发明名称 Hybriddrehflügelflugzeug
摘要 <p>The aircraft i.e. helicopter (1) has two propulsive propellers (30) on either side of a fuselage (2) and positioned on respective half-wings (21, 22), and a transmission system (40) connecting a power plant (10) to each propeller via a differential mechanism (50). The mechanism includes an inlet gearwheel (51) secured to a shell (52) carrying a planet gear (54), an idler shaft (55) passing through the gearwheel, and a propeller shaft (58) rotating with an outlet sun gear (57). A propeller brake (60) brakes the propeller shaft, and an inlet brake (65) brakes the idler shaft.</p>
申请公布号 EP2574546(A1) 申请公布日期 2013.04.03
申请号 EP20120006365 申请日期 2012.09.11
申请人 EUROCOPTER 发明人 MORET, ROBIN
分类号 B64C27/26;B64C27/12;B64C27/82 主分类号 B64C27/26
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