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US5087491A
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Vibration-damping structural member
Assignee: United States Department of the Navy
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Filing: 1990-02-09
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Granted: 1992-02-11
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Expires: 2010-02-09
Abstract
Abstract A structural element or member is disclosed that resists or damps vibrationrom loads applied along a given axis without significantly sacrificing stiffness, through the use of stress coupling within an anisotropic material. Essentially, the structural member comprises alternating layers or laminates of stiff and viscoelastic or damping material bonded together to form a laminated structrue. The laminated structural member is oriented to receive the applied load in a direction that is parallel to the laminates. At least one of the stiff laminates shows anisotropic behavior when acted upon by the axial load, causing shear strain and concomitant transverse displacement therewithin, thereby loading the viscoelastic laminate in shear.
Inventors
- 👤 David J. Barrett
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-29 20:05
CPC Classifications
F; F16; F16F; F16F1/00; F16F1/36; F16F1/371; B; B32; B32B; B32B1/00; B32B1/08; B32B15/00; B32B15/04; B32B15/10; B32B21/00; B32B21/04; B32B21/08; B32B21/13; B32B7/00; B32B7/02; B32B7/022; B32B7/04; B32B7/12; F16F3/00; F16F3/08; B32B2307/00; B32B2307/50; B32B2307/56; B32B2307/70; B32B2307/706; B32B2315/00; B32B2315/02; B32B2317/00; B32B2317/16; B32B2363/00; Y; Y10; Y10T; Y10T428/00; Y10T428/13; Y10T428/131; Y10T428/1314; Y10T428/24; Y10T428/24942; Y10T428/24992; Y10T428/30; Y10T428/31504; Y10T428/31511; Y10T428/31515; Y10T428/31518; Y10T428/31855; Y10T428/3188; Y10T428/31895
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
138 words
A laminated structural member in the shape of a cylinder which supports axial loads which are colinear with the cylinder's axis and damps vibrations therefrom, comprising at least one cylindrical layer of viscoelastic material bonded on the outside thereof to a first cylindrical layer of orthotropic load-bearing material and on the inside thereof to a second cylindrical layer of orthotropic load-bearing material, said first orthotropic load-bearing layer having its preferred direction of stiffness at a first angle with respect to the cylinder's axis and said second orthotropic load-bearing layer having its preferred direction of stiffness at a second opposite angle with respect to the cylinder's axis, whereby the axial load causes said first and second load-bearing layers to displace circumferentially and in opposite relative directions, thereby shearing said viscoelastic layer in a direction transverse to the axial load.
Claim 2
Dependent Claim
138 words
A laminated structural member in the shape of a cylinder which supports axial loads which are colinear with the cylinder's axis and damps vibrations therefrom, comprising at least one cylindrical layer of viscoelastic material bonded on the outside thereof to a first cylindrical layer of orthotropic load-bearing material and on the inside thereof to a second cylindrical layer of orthotropic load-bearing material, said first orthotropic load-bearing layer having its preferred direction of stiffness at a first angle with respect to the cylinder's axis and said second orthotropic load-bearing layer having its preferred direction of stiffness at a second opposite angle with respect to the cylinder's axis, whereby the axial load causes said first and second load-bearing layers to displace circumferentially and in opposite relative directions, thereby shearing said viscoelastic layer in a direction transverse to the axial load.
Claim 3
Dependent Claim
14 words
The laminated structural member of claim 1 wherein said viscoelastic material is an adhesive.
Claim 4
Dependent Claim
14 words
The laminated structural member of claim 1 wherein said orthotropic load-bearing material is graphite/epoxy.
Claim 5
Dependent Claim
63 words
The laminated structural member of claim 1, further comprising a plurality of additional cylindrical layers of alternately viscoelastic and orthotropic load-bearing material bonded to the outside of said first cylindrical layer of orthotropic load-bearing material, each successive outer additional orthotropic load-bearing layer having its preferred direction of stiffness at an opposite angle with respect to the cylinder's axis as the previous orthotropic layer.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1995-02-10 | 1995-08-12 | 1996-02-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-02-10 | 1999-08-12 | 2000-02-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-02-10 | 2003-08-12 | 2004-02-11 | $7700.00 | Window Closed / Lapsed |