Shroud ring for use in a gas turbine engine
作者： John H. Young , Anthony R. De Cosmo
DOI:
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摘要: A shroud ring (22) for a gas turbine engine having stator structure (14) and an array of inwardly extending vanes (20) is disclosed. The circumferentially segmented to accommodate inward outward movement the structure. has outer (28) inner (30). engages support position integral seal member (24) about rotor In one embodiment are rotatable spanwise axis S. second embodiment, (120) integrally attached (122).
google.co.uk 参考文章(5)
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