发明名称 Gas turbine engine stator vane assembly with inner shroud
摘要 A stator vane assembly (38) includes a vane (42) having an inner end (44). In one example, the vane (42) is aluminum. An inner shroud (46) has an aperture (48) receiving the inner end (44). A flexible material (68) secures the inner end (44) to the inner shroud (46). The material has an inner surface (69) opposite the vane (42) providing a seal land in one example. The inner shroud provides an arcuate inner shroud segment (46), which is constructed of either cast aluminum or stamped sheet steel. An inner shroud segment (46) has an arcuate wall (50) providing multiple apertures (48), for example. First and second flanges (52,54) are integral with and extending radially inwardly from a concave side of the wall (50).
申请公布号 EP2620591(A2) 申请公布日期 2013.07.31
申请号 EP20130151894 申请日期 2013.01.18
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 DUBE, DAVID P.;MCMAHON, MICHAEL E.;FEIGLESON, STEVEN J.
分类号 F01D9/04;F01D11/00;F01D25/06 主分类号 F01D9/04
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