Damper for an integrally bladed rotor
View Patent ↗A rotor comprises a disk having a rim. The rim has an axial face facing one of a forward or rearward direction. The rim defines a circumferential groove. A damper engages with the rim at both the axial face and the circumferential groove. The disk includes a rotor hub having a hub inner surface facing a longitudinal axis about which the rotor hub rotates. The rim is spaced radially outwardly relative to the hub inner surface. The axial face extends radially inwardly from the rim to the hub inner surface. The circumferential groove is formed within the hub inner surface. The damper comprises a split ring damper with a first leg mounted within the circumferential groove and a second leg that extends from the first leg, surrounds a radial lip of the hub inner surface, and extends radially outwardly to contact the axial face. An integrally bladed rotor is also disclosed.
1. A rotor comprising:
a disk having a rim, said rim having an axial face facing one of a forward or rearward direction, said rim defines a circumferential groove;
a damper engaged with said rim at both said axial face and said circumferential groove;
wherein said disk includes a rotor hub having a hub inner surface facing a longitudinal axis about which said rotor hub rotates and said rim being spaced radially outwardly relative to said hub inner surface, and wherein said axial face extends radially inwardly from said rim to said hub inner surface; and
wherein said circumferential groove is formed within said hub inner surface, and wherein said damper comprises a split ring damper with a first leg mounted within said circumferential groove and a second leg that extends from said first leg, surrounds a radial lip of said hub inner surface, and extends radially outwardly to contact said axial face.
2. The rotor as recited in claim 1 , wherein said axial face is a front face.
3. The rotor as recited in claim 1 , wherein said axial face is a rear face.
4. The rotor as recited in claim 1 , wherein said split ring damper is U-shaped in cross section.
5. The rotor as recited in claim 1 , wherein said second leg is longer than said first leg in a radial direction.
6. The rotor as recited in claim 1 , wherein said first leg is wider than said second leg in an axial direction.
7. The rotor as recited in claim 6 , wherein said circumferential groove is wider than said first leg in the axial direction.
8. The rotor as recited in claim 1 , wherein a distal end of said second leg includes a bulbed end that engages said axial face such that a remaining portion of said second leg is spaced from said axial face.
9. The rotor as recited in claim 1 , wherein a tab on the split ring damper engages a slot on the radial lip generally opposite a split in the split ring damper.
10. The rotor as recited in claim 1 , wherein the first leg extends to a distal tip that includes a plurality of radially inwardly extending scallops.
11. The rotor as recited in claim 1 , wherein the first leg includes a plurality of lightening apertures extending through a width of the first leg.
12. An integrally bladed rotor comprising:
a rotor hub that defines a hub face facing one of a forward or rearward direction and a hub inner surface with a circumferential groove within said hub inner surface;
a split ring damper mounted within said circumferential groove and in contact with said hub face;
wherein said split ring damper includes a first leg and a second leg, said first leg engaged within said circumferential groove and said second leg in contact with said hub face; and
wherein said second leg includes a multiple of radial slits.
13. The integrally bladed rotor as recited in claim 12 , wherein said first leg includes a multiple of scallops.
14. The integrally bladed rotor as recited in claim 12 , wherein said first leg includes a multiple of lightening apertures.
15. The integrally bladed rotor as recited in claim 12 , further comprising a hub rim opposite said hub inner surface, a multiple of airfoils integral with said hub rim.
16. The integrally bladed rotor as recited in claim 12 , wherein said split ring damper defines a coefficient of friction in the range of 0.20 to 0.60.
17. The integrally bladed rotor as recited in claim 12 , wherein said hub inner surface faces a longitudinal center axis about which said rotor hub rotates and wherein rotor hub includes an outer hub rim that is spaced radially outwardly relative to said hub inner surface, said outer hub rim supporting a plurality of airfoils, and wherein said hub face extends radially inwardly from said outer hub rim to said hub inner surface.
18. An integrally bladed rotor comprising:
a rotor hub that defines a hub face facing one of a forward or rearward direction and a hub inner surface with a circumferential groove within said hub inner surface;
a split ring damper mounted within said circumferential groove and in contact with said hub face;
wherein said hub inner surface faces a longitudinal center axis about which said rotor hub rotates and wherein rotor hub includes an outer hub rim that is spaced radially outwardly relative to said hub inner surface, said outer hub rim supporting a plurality of airfoils, and
wherein said circumferential groove is formed within said hub inner surface, and wherein said split ring damper includes a first leg mounted within said circumferential groove and a second leg that extends from said first leg, surrounds a radial lip of said hub inner surface, and extends radially outwardly to contact said hub face.
19. The integrally bladed rotor as recited in claim 18 wherein said hub face comprises a front face facing the forward direction.
20. The integrally bladed rotor as recited in claim 18 wherein said hub face comprises a rear face facing the rearward direction.