Patent ID: 11884410
Assignee: GENERAL ELECTRIC COMPANY
Field: Engines, pumps, turbines (Mechanical engineering)
Classification: CPC B  F | IPC B  F

Claim 16:
17. A gas turbine engine coupled to a pylon, the gas turbine engine defining a roll axis, a yaw axis, and a pitch axis, the gas turbine engine comprising:
a casing;
a mount to couple the casing to the pylon, the mount including:
a first pin;
a second pin;
a third pin; and
a fourth pin;
a first linkage portion including the first pin, the first linkage portion including:
a first member; and
a second member, the first member and the second member forming a first clevis with the first pin and the pylon, the first member and the second member forming a second clevis with the second pin and the casing;

a second linkage portion, the second linkage portion forming a first load path between the gas turbine engine and the pylon, the second linkage portion arranged with respect to the first linkage portion such that a gap prevents the first linkage portion from forming a second load path between the gas turbine engine and the pylon, the second linkage portion further including;
a third member; and
a fourth member, the third member and the fourth member forming a third clevis with the third pin and the pylon, the third member and the fourth member forming a fourth clevis with the fourth pin and the casing.