An aircraft engine apparatus (1) includes: a rotating shaft (6); a fan (10) driven by the rotating shaft; a fan case surrounding the fan; aircraft equipment (28) disposed upstream of the fan and, in a radial direction of the rotating shaft, disposed inward of a peripheral edge of the fan case; a casing (2) that accommodates at least part of the rotating shaft and supports the fan case; a first motive force transmitter (9) coupled to the rotating shaft and the fan; a second motive force transmitter (32) disposed inward of the first motive force transmitter in the radial direction of the rotating shaft and coupled to the rotating shaft and the aircraft equipment; and a support member (12) disposed between the first motive force transmitter and the second motive force transmitter, the support member coupling the casing and the aircraft equipment and supporting the aircraft equipment.
AIRCRAFT ENGINE DEVICE
FLUGZEUGTRIEBWERKSVORRICHTUNG
DISPOSITIF DE MOTEUR D'AVION
2019-07-17
Patent
Elektronische Ressource
Englisch
AIRCRAFT, AIRCRAFT ENGINE, AND AIRCRAFT ENGINE NACELLE
Europäisches Patentamt | 2017
|AIRCRAFT, AIRCRAFT ENGINE, AND AIRCRAFT ENGINE NACELLE
Europäisches Patentamt | 2019
|Aircraft, aircraft engine, and aircraft engine nacelle
Europäisches Patentamt | 2019
|Aircraft engine attachment device, and corresponding aircraft
Europäisches Patentamt | 2017
|