Claims
- 1. A damper for damping vibration of a structural member of a turbine engine, the structural member having a neutral axis and an annular extension, said damper comprising a damper ring comprising a generally axially extending outer surface having first and second axial ends, a generally axially extending inner surface, an annular stiffener extending from said inner surface, at least one first axial retainer extending radially outward from said first axial end of said outer surface, and at least one second axial retainer extending radially outward from said second axial end of said outer surface, said damper ring further comprising an annular extension protruding substantially axially from said annular stiffener, said damper ring having a neutral axis, and said axial retainers adaptable for mounting said damper ring on the annular extension of the structural member so that said neutral axis of said damper ring is radially spaced from the neutral axis of the structural member.
- 2. A damper in accordance with claim 1 wherein each of said first and second axial retainers comprises at least one extension extending radially outward from said first and second ends respectively.
- 3. A damper in accordance with claim 2 wherein said first and second axial retainers comprise a pair of continuous circumferential extensions.
- 4. A damper in accordance with claim 2 wherein said first and second axial retainers comprise a plurality of tabular extensions circumferentially aligned.
- 5. A damper in accordance with claim 2 wherein said first and second axial retainers comprise a plurality of tabular extensions circumferentially offset.
- 6. A damper in accordance with claim 1 wherein the structural member annular extension comprises a flange.
- 7. A damper in accordance with claim 1, wherein said damper ring is severed for enabling diametrical expansion and contraction thereof.
- 8. A damper for damping vibration of an annular structural member including a neutral axis and an annular flange, said damper comprising a damper ring comprising:
- a generally axially extending outer surface having first and second axial ends,
- a generally axially extending inner surface,
- an annular stiffener protruding radially inward from said inner surface so that said damper ring is stiffened,
- an annular extension protruding substantially axially from said annular stiffener, and
- a plurality of axial retainers comprising a plurality of circumferentially aligned tabular extensions protruding radially outward from said first and second ends of said outer surface so that relative axial movement between said damper ring and the flange is restricted, and
- said damper ring having a neutral axis and being severed for enabling diametrical expansion and contraction thereof, and
- said axial retainers adaptable for mounting said damper ring on the annular flange so that the neutral axis of said damper ring is radially spaced from the neutral axis of the structural member.
- 9. A damper for damping vibration of a structural member of a turbine engine, the structural member having a neutral axis and an annular extension, said damper comprising a damper ring comprising a generally axially extending outer surface having first and second axial ends, a generally axially extending inner surface, and an annular stiffener extending from said inner surface, a length of said annular stiffener selected to provide a preselected separation between neutral axes of the structural member and said damper.
- 10. A damper in accordance with claim 9 further comprising at least one first axial retainer extending radially outward from said first axial end of said outer surface, and at least one second axial retainer extending radially outward from said second axial end of said outer surface.
- 11. A damper in accordance with claim 10 wherein each of said first and second axial retainers comprises at least one extension extending radially outward from said first and second ends respectively.
- 12. A damper in accordance with claim 11 wherein said first and second axial retainers comprise a pair of continuous circumferential extensions.
- 13. A damper in accordance with claim 11 wherein said first and second axial retainers comprise a plurality of tabular extensions circumferentially aligned.
- 14. A damper in accordance with claim 11 wherein said first and second axial retainers comprise a plurality of tabular extensions circumferentially offset.
- 15. A damper in accordance with claim 9 wherein said damper ring further comprises an annular extension protruding substantially axially from said annular stiffener.
- 16. A damper in accordance with claim 10 wherein the structural member annular extension comprises a flange.
- 17. A damper in accordance with claim 9 wherein said damper ring is severed for enabling diametrical expansion and contraction thereof.
GOVERNMENT RIGHTS STATEMENT
The United States Government has rights in this invention pursuant to Contract No. F33657-88-C-2133 awarded by the Department of the Air Force.
US Referenced Citations (5)