发明名称 Aircraft propulsion system with foldable propeller - has rigid blades on hub hinged to shaft with spring pulling hinge closed
摘要 <p>The propulsion system with a foldable propeller, partic. for motorised glider has a rigid blade unit (5) fixed to a hub (2) connected to the propeller shaft (1) by a hinge joint (3), the blade axis (6) being perpendicular to that of the hinge. A tension spring (8) across the hinge tends to tilt the propeller until blade- and shaft-axes (6,7) are nearly parallel, with one tip (13) resting against a (fixed or movable) stop (9). This movement can be either automatic or arbitrarily controllable, with a locking mechanism. Mass balance about the shaft axis is provided by aerofoil-shaped adjustable counter-weights (11) on the propeller-hub assembly.</p>
申请公布号 DE2911801(A1) 申请公布日期 1980.10.16
申请号 DE19792911801 申请日期 1979.03.26
申请人 WIEMER,HARDO,DIPL.-ING. 发明人 WIEMER,HARDO,DIPL.-ING.
分类号 B64C11/00;B64C31/024;(IPC1-7):64C11/00 主分类号 B64C11/00
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