发明名称 COMPOSITE REINFORCED SWASHPLATE
摘要 A swashplate of a blade pitch control assembly is provided including a metal component having one or more interfacing features. The metal component includes a hollow first cylinder having a first flange extending outwardly from a first end thereof and a second flange extending outwardly from a second end thereof. A sidewall extends between the first and second flanges such that a cavity is defined between the first flange, the second flange, and the sidewall. A plurality of connecting members is connected to a portion of the first flange and the second flange and is spaced about a periphery of the first cylinder. A tubular composite component is arranged at least partially within the cavity between adjacent pairs of the connecting members.
申请公布号 WO2016081057(A1) 申请公布日期 2016.05.26
申请号 WO2015US50858 申请日期 2015.09.18
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 LAITENBERGER, KEVIN;POULIN, STEPHEN V.;BYRNE, ERIK
分类号 B64C27/605 主分类号 B64C27/605
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