发明名称 INDEPENDENT BLADE CONTROL SYSTEM WITH HYDRAULIC PITCH LINK
摘要 According to one embodiment, a rotorcraft pitch link includes a housing and a piston assembly. The housing comprises a first chamber and a second chamber. A first housing opening allows a first fluid to flow into the first chamber, and a second housing allows a second fluid to flow into the second chamber. The piston assembly is at least partially disposed within the housing and comprises a piston head and a piston rod coupled to the piston head. The piston head separates the first chamber from the second chamber.
申请公布号 US2014034777(A1) 申请公布日期 2014.02.06
申请号 US201213565554 申请日期 2012.08.02
申请人 FENNY CARLOS A.;BELL HELICOPTER TEXTRON INC. 发明人 FENNY CARLOS A.
分类号 B64C27/64;F01D7/00 主分类号 B64C27/64
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