Damping system for an integrally bladed rotor
An integrally bladed disk is provided that includes a disk and a plurality of rotor blades. The disk has an outer radial hub and is configured for rotation around a rotational axis. Each rotor blade of the plurality of rotor blades has an airfoil that extends chordwise between a leading edge and a trailing edge, and extends spanwise between a base end and a blade tip. Each rotor blade includes a damper pocket, a damper body, and a plug. The damper pocket extends into the airfoil from the base end and has a first tapered configuration. The damper body is disposed within the damper pocket, and has a second tapered configuration. The second tapered configuration of the damper body mates with the first tapered configuration of the damper pocket. The plug is disposed to retain the damper body within the damper pocket.
1. An integrally bladed disk, comprising:
a disk having an outer radial hub, the disk configured for rotation around a rotational axis;
a plurality of rotor blades, each having an airfoil, the airfoil extending chordwise between a leading edge and a trailing edge, and extending spanwise between a base end and a blade tip;
wherein each said rotor blade includes:
a damper pocket (DP) extending into the airfoil from the base end, the damper pocket having a first tapered configuration, the first tapered configuration including a first DP side surface and a second DP side surface, the damper pocket including a DP top end surface that extends between the first DP side surface and the second DP side surface, and the first DP side surface and the second DP side surface converge toward one another;
a damper body (DB) disposed within the damper pocket, wherein the damper body has a second tapered configuration, the damper body including a DB top end surface that extends between a first DB side surface and a second DB side surface, wherein the second tapered configuration of the damper body mates with the first tapered configuration of the damper pocket, the second tapered configuration including the first DB side surface and the second DB side surface, and the first DB side surface and the second DB side surface converge toward one another;
a weld collar affixed to the base end of the airfoil, and the weld collar includes a weld collar aperture that is aligned with the damper pocket and configured to receive the damper body; and
a plug disposed to retain the damper body within the damper pocket;
wherein each said rotor blade is affixed to a surface of the outer radial hub of the disk at the weld collar;
wherein the damper pocket and the damper body are disposable in an engaged configuration wherein the first DP side surface is in contact with the first DB side surface and the second DP side surface is in contact with the second DB side surface, and in the engaged configuration, the DB top end surface is spaced apart from the DP top end surface.
2. The integrally bladed disk of claim 1 , wherein the plug for each said rotor blade is affixed to the weld collar.
3. The integrally bladed disk of claim 1 , wherein the damper body is a unitary body.
4. The integrally bladed disk of claim 1 , wherein the damper body includes a plurality of components that collectively form the damper body.
5. The integrally bladed disk of claim 4 , wherein the plurality of components that collectively form the damper body includes a first tapered damper body component, a second tapered damper body component, and a central damper body component.
6. The integrally bladed disk of claim 1 , wherein the damper body comprises a shape memory alloy.
7. An integrally bladed disk, comprising:
a disk having an outer radial hub, the disk configured for rotation around a rotational axis;
a plurality of rotor blades, each having an airfoil, the airfoil extending chordwise between a leading edge and a trailing edge, and extending spanwise between a base end and a blade tip;
wherein each said rotor blade includes:
a damper pocket (DP) extending into the airfoil from the base end, the damper pocket having a first tapered configuration and a DP top end, the first tapered configuration of the damper pocket includes a first DP side surface and a second DP side surface, the first DP side surface and the second DP side surface converge toward one another, and the DP top end extends between the first DP side surface and the second DP side surface;
a damper body (DB) disposable within the damper pocket in an engaged configuration, wherein the damper body has a second tapered configuration, the second tapered configuration of the damper body includes a first DB side surface and a second DB side surface, and the first DB side surface and the second DB side surface converge toward one another, the damper body including a DB top end surface that extends between the first DB side surface and the second DB side surface, wherein the second tapered configuration of the damper body mates with the first tapered configuration of the damper pocket; and
a plug disposed to retain the damper body within the damper pocket;
wherein in the engaged configuration:
the DB top end surface is spaced apart from the DP top end, and
the first DP side surface is in contact with the first DB side surface and the second DP side surface is in contact with the second DB side surface.
8. The integrally bladed disk of claim 7 , wherein each said rotor blade includes a weld collar affixed to the base end of the airfoil, and the weld collar includes a weld collar aperture that is aligned with the damper pocket and configured to receive the damper body.
9. The integrally bladed disk of claim 8 , wherein the plug for each said rotor blade is affixed to the weld collar.
10. The integrally bladed disk of claim 9 , wherein each said rotor blade is affixed to the outer radial hub of the disk at the weld collar.
11. The integrally bladed disk of claim 7 , wherein the damper body is a unitary body.
12. The integrally bladed disk of claim 7 , wherein the damper body includes a plurality of components that collectively form the damper body.