专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

51. 发明申请

US20140190167A1 Ceramic combustor can for a gas turbine engine 有权
标题翻译：陶瓷燃烧器可用于燃气涡轮发动机
公开(公告)号：US20140190167A1
公开(公告)日：2014-07-10
申请号：US11494083
申请日：2006-07-27
申请人： Jun Shi , David J. Bombara , Jason Lawrence , Richard S. Tuthill , Jeffery D. Melman
发明人： Jun Shi , David J. Bombara , Jason Lawrence , Richard S. Tuthill , Jeffery D. Melman
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。

52. 发明授权

US08745989B2 Reverse flow ceramic matrix composite combustor 有权
标题翻译：逆流陶瓷基体复合燃烧器
公开(公告)号：US08745989B2
公开(公告)日：2014-06-10
申请号：US12420973
申请日：2009-04-09
申请人： Lev Alexander Prociw , Aleksander Kojovic , David C. Jarmon , Jun Shi , Shaoluo L. Butler
发明人： Lev Alexander Prociw , Aleksander Kojovic , David C. Jarmon , Jun Shi , Shaoluo L. Butler
IPC分类号： F02C1/00 , F23R3/00 , F23R3/54 , F02C3/14
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。

53. 发明授权

US08642766B2 Synthesis of (+) cortistatin A and related compounds 失效
标题翻译：（+）皮质抑素A及相关化合物的合成
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。

54. 发明授权

US08511980B2 Segmented ceramic matrix composite turbine airfoil component 有权
标题翻译：分段陶瓷基体复合涡轮机翼型件
公开(公告)号：US08511980B2
公开(公告)日：2013-08-20
申请号：US13555877
申请日：2012-07-23
申请人： Tracy A. Propheter-Hinckley , Jun Shi
发明人： Tracy A. Propheter-Hinckley , Jun Shi
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。

55. 发明申请

US20130011248A1 REDUCTION IN THERMAL STRESSES IN MONOLITHIC CERAMIC OR CERAMIC MATRIX COMPOSITE SHROUD 审中-公开
标题翻译：单晶陶瓷或陶瓷基复合材料中的热应力减少
公开(公告)号：US20130011248A1
公开(公告)日：2013-01-10
申请号：US13176112
申请日：2011-07-05
申请人： Paul F. Croteau , Kevin E. Green , Jun Shi
发明人： Paul F. Croteau , Kevin E. Green , Jun Shi
IPC分类号： F01D25/24
CPC分类号： F01D9/04 , F01D11/08 , F01D25/246 , F05D2230/53 , F05D2230/642 , F05D2250/294 , F05D2300/6033
摘要： A shroud for use in a gas turbine engine has a ring with a plurality of protrusions and a plurality of slots and each of the protrusions having an arc length and parallel sides.
摘要翻译：用于燃气涡轮发动机的护罩具有多个突起和多个槽的环，并且每个突起具有弧形长度和平行的边。

56. 发明授权

US08206098B2 Ceramic matrix composite turbine engine vane 有权
标题翻译：陶瓷基复合涡轮发动机叶片
公开(公告)号：US08206098B2
公开(公告)日：2012-06-26
申请号：US11824174
申请日：2007-06-28
申请人： Lisa A. Prill , Jeffery R. Schaff , Jun Shi
发明人： Lisa A. Prill , Jeffery R. Schaff , Jun Shi
IPC分类号： F04D29/54
CPC分类号： F01D5/284 , F01D9/041 , F05D2240/11 , F05D2300/50212 , F05D2300/603 , F05D2300/6033 , F05D2300/614
摘要： A vane has an airfoil shell and a spar within the shell. The vane has an outboard shroud at an outboard end of the shell and an inboard platform at an inboard end of the shell. The shell includes a region having a depth-wise coefficient of thermal expansion and a second coefficient of thermal expansion transverse thereto, the depth-wise coefficient of thermal expansion being greater than the second coefficient of thermal expansion.
摘要翻译：叶片具有翼壳和壳内的翼梁。叶片在外壳的外侧具有外侧护罩，在外壳的内侧具有内侧平台。壳体包括具有深度方向的热膨胀系数和横向于其的第二热膨胀系数的区域，深度方面的热膨胀系数大于第二热膨胀系数。

57. 发明授权

US08191102B2 Method of transmitting interactive television 有权
标题翻译：交互式电视传输方式
公开(公告)号：US08191102B2
公开(公告)日：2012-05-29
申请号：US10541051
申请日：2003-12-05
申请人： Philip Steven Newton , Declan Patrick Kelly , Jingwei Tan , Jun Shi , Liang Gan
发明人： Philip Steven Newton , Declan Patrick Kelly , Jingwei Tan , Jun Shi , Liang Gan
IPC分类号： H04N7/16
CPC分类号： H04N21/4433 , H04H20/16 , H04L65/4076 , H04N5/76 , H04N7/163 , H04N21/235 , H04N21/4331 , H04N21/4334 , H04N21/4345 , H04N21/4348 , H04N21/435 , H04N21/6433 , H04N21/6547 , H04N21/8166 , H04N21/8352 , H04N21/8545
摘要： A method (1) of transmitting interactive television, whereby interactive television applications are transmitted inside application-modules. These modules are transmitted in a broadcast stream. Recording systems cannot decide which modules are to be recorded. Therefore storage related information of said modules is signalled in the broadcast stream. Module identification information related is implemented in the Application Information Table (AIT) and/or in the Download Information Indication (DII) message. Thus information is included in the broadcast stream concerning categories stating whether application modules are mandatory, optional or forbidden to record. Alternatively properties of a module are chosen from Code/Data/Both and/or Fixed/Variable. Recording systems use this information do decide if application modules are to be recorded or disregarded. Alternatively, application module identification information is transmitted in said broadcast stream. A module identification number is used to avoid multiple recordings. Application modules having the same category are preferably grouped together.
摘要翻译：一种发送交互式电视的方法（1），由此在应用模块内传输交互式电视应用。这些模块以广播流传输。记录系统无法决定要记录的模块。因此，所述模块的存储相关信息在广播流中被通知。相关的模块识别信息在应用信息表（AIT）和/或下载信息指示（DII）消息中实现。因此，关于涉及应用模块是强制性的，可选的或被禁止记录的类别的广播流中包括信息。或者，代码/数据/两者和/或固定/变量都选择模块的属性。记录系统使用这些信息确定应用程序模块是要被记录还是被忽略。或者，在所述广播流中发送应用模块识别信息。模块识别号用于避免多次录音。具有相同类别的应用模块优选地被分组在一起。

58. 发明申请

US20120007286A1 LOW TRANSIENT AND STEADY STATE THERMAL STRESS DISK SHAPED COMPONENTS 有权
标题翻译：低瞬态和稳态热应变片形成组件
公开(公告)号：US20120007286A1
公开(公告)日：2012-01-12
申请号：US13234249
申请日：2011-09-16
申请人： Jun Shi
发明人： Jun Shi
IPC分类号： C04B35/64 , B29C47/00 , B29C35/08
CPC分类号： F01D5/34 , B22F5/009 , B22F5/106 , B22F2998/00 , B23P15/006 , B33Y70/00 , B33Y80/00 , F01D5/048 , F01D5/282 , F04D29/023 , F05D2300/50212 , F05D2300/603 , F05D2300/6032 , F05D2300/6033 , Y02P10/295 , Y10T428/21 , Y10T428/218 , Y10T428/2927 , Y10T428/2933 , Y10T428/31504 , B22F2207/01 , B22F3/008 , B22F3/1055 , B22F3/115
摘要： A process for manufacturing a disk shaped component comprising fabricating a disk shaped component using a composite material having at least a first material and a second material, wherein the first material is disposed at and proximate to a center portion of the disk shaped component and the second material is disposed at and proximate to a rim of the disk shaped component, wherein the first material comprises a first coefficient of thermal expansion, a first stress value and a first oxidation resistance, and the second material comprises a second coefficient of thermal expansion, a second stress value and a second oxidation resistance, wherein the first coefficient of thermal expansion is greater than the second coefficient of thermal expansion, the first stress value is greater than the second stress value and the first oxidation resistance is less than the second oxidation resistance.
摘要翻译：一种用于制造盘形部件的方法，包括使用具有至少第一材料和第二材料的复合材料制造盘形部件，其中所述第一材料设置在所述盘形部件的中心部分处并且靠近所述盘形部件的中心部分，材料设置在盘形部件的边缘处并且靠近盘形部件的边缘，其中第一材料包括第一热膨胀系数，第一应力值和第一抗氧化性，第二材料包括第二热膨胀系数，第二应力值和第二抗氧化性，其中所述第一热膨胀系数大于所述第二热膨胀系数，所述第一应力值大于所述第二应力值，并且所述第一抗氧化性小于所述第二抗氧化性。

59. 发明申请

US20110274538A1 CERAMIC GAS TURBINE SHROUD 有权
标题翻译：陶瓷气体涡轮机
公开(公告)号：US20110274538A1
公开(公告)日：2011-11-10
申请号：US12776673
申请日：2010-05-10
申请人： Jun Shi , Kevin E. Green
发明人： Jun Shi , Kevin E. Green
IPC分类号： F01D25/24
CPC分类号： F01D11/08 , F01D25/26 , F01D25/28 , F05D2240/11 , F05D2260/94 , F05D2260/941 , F05D2300/21
摘要： An example gas turbine engine shroud includes a first annular ceramic wall having an inner side for resisting high temperature turbine engine gasses and an outer side with a plurality of radial slots. A second annular metallic wall is positioned radially outwardly of and enclosing the first annular ceramic wall and has a plurality of tabs in communication with the slot of the first annular ceramic wall. The tabs of the second annular metallic wall and slots of the first annular ceramic wall are in communication such that the first annular ceramic wall and second annular metallic wall are affixed.
摘要翻译：示例性燃气涡轮发动机罩包括具有用于抵抗高温涡轮发动机气体的内侧的第一环形陶瓷壁和具有多个径向槽的外侧。第二环形金属壁位于第一环形陶瓷壁的径向外部并且包围第一环形陶瓷壁，并且具有与第一环形陶瓷壁的槽连通的多个突片。第二环形金属壁的突片和第一环形陶瓷壁的槽与第一环形陶瓷壁和第二环形金属壁相连接。

60. 发明授权

US07967570B2 Low transient thermal stress turbine engine components 有权
标题翻译：低瞬态热应力涡轮发动机部件
公开(公告)号：US07967570B2
公开(公告)日：2011-06-28
申请号：US11829391
申请日：2007-07-27
申请人： Jun Shi , Wayde R. Schmidt
发明人： Jun Shi , Wayde R. Schmidt
IPC分类号： F01D5/28
CPC分类号： F01D5/147 , B33Y80/00 , F01D5/28 , F05D2230/30 , F05D2300/50212 , Y10T29/4932
摘要： A turbine vane includes a platform; and at least one airfoil mounted to the platform and having a trailing edge and a leading edge, wherein the vane is composed of a functionally graded material having a first material and a second material, wherein the trailing edge includes a greater amount of the first material than the second material, and the leading edge includes a greater amount of the second material than the first material.
摘要翻译：涡轮叶片包括平台; 以及安装到所述平台并具有后缘和前缘的至少一个翼型件，其中所述叶片由具有第一材料和第二材料的功能梯度材料组成，其中所述后缘包括更大量的所述第一材料并且前缘包括比第一材料更多的第二材料。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式