发明名称 |
Turbine with a supplemental seal for the chordal hinge seal and method of installation |
摘要 |
<p>In a gas turbine, a supplemental seal (60) is provided between an annular axially facing sealing surface (54) of a nozzle support ring (44) and an annular axially opposed sealing surface (50) formed by circumferentially adjacent nozzle segments. Each segment carries an inner rail (52) mounting a chordal hinge seal which engages the sealing surface of the nozzle support ring. That seal is supplemented by a generally arcuate V-shaped seal (60) between the sealing surfaces which opens radially inwardly toward a high pressure leakage path past the chordal hinge seal. The supplemental seal is initially compressed and maintained in a compressed condition during installation by application of a solder. At operating temperature, the solder melts away, releasing the supplemental seal to seal between the nozzle support ring and nozzle segments. <IMAGE></p> |
申请公布号 |
EP1323892(B1) |
申请公布日期 |
2007.02.14 |
申请号 |
EP20020258850 |
申请日期 |
2002.12.23 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MOHAMMED-FAKIR, ABDUL-AZEEZ;AKSIT, MAHMUT FARUK;SAFI, AHMAD;VEDANTAM, SRIKANTH;FANG, NING |
分类号 |
F01D11/00;F01D25/24;F02C7/28;F16J15/08 |
主分类号 |
F01D11/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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