| 摘要 |
Disclosed herein is a gas turbine (100) with a plurality of tie rods (160). The gas turbine (100) includes a compressor section (110) having a plurality of compressor-side rotor disks, a turbine section (120) having a plurality of turbine-side rotor disks arranged downstream of the compressor-side rotor disks, a first tie rod (160) penetrating central portions of the rotor disks provided in the compressor section (110) to press the compressor-side rotor disks against each other, a plurality of second tie rods (160) penetrating vicinities of edges of the rotor disks provided in the turbine section (120) to press the turbine-side rotor disks against each other, and a torque transfer member coupled to the first and second tie rods (160) so as to transfer rotational torque generated by the turbine section (120) to the compressor section (110). |
