Rotor assembly having a multistage disk

Details Rotor assembly having a multistage disk Rotor assembly having a multistage disk

F - Mech Eng,Light,Heat,Weapons

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F01D 5/06 (2006.01) F01D 5/02 (2006.01) F01D 5/08 (2006.01)

Patent

CA 1126658

ROTOR ASSEMBLY HAVING A MULTISTAGE DISK ABSTRACT OF THE DISCLOSURE A lightweight, rotor assembly for a gas turbine engine having a critical speed characteristic well above the operating speed is disclosed. Various construction details which enhance the axial stiffness of the rotor assembly and which shield a portion of the disk from working medium gases are developed. The rotor assembly employs a frustoconical member to connect a shaft to the disk. EH-6507

349050

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