Patent attributes
A turbine blade includes an airfoil and a shroud coupled to a tip of the airfoil. The shroud includes a mid portion positioned directly above the tip of the airfoil. The mid portion includes a ramped radially outer surface extending from a first edge to a second edge in the direction from a pressure side toward a suction side of the airfoil, the second edge being positioned further radially inward than the first edge. In a first aspect, the shroud may include a curved pressure side portion positioned upstream of the pressure side of the airfoil, the pressure side portion being curved radially inward. In a second aspect, the shroud may include a curved suction side portion positioned downstream of the suction side of the airfoil, the suction side portion being curved radially outward.