合板，其使用强化机构连接在一起以加强陶瓷板，同时允许所得的陶瓷制品用作涡轮机部件的替代品 通常是金属的系统，从而利用由陶瓷材料提供的性质。 加强机构可以包括螺栓或多个螺栓，其被设计成在使用时防止陶瓷板在通过保持陶瓷板压缩时分层。

    Stacked laminate fiber wrapped segment
    3.
    发明申请
    Stacked laminate fiber wrapped segment 有权
    堆叠层压纤维包裹片段

    公开(公告)号：US20080107521A1

    公开(公告)日：2008-05-08

    申请号：US11591907

    申请日：2006-11-02

    申请人： Jay A. Morrison ,  David C. Radonovich ,  Anthony L. Schiavo ,  Gary B. Merrill ,  Malberto F. Gonzalez

    发明人： Jay A. Morrison ,  David C. Radonovich ,  Anthony L. Schiavo ,  Gary B. Merrill ,  Malberto F. Gonzalez

    IPC分类号： F01D11/08 ,  F04D29/08 ,  B32B18/00

    CPC分类号： F01D11/08 ,  F01D9/04 ,  F05D2240/11 ,  F05D2300/603 ,  Y10T29/49888

    摘要： A ceramic ring segment for a turbine engine that may be used as a replacement for one or more metal components. The ceramic ring segment may be formed from a plurality of ceramic plates, such as ceramic matrix composite plates, that are joined together using a strengthening mechanism to reinforce the ceramic plates while permitting the resulting ceramic article to be used as a replacement for components for turbine systems that are typically metal, thereby taking advantage of the properties provided by ceramic materials. The strengthening mechanism may include a ceramic matrix composite overwrap or plurality of overwraps designed to help prevent delamination of the ceramic plates when the ceramic article is in use by placing the plates in compression.

    摘要翻译： 用于涡轮发动机的陶瓷环段，其可用作一种或多种金属组分的替代物。 陶瓷环段可以由多个陶瓷板形成，例如陶瓷基复合板，其使用强化机构连接在一起以加强陶瓷板，同时允许所得的陶瓷制品用作涡轮机部件的替代品 通常是金属的系统，从而利用由陶瓷材料提供的性质。 加强机构可以包括陶瓷基复合材料外包装或多个外包装，其被设计成当陶瓷制品在使用时通过将板放置在压缩中来帮助防止陶瓷板的分层。

    Stacked laminate fiber wrapped segment
    4.
    发明授权
    Stacked laminate fiber wrapped segment 有权
    堆叠层压纤维包裹片段

    公开(公告)号：US07686577B2

    公开(公告)日：2010-03-30

    申请号：US11591907

    申请日：2006-11-02

    申请人： Jay A. Morrison ,  David C. Radonovich ,  Anthony L. Schiavo ,  Gary B. Merrill ,  Malberto F. Gonzalez

    发明人： Jay A. Morrison ,  David C. Radonovich ,  Anthony L. Schiavo ,  Gary B. Merrill ,  Malberto F. Gonzalez

    IPC分类号： F01D25/26

    CPC分类号： F01D11/08 ,  F01D9/04 ,  F05D2240/11 ,  F05D2300/603 ,  Y10T29/49888

    摘要： A ceramic ring segment for a turbine engine that may be used as a replacement for one or more metal components. The ceramic ring segment may be formed from a plurality of ceramic plates, such as ceramic matrix composite plates, that are joined together using a strengthening mechanism to reinforce the ceramic plates while permitting the resulting ceramic article to be used as a replacement for components for turbine systems that are typically metal, thereby taking advantage of the properties provided by ceramic materials. The strengthening mechanism may include a ceramic matrix composite overwrap or plurality of overwraps designed to help prevent delamination of the ceramic plates when the ceramic article is in use by placing the plates in compression.

    摘要翻译： 用于涡轮发动机的陶瓷环段，其可用作一种或多种金属组分的替代物。 陶瓷环段可以由多个陶瓷板形成，例如陶瓷基复合板，其使用强化机构连接在一起以加强陶瓷板，同时允许所得的陶瓷制品用作涡轮机部件的替代品 通常是金属的系统，从而利用由陶瓷材料提供的性质。 加强机构可以包括陶瓷基复合材料外包装或多个外包装，其被设计成当陶瓷制品在使用时通过将板放置在压缩中来帮助防止陶瓷板的分层。

    Ceramic matrix composite turbine engine component
    5.
    发明申请
    Ceramic matrix composite turbine engine component 审中-公开
    陶瓷基复合涡轮发动机部件

    公开(公告)号：US20090324393A1

    公开(公告)日：2009-12-31

    申请号：US11698225

    申请日：2007-01-25

    申请人： Malberto F. Gonzalez ,  Jay A. Morrison

    发明人： Malberto F. Gonzalez ,  Jay A. Morrison

    IPC分类号： F02C7/28 ,  B23P11/00

    CPC分类号： F01D11/08 ,  F05D2230/20 ,  F05D2230/60 ,  F05D2240/11 ,  F23R3/007 ,  F23R2900/00017 ,  Y10T29/4932

    摘要： Aspects of the invention are directed to a gas turbine component such as a ring seal segment or combustor heat shield having a base and a plurality of walls defining a volume. The base and the walls are independently formed and are formed from ceramic matrix composite plates. The base and walls can have interconnection structures that allow for assembly. The base and walls can be coated or otherwise wrapped for connection. Locking mechanisms, such as self locking lugs, can be used for assembly.

    摘要翻译： 本发明的方面涉及一种燃气轮机部件，例如具有限定容积的底座和多个壁的环形密封段或燃烧器热屏蔽件。 基体和壁独立地形成，并由陶瓷基复合板形成。 基座和墙壁可以具有允许组装的互连结构。 底座和墙壁可以涂覆或以其他方式包裹以进行连接。 锁定机构，如自锁凸耳，可用于组装。

    Hybrid ceramic structure with internal cooling arrangements
    6.
    发明授权
    Hybrid ceramic structure with internal cooling arrangements 有权
    具有内部冷却装置的混合陶瓷结构

    公开(公告)号：US08202588B2

    公开(公告)日：2012-06-19

    申请号：US12099434

    申请日：2008-04-08

    申请人： Dougas A. Keller ,  Malberto F. Gonzalez ,  Jay A. Morrison

    发明人： Dougas A. Keller ,  Malberto F. Gonzalez ,  Jay A. Morrison

    IPC分类号： B32B1/08 ,  F16L9/10 ,  F16L9/14 ,  F16L9/18

    CPC分类号： B32B18/00 ,  C04B2235/5224 ,  C04B2237/341 ,  C04B2237/343 ,  C04B2237/38 ,  C04B2237/62 ,  C04B2237/76 ,  F01D5/282 ,  F01D25/12 ,  F05D2300/5024 ,  F05D2300/6033 ,  Y10T428/131 ,  Y10T428/1314 ,  Y10T428/1317 ,  Y10T428/249973

    摘要： A structure for use in high temperature applications is provided. The structure may include an inner ceramic matrix composite (CMC) material (12). At least a portion of this CMC material includes waves that define a first wavy surface (140 and an opposed second wavy surface (16). A ceramic insulation material (18) may be bonded with the first wavy surface and includes a distal surface (20) for exposure to a high temperature environment. A core material (22) is bonded with at least a portion of the second wavy surface. One or more cooling channels (24) are disposed in the core material. An outer CMC material (26) may be joined to a portion of the inner CMC material. The core material is a material different than a matrix material of the inner CMC material.

    摘要翻译： 提供了一种用于高温应用的结构。 该结构可以包括内部陶瓷基质复合材料（CMC）材料（12）。 该CMC材料的至少一部分包括限定第一波形表面（140和相对的第二波浪表面）的波浪，陶瓷绝缘材料（18）可以与第一波浪表面结合并且包括远端表面（20 ），用于暴露在高温环境中的芯材（22）与第二波状表面的至少一部分结合，一个或多个冷却通道（24）设置在芯材中，外部CMC材料（26） 可以连接到内部CMC材料的一部分。芯材料是与内部CMC材料的基质材料不同的材料。

    STACKED LAMINATE BOLTED RING SEGMENT
    8.
    发明申请
    STACKED LAMINATE BOLTED RING SEGMENT 有权
    堆叠层压板环

    公开(公告)号：US20100150703A1

    公开(公告)日：2010-06-17

    申请号：US11526256

    申请日：2006-09-22

    申请人： Malberto F. Gonzalez ,  David C. Radonovich ,  Anthony L. Schiavo ,  Jay A. Morrison ,  Steven J. Vance

    发明人： Malberto F. Gonzalez ,  David C. Radonovich ,  Anthony L. Schiavo ,  Jay A. Morrison ,  Steven J. Vance

    IPC分类号： F01D11/08 ,  F04D29/02 ,  F04D29/40 ,  B23P17/00

    CPC分类号： F01D9/04 ,  F01D11/08 ,  F01D25/246 ,  F05D2300/21 ,  Y10T29/49236

    摘要： A ceramic ring segment for a turbine engine that may be used as a replacement for one or more metal components. The ceramic ring segment may be formed from a plurality of ceramic plates, such as ceramic matrix composite plates, that are joined together using a strengthening mechanism to reinforce the ceramic plates while permitting the resulting ceramic article to be used as a replacement for components for turbine systems that are typically metal, thereby taking advantage of the properties provided by ceramic materials. The strengthening mechanism may include a bolt or a plurality of bolts designed to prevent delamination of the ceramic plates when in use by keeping the ceramic plates in compression.

    摘要翻译： 用于涡轮发动机的陶瓷环段，其可用作一种或多种金属组分的替代物。 陶瓷环段可以由多个陶瓷板形成，例如陶瓷基复合板，其使用强化机构连接在一起以加强陶瓷板，同时允许所得的陶瓷制品用作涡轮机部件的替代品 通常是金属的系统，从而利用由陶瓷材料提供的性质。 加强机构可以包括螺栓或多个螺栓，其被设计成在使用时防止陶瓷板在通过保持陶瓷板压缩时分层。

    HYBRID CERAMIC STRUCTURE WITH INTERNAL COOLING ARRANGEMENTS
    9.
    发明申请
    HYBRID CERAMIC STRUCTURE WITH INTERNAL COOLING ARRANGEMENTS 有权
    具有内部冷却安排的混合陶瓷结构

    公开(公告)号：US20090252907A1

    公开(公告)日：2009-10-08

    申请号：US12099434

    申请日：2008-04-08

    申请人： Douglas A. Keller ,  Malberto F. Gonzalez ,  Jay A. Morrison

    发明人： Douglas A. Keller ,  Malberto F. Gonzalez ,  Jay A. Morrison

    IPC分类号： B32B1/08

    CPC分类号： B32B18/00 ,  C04B2235/5224 ,  C04B2237/341 ,  C04B2237/343 ,  C04B2237/38 ,  C04B2237/62 ,  C04B2237/76 ,  F01D5/282 ,  F01D25/12 ,  F05D2300/5024 ,  F05D2300/6033 ,  Y10T428/131 ,  Y10T428/1314 ,  Y10T428/1317 ,  Y10T428/249973

    摘要： A structure for use in high temperature applications is provided. The structure may include an inner ceramic matrix composite (CMC) material (12). At least a portion of this CMC material includes waves that define a first wavy surface (140 and an opposed second wavy surface (16). A ceramic insulation material (18) may be bonded with the first wavy surface and includes a distal surface (20) for exposure to a high temperature environment. A core material (22) is bonded with at least a portion of the second wavy surface. One or more cooling channels (24) are disposed in the core material. An outer CMC material (26) may be joined to a portion of the inner CMC material. The core material is a material different than a matrix material of the inner CMC material.

    摘要翻译： 提供了一种用于高温应用的结构。 该结构可以包括内部陶瓷基质复合材料（CMC）材料（12）。 该CMC材料的至少一部分包括限定第一波形表面（140和相对的第二波浪表面）的波浪，陶瓷绝缘材料（18）可以与第一波浪表面结合并且包括远端表面（20 ），用于暴露在高温环境中的芯材（22）与第二波状表面的至少一部分结合，一个或多个冷却通道（24）设置在芯材中，外部CMC材料（26） 可以连接到内部CMC材料的一部分。芯材料是与内部CMC材料的基质材料不同的材料。

    GAS TURBINE ENGINE DUCTING ARRANGEMENT HAVING DISCRETE INSERT
    10.
    发明申请
    GAS TURBINE ENGINE DUCTING ARRANGEMENT HAVING DISCRETE INSERT 审中-公开
    具有分离插件的气体涡轮发动机排气装置

    公开(公告)号：US20150132117A1

    公开(公告)日：2015-05-14

    申请号：US14074776

    申请日：2013-11-08

    申请人： John J. Marra ,  Jay A. Morrison ,  Ernie B. Campbell

    发明人： John J. Marra ,  Jay A. Morrison ,  Ernie B. Campbell

    IPC分类号： F01D9/02 ,  F23R3/46

    CPC分类号： F01D9/023 ,  F05D2260/941 ,  F05D2270/114 ,  F23R3/425 ,  F23R3/46

    摘要： A ducting arrangement (10), including: a plurality of discrete ducts (18), each defining a flow path and configured to receive a flow of combustion gases from a respective combustor can, where the plurality of discrete ducts merge to form a common duct structure; and a throat insert (50) configured to define at least part of a junction of one of the discrete ducts and the common duct structure.

    摘要翻译： 一种管道装置（10），包括：多个分立的管道（18），每个分配的管道（18）各限定一个流动路径并且被构造成从相应的燃烧器罐接收燃烧气体流，其中所述多个离散管道合流以形成公共管道 结构体; 以及喉部插入件（50），其构造成限定所述离散管道和所述公共管道结构中的一个的至少部分接合部。