发明名称 ABRADABLE SEAL HAVING NANOLAYER MATERIAL
摘要 A gas turbine engine includes a plurality of circumferentially-spaced blades (62). The blades (62) have a polymeric coating (62a) thereon. An abradable seal (64) circumscribes the blades and includes a polymeric matrix (68) with a dispersion of a nanolayer material (70).
申请公布号 EP2894300(A1) 申请公布日期 2015.07.15
申请号 EP20150151093 申请日期 2015.01.14
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 AMINI, SHAHRAM;STROCK, CHRISTOPHER W.
分类号 F01D11/12 主分类号 F01D11/12
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