Tunable mass damper assembly for a rotor blade
A tunable mass damper assembly is attachable to a rotor blade. The tunable mass damper assembly comprises a base configured to be attached to the rotor blade and a pendulum mass structure movably attached to the base and configured to move relative to the base in accordance with a rotational speed of the rotor blade about a rotor axis. The pendulum mass structure is configured to reduce vibratory forces of the rotor blade induced by a rotation of the rotor blade about the rotor axis. An entirety of the pendulum mass structure being configured to be contained within and enclosed by the rotor blade.
1. A tunable mass damper assembly attachable to a rotor blade configured to rotate about a rotor axis, the tunable mass damper assembly comprising:
a base configured to be attached to the rotor blade; and
a pendulum mass structure comprising:
a first end rotatably coupled to the base about a pivot axis substantially perpendicular to a plane containing the rotor axis;
a second end configured to rotate freely and without restraints on motion between two end stops about the pivot axis in accordance with a rotational speed of the rotor blade about the rotor axis, wherein when the base is attached to the rotor blade, the pendulum mass structure is coupled to the rotor blade only via the first end,
the pendulum mass structure being configured to reduce vibratory forces of the rotor blade induced by a rotation of the rotor blade about the rotor axis, and
an entirety of the pendulum mass structure being configured to be contained within and enclosed by the rotor blade.
2. The tunable mass damper assembly of claim 1 , wherein an entirety of the base is configured to be positioned within and completely enclosed by the rotor blade.
3. The tunable mass damper assembly of claim 1 , wherein the pendulum mass structure comprises a pendulum mass at the second end and at least one pendulum arm at the first end, wherein a first arm end of the at least one pendulum arm is attached to the base and a second arm end of the at least one pendulum arm is attached to the pendulum mass.
4. The tunable mass damper assembly of claim 3 , wherein the at least one pendulum arm is rotatably attached to both the pendulum mass and the base.
5. The tunable mass damper assembly of claim 1 , wherein the pendulum mass structure is configured to be positioned along a feathering axis of the rotor blade.
6. The tunable mass damper assembly of claim 1 , wherein the base is configured to be rigidly secured to the rotor blade.
7. The tunable mass damper assembly of claim 1 , wherein the base is configured to be movably secured to the rotor blade such that the base and the pendulum mass structure do not rotate with the rotor blade when the rotor blade rotates about a feathering axis to change a pitch angle.
8. The tunable mass damper assembly of claim 1 , wherein the tunable mass damper assembly is configured to be positioned within a rotor blade that is part of a coaxial rotor system.
9. The tunable mass damper assembly of claim 1 , wherein the tunable mass damper assembly is configured to be positioned within a rotor blade that is part of a rigid rotor system.
10. The tunable mass damper assembly of claim 1 , further comprising a center block, wherein the base and the pendulum mass structure are positioned within the center block.
11. The tunable mass damper assembly of claim 10 , wherein the base is rotatably coupled to the center block.
12. The tunable mass damper assembly of claim 10 , further comprising a first bearing block configured to statically couple to the rotor blade, a second bearing block configured to statically couple to the rotor blade, wherein the center block is rotatably coupled to the first bearing block and the second bearing block.
13. The tunable mass damper assembly of claim 1 , wherein the base is rotatably coupled to the rotor blade.
14. The tunable mass damper assembly of claim 4 , wherein the at least one pendulum arm comprises a first pendulum arm arranged substantially parallel to a second pendulum arm.
15. The tunable mass damper assembly of claim 3 , wherein a first side of the pendulum mass is coupled to the at least one pendulum arm, wherein a cross-section of the first side is larger than a cross-section of a second side of the pendulum mass, the second side opposite the first side.
16. A tunable mass damper assembly attachable to a rotor blade configured to rotate about a rotor axis, the tunable mass damper assembly comprising:
a base configured to be attached to the rotor blade; and
a pendulum mass structure comprising:
a first end rotatably coupled to the base about a pivot axis substantially perpendicular to a plane containing the rotor axis;
a second end configured to rotate freely about the pivot axis in accordance with a rotational speed of the rotor blade about the rotor axis, wherein when the base is attached to the rotor blade, the pendulum mass structure is coupled to the rotor blade only via the first end,
the pendulum mass structure being configured to reduce vibratory forces of the rotor blade induced by a rotation of the rotor blade about the rotor axis, and
an entirety of the pendulum mass structure being configured to be contained within and enclosed by the rotor blade,
wherein the pendulum mass structure comprises a pendulum mass at the second end and at least one pendulum arm at the first end, wherein a first arm end of the at least one pendulum arm is attached to the base and a second arm end of the at least one pendulum arm is attached to the pendulum mass,
wherein the at least one pendulum arm is rotatably attached to both the pendulum mass and the base,
wherein the at least one pendulum arm comprises a first pendulum arm arranged substantially parallel to a second pendulum arm,
wherein the base, the first pendulum arm, the second pendulum arm, and the pendulum mass form a four-bar linkage.
17. The tunable mass damper assembly of claim 16 , wherein the base comprises a first stop configured to limit rotation of the first pendulum arm and a second stop configured to limit rotation of the second pendulum arm.
18. A method of dampening vibratory forces in a rotor blade configured to rotate about a rotor axis, the method comprising:
coupling a base of a tunable mass damper to the rotor blade such that an entirety of the tunable mass damper is contained within and enclosed by the rotor blade, the tunable mass damper further comprising a pendulum mass structure including:
a first end rotatably coupled to the base about a pivot axis substantially perpendicular to a plane containing the rotor axis; and
a second end configured to rotate about the pivot axis, wherein when the base is attached to the rotor blade, the pendulum mass structure is coupled to the rotor blade only via the first end; and
allowing the second end of the pendulum mass structure to rotate freely and without restraints on motion between two end stops in accordance with a rotational speed of the rotor blade about the rotor axis to reduce vibratory forces of the rotor blade induced by a rotation of the rotor blade about the rotor axis.