发明公开
EP1323957A2 Composite tubular woven seal for gas turbine nozzle and shroud interface 有权
VerbundgewebeschlauchdichtungfüreineKontaktflächezwischen Mantel andGasturbinendüse

Composite tubular woven seal for gas turbine nozzle and shroud interface
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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