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公开(公告)号：US07762076B2
公开(公告)日：2010-07-27
申请号：US11254876
申请日：2005-10-20
申请人： Jun Shi , Jason Lawrence , David J. Bombara , David C. Jarmon , Michael T. Weber , Richard S. Tuthill , Jeffrey D. Melman
发明人： Jun Shi , Jason Lawrence , David J. Bombara , David C. Jarmon , Michael T. Weber , Richard S. Tuthill , Jeffrey D. Melman
CPC分类号： F23R3/007 , F16L25/0072 , F16L49/02 , F16L49/06 , F23R3/002 , F23R3/60 , F23R2900/00017
摘要： A combustor assembly includes a metal section having an axial slot that receives a ceramic section. A clamp is received about the axial slot to secure the metal section and ceramic section together. Tabs on the metal section, a gasket between the metal section and the ceramic section, and springs within the clamp deform an amount that is greater than a thermal expansion difference between the metal section and the ceramic section to maintain a clamping force of the clamp.
摘要翻译： 燃烧器组件包括具有容纳陶瓷部分的轴向槽的金属部分。 夹持件围绕轴向槽被容纳以将金属部分和陶瓷部分固定在一起。 金属部分上的金属片，金属部分和陶瓷部分之间的垫片以及夹具内的弹簧变形的量大于金属部分和陶瓷部分之间的热膨胀差，以保持夹具的夹紧力。
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公开(公告)号：US20080010990A1
公开(公告)日：2008-01-17
申请号：US11254876
申请日：2005-10-20
申请人： Jun Shi , Jason Lawrence , David J. Bombara , David C. Jarmon , Michael T. Weber , Richard S. Tuthill , Jeffrey D. Melman
发明人： Jun Shi , Jason Lawrence , David J. Bombara , David C. Jarmon , Michael T. Weber , Richard S. Tuthill , Jeffrey D. Melman
IPC分类号： F23R3/00
CPC分类号： F23R3/007 , F16L25/0072 , F16L49/02 , F16L49/06 , F23R3/002 , F23R3/60 , F23R2900/00017
摘要： A combustor assembly includes a metal section having an axial slot that receives a ceramic section. A clamp is received about the axial slot to secure the metal section and ceramic section together. Tabs on the metal section, a gasket between the metal section and the ceramic section, and springs within the clamp deform an amount that is greater than a thermal expansion difference between the metal section and the ceramic section to maintain a clamping force of the clamp.
摘要翻译： 燃烧器组件包括具有容纳陶瓷部分的轴向槽的金属部分。 夹持件围绕轴向槽被容纳以将金属部分和陶瓷部分固定在一起。 金属部分上的金属片，金属部分和陶瓷部分之间的垫片以及夹具内的弹簧变形的量大于金属部分和陶瓷部分之间的热膨胀差，以保持夹具的夹紧力。
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3.发明申请COMPLIANT METAL SUPPORT FOR CERAMIC COMBUSTOR LINER IN A GAS TURBINE ENGINE 有权气体涡轮发动机中陶瓷燃烧器衬里的合格金属支撑公开(公告)号：US20100101232A1
公开(公告)日：2010-04-29
申请号：US12612764
申请日：2009-11-05
摘要： A combustion system for an engine, such as a gas turbine engine is provided. The combustion system has a ceramic component, such as ceramic combustor liner, and at least one metal support component, such as a metal ring or a plurality of metal cones, for providing radial and axial support to the ceramic component. The at least one metal support component includes a structure, such as axial slots or radial slots, for minimizing stress and for increasing compliance of the metal support component with respect to the ceramic component.
摘要翻译： 提供了一种用于发动机的燃烧系统，例如燃气轮机。 燃烧系统具有陶瓷部件，例如陶瓷燃烧器衬套，以及用于向陶瓷部件提供径向和轴向支撑的至少一个金属支撑部件，例如金属环或多个金属锥。 所述至少一个金属支撑部件包括用于最小化应力并增加金属支撑部件相对于陶瓷部件的顺应性的结构，例如轴向槽或径向槽。
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公开(公告)号：US08863528B2
公开(公告)日：2014-10-21
申请号：US11494083
申请日：2006-07-27
CPC分类号： F23R3/286 , F23M2900/05002 , F23R3/007 , F23R3/283 , F23R3/60 , F23R2900/00017
摘要： A combustor assembly having a support assembly between a metal support assembly and a ceramic combustor can section that accommodates a thermal expansion difference therebetween. An air fuel mixer and an igniter are mounted to the support assembly secured to the ceramic combustion can which receives the ignition products of the ignited fuel and air mixture.
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5.发明授权Compliant metal support for ceramic combustor liner in a gas turbine engine 有权用于燃气轮机发动机的陶瓷燃烧器衬套的金属支架公开(公告)号：US08122727B2
公开(公告)日：2012-02-28
申请号：US12612764
申请日：2009-11-05
摘要： A combustion system for an engine, such as a gas turbine engine is provided. The combustion system has a ceramic component, such as ceramic combustor liner, and at least one metal support component, such as a metal ring or a plurality of metal cones, for providing radial and axial support to the ceramic component. The at least one metal support component includes a structure, such as axial slots or radial slots, for minimizing stress and for increasing compliance of the metal support component with respect to the ceramic component.
摘要翻译： 提供了一种用于发动机的燃烧系统，例如燃气轮机。 燃烧系统具有陶瓷部件，例如陶瓷燃烧器衬套，以及用于向陶瓷部件提供径向和轴向支撑的至少一个金属支撑部件，例如金属环或多个金属锥。 所述至少一个金属支撑部件包括用于最小化应力并增加金属支撑部件相对于陶瓷部件的顺应性的结构，例如轴向槽或径向槽。
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6.发明授权Compliant metal support for ceramic combustor liner in a gas turbine engine 有权用于燃气轮机发动机的陶瓷燃烧器衬套的金属支架公开(公告)号：US07647779B2
公开(公告)日：2010-01-19
申请号：US11117599
申请日：2005-04-27
摘要： A combustion system for an engine, such as a gas turbine engine is provided. The combustion system has a ceramic component, such as ceramic combustor liner, and at least one metal support component, such as a metal ring or a plurality of metal cones, for providing radial and axial support to the ceramic component. The at least one metal support component includes a structure, such as axial slots or radial slots, for minimizing stress and for increasing compliance of the metal support component with respect to the ceramic component.
摘要翻译： 提供了一种用于发动机的燃烧系统，例如燃气轮机。 燃烧系统具有陶瓷部件，例如陶瓷燃烧器衬套，以及用于向陶瓷部件提供径向和轴向支撑的至少一个金属支撑部件，例如金属环或多个金属锥。 所述至少一个金属支撑部件包括用于最小化应力并增加金属支撑部件相对于陶瓷部件的顺应性的结构，例如轴向槽或径向槽。
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公开(公告)号：US20140190167A1
公开(公告)日：2014-07-10
申请号：US11494083
申请日：2006-07-27
IPC分类号： F23R3/28
CPC分类号： F23R3/286 , F23M2900/05002 , F23R3/007 , F23R3/283 , F23R3/60 , F23R2900/00017
摘要： A combustor assembly having a support assembly between a metal support assembly and a ceramic combustor can section that accommodates a thermal expansion difference therebetween. An air fuel mixer and an igniter are mounted to the support assembly secured to the ceramic combustion can which receives the ignition products of the ignited fuel and air mixture.
摘要翻译： 一种燃烧器组件，其具有在金属支撑组件和陶瓷燃烧器罐部分之间的支撑组件，其容纳其间的热膨胀差。 空气燃料混合器和点火器安装到固定到陶瓷燃烧罐的支撑组件上，陶瓷燃烧罐接收点燃的燃料和空气混合物的点燃产物。
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公开(公告)号：US20120328996A1
公开(公告)日：2012-12-27
申请号：US13167167
申请日：2011-06-23
申请人： Jun Shi , David C. Jarmon , Lee A. Hoffman , David J. Bombara , Shaoluo L. Butler , Lev A. Prociw
发明人： Jun Shi , David C. Jarmon , Lee A. Hoffman , David J. Bombara , Shaoluo L. Butler , Lev A. Prociw
IPC分类号： F23Q2/32
摘要： A reverse flow combustor has an inlet end. A flowpath extends downstream from the inlet end through a turn. The turn directs the flowpath radially inward and reversing an axial flow direction. A large exit duct (LED) is along the turn. A small exit duct (SED) is along the turn and joined by a joint to a mounting structure to resist separation in a first axial direction. The joint comprises: a first surface on the SED facing partially radially inward; and a mounting feature engaging the first surface.
摘要翻译： 逆流燃烧器具有入口端。 流路从入口端向下游延伸一圈。 转动将径向向内引导并使轴向流动方向反向。 大出口（LED）沿着转弯。 小出口管道（SED）沿着转弯并且通过接头连接到安装结构以抵抗在第一轴向上的分离。 接头包括：SED上的第一表面部分径向向内; 以及与第一表面接合的安装特征。
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公开(公告)号：US08864492B2
公开(公告)日：2014-10-21
申请号：US13167167
申请日：2011-06-23
申请人： Jun Shi , David C. Jarmon , Lee A. Hoffman , David J. Bombara , Shaoluo L. Butler , Lev A. Prociw , Aleksandar Kojovic
发明人： Jun Shi , David C. Jarmon , Lee A. Hoffman , David J. Bombara , Shaoluo L. Butler , Lev A. Prociw , Aleksandar Kojovic
摘要： A reverse flow combustor has an inlet end. A flowpath extends downstream from the inlet end through a turn. The turn directs the flowpath radially inward and reversing an axial flow direction. A large exit duct (LED) is along the turn. A small exit duct (SED) is along the turn and joined by a joint to a mounting structure to resist separation in a first axial direction. The joint comprises: a first surface on the SED facing partially radially inward; and a mounting feature engaging the first surface.
摘要翻译： 逆流燃烧器具有入口端。 流路从入口端向下游延伸一圈。 转动将径向向内引导并使轴向流动方向反向。 大出口（LED）沿着转弯。 小出口管道（SED）沿着转弯并且通过接头连接到安装结构以抵抗在第一轴向上的分离。 接头包括：SED上的第一表面部分径向向内; 以及与第一表面接合的安装特征。
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公开(公告)号：US08745989B2
公开(公告)日：2014-06-10
申请号：US12420973
申请日：2009-04-09
CPC分类号： F23R3/007 , F02C3/145 , F05D2300/21 , F05D2300/603 , F05D2300/6033 , F23R3/002 , F23R3/54 , F23R2900/00018
摘要： A gas turbine engine has an annular reverse-flow combustor with a combustor inner liner enclosing a combustion chamber. The inner liner having a dome portion at an upstream end of the combustor and a downstream combustor exit defined between a small exit duct portion and a large exit duct portion. At least one of the dome portion, the small exit duct portion and the large exit duct portion is made of a separately formed hemi-toroidal shell composed of a ceramic matrix composite.
摘要翻译： 燃气涡轮发动机具有环形逆流燃烧器，其具有包围燃烧室的燃烧器内衬。 内衬具有位于燃烧器上游端的圆顶部分和限定在小出口管道部分和大出口管道部分之间的下游燃烧器出口。 圆顶部分，小出口管道部分和大出口管道部分中的至少一个由单独形成的由陶瓷基体复合材料构成的半环形壳体制成。
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