发明名称 MAIN TRANSMISSION GEAR BOX FOR A TWO-ENGINE HELICOPTER
摘要 In a main transmission gearbox for a helicopter having two engines, a lifting rotor and an anti-torque rotor, each of the two engines drives a main kinematic chain comprising from upstream down, an input shaft, a twistable shaft, a gear train forming a first reduction stage having a first bevel pinion meshing with a second bevel pinion which drives in rotation a vertical shaft bearing having a third pinion in mesh with a gearwheel which is common to the two main chains and forms with the third pinions a second reduction stage. The torque received at the gearwheel is transmitted to the driving shaft of the main rotor by way of a supplementary reduction stage of epicyclic type. A third chain comprising two input pinions each of which is mounted upon one of the input shafts and an intermediate pinion which drives the driving shaft of the anti-torque rotor, ensures the distribution of power over the two main chains in the event of breakdown of one engine.
申请公布号 DE3560771(D1) 申请公布日期 1987.11.19
申请号 DE19853560771 申请日期 1985.08.05
申请人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE 发明人 MOUILLE, RENE LOUIS
分类号 B64C27/12;B64C27/14;B64D35/00;B64D35/08;(IPC1-7):B64C27/14 主分类号 B64C27/12
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