Patent ID: 8056227

Claim:
A method comprising: obtaining a turbine blade including: a root section at an end of the turbine blade, a first airfoil section adjacent to the root section, a midspan section adjacent to the first airfoil section and including a first material block, a second airfoil section adjacent to the midspan section, and a tip section adjacent to the second airfoil section and including a second material block, the first and second material block being incongruous with any adjacent airfoil section; selectively machining the second material block to include a tip shroud at a selected length for the turbine blade; removing a last stage turbine blade from a root mount of a rotating shaft of a turbine; adjusting a radial position of the root mount, wherein the selected length is chosen to be compatible with the adjusted radial position of the root mount, wherein the radial position is less than a previous radial position of the root mount and the adjusting of the radial position of the root mount includes removing at least one other root mount within a stage to which the root mount belongs; and replacing the last stage turbine blade with the turbine blade.