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专利名称：Injection Molded Composite Fan Platform发明人：James R. Murdock申请号：US14400929申请日：20140221
公开号：US20150132134A1公开日：20150514
专利附图：
摘要：A fan platform for a gas turbine engine may include an outer flow path surfaceextending between a first side and a second side. An inner surface extends between thefirst side and the second side, and faces radially oppositely the outer flow path surface. Aplurality of platform hooks may extend radially inwardly from the inner surface.
申请人：United Technologies Corporation
地址：Hartford CT US
国籍：US
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