发明名称 Aircraft propeller has a swashplate pitch control to vary the direction of thrust
摘要 <p>An improved effect aircraft propeller has a swashplate mounting with a two part construction; one fixed part (1) and one movable part, linked by a bearing. A control linkage (3) varies the blade pitch cyclically, as for a helicopter rotor, to vary the airflow onto the control and support planes to generate lift and steering control even at low speeds.</p>
申请公布号 DE102004014850(A1) 申请公布日期 2005.11.10
申请号 DE20041014850 申请日期 2004.03.24
申请人 GRUENTJENS, NORBERT 发明人
分类号 B64C11/30;(IPC1-7):B64C11/30 主分类号 B64C11/30
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