发明名称 Rotorcraft with independent blade control system with hydraulic pitch link
摘要 According to one embodiment, a rotorcraft pitch link (118, 830a-830d) includes a housing and a piston assembly (832a). The housing comprises a first chamber (831a) and a second chamber (833a). 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 (832a) 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 (831a) from the second chamber (833a).
申请公布号 EP2692635(B1) 申请公布日期 2016.08.10
申请号 EP20120188719 申请日期 2012.10.16
申请人 BELL HELICOPTER TEXTRON INC. 发明人 FENNY, CARLOS A.
分类号 B64C27/605;B64C27/72;F15B15/26 主分类号 B64C27/605
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