Patent ID: 10508546

Abstract:
A turbomachine includes a turbine section including a turbine, the turbine having a plurality of turbine rotor blades spaced along the axial direction, each turbine rotor blade extending generally along the radial direction between a radial inner end and a radial outer end. The plurality of turbine rotor blades includes a first turbine rotor blade; and a second turbine rotor blade spaced from the first turbine rotor blade along the axial direction, the radial outer end of the first turbine rotor blade coupled to the radial outer end of the second turbine rotor blade. The plurality of turbine rotor blades additionally includes a third turbine rotor blade spaced from the second turbine rotor blade along the axial direction, the radial inner end of the second turbine rotor blade coupled to the radial inner end of the third turbine rotor blade.