Structure of multilayer component

US2016009053A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016009053-A1
Application numberUS-201414770518-A
CountryUS
Kind codeA1
Filing dateFeb 24, 2014
Priority dateFeb 27, 2013
Publication dateJan 14, 2016
Grant date

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

A structure of a multilayer component in which a rigid core material, a soft surface material, and a cushioned foam layer provided between the core material and the surface material are integrated, wherein the core material includes an exposed core material portion without having the surface material and the form layer, the exposed core material portion is obtained by cutting off at least the surface material to be eliminated, and a cutting assist portion that projects toward the surface material or toward an opposite side of the surface material to assist cutting off with a cutting tool is provided in a part of the core material on which the surface material is cut off.

First claim

Opening claim text (preview).

1 . A structure of a multilayer component in which a rigid core material, a soft surface material, and a cushioned foam layer provided between the core material and the surface material are integrated, wherein the core material includes an exposed core material portion without having the surface material and the foam layer, the exposed core material portion is obtained by cutting off at least the surface material to be eliminated, and a cutting assist portion that projects toward the surface material or toward an opposite side of the surface material to assist cutting off with a cutting tool is provided in a part of the core material on which the surface material is cut off. 2 . A structure of a multilayer component in which a rigid core material, a soft surface material, and a cushioned foam layer provided between the core material and the surface material are integrated, wherein the surface material includes a seam line portion formed by sewing, the core material includes an exposed core material portion without having the surface material and the foam layer, the exposed core material portion is obtained by cutting off the surface material along with the seam line portion to be eliminated, and a cutting assist portion that projects toward the surface material or toward an opposite side of the surface material to assist cutting off of the seam line portion with a cutting tool is provided in a part of the core material on which the seam line portion formed in the surface material is cut off. 3 . The structure of the multilayer component according to claim 2 , wherein the cutting assist portion is a tool receiving portion provided in a position facing the cutting tool to directly receive the cutting tool. 4 . A structure of a multilayer component in which a rigid core material, a soft surface material, and a cushioned foam layer provided between the core material and the surface material are integrated, wherein the surface material includes a seam line portion formed by sewing, the core material includes an exposed core material portion without having the surface material and the foam layer, the exposed core material portion is obtained by cutting off at least the surface material along with the seam line portion to be eliminated, the core material is provided with a cutting assist portion that projects toward the surface material to assist cutting off of the seam line portion with a cutting tool, the cutting assist portion includes a pair of seam line receiving bases provided on both sides of the position facing the cutting tool to sandwich and hold two positions of the seam line portion on both sides of a cutting off position of the seam line portion with an external seam line pressing holder, and at least one of the seam line receiving bases has a non-slip portion that prevents the surface material or the seam line portion from being slipped. 5 . The structure of the multilayer component according to claim 1 , wherein the multilayer component is a vehicle interior component. 6 . The structure of the multilayer component according to claim 2 , wherein the multilayer component is a vehicle interior component. 7 . The structure of the multilayer component according to claim 3 , wherein the multilayer component is a vehicle interior component. 8 . The structure of the multilayer component according to claim 4 , wherein the multilayer component is a vehicle interior component.

Assignees

Inventors

Classifications

  • by mechanical deformation, e.g. crushing, embossing, stretching · CPC title

  • Non-slip, anti-slip · CPC title

  • B32B5/18Primary

    characterised by features of a layer {of} foamed material · CPC title

  • Instrument panels · CPC title

  • Joining preformed parts by the expanding material · CPC title

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What does patent US2016009053A1 cover?
A structure of a multilayer component in which a rigid core material, a soft surface material, and a cushioned foam layer provided between the core material and the surface material are integrated, wherein the core material includes an exposed core material portion without having the surface material and the form layer, the exposed core material portion is obtained by cutting off at least the s…
Who is the assignee on this patent?
Calsonic Kansei Corp
What technology area does this patent fall under?
Primary CPC classification B32B5/18. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Thu Jan 14 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (A1). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).