发明公开
EP1323957A2 Composite tubular woven seal for gas turbine nozzle and shroud interface
有权
VerbundgewebeschlauchdichtungfüreineKontaktflächezwischen Mantel andGasturbinendüse
- 专利标题: Composite tubular woven seal for gas turbine nozzle and shroud interface
- 专利标题(中): VerbundgewebeschlauchdichtungfüreineKontaktflächezwischen Mantel andGasturbinendüse
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申请号: EP02258877.6申请日: 2002-12-23
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公开(公告)号: EP1323957A2公开(公告)日: 2003-07-02
- 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
- 申请人: General Electric Company
- 申请人地址: 1 River Road Schenectady, NY 12345 US
- 专利权人: General Electric Company
- 当前专利权人: General Electric Company
- 当前专利权人地址: 1 River Road Schenectady, NY 12345 US
- 代理机构: Goode, Ian Roy
- 优先权: US29216 20011228
- 主分类号: F16J15/12
- IPC分类号: F16J15/12 ; F01D11/00
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.
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