Damper pin having elongated bodies for damping adjacent turbine blades

A turbine engine, comprising:

• a rotor shaft that extends axially within the turbine engine;
• a plurality of turbine blades coupled to the rotor shaft and extending radially outwardly therefrom, each turbine blade having an airfoil that extends radially outwardly from a platform, the plurality of turbine blades including a first turbine blade and a second turbine blade adjacent to the first turbine blade, wherein the first and second turbine blades define a groove therebetween;
• and
• a damper pin disposed within the groove, the damper pin comprising:
• a first elongated body having a center portion disposed between a first end portion and a second end portion, wherein the first end portion, center portion and second end portion define a generally arcuate top portion of the first elongated body, wherein the first elongated body defines a slot that extends axially therethrough;
• a second elongated body having a generally arcuate top portion, wherein the second elongated body is at least partially disposed within the slot, and wherein the second elongated body is slideably engaged in an axial direction with the first elongated body, wherein the first end portion of the first elongated body and the generally arcuate top portion of the second elongated body collectively define a first semi-cylindrical shape, and wherein the second end portion of the first elongated body and the generally arcuate top portion of the second elongated body collectively define a second semi-cylindrical shape.

A turbine engine, comprising:

• a rotor shaft that extends axially within the turbine engine;
• a plurality of turbine blades coupled to the rotor shaft and extending radially outwardly therefrom, each turbine blade having an airfoil that extends radially outwardly from a platform, the plurality of turbine blades including a first turbine blade and a second turbine blade adjacent to the first turbine blade, wherein the first and second turbine blades define a groove therebetween;
• and
• a damper pin disposed within the groove, the damper pin comprising:
• a first elongated body having a center portion disposed between a first end portion and a second end portion, wherein the first end portion, center portion and second end portion define a generally arcuate top portion of the first elongated body, wherein the first elongated body defines a slot that extends axially therethrough;
• a second elongated body having a generally arcuate top portion, wherein the second elongated body is at least partially disposed within the slot, and wherein the second elongated body is slideably engaged in an axial direction with the first elongated body, wherein the slot and the second elongated body are substantially wedge shaped.

A turbine engine, comprising:

• a rotor shaft that extends axially within the turbine engine;
• a plurality of turbine blades coupled to the rotor shaft and extending radially outwardly therefrom, each turbine blade having an airfoil that extends radially outwardly from a platform, the plurality of turbine blades including a first turbine blade and a second turbine blade adjacent to the first turbine blade, wherein the first and second turbine blades define a groove therebetween;
• and
• a damper pin disposed within the groove, the damper pin comprising:
• a first elongated body having a center portion disposed between a first end portion and a second end portion, wherein the first end portion, center portion and second end portion define a generally arcuate top portion of the first elongated body, wherein the first elongated body defines a slot that extends axially therethrough;
• a second elongated body having a generally arcuate top portion, wherein the second elongated body is at least partially disposed within the slot, and wherein the second elongated body is slideably engaged in an axial direction with the first elongated body, wherein the slot is dovetail shaped.