Vibration-damping structural member
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorDavid J. Barrett
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Abstract
A structural element or member is disclosed that resists or damps vibration rom 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.
Claims4
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.
Dependencies are inferred from the claim text.