Torsional vibration damper
A rotor assembly has a drive shaft and a bladed rotor mounted to the drive shaft for rotation therewith. A dampening material is bonded to the rotor at a location where there is torsional strain energy present. Shear forces in the damping material are used to convert the torsional strain energy into heat energy, thereby providing torsional vibration damping.
1. A cooling fan comprising:
a drive shaft with an axis of rotation;
a rotor having a hub mounted on the drive shaft, a web extending from the hub away from the axis of rotation, a circumferentially spaced array of blades on an air flow surface of the web, and a rear surface of the rotor, the rear surface having an annular concave recess around the drive shaft;
a housing surrounding the rotor and a portion of the drive shaft, the housing having an air inlet and an air outlet, the housing defining an air flow passage with the air flow surface of the web and a shielded plenum with the rear surface of the rotor; and
a vibration dampening material bonded to the rear surface of the rotor in the annular concave recess, the vibration dampening material bonded in a maximal strain zone of the rotor.
2. The cooling fan according to claim 1 wherein the vibration dampening material comprises material selected from the group consisting of: rubber; silicon; polyethylene; metal alloy; carbon fiber and resin composite; and combinations thereof.
3. The cooling fan according to claim 2 wherein the vibration dampening material comprises a plurality of bonded layers of said combinations.
4. The cooling fan according to claim 1 wherein the rear surface of the rotor and the vibration dampening material are bonded with adhesive.
5. The cooling fan according to claim 1 wherein the vibration dampening material comprises one of: particles; and droplets deposited on the rear surface of the rotor.
6. The cooling fan according to claim 5 wherein the vibration dampening material comprises one of: a coating; a metal spray deposition layer; and an additive manufacturing layer.
7. The cooling fan according to claim 1 , wherein the annular concave recess has a maximum axial depth region at a junction between the hub and the web, the vibration dampening material being provided in the maximum axial depth region.
8. The cooling fan according to claim 1 , wherein the rear surface of the web includes one of: protrusions; ribs; fins; knurling; and grooves for bonding to the vibration dampening material.
9. A method of reducing torsional vibration of a cooling fan,
the cooling fan including a rotor having a hub mounted on a drive shaft, a web extending away from the hub, a circumferentially spaced array of fan blades on an air flow surface of the web, and a rear surface of the rotor, the method comprising:
bonding a vibration dampening material to the rear surface of the rotor, wherein the vibration dampening material is bonded to the rear surface of the rotor at a maximal strain zone, and wherein the method further comprises determining the maximal strain zone using one of: finite element analysis; and empirical testing.
10. The method according to claim 9 wherein the vibration dampening material is manufactured separately from the rotor and is bonded to the rotor with adhesive.
11. The method according to claim 9 wherein the vibration dampening material is applied to the rotor as one of: a coating; a metal spray deposition layer; and an additive manufacturing layer.
12. The method according to claim 9 wherein the vibration dampening material comprises material selected from the group consisting of: rubber; silicon; polyethylene; metal alloy; carbon fiber and resin composite; and combinations thereof.
13. The method according to claim 12 , wherein the vibration dampening material is bonded to the rear surface of the rotor in a plurality of bonded layers of said combinations.
14. The method according to claim 9 , wherein the rear surface of the rotor is prepared before bonding the vibration dampening material by forming thereon at least one of: protrusions; ribs; fins; knurling; and grooves.
15. A lightweight high speed rotor comprising:
a drive shaft rotatable about an axis of rotation;
a rotor carrying a plurality of blades, the rotor mounted to the drive shaft for rotation therewith, the rotor having a rear cavity; and
a torsional damper bonded in the rear cavity of the rotor where torsional strain energy is present, wherein the torsional damper is composed of a vibration dampening material consisting of one of: particles; and droplets deposited on a surface of the rear cavity of the rotor.
16. The lightweight high speed rotor according to claim 15 , wherein said torsional damper comprises a mass of resilient material bonded to a surface of the rotor inside said rear cavity.
17. The lightweight high speed rotor according to claim 15 , wherein the rotor comprises a hub and a web joining the plurality of blades to the hub, the web and the hub being integral.
18. The lightweight high speed rotor according to claim 15 , wherein the surface of the rear cavity of the rotor includes one of: protrusions; ribs; fins; knurling; and grooves for bonding to the vibration dampening material.