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公开(公告)号：US06547256B2
公开(公告)日：2003-04-15
申请号：US09747014
申请日：2000-12-26
IPC分类号： F16J1502
CPC分类号： F16J15/3288 , F01D11/005 , F16J15/0812 , F16J15/104 , F23J2213/204 , F23J2213/301 , F23R3/002
摘要： A seal assembly including a low flow cloth ring seal having a cloth assemblage is provided for sealing a tubular cavity disposed between a tubular member and a mating body. The density of the cloth assemblage may be set according to a desired flow rate of gas through the cloth ring seal. In applications where more stiffness and strength is desired, the cloth ring seal may include a shim assemblage surrounded by the cloth assemblage.
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公开(公告)号：US06537023B1
公开(公告)日：2003-03-25
申请号：US10028926
申请日：2001-12-28
申请人： Mahmut Faruk Aksit , Ahmad Safi , Abdul-Azeez Mohammed-Fakir , Gilbert Joseph Dean , Thomas Paul Martin
发明人： Mahmut Faruk Aksit , Ahmad Safi , Abdul-Azeez Mohammed-Fakir , Gilbert Joseph Dean , Thomas Paul Martin
IPC分类号： F01D904
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 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 rail of the nozzle segment on a high pressure side of the chordal hinge seal. The supplemental seal includes a sheet metal seal supported by a bracket secured to the back side and radial inner surfaces of the inner rail. The sheet metal seal has a flexible margin which is preloaded and bears against the annular sealing surface of the nozzle support ring. The bracket is bolted or welded to the inner rail with the sheet metal seal therebetween inhibiting or precluding leakage past the back side of the supplemental seal.
摘要翻译： 在具有在每个喷嘴段的内轨道和喷嘴支撑环的环形轴向相对的密封表面之间具有弦状铰链密封件的燃气轮机中，在高压下在喷嘴段的支撑环和内轨道之间设置补充密封 侧面铰链密封。 补充密封件包括由固定到内轨的后侧和径向内表面的支架支撑的金属板密封件。 金属板密封件具有预先加载并抵靠喷嘴支撑环的环形密封表面的柔性边缘。 支架被螺栓连接或焊接到内轨上，其间的金属板密封件阻止或排除通过辅助密封件背面的泄漏。
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公开(公告)号：US06502825B2
公开(公告)日：2003-01-07
申请号：US09745841
申请日：2000-12-26
IPC分类号： F16J1532
CPC分类号： F16J15/3288 , F23R3/60
摘要： A seal assembly includes a cloth seal for sealing a cavity between a first mating body and a second mating body, the seal dividing the cavity into a high pressure region and a low pressure region. The cloth seal has a shim assemblage and a cloth assemblage. A first peripheral portion of the cloth seal may include a portion of the cloth assemblage and/or the shim assemblage which contacts the high pressure region and a second peripheral portion including a portion of the cloth assemblage adapted to contact the low pressure region. Knowing the flow conditions and pressure differential through the seal, the density of the cloth seal may be calibrated to control leakage and the shim and cloth assemblages may be designed to minimize contact loads on a mating body.
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公开(公告)号：US06250062B1
公开(公告)日：2001-06-26
申请号：US09376171
申请日：1999-08-17
IPC分类号： F02C100
CPC分类号： F23R3/283 , Y10T29/49879
摘要： A fuel nozzle centering assembly and method employ bodies of a substantially wearable and sacrificial material mounted to an outer periphery of a tip of a burner fuel nozzle for a gas turbine combustor. The tip of the fuel nozzle extends through an opening of an annular collar attached to a liner of a main combustion chamber of the gas turbine combustor and an outer periphery of the tip is disposed radially inwardly from the annular collar such that the bodies of sacrificial material are disposed between the outer periphery of the fuel nozzle tip and the annular collar of the liner and space the fuel nozzle tip from the liner collar. The bodies of material prevent the fuel nozzle tip from contacting the liner collar during assembling of the fuel nozzle into the liner. The bodies wear away substantially upon initial operation of the combustor such that the bodies will reduce contact with the liner collar during further operation of the combustor and the fuel nozzle tip will remain spaced from and out of contact with the liner collar during operation of the combustor.
摘要翻译： 燃料喷嘴中心组件和方法采用安装在用于燃气轮机燃烧器的燃烧器燃料喷嘴的末端的外周的基本上可穿戴和牺牲材料的主体。 燃料喷嘴的尖端延伸穿过连接到燃气轮机燃烧器的主燃烧室的衬套的环形轴环的开口，并且尖端的外周从环形轴环径向向内设置，使得牺牲材料体 设置在燃料喷嘴头的外周边和衬套的环形套环之间，并且使燃料喷嘴尖端与衬套相交。 在将燃料喷嘴组装到衬套中期间，材料体防止燃料喷嘴尖端接触衬套。 在燃烧器的初始操作时，物体基本上磨损，使得在燃烧器的进一步操作期间，主体将减少与衬套的接触，并且在燃烧器的操作期间燃料喷嘴头将保持与衬套的间隔开和脱离接触 。
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25.发明授权Supports for connecting a flow sleeve and a liner in a gas turbine combustor 有权支撑用于连接燃气轮机燃烧器中的流动套筒和衬套公开(公告)号：US06216442B1
公开(公告)日：2001-04-17
申请号：US09412965
申请日：1999-10-05
申请人： Keith C. Belsom , Abdul-Azeez Mohammed-Fakir , Calvin L. Sims , Charles E. Steber , Daniel R. Tegel , Henry J. Wiersma
发明人： Keith C. Belsom , Abdul-Azeez Mohammed-Fakir , Calvin L. Sims , Charles E. Steber , Daniel R. Tegel , Henry J. Wiersma
IPC分类号： F02C720
CPC分类号： F23R3/60 , F02C7/20 , F05B2260/301 , F05D2230/642
摘要： In a combustor having an axis, a flow sleeve and a liner, a plurality of circumferentially spaced supports interconnect the upstream ends of the liner and flow sleeve to limit wear on the supports and accommodate relative thermal expansion of the liner and flow sleeve. Each support includes a flow sleeve stop having an angled surface, a groove and a female threaded aperture and a liner stop having a complementary angled surface, a rib and an enlarged opening. By inserting the liner axially through the open upstream end of the flow sleeve, the rib of the liner stop engages the slot of the flow sleeve stop. By passing a bolt having a spring through the enlarged opening of the liner stop and threading the bolt to the flow sleeve stop, the liner is biased for axial downstream movement to maintain the complementary inclined surfaces of the stops in contact with one another, thereby limiting wear and accommodating relative thermal expansion of the flow sleeve and liner.
摘要翻译： 在具有轴线，流动套筒和衬套的燃烧器中，多个周向间隔开的支撑件将衬套和流动套筒的上游端互连以限制支撑件上的磨损并且适应衬套和流动套筒的相对热膨胀。 每个支撑件包括具有成角度表面的流动套筒止动件，凹槽和内螺纹孔，以及具有互补的倾斜表面，肋和扩大开口的衬套止动件。 通过将衬套轴向插入穿过流动套管的敞开的上游端，衬套止挡件的肋接合流动套筒止动件的槽。 通过使具有弹簧的螺栓穿过衬套止动器的扩大的开口并将螺栓螺纹连接到流动套筒止动件，衬套被偏压用于轴向下游运动，以使止动件的互补倾斜表面彼此接触，从而限制 磨损和容纳流动套筒和衬套的相对热膨胀。
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