发明授权
- 专利标题: Supplemental seal for the chordal hinge seals in a gas turbine
- 专利标题(中): 燃气轮机中的弦铰链密封的补充密封
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申请号: US10029228申请日: 2001-12-28
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公开(公告)号: US06572331B1公开(公告)日: 2003-06-03
- 发明人: Abdul-Azeez Mohammed-Fakir , Mahmut Faruk Aksit , Ahmad Safi , Srikanth Vedantam , Ning Fang
- 申请人: Abdul-Azeez Mohammed-Fakir , Mahmut Faruk Aksit , Ahmad Safi , Srikanth Vedantam , Ning Fang
- 主分类号: F01D904
- IPC分类号: F01D904
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. 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.
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