| 摘要 |
PROBLEM TO BE SOLVED: To provide a power-generating device for an aircraft, which prohibits an increase in an area of a front face of an aircraft engine with respect to the aircraft engine and which can cope with a large change in a change ratio even when configured to generate a large power. SOLUTION: The power-generating device 1 includes a traction transmission 22 connected to the rotary shaft 9 of an engine E, a generator 23 arranged above the traction transmission 22 and driven by the output from the traction 22, and an oil pump unit 24 for lubricating oil arranged below the traction transmission 22 and driven by the output from the traction 22, and it is driven by the engine E. COPYRIGHT: (C)2010,JPO&INPIT
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