Patent ID: 8672261

Claim:
An engine mount of an aircraft for suspending an engine of the aircraft at a pylon strut fixed to a wing of said aircraft, comprising: a front engine mount which connects a fan section to said pylon strut, said fan section being provided at a front of said engine; and a rear engine mount which connects an engine core section to said pylon strut, said engine core section being provided at a rear of said engine and said engine core section having an outside diameter smaller than that of said fan section, wherein at least said rear engine mount is configured by connecting an engine side mount member provided at a side of said engine core section to a pylon side mount member provided at a side of said pylon strut, wherein said pylon side mount member comprises: a pair of plate-shaped main mount members provided to sandwich said pylon strut therebetween, and a reinforcing mount member which is sandwiched between said pair of main mount members, and reinforces support strength of said main mount member in a direction to connect said pair of main mount members.