Rotating airfoil assembly
A rotating airfoil including a body and a vibration absorber located within the body. The body has a root end and a tip. The rotating airfoil has a natural frequency, and the vibration absorber has a natural frequency. The natural frequency of the vibration absorber is different than the natural frequency of the rotating airfoil.
1. A rotating airfoil comprising:
a body having a root end and a tip;
a cavity formed in the body, the cavity including a plurality of walls defining the cavity; and
a vibration absorber located within the cavity and arranged in the cavity to move within the cavity without contacting the walls of the cavity when an excitation frequency is applied to the rotating airfoil,
wherein the rotating airfoil has a natural frequency, and the vibration absorber has a natural frequency, the natural frequency of the vibration absorber being different than the natural frequency of the rotating airfoil by at least ten percent.
2. The rotating airfoil of claim 1 , wherein the natural frequency of the vibration absorber is from twenty-five percent of the natural frequency of the rotating airfoil to ninety percent of the natural frequency of the rotating airfoil.
3. The rotating airfoil of claim 1 , wherein the vibration absorber is actively adjustable, the vibration absorber being operatively coupled to a controller, and the controller being programmed to adjust the natural frequency of the vibration absorber based on an input.
4. The rotating airfoil of claim 1 , wherein the vibration absorber is passively adjustable, the vibration absorber including an adjustable mass movable to change the natural frequency of the vibration absorber, the position of the adjustable mass being based on the rotational speed of the rotating airfoil.
5. The rotating airfoil of claim 1 , wherein the vibration absorber is a first vibration absorber having a first natural frequency, and the rotating airfoil further comprises a second vibration absorber having a second natural frequency different from the first natural frequency, wherein the first natural frequency and the second natural frequency are different than the natural frequency of the rotating airfoil.
6. The rotating airfoil of claim 1 , wherein the body includes foam, the vibration absorber being located within the foam.
7. The rotating airfoil of claim 1 , further comprising a spar, the spar being a portion of the body and the vibration absorber being located within the spar.
8. The rotating airfoil of claim 7 , wherein the cavity is formed in the spar.
9. The rotating airfoil of claim 8 , wherein the rotating airfoil has a longitudinal direction, the spar extending to the tip and the cavity being a bore extending inward from the tip in the longitudinal direction of the rotating airfoil.
10. The rotating airfoil of claim 1 , wherein the vibration absorber is a cantilevered beam having an attachment end and a free end, the attachment end being attached to at least one wall of the plurality of walls defining the cavity, the vibration absorber being sized and positioned within the cavity such that the free end is able to vibrate within the cavity when subjected to an excitation frequency.
11. The rotating airfoil of claim 10 , wherein the rotating airfoil has a longitudinal direction, each of the cavity and the vibration absorber being elongated in the longitudinal direction.
12. The rotating airfoil of claim 10 , wherein the free end includes an adjustable mass movable with respect to the attached end to change the natural frequency of the vibration absorber.
13. The rotating airfoil of claim 10 , wherein the vibration absorber is sized and positioned within the cavity such that a gap is formed between the vibration absorber and sidewalls of the cavity.
14. The rotating airfoil of claim 13 , wherein the gap is sized such that the free end of the vibration absorber is able vibrate within the cavity, without contacting the sidewalls of the cavity, when the rotating airfoil is subjected to an excitation frequency that is less than the natural frequency of the rotating airfoil.
15. A rotating airfoil assembly comprising:
a rotation axis; and
a plurality of rotating airfoils of claim 1 , the plurality of the rotating airfoils being rotatable about the rotation axis.
16. A rotating airfoil assembly of claim 15 , wherein the rotating airfoil assembly produces an excitation frequency because of asymmetric loading of the plurality of rotating airfoils when the rotation axis is at an angle relative to an airflow direction of air flowing into the plurality of the rotating airfoils, the natural frequency of the vibration absorber being the excitation frequency.
17. A rotating airfoil assembly of claim 15 , wherein the plurality of the rotating airfoils is rotatable about the rotation axis at a rotational speed, the natural frequency of the vibration absorber being from ninety percent to one hundred ten percent of the rotational speed.
18. An engine comprising:
the rotating airfoil assembly of claim 15 ; and
a torque producing system coupled to the rotating airfoil assembly to rotate the rotating airfoil assembly about the rotation axis of the rotating airfoil assembly.
19. The engine of claim 18 , wherein the engine is an unducted single fan engine, the torque producing system being a turbomachine of a gas turbine engine, and the rotating airfoil assembly being a fan with each of the plurality of rotating airfoils being a fan blade.