发明名称 Dual mode rotor hub assembly
摘要 <p>A rotor hub assembly (103, 203, 301) and method for controlling movement of a rotor blade (107, 303) relative to a swashplate (305). The hub assembly having an attachment device (315) operably associated with the rotor blade and the swashplate. The attachment device provides pivot and rotational blade movement relative to the swashplate. A dual spring-rate damper (321, 323) is operably associated with the attachment device. The damper (321, 323) switches between a first spring rate and a second spring rate during flight to control movement of the rotor blade. The method includes the process of switching the damper between the first spring rate and the second spring rate during flight.</p>
申请公布号 EP2594483(A1) 申请公布日期 2013.05.22
申请号 EP20120175816 申请日期 2011.12.22
申请人 BELL HELICOPTER TEXTRON INC. 发明人 STAMPS, FRANK B;TISDALE, PATRICK;CORRIGAN, JOHN J
分类号 B64C27/51;B64C29/00 主分类号 B64C27/51
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