发明名称 PITCH CONTROL SYSTEM FOR VARIABLE PITCH PROPELLER
摘要 <p>Pitch Control System For Variable Pitch Propeller A propeller pitch control system having a mechanical low pitch stop which includes an electrical backup therefor. The backup comprises an electrically operatable means (245) to effect blade pitch adjustment toward feather under conditions of failure of the low pitch stop indicated by propeller operation at pitch angles in the range of beta operation, but power settings in the range of normal engine speed governor pitch control. Such operating conditions actuate a pair of switches (190 and 195) connecting the means (245) to a voltage source to increase blade pitch toward feather, thereby preventing overspeed operation of the propeller.</p>
申请公布号 CA1246519(A) 申请公布日期 1988.12.13
申请号 CA19840462199 申请日期 1984.08.30
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 DUCHESNEAU, JEROME G.;SCHWARTZ, ROBERT A.
分类号 B63H3/10;B64C11/40;F02D29/02;(IPC1-7):B64C11/40 主分类号 B63H3/10
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