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公开(公告)号：US08511980B2
公开(公告)日：2013-08-20
申请号：US13555877
申请日：2012-07-23
IPC分类号： F01D9/02
CPC分类号： F01D5/284 , F01D5/3015 , F05D2240/80 , Y02T50/672 , Y02T50/673
摘要： A segmented component for use with a gas turbine engine comprises a radially extending gas path portion. The gas path portion is for interacting with gas flow from the gas turbine engine. The gas path portion comprises a forward portion forming a leading edge of a stationary vane, an aft portion forming a trailing edge of the stationary vane, and a plurality of middle portions forming a pressure side and a suction side of the stationary vane. The component is divided into axially aligned segments comprising a forward segment, an aft segment, and a plurality of middle segments disposed between the forward segment and the aft segment. The middle segments comprise radially elongate ceramic matrix composite material plates.
摘要翻译： 用于燃气涡轮发动机的分段部件包括径向延伸的气体路径部分。 气体路径部分用于与来自燃气涡轮发动机的气体流相互作用。 气体路径部包括形成静止叶片的前缘的前部，形成静止叶片的后缘的后部，以及形成静止叶片的压力侧和吸力侧的多个中间部。 该部件被分成轴向对准的段，其包括前段，后段和设置在前段和后段之间的多个中段。 中间段包括径向细长的陶瓷基复合材料板。
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2.发明申请公开(公告)号：US20100189556A1
公开(公告)日：2010-07-29
申请号：US12361192
申请日：2009-01-28
CPC分类号： F01D5/284 , F01D5/3015 , F05D2240/80 , Y02T50/672 , Y02T50/673
摘要： A segmented component for use with a gas turbine engine comprises a radially extending gas path portion. The gas path portion is for interacting with gas flow from the gas turbine engine. The component is divided into axially aligned segments comprising a forward segment, an aft segment, and a plurality of middle segments disposed between the forward segment and the aft segment. The middle segments comprise radially elongate ceramic matrix composite material plates. In one embodiment, the gas path portion comprises an airfoil for a turbine blade. In another embodiment, the gas path portion comprises a removable platform for a turbine blade. In another embodiment, the gas path portion comprises an airfoil for a turbine vane.
摘要翻译： 用于燃气涡轮发动机的分段部件包括径向延伸的气体路径部分。 气体路径部分用于与来自燃气涡轮发动机的气体流相互作用。 该部件被分成轴向对准的段，其包括前段，后段和设置在前段和后段之间的多个中段。 中间段包括径向细长的陶瓷基复合材料板。 在一个实施例中，气体路径部分包括用于涡轮机叶片的翼型件。 在另一个实施例中，气体通道部分包括用于涡轮叶片的可移除平台。 在另一个实施例中，气体通道部分包括用于涡轮叶片的翼型件。
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3.发明申请公开(公告)号：US20130004296A1
公开(公告)日：2013-01-03
申请号：US13555877
申请日：2012-07-23
IPC分类号： F01D9/02
CPC分类号： F01D5/284 , F01D5/3015 , F05D2240/80 , Y02T50/672 , Y02T50/673
摘要： A segmented component for use with a gas turbine engine comprises a radially extending gas path portion. The gas path portion is for interacting with gas flow from the gas turbine engine. The gas path portion comprises a forward portion forming a leading edge of a stationary vane, an aft portion forming a trailing edge of the stationary vane, and a plurality of middle portions forming a pressure side and a suction side of the stationary vane. The component is divided into axially aligned segments comprising a forward segment, an aft segment, and a plurality of middle segments disposed between the forward segment and the aft segment. The middle segments comprise radially elongate ceramic matrix composite material plates.
摘要翻译： 用于燃气涡轮发动机的分段部件包括径向延伸的气体路径部分。 气体路径部分用于与来自燃气涡轮发动机的气体流相互作用。 气体路径部包括形成静止叶片的前缘的前部，形成静止叶片的后缘的后部，以及形成静止叶片的压力侧和吸力侧的多个中间部。 该部件被分成轴向对准的段，其包括前段，后段和设置在前段和后段之间的多个中段。 中间段包括径向细长的陶瓷基复合材料板。
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公开(公告)号：US08251651B2
公开(公告)日：2012-08-28
申请号：US12361192
申请日：2009-01-28
IPC分类号： F01D9/02
CPC分类号： F01D5/284 , F01D5/3015 , F05D2240/80 , Y02T50/672 , Y02T50/673
摘要： A segmented component for use with a gas turbine engine comprises a radially extending gas path portion. The gas path portion is for interacting with gas flow from the gas turbine engine. The component is divided into axially aligned segments comprising a forward segment, an aft segment, and a plurality of middle segments disposed between the forward segment and the aft segment. The middle segments comprise radially elongate ceramic matrix composite material plates. In one embodiment, the gas path portion comprises an airfoil for a turbine blade. In another embodiment, the gas path portion comprises a removable platform for a turbine blade. In another embodiment, the gas path portion comprises an airfoil for a turbine vane.
摘要翻译： 用于燃气涡轮发动机的分段部件包括径向延伸的气体路径部分。 气体路径部分用于与来自燃气涡轮发动机的气体流相互作用。 该部件被分成轴向对准的段，其包括前段，后段和设置在前段和后段之间的多个中段。 中间段包括径向细长的陶瓷基复合材料板。 在一个实施例中，气体路径部分包括用于涡轮机叶片的翼型件。 在另一个实施例中，气体通道部分包括用于涡轮叶片的可移除平台。 在另一个实施例中，气体通道部分包括用于涡轮叶片的翼型件。
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公开(公告)号：US20170044920A1
公开(公告)日：2017-02-16
申请号：US14721651
申请日：2015-05-26
CPC分类号： F01D11/12 , F01D9/02 , F01D25/246 , F05D2220/32 , F05D2240/11 , F05D2250/15 , F05D2260/30 , F05D2260/38 , F05D2260/941 , F05D2300/6033
摘要： A segmented turbine shroud for radially encasing a rotatable turbine in a gas turbine engine comprising a carrier, a ceramic matrix composite (CMC) seal segment, and an elongated pin. The carrier defines a pin-receiving carrier bore and the CMC seal segment defines a pin-receiving seal segment bore. The elongated pin extends through the carrier bore and the seal segment bore. The pin-receiving carrier bore includes a cantilevered member such that the carrier bore has a length sufficient to effect radial flexion between the carrier bore and the pin received within the carrier bore during operation of the turbine.
摘要翻译： 一种用于在包括载体，陶瓷基体复合（CMC）密封段和细长销）的燃气涡轮发动机中径向包围可旋转涡轮机的分段涡轮机罩。 载体限定销接收载体孔，CMC密封段限定销接收密封部分孔。 细长销延伸穿过承载孔和密封段孔。 销接收载体孔包括悬臂构件，使得载体孔的长度足以在涡轮机的运行期间在承载孔和承载孔内的销之间实现径向弯曲。
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公开(公告)号：US20160348528A1
公开(公告)日：2016-12-01
申请号：US14721705
申请日：2015-05-26
申请人： Daniel Kent Vetters , David J. Thomas , Ted Freeman , Douglas David Dierksmeier , Jun Shi , Todd Engel
发明人： Daniel Kent Vetters , David J. Thomas , Ted Freeman , Douglas David Dierksmeier , Jun Shi , Todd Engel
CPC分类号： F01D11/08 , F01D9/04 , F01D25/24 , F01D25/246 , F05D2220/32 , F05D2240/24 , F05D2300/6033
摘要： A ceramic matrix composite (CMC) seal segment for use in a segmented turbine shroud for radially encasing a turbine in a gas turbine engine. The CMC seal segment comprises an arcuate flange having a surface facing the turbine and a portion defining a bore for receiving an elongated pin, with the bore having a length that is at least 70% of the length of the elongated pin received therein. The CMC seal segment is carried by the carrier by at least one of the elongated pins being received within the bore. The CMC seal segment portion defining a pin-receiving bore is radially spaced from the arcuate flange by a spacing flange extending radially outward from the arcuate flange.
摘要翻译： 一种陶瓷基体复合材料（CMC）密封段，用于分段涡轮机罩，用于在燃气涡轮发动机中径向包围涡轮机。 CMC密封段包括具有面向涡轮的表面的弧形凸缘和限定用于接收细长销的孔的部分，孔的长度为其中接收的细长销的长度的至少70％。 CMC密封段由载体承载，其中至少一个细长销被接收在孔内。 限定销接收孔的CMC密封段部分通过从弧形凸缘径向向外延伸的间隔凸缘与弓形凸缘径向间隔开。
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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：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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公开(公告)号：US08642766B2
公开(公告)日：2014-02-04
申请号：US12991081
申请日：2009-04-30
申请人： Ryan A. Shenvi , Carlos A. Guerrero , Jun Shi , Chuang-Chuang Li , Phil S. Baran
发明人： Ryan A. Shenvi , Carlos A. Guerrero , Jun Shi , Chuang-Chuang Li , Phil S. Baran
IPC分类号： C07D217/00 , C07D311/00
CPC分类号： C07D498/22 , C07D317/72 , C07D319/08 , C07D491/153 , C07D493/08 , C07D493/18 , C07J41/0005 , C07J63/004 , C07J71/0005 , C07J71/0057
摘要： An in vitro synthesis of (+) cortistatin A from readily available precursors is disclosed, as are the syntheses of related 17-aryl substituted compounds, the 17-aryl substituted compounds themselves and novel compounds useful in their preparation.
摘要翻译： 公开了来自容易获得的前体的（+）皮质激素A的体外合成，以及相关的17-芳基取代的化合物，17-芳基取代的化合物本身和用于其制备的新化合物的合成。
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10.发明授权Method and apparatus for establishing communications in low signal to noise ratio environments 有权用于在低信噪比环境下建立通信的方法和装置公开(公告)号：US08571494B2
公开(公告)日：2013-10-29
申请号：US12692099
申请日：2010-01-22
IPC分类号： H04B1/66
摘要： An apparatus is disclosed having a receiver configured to communicate, by a first apparatus, with a second apparatus in a first mode; determine side information by the first apparatus based on the communication during the first mode; and store the side information by the first apparatus for communication in a second mode with the second apparatus, wherein the first and second modes of communication have different date rates. A method for wireless communications is also disclosed.
摘要翻译： 公开了一种装置，其具有被配置为以第一模式与第二装置通信的第一装置的接收器; 基于第一模式期间的通信确定第一装置的侧信息; 并且利用第二装置以第二模式存储第一装置进行通信的侧信息，其中第一和第二通信模式具有不同的日期速率。 还公开了一种用于无线通信的方法。
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