发明名称 Control device for main rotor of helicopter, has control rods which enable control of angles of adjustable rotor blades
摘要 <p>The control device includes control rods (2) which are connected to a pivotal point (1) located in the center of a rotor mast. The control rods are connected to the main rotor (4) via rotor blade control points (3). The control rods enable the control of the angles of adjustable rotor blades. An independent claim is also included for a method for controlling the main rotor of a helicopter.</p>
申请公布号 DE10318531(A1) 申请公布日期 2004.11.25
申请号 DE2003118531 申请日期 2003.04.24
申请人 ZF FRIEDRICHSHAFEN AG 发明人 PLATZER, MICHAEL
分类号 B64C27/59;(IPC1-7):B64C27/59 主分类号 B64C27/59
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