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公开(公告)号：EP1323897B1
公开(公告)日：2007-08-22
申请号：EP02258883.4
申请日：2002-12-23
发明人： Mohammed-Fakir, Abdul-Azeez , Safi, Ahmad , Fang, Ning , Aksit, Mahmut Faruk , Vedantam, Srikanth
CPC分类号： F01D11/005 , F02C7/28 , F16J15/0887
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公开(公告)号：EP1323891A3
公开(公告)日：2004-05-26
申请号：EP02258830.5
申请日：2002-12-23
发明人： Mohammed-Fakir, Abdul-Azeez , Aksit, Mahmut Faruk , Safi, Ahmad , Vedantam, Srikanth , Fang, Ning
IPC分类号： F01D11/00
CPC分类号： F16J15/0887 , F01D11/005
摘要： In a gas turbine having a chordal hinge seal (46) between an inner rail (52) of each nozzle segment and an annular axially facing sealing surface (54) of a nozzle support ring (44), a flexible supplemental seal (70) is disposed between the support ring and inner band (52) of the nozzle segment radially inwardly of the chordal hinge seal. To minimize or prevent leakage flow across the chordal hinge seal, the flexible seal extends between the inner rail and the sealing surface of the support ring radially inwardly of the chordal hinge seal. A first margin (74) of the flexible seal engages in a linear groove carried by the inner rail. The opposite margin (78) extends arcuately in sealing engagement with the nozzle support ring.
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3.发明公开Supplemental seal for the chordal hinge seals in a gas turbine 有权ZusatzdichtungfürStatorelemente einer Gurburbine
公开(公告)号：EP1323894A2
公开(公告)日：2003-07-02
申请号：EP02258863.6
申请日：2002-12-23
发明人： Mohammed-Fakir, Abdul-Azeez , Safi, Ahmad , Fang, Ning , Aksit, Mahmut Faruk , Vedantam, Srikanth
CPC分类号： F16J15/0887 , F01D11/005 , F02C7/28
摘要： In a gas turbine having a chordal hinge seal between an inner rail (52) of each nozzle segment and an annular axially facing sealing surface (54) of a nozzle support ring (44), a supplemental seal (70) is disposed between the support ring and inner bands of the nozzle segments on a lower pressure side of the chordal hinge seals. To minimize or prevent leakage flow across the chordal hinge seals, a generally U-shaped supplemental seal (70) having reversely folded U-shaped marginal portions (74) is received in a cavity formed in the axially extending sealing surface of the inner rail (52) of the nozzle segment. At operating conditions, the marginal portions (74) seal against the base of the cavity and the annular sealing surface (54) of the nozzle support ring to prevent leakage flow past the chordal hinge seal from entering the hot gas path. To install the supplemental seal, the seal is first compressed and maintained in a compressed state by applying one or more wraps about the supplemental seal or an epoxy to secure the seal when compressed in the cavity. At operating temperatures, the retention means releases the seal to engage marginal portions against opposite sealing surfaces of the nozzle segment and support ring.
摘要翻译： 在具有在每个喷嘴段的内部轨道（52）和喷嘴支撑环（44）的环形轴向面对的密封表面（54）之间的弦状铰链密封件的燃气轮机中，辅助密封件（70）设置在支撑件 弦和铰链密封件的下压侧上的喷嘴段的环和内带。 为了最小化或防止跨弦铰链密封件的泄漏流动，具有反向折叠的U形边缘部分（74）的大致U形补充密封件（70）被容纳在形成在内轨道的轴向延伸的密封表面中的空腔中 52）。 在操作条件下，边缘部分（74）密封空腔的基部和喷嘴支撑环的环形密封表面（54），以防止经过铰链密封件的泄漏流进入热气路径。 为了安装补充密封件，首先将密封件压缩并保持在压缩状态，通过在补充密封件或环氧树脂周围施加一个或多个包装件以在压缩在腔体中时固定密封件。 在操作温度下，保持装置释放密封件以将边缘部分接合在喷嘴段和支撑环的相对的密封表面上。
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4.发明公开Supplemental seal for the chordal hinge seals in a gas turbine 有权ErgänzungsdichtungfürVerdichtung einer SehnenscharnierbefestigungfürGasturbinen
公开(公告)号：EP1323891A2
公开(公告)日：2003-07-02
申请号：EP02258830.5
申请日：2002-12-23
发明人： Mohammed-Fakir, Abdul-Azeez , Aksit, Mahmut Faruk , Safi, Ahmad , Vedantam, Srikanth , Fang, Ning
IPC分类号： F01D11/00
CPC分类号： F16J15/0887 , F01D11/005
摘要： In a gas turbine having a chordal hinge seal (46) between an inner rail (52) of each nozzle segment and an annular axially facing sealing surface (54) of a nozzle support ring (44), a flexible supplemental seal (70) is disposed between the support ring and inner band (52) of the nozzle segment radially inwardly of the chordal hinge seal. To minimize or prevent leakage flow across the chordal hinge seal, the flexible seal extends between the inner rail and the sealing surface of the support ring radially inwardly of the chordal hinge seal. A first margin (74) of the flexible seal engages in a linear groove carried by the inner rail. The opposite margin (78) extends arcuately in sealing engagement with the nozzle support ring.
摘要翻译： 在具有在每个喷嘴段的内部轨道（52）和喷嘴支撑环（44）的环形轴向面对的密封表面（54）之间的弦状铰链密封件（46）的燃气轮机中，柔性补充密封件（70）是 设置在所述支撑环和所述喷嘴段的内带（52）之间，所述内带（52）在所述弦铰链密封件的径向内侧。 为了最小化或防止跨过铰链密封件的泄漏流动，柔性密封件在内侧轨道和支撑环的密封表面之间在弦向铰链密封件的径向向内延伸。 柔性密封件的第一边缘（74）接合由内轨道承载的直线槽。 相对的边缘（78）与喷嘴支撑环的密封接合弓形延伸。
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5.发明公开Method and apparatus for segregated oil supply and scavenge in a gas turbine engine 审中-公开在einem Gasturbinenmotor中的Verfahren und VorrichtungfürgetrennteÖlzufuhrund-rücklauf
公开(公告)号：EP2565385A2
公开(公告)日：2013-03-06
申请号：EP12182821.4
申请日：2012-09-03
IPC分类号： F01D9/06
CPC分类号： F01D9/065 , F01D25/162 , F01D25/18 , F05D2260/609 , F05D2260/98
摘要： A gas turbine engine oil supply and scavenge apparatus includes: a stationary first frame comprising a first hub and a first outer ring interconnected by an array of radially-extending hollow first struts; a forward wet cavity defined radially inboard of the first frame, having a first rolling element bearing disposed therein; a supply line extending from the first outer ring through one of the first struts and communicating with the forward wet cavity, the supply line adapted to discharge oil to the forward wet cavity; a stationary second frame comprising a second hub and a second outer ring interconnected by an array of radially-extending hollow second struts, the second frame disposed aft of the first frame; and a scavenge path communicating with the forward wet cavity and adapted to remove oil-air mist from the forward wet cavity, the scavenge path defined at least in part by the second frame.
摘要翻译： 燃气涡轮发动机机油供应和清除装置包括：固定的第一框架，包括第一轮毂和通过径向延伸的中空的第一支柱的阵列互连的第一外环; 径向地限定在第一框架内侧的前向湿腔，其中设置有第一滚动元件轴承; 供应管线从第一外环通过第一支柱中的一个延伸并与前部湿空腔连通，供应管线适于将油排放到前部湿空腔; 固定的第二框架，包括通过径向延伸的中空的第二支柱的阵列互连的第二轮毂和第二外环，所述第二框架设置在所述第一框架的后面; 以及与前进湿腔相通并适于从前方湿腔去除油气雾的清除路径，所述清除路径至少部分地由第二框架限定。
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6.发明公开Lubricant distribution weir for lubricating rotating machine elements 审中-公开Schmiermittelverteilungswehr zum Schmieren von drehenden Maschinenelementen
公开(公告)号：EP1640627A1
公开(公告)日：2006-03-29
申请号：EP05255841.8
申请日：2005-09-21
发明人： Wilton, Stephen Anthony , Fang, Ning , Themudo, Ramon , Whitford, David Scott , Kinnard, Ray Harris , Fisher, Kenneth Lee
CPC分类号： F16D3/06 , F01D25/18 , F16C19/26 , F16C33/586 , F16C33/6651 , F16C33/6674 , F16C33/6677 , F16C2360/23
摘要： A device (14) and method for uniformly providing lubricant to rotating machine parts is provided. The device (14) comprises an axially mounted rotating circumferential lubricant reservoir (20) with a weir (22) comprising one side of the lubricant reservoir (20). The reservoir (20) and weir (22) are disposed at uniform radius and circumferentially about an axis of rotation causing lubricant added to the reservoir (20) to flow uniformly over the weir 22 about the circumference of the weir (22) when the device (14) is in high speed rotational motion. Because of the uniform flow of lubricant over the top of the weir (28) around the circumference of the weir (22), lubricant can be directed to machine parts requiring lubrication in a uniform manner around the circumference of the moving device (14).
摘要翻译： 提供了一种用于向旋转机器部件均匀地提供润滑剂的装置（14）和方法。 装置（14）包括轴向安装的旋转周向润滑剂储存器（20），其中包括润滑剂储存器（20）的一侧的堰（22）。 储存器（20）和堰（22）以均匀的半径设置并围绕旋转轴线周向地设置，使得当设备（20）和堰（22）处于围绕堰（22）的周边时，添加到储存器（20）的润滑剂均匀地流过堰22 （14）处于高速旋转运动。 由于润滑剂在堰（22）周围的堰（28）的顶部上的均匀流动，所以润滑剂可以以围绕移动装置（14）的圆周的均匀方式被引导到需要润滑的机器零件。
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公开(公告)号：EP1323897A3
公开(公告)日：2004-04-14
申请号：EP02258883.4
申请日：2002-12-23
发明人： Mohammed-Fakir, Abdul-Azeez , Safi, Ahmad , Fang, Ning , Aksit, Mahmut Faruk , Vedantam, Srikanth
CPC分类号： F01D11/005 , F02C7/28 , F16J15/0887
摘要： In a gas turbine having a chordal hinge seal between an inner rail (52) of each nozzle segment and an annular axially facing sealing surface of a nozzle support ring, a supplemental seal is disposed between the support ring and inner band (52) of the nozzle segment on a lower pressure side of the chordal hinge seal. The supplemental seal includes a flexible sheet metal seal having a margin (78) secured in a groove (74) of the inner rail (52) of the nozzle segments with a bent-over edge (80) to form a seal therewith. The opposite margin of the seal has an edge which bears against the axially opposed sealing surface of the nozzle support ring. Leakage flow past the chordal hinge seal exerts sealing pressure against the preloaded flexible seal to maintain the seal between the sealing surfaces of the support ring and segments. The supplemental seal extends circumferentially and spans the joint between adjacent nozzle segments.
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8.发明公开Composite tubular woven seal for gas turbine nozzle and shroud interface 有权VerbundgewebeschlauchdichtungfüreineKontaktflächezwischen Mantel andGasturbinendüse
公开(公告)号：EP1323957A2
公开(公告)日：2003-07-02
申请号：EP02258877.6
申请日：2002-12-23
发明人： Mohammed-Fakir, Abdul-Azeez , Aksit, Mahmut Faruk , Safi, Ahmad , Vedantam, Srikanth , Fang, Ning , Goetze, Gayle Hobbs , Arness, Brian Peter , Chi, Wei-Ming , Greene, John Ellington
CPC分类号： F16J15/0887 , F01D11/005 , F16J15/0812
摘要： A compliant woven tubular seal (70) is provided in an arcuate cavity opening through an axial face of a plurality of shroud segments in opposition to a nozzle retaining ring. The annular composite tubular woven compliant seal includes a stainless steel inner metal core (78) surrounded by an annular layer of silica fiber (80). Surrounding the silica fiber is a metal foil (82) which prevents flow past the supplemental seal. an outer wear-resistant braiding (84) serves as a protective covering and wear surface.
摘要翻译： 柔性织造管状密封件（70）设置在通过与喷嘴保持环相对的多个护罩段的轴向面开口的弓形腔中。 环形复合管状编织柔性密封件包括由二氧化硅纤维（80）的环形层包围的不锈钢内金属芯（78）。 围绕二氧化硅纤维是金属箔（82），其防止流过补充密封件。 外部耐磨编织物（84）用作保护性覆盖物和磨损表面。
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9.发明公开Method and apparatus for segregated oil supply and scavenge in a gas turbine engine 审中-公开在燃气轮机发动机中分离供油和清除的方法和装置
公开(公告)号：EP2565385A3
公开(公告)日：2018-03-21
申请号：EP12182821.4
申请日：2012-09-03
IPC分类号： F01D9/06
CPC分类号： F01D9/065 , F01D25/162 , F01D25/18 , F05D2260/609 , F05D2260/98
摘要： A gas turbine engine oil supply and scavenge apparatus includes: a stationary first frame comprising a first hub and a first outer ring interconnected by an array of radially-extending hollow first struts; a forward wet cavity defined radially inboard of the first frame, having a first rolling element bearing disposed therein; a supply line extending from the first outer ring through one of the first struts and communicating with the forward wet cavity, the supply line adapted to discharge oil to the forward wet cavity; a stationary second frame comprising a second hub and a second outer ring interconnected by an array of radially-extending hollow second struts, the second frame disposed aft of the first frame; and a scavenge path communicating with the forward wet cavity and adapted to remove oil-air mist from the forward wet cavity, the scavenge path defined at least in part by the second frame.
摘要翻译： 一种燃气涡轮发动机机油供应和清除装置包括：静止的第一框架，其包括由一排径向延伸的中空第一支柱相互连接的第一轮毂和第一外环; 在第一框架的径向内侧限定的前部湿腔，其中设置有第一滚动元件轴承; 供应管线，所述供应管线从所述第一外环延伸穿过所述第一支柱中的一个并且与所述前部湿腔连通，所述供应管线适于将油排放到所述前部湿腔; 静止的第二框架，其包括由径向延伸的中空第二支柱阵列互连的第二轮毂和第二外环，所述第二框架布置在所述第一框架的后面; 以及与所述前部湿腔连通并适于从所述前部湿腔移除油雾气的清扫路径，所述清扫路径至少部分地由所述第二框架限定。
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公开(公告)号：EP2157289A3
公开(公告)日：2012-04-04
申请号：EP09165854.2
申请日：2009-07-20
发明人： Fang, Ning , Kinnaird, Ray Harris , Moscarino, Gary Paul , Fisher, Kenneth Lee , Scheetz, Jonothan Allen , Pugh, Dave William , Grace, Edward William , Anstead, Duane Howard , Corattiyil, Bala , Kane, Prasad
CPC分类号： F01D25/183 , F01D11/02
摘要： A rotating seal (54) for a gas turbine engine includes: (a) an annular seal body; (b) a sealing component (60, 62) carried by the seal body which is adapted to form one-half of a rotating seal interface; and (c) an impeller (64) carried by the seal body which comprises a plurality of radially-inwardly-extending impeller blades (74).
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