Transient Response of a Simulated Aeroengine with a Fusing Structure during a Fan-Blade Out Event

Table 1

Dimensions of shafts in the low-pressure rotor.

Shaft number	Length (mm)	Internal diameter (mm)	External diameter (mm)
L1	300	70	80
L2	300	70	80
L3	100	35	40
L4	200	35	40
L5	600	35	40
L6	100	35	40
L7	220	35	40
L8	180	35	40