Unitary deflection member for making fibrous structures having increased surface area and process for making same

US10933577B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10933577-B2
Application numberUS-201615132295-A
CountryUS
Kind codeB2
Filing dateApr 19, 2016
Priority dateMay 1, 2015
Publication dateMar 2, 2021
Grant dateMar 2, 2021

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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 unitary deflection member and a method for making a unitary deflection member is disclosed. The method can include the steps of: providing an additive manufacturing making apparatus; providing a material for the unitary deflection member, the material being compatible for use with the additive manufacturing making apparatus; generating a 3-D digital image of objects in a repeat element of the unitary deflection member, the objects including at least a reinforcing member and at least one protuberance of the unitary deflection member; assembling the objects into a digitized file including the at least one protuberance being on said reinforcing member; importing the digitized file to make numerical control file; and depositing the material using the additive manufacturing making apparatus to make the unitary deflection member.

First claim

Opening claim text (preview).

What is claimed is: 1. A method for making a unitary deflection member that is utilized for making fibrous webs, the method comprising the steps of: a. providing an additive manufacturing making apparatus; b. providing at least one material for the unitary deflection member that is utilized for making fibrous webs, the material being compatible for use with the additive manufacturing making apparatus; c. generating a 3-D digital image of objects in a repeat element of the unitary deflection member, the objects including at least a reinforcing member comprising a first plurality MD-oriented elements along an MD axis and a second plurality of CD-oriented elements along a CD axis, the MD and CD-oriented elements being unitary with each other and also being unitary with a plurality of regularly spaced protuberances of the unitary deflection member, such that, in cross-section, the MD and CD-oriented elements and the plurality of protuberances are a single unit not formed from separate parts, wherein the regularly spaced protuberances extend from the reinforcing member in a Z direction and at least two of said protuberances are similar in size and shape, each said protuberance having a transition portion having a transition portion width and a forming portion having a forming portion width, and wherein the transition portion width is less than the forming portion width; d. assembling the objects into a digitized file including the at least one protuberance being on said reinforcing member; e. importing the digitized file to make a numerical control file of the additive manufacturing making apparatus; and f. depositing the material using the additive manufacturing making apparatus to make the unitary deflection member that is utilized for making fibrous webs. 2. The method for making a unitary deflection member of claim 1 , wherein the additive manufacturing making apparatus is a 3-D printer. 3. The method for making a unitary deflection member of claim 1 , wherein the digitized file describes a unitary deflection member having at least two of said protuberances are adjacent one another and separated by a void defining a deflection conduit. 4. The method for making a unitary deflection member of claim 1 , wherein the digitized file describes a reinforcing member defining an X-Y plane, and a plurality of regularly spaced protuberances, wherein each protuberance has a three-dimensional shape such that any cross-sectional area of the protuberance parallel to the X-Y plane has an equal or lesser area than any cross-sectional area of the protuberance being a greater distance from the X-Y plane in the Z-direction. 5. The method for making a unitary deflection member of claim 4 , wherein the plurality of regularly spaced protuberances are discrete units disposed in a regular, spaced apart configuration in both the MD and CD, each discrete unit having a cross-sectional shape, the cross-sectional shape being selected from key-hole-shaped, mushroom-shaped, circular, oval, inverted triangle, T-shaped, inverted L-shaped, egg- or pebble-shaped, and combinations thereof. 6. The method for making a unitary deflection member of claim 4 , wherein the plurality of regularly spaced protuberances are disposed in a regular, spaced apart configuration of discrete units in the X-Y plane and distributed in both the MD and CD in a regular, spaced pattern. 7. A method for making a unitary deflection member that is utilized for making fibrous webs, the method comprising the steps of: a. providing an additive manufacturing making apparatus; b. providing at least one material for the unitary deflection member that is utilized for making fibrous webs, the material being compatible for use with the additive manufacturing making apparatus; c. generating a 3-D digital image of objects in an element of the unitary deflection member, the objects including at least a reinforcing member comprising a first plurality MD-oriented elements along an MD axis and a second plurality of CD-oriented elements along a CD axis, the MD and CD-oriented elements being unitary with each other and also being unitary with a plurality of regularly spaced protuberances of the unitary deflection member, such that, in cross-section, the MD and CD-oriented elements and the plurality of protuberances are a single unit not formed from separate parts, wherein the regularly spaced tuberances extend from the reinforcing member in a Z-direction and at least two of said protuberances are similar in size and shape, each said protuberance having a transition portion having a transition portion width and a forming portion having a forming portion width, and wherein the transition portion width is less than the forming portion width; d. assembling the objects into a digitized file including the at least one protuberance being on said reinforcing member; e. importing the digitized file to make a numerical control file of the additive manufacturing making apparatus; and f. depositing the material using the additive manufacturing making apparatus to make the unitary deflection member that is utilized for making fibrous webs. 8. The method for making a unitary deflection member of claim 7 , wherein the additive manufacturing making apparatus is a 3-D printer. 9. The method for making a unitary deflection member of claim 7 , wherein the digitized file describes a unitary deflection member having at least two of said protuberances are adjacent one another and separated by a void defining a deflection conduit. 10. The method for making a unitary deflection member of claim 7 , wherein the digitized file describes a reinforcing member defining an X-Y plane, and a plurality of regularly spaced protuberances, wherein each protuberance has a three-dimensional shape such that any cross-sectional area of the protuberance parallel to the X-Y plane has an equal or lesser area than any cross-sectional area of the protuberance being a greater distance from the X-Y plane in the Z-direction. 11. The method for making a unitary deflection member of claim 10 , wherein the plurality of regularly spaced protuberances are discrete units disposed in a regular, spaced apart configuration in both the MD and CD, each discrete unit having a cross-sectional shape, the cross-sectional shape being selected from key-hole-shaped, mushroom-shaped, circular, oval, inverted triangle, T-shaped, inverted L-shaped, egg- or pebble-shaped, and combinations thereof. 12. The method for making a unitary deflection member of claim 10 , wherein the plurality of regularly spaced protuberances are disposed in a regular, spaced apart configuration of discrete units in the X-Y plane and distributed in both the MD and CD in a regular, spaced pattern. 13. A method for making a unitary deflection member that is utilized for making fibrous webs, the method comprising the steps of: a. providing 3-D printer apparatus; b. providing at least one material for the unitary deflection member that is utilized for making fibrous webs, the material being compatible for use with the additive manufacturing making apparatus; c. generating a 3-D digital image of objects in an element of the unitary deflection member, the objects including at least a reinforcing member comprising a first plurality MD-oriented elements along an MD axis and a second plurality of CD-oriented elements along a CD axis, the MD and CD-oriented elements being unitary with each other and also being unitary with a plurality of regularly spaced protuberances, such that, in cross-section, the MD and CD-oriented elements and the plurality of protuberances are a single unit not formed from separate parts, wherein the regularly spaced tu

Assignees

Inventors

Classifications

  • B29C64/00Primary

    Additive manufacturing, i.e. manufacturing of three-dimensional [3D] objects by additive deposition, additive agglomeration or additive layering, e.g. by 3D printing, stereolithography or selective laser sintering · CPC title

  • Making patterned paper · CPC title

  • Felts · CPC title

  • Fibre-rearranging devices · CPC title

  • Substantially impermeable for transferring fibrous webs · CPC title

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Frequently asked questions

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What does patent US10933577B2 cover?
A unitary deflection member and a method for making a unitary deflection member is disclosed. The method can include the steps of: providing an additive manufacturing making apparatus; providing a material for the unitary deflection member, the material being compatible for use with the additive manufacturing making apparatus; generating a 3-D digital image of objects in a repeat element of the…
Who is the assignee on this patent?
Procter & Gamble
What technology area does this patent fall under?
Primary CPC classification B29C64/00. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Mar 02 2021 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 12 related publications on this page (citations in our corpus or others sharing the same primary CPC).