发明名称 INJECTION MOLDED COMPOSITE FAN PLATFORM
摘要 A fan platform for a gas turbine engine may include an outer flow path surface extending between a first side and a second side. An inner surface extends between the first side and the second side, and faces radially oppositely the outer flow path surface. A plurality of platform hooks may extend radially inwardly from the inner surface.
申请公布号 EP2971552(A1) 申请公布日期 2016.01.20
申请号 EP20140768813 申请日期 2014.02.21
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 MURDOCK, JAMES, R.
分类号 F01D5/22;F01D5/14;F01D11/00;F02C7/00 主分类号 F01D5/22
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