Composite passive damping struts for large precision structures
AssigneeThe United States of America as represented by the Administrator of the National Aeronautics and Space Administration
InventorBenjamin P. Dolgin
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Abstract
In the field of viscoelastic dampers, a new strut design comprises a viscoelastic material sandwiched between multiple layers, some of which layers bear and dampen load force. In one embodiment, the layers are composite plies of opposing orientation. In another embodiment, the strut utilizes a viscoelastic layer sandwiched between V-shaped composite plies. In a third embodiment, a viscoelastic layer is sandwiched between sine-shaped plies. Strut strength is equal to or greater than conventional aluminum struts due to the unique high interlaminar shear ply design.
Claims11
An energy absorbing strut, comprising at least two tubular members disposed one inside the other, said tubular members being separated by a viscoelastic material for bearing stress when a load force is applied to the strut, at least two of said tubular members being reactively designed such that some of said load force applied to the strut ma be dampened by a combined action of the reactive tubular members, wherein the tubular members surrounding the viscoelastic material experience interlaminar shear when the load force is applied, all of said tubular members being laminate reactive tubular members having a composite ply, and the composite ply of each of said laminate tubular members surrounding said viscoelastic material having an opposing orientation to the composite ply of the tubular member inside said viscoelastic material.
An energy absorbing strut, comprising two composite ply tubular members disposed one inside the other, said composite ply tubular members being separated by a viscoelastic material for bearing stress when a load force is applied to the strut, said composite ply tubular members being reactively designed such that some of said load force applied to the strut may be dampened by a combined action of the reactive composite ply tubular members, and wherein each reactive composite ply tubular member surrounding the viscoelastic material has a ply orientation, the orientation of one opposing the orientation of the other such that the viscoelastic material between the composite ply tubular members experiences a change in interlaminar shear when the load force is applied and at least one of said reactive composite ply tubular members is a V-shaped ply.
An energy absorbing strut, comprising two composite ply tubular members disposed one inside the other, said tubular members being separated by a viscoelastic material for bearing stress when a load force is applied to the strut, said composite ply tubular members being reactively designed such that some of said load force applied to the strut may be dampened by a combined action of the reactive composite ply tubular members, and wherein each reactive composite ply tubular member surrounding the viscoelastic material has a ply orientation, the orientation of one opposing the orientation of the other such that the viscoelastic material between the composite ply tubular members experiences a change in interlaminar shear when the load force is applied and at least one of said reactive tubular members is a sine-shaped ply.
An energy absorbing strut, comprising two composite ply tubular members disposed one inside the other, said composite ply tubular members being separated by a viscoelastic material for bearing stress when a load force is applied to the strut, said tubular members being reactively designed such that some of said load force applied to the strut may be dampened by a combined action of the reactive composite ply tubular members, and wherein each reactive composite ply tubular member surrounding the viscoelastic material has a ply orientation, the orientation of one opposing the orientation of the other such that the viscoelastic material between the composite ply tubular members experiences a change in interlaminar shear when the load force is applied and at least one of said reactive tubular members is a metallic cylinder having chevron-shaped grooves.
An energy absorbing apparatus, comprising:
- (a) a first layer including a composite ply having a first orientation;
- (b) a second layer including a composite ply having a second orientation opposing said first orientation such that said first and second layers experience interlaminar shear when a load is applied to the apparatus;
- and
- (c) a viscoelastic layer disposed between said first and second layers such that stress is borne by said viscoelastic layer when a load is applied to the apparatus.
Dependencies are inferred from the claim text.