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    • 32. 发明授权
    • Supplemental seal for the chordal hinge seal in a gas turbine
    • 燃气轮机中的弦铰链密封的补充密封
    • US06637752B2
    • 2003-10-28
    • US10028929
    • 2001-12-28
    • Mahmut Faruk AksitAhmad SafiAbdul-Azeez Mohammed-Fakir
    • Mahmut Faruk AksitAhmad SafiAbdul-Azeez Mohammed-Fakir
    • F16J1508
    • F16J15/0887F01D11/005F16J15/0812
    • 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 pair of sheet metal shims overlaid by a woven metallic cloth supported by a bracket secured to the nozzle support ring. The radially outer end of the cloth seal bears against a back side of the inner rail. The shims of the legs of the supplemental seal are slit along their distal margin and staggered in a circumferential direction relative to one another to provide flexibility and effective sealing engagement with the inner rail.
    • 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。 辅助密封件包括一对金属垫片,该金属垫片由被固定到喷嘴支撑环上的支架支撑的编织金属布覆盖。 布密封件的径向外端抵靠内轨的后侧。 补充密封件的腿的垫片沿着它们的远侧边缘被切开,并且在相对于彼此的圆周方向上交错,以提供与内轨道的柔性和有效的密封接合。
    • 33. 发明授权
    • Supplemental seal for the chordal hinge seal in a gas turbine
    • 燃气轮机中的弦铰链密封的补充密封
    • US06609885B2
    • 2003-08-26
    • US10028931
    • 2001-12-28
    • Abdul-Azeez Mohammed-FakirMahmut Faruk AksitAhmad SafiIain Robertson Kellock
    • Abdul-Azeez Mohammed-FakirMahmut Faruk AksitAhmad SafiIain Robertson Kellock
    • F01D904
    • F01D11/005F01D9/041F16J15/0812
    • 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 pair of sheet metal shims overlaid by a woven metallic cloth. A bracket and a portion of the supplemental seal are received in a groove along a radial inward facing surface of the inner rail. The projecting margin of the cloth seal bears against the annular sealing surface of the nozzle support ring. The shims of the distal margin of the supplemental seal are slit and staggered in a chord-wise direction relative to one another to provide flexibility and effective sealing engagement with the nozzle support ring.
    • 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。 补充密封件包括由金属编织布覆盖的一对钣金垫片。 支架和补充密封件的一部分被容纳在沿着内轨的径向向内的表面的凹槽中。 布密封件的突出部分靠在喷嘴支撑环的环形密封表面上。 辅助密封件的远侧边缘的垫片相对于彼此沿着弦向方向被切开并交错,以提供与喷嘴支撑环的柔性和有效的密封接合。
    • 35. 发明授权
    • Supplemental seal for the chordal hinge seals in a gas turbine
    • 燃气轮机中的弦铰链密封的补充密封
    • US06572331B1
    • 2003-06-03
    • US10029228
    • 2001-12-28
    • Abdul-Azeez Mohammed-FakirMahmut Faruk AksitAhmad SafiSrikanth VedantamNing Fang
    • Abdul-Azeez Mohammed-FakirMahmut Faruk AksitAhmad SafiSrikanth VedantamNing Fang
    • F01D904
    • F01D11/005F16J15/0887
    • 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. The supplemental seal is formed of a preloaded flexible sheet metal seal having a first margin secured in a linear groove extending in a tangential direction along the inner rail of the nozzle segments with a bent-over edge to form a seal therewith. The opposite second margin has an edge which bears against the axially opposed sealing surface of the nozzle support ring. Sealing pressure against the preloaded flexible seal from a high pressure region maintains the seal between the sealing surfaces of the support ring and segments. The supplemental seal extends tangentially and end edges thereof overlap one another to form a seal between adjacent nozzle segments.
    • 在具有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,在喷嘴段的支撑环和内轨道之间设置补充密封。 辅助密封件由预加载的柔性金属片密封件形成,该密封件具有固定在沿着沿喷嘴段的内轨道的切线方向延伸的直线槽中的第一边缘,具有弯曲边缘以与其形成密封。 相对的第二边缘具有抵靠喷嘴支撑环的轴向相对的密封表面的边缘。 从高压区域对预加载的柔性密封件的密封压力保持了支撑环的密封表面和段之间的密封。 辅助密封件切向延伸并且其端部边缘彼此重叠以在相邻的喷嘴段之间形成密封。