Gas turbine engine assembly and method of assembling same

Details Gas turbine engine assembly and method of assembling same Gas turbine engine assembly and method of assembling same

F - Mech Eng,Light,Heat,Weapons

02

C

F02C 7/36 (2006.01)

Patent

CA 2602322

A gas turbine engine assembly (10) includes a core gas turbine engine (13) and a fan assembly (12) coupled to the core gas turbine engine. The fan assembly is upstream from the core gas turbine engine. A low-pressure turbine (20) is coupled to the core gas turbine engine and is disposed downstream from the core gas turbine engine. The low-pressure turbine includes a disk (105) including a flange (107) and a plurality of splines (108) formed in the flange. A shaft (31) includes a first end (120) coupled to the fan assembly and a second end (122) that includes a plurality of splines (110). The shaft splines are configured to mesh with the flange splines such that torque is transmitted from the low-pressure turbine to the fan assembly via the shaft.

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