| 摘要 |
PROBLEM TO BE SOLVED: To provide an engine device for an aircraft which is light-weight, has a simple structure, and inhibits increase in a front area while including a device for an aircraft which is driven by a driving force of an engine for an aircraft.SOLUTION: An engine device 1 for an aircraft includes: a rotary shaft 6; a fan 10 driven by the rotary shaft; a fan case enclosing the fan; a device 28 for an aircraft which is disposed at the upstream side relative to the fan and the inner side relative to a periphery of the fan case in a radial direction of the rotary shaft; a housing 2 which houses at least a part of the rotary shaft and supports the fan case; a first power transmission part 9 connected to the rotary shaft and the fan; a second power transmission part 32 which is located at the inner side relative to the first power transmission part in the radial direction of the rotary shaft and connected to the rotary shaft and the device for the aircraft; and a support member 12 which is disposed between the first power transmission part and the second power transmission part and supports the device for the aircraft while connecting the housing with the device for the aircraft.SELECTED DRAWING: Figure 2 |
