发明名称 Compact co-axial rotor system for a rotary wing aircraft and a control system therefor
摘要 A dual, counter rotating, coaxial rotor system provides an upper and lower rotor system, with a reduced axial rotor separation distance along a common axis by way of rotor tip position sensing and rotor position controls to avoid tip contact.
申请公布号 US2006273220(A1) 申请公布日期 2006.12.07
申请号 US20060446352 申请日期 2006.06.02
申请人 SCOTT MARK W 发明人 SCOTT MARK W.
分类号 B64C27/54;B64C27/08;B64C27/10;B64C27/32;B64C27/46;B64C27/605;B64C27/615 主分类号 B64C27/54
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