Composite material
US-2017232708-A1 · Aug 17, 2017 · US
US9903433B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9903433-B2 |
| Application number | US-201414899679-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 24, 2014 |
| Priority date | Jul 3, 2013 |
| Publication date | Feb 27, 2018 |
| Grant date | Feb 27, 2018 |
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An anti-vibration structure includes an inner elastic body that is a separate body to a multi-layered material and that is disposed in a through-hole piercing through a layering direction of the multi-layered material, and a restricting member that has at least a portion embedded in the inner elastic body, that has one end coupled to an upper plate and another end coupled to a lower plate and that restricts separation of the upper plate and the lower plate.
Opening claim text (preview).
The invention claimed is: 1. An anti-vibration structure comprising: a multi-layered material in which a plurality of rigid hard plates and a plurality of soft plates with viscoelastic properties are layered alternately to each other; an upper plate and a lower plate that are respectively layered at each layering direction side of the multi-layered material; an inner elastic body that is a separate body from the multi-layered material and that is disposed in a through-hole piercing through the multi-layered material in the layering direction; and a restricting member that has at least a portion embedded in the inner elastic body, that has one end coupled to the upper plate and another end coupled to the lower plate, and that restricts separation of the upper plate and the lower plate, wherein the multi-layered material is pre-compressed in the layering direction by the restricting member when the restricting member is in a tensed state. 2. The anti-vibration structure of claim 1 , wherein the inner elastic body is pre-compressed by the restricting member. 3. The anti-vibration structure of claim 1 , wherein an outer circumferential face of the inner elastic body and an inner circumferential face of the multi-layered material abut each other without a gap due to the pre-compression. 4. The anti-vibration structure of claim 1 , wherein at least one of the through-hole or the inner elastic body has a tapered shape in which one end side in the layering direction has a smaller diameter. 5. The anti-vibration structure as claimed in claim 1 , wherein an outer circumferential face of the inner elastic body and an inner circumferential face of the multi-layered material abut each other due to the pre-compression. 6. The anti-vibration structure as claimed in claim 1 , wherein the restricting member includes annular shaped link pieces of an upper link, a center link, and a lower link, and the entirety of the center link is embedded in the inner elastic body, such that the inside of the annular shape of the center link is filled with the inner elastic body. 7. An anti-vibration structure comprising: a multi-layered material in which a plurality of rigid hard plates and a plurality of soft plates with viscoelastic properties are layered alternately to each other; an upper plate and a lower plate that are respectively layered at each layering direction side of the multi-layered material; an inner elastic body that is a separate body from the multi-layered material and that is disposed in a through-hole piercing through the multi-layered material in the layering direction; and a restricting member that has at least a portion embedded in the inner elastic body, that has one end coupled to the upper plate and another end coupled to the lower plate, and that restricts separation of the upper plate and the lower plate, wherein the inner elastic body is pre-compressed in the layering direction by the restricting member when the restricting member is in a tensed state. 8. A method of using an anti-vibration structure, wherein the anti-vibration structure comprises; a multi-layered material in which a plurality of rigid hard plates and a plurality of soft plates with viscoelastic properties are layered alternately to each other; an upper plate and a lower plate that are respectively layered at each layering direction side of the multi-layered material; an inner elastic body that is a separate body from the multi-layered material and that is disposed in a through-hole piercing through the multi-layered material in the layering direction; and a restricting member that has at least a portion embedded in the inner elastic body, that has one end coupled to the upper plate and another end coupled to the lower plate, and that restricts separation of the upper plate and the lower plate; and wherein the multi-layered material is pre-compressed in the layering direction by the restricting member when the restricting member is in a tensed state at an initial installation of the anti-vibration structure in a vehicle. 9. The method of using the anti-vibration structure of claim 8 , wherein the inner elastic body is pre-compressed by the restricting member. 10. The method of using the anti-vibration structure of claim 8 , wherein an outer circumferential face of the inner elastic body and an inner circumferential face of the multi-layered material abut each other without a gap due to the pre-compression. 11. The method of using the anti-vibration structure of claim 8 , wherein at least one of the through-hole or the inner elastic body has a tapered shape in which one end side in the layering direction has a smaller diameter. 12. The method of using the anti-vibration structure as claimed in claim 8 , wherein an outer circumferential face of the inner elastic body and an inner circumferential face of the multi-layered material abut each other due to the pre-compression. 13. The method of using the anti-vibration structure as claimed in claim 8 , wherein the restricting member includes annular shaped link pieces of an upper link, a center link, and a lower link, and the entirety of the center link is embedded in the inner elastic body, such that the inside of the annular shape of the center link is filled with the inner elastic body.
with rubber springs {(grommet- or bushing-type resilient mountings F16F1/3732, F16F1/38); with springs made of rubber and metal (arrangement of internal-combustion or jet-propulsion units B60K5/12; mounting of propulsion plants on vessels B63H21/30; mounting of vehicle drivers' cabs B62D33/0604)} · CPC title
consisting of a stack of similar elements separated by non-elastic intermediate layers {(F16F9/306 takes precedence; laminated constructions to protect buildings against abnormal external influences, e.g. earthquakes, E04H9/022)} · CPC title
using elastic means (single elements or their attachment F16F1/00 - F16F13/00); {(F16F15/023, F16F15/03 take precedence)} · CPC title
of the same material or the material not being specified · CPC title
with, or used as an end stop or buffer; Limiting excessive axial separation · CPC title
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