The utility model discloses a lacing hole structure of
turbine blades and a loose lacing wire installation structure of the same
turbine blades. The lacing hole structure of
turbine blades comprises a straight circular boss structure, the straight circular boss structure is disposed on the turbine blades, the axis of the straight circular boss structure is perpendicular to the normal of the blade-shaped cross section of the turbine blades and is tangentially parallel to the
impeller, a pressure side and a suction side of the blades protrude from the straight circular boss structure, a lacing hole is formed in the middle of the straight circular boss structure, the axis of the lacing hole and the axis of the straight circular boss structure are in the same direction, two small boss structures are arranged at the two ends of the lacing hole, the two ends are on one side of the lacing hole near to the top of the blades, and pits are formed on the side of the lacing hole near to the top of the blades. The loose lacing wire and the lacing hole have two contact points, thereby effectively improving the
damping capacity of the loose lacing wire structure, shorting the free
segment length of the loose lacing wire, reducing the
stress level of the loose lacing wire structure, enabling the loose lacing wire to use
alloy steels with good damping effect to replace
titanium alloys, and being capable of controlling the
stress level of the loose lacing wire structure and improving the
damping capacity of the loose lacing wire structure at the same time.