发明名称 Propeller with reduction gear in hub - uses pinion on end of engine shaft engaging internal toothed ger
摘要 The noise generated by an aircraft propeller is reduced if the rotational speed of the propeller is reduced. Many aircraft engines incorporate a speed reduction gear to achieve this result. For those engines which do not incorporate a speed reduction gear, there is a speed reduction gear (1) which is incorporated in the propeller hub. The speed reduction gear consists of a shaft with an attached flange which can be bolted to the engine flywheel. This shaft carries a pinion which meshes with an internally toothed gear which forms part of the propeller hub. USE/ADVANTAGE - Propeller with speed reduction gear incorporated in the hub for reducing propeller noise.
申请公布号 DE4130670(A1) 申请公布日期 1992.05.14
申请号 DE19914130670 申请日期 1991.09.14
申请人 HOFFMANN GMBH & CO KG, 8200 ROSENHEIM, DE 发明人 MADELUNG, GERO, PROF. DIPL.-ING., 8000 MUENCHEN, DE
分类号 B64D35/00 主分类号 B64D35/00
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