发明申请
US20100166559A1 ROTOR OF A GAS TURBINE 有权
燃气轮机转子

ROTOR OF A GAS TURBINE
摘要:
A rotor of a thermal turbomachine, particularly a gas turbine, is provided. The rotor includes a plurality of individual rotor components that are held together by a tie-bold and combined into a unit. The tie-bolt is supported by the assembly of the surrounding rotor components including the tie-bolt and the rotor disks. A hollow shaft which is made up of two tubular sections and a support wheel further support the rotor.
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