AIRCRAFT ENGINE DEVICE

摘要

An aircraft engine device (1) comprising: a rotating shaft (6); a fan (10) driven by the rotating shaft; a fan case that surrounds the fan; an aircraft apparatus (28) disposed upstream of the fan and further inward in the radial direction of the rotating shaft than the peripheral edge of the fan case; a housing (2) which accommodates at least one part of the rotating shaft and supports the fan case; a first power transmission unit (9) which is linked to the rotating shaft and the fan; a second power transmission unit (32) which is disposed further inward in the radial direction of the rotating shaft than the first power transmission unit and is linked to the rotating shaft and the aircraft apparatus; and a support member (12) which is disposed between the first power transmission unit and the second power transmission unit and supports the aircraft apparatus by linking the housing and the aircraft apparatus.