发明名称 Power transmission-train installation, especially for a helicopter transmission
摘要 To accommodate variations and sudden changes in power to one of two input shafts (1), two gears (10) are mounted with axial freedom but secured in rotation to their drive shafts (9). By action of the compensating linkage (13) on the bearing supports (14) the conical helical gears (2) are firmly meshed with output drive gears (3).Clutches (8) release the drive from input shafts (1) to drive shafts (9) in the event of input power failure. A separate output shaft (7) is driven through intermediate gears (6) engaging both input drive shafts (9)
申请公布号 FR2777961(A1) 申请公布日期 1999.10.29
申请号 FR19980005015 申请日期 1998.04.22
申请人 EUROCOPTER DEUTSCHLAND GMBH 发明人 ROHRDANZ JURGEN
分类号 B64C27/12;F16H1/22;F16H55/20;F16H57/12;(IPC1-7):F16H55/18;F16H37/06 主分类号 B64C27/12
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