Unitary Deflection Member for Making Fibrous Structures Having Increased Surface Area and Process for Making Same

US2016354979A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016354979-A1
Application numberUS-201615132295-A
CountryUS
Kind codeA1
Filing dateApr 19, 2016
Priority dateMay 1, 2015
Publication dateDec 8, 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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  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, the method comprising the steps of: a. providing an additive manufacturing making apparatus; b. providing at least one material for the unitary deflection member, 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 and at least one protuberance of the unitary deflection member; d. optionally, 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. 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 objects further include transition portions and forming portions on said at least one protuberance, and the digitized file describes a unitary deflection member comprising a plurality of regularly spaced protuberances extending from said reinforcing member, at least two of said protuberances being 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. 5 . 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. 6 . The method for making a unitary deflection member of claim 5 , 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. 7 . The method for making a unitary deflection member of claim 5 , 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. 8 . A method for making a unitary deflection member, the method comprising the steps of: a. providing an additive manufacturing making apparatus; b. providing at least one material for the unitary deflection member, 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 and at least one protuberance of the unitary deflection member; d. optionally, 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. 9 . The method for making a unitary deflection member of claim 8 , wherein the additive manufacturing making apparatus is a 3-D printer. 10 . The method for making a unitary deflection member of claim 8 , 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. 11 . The method for making a unitary deflection member of claim 8 , wherein the objects further include transition portions and forming portions on said at least one protuberance, and the digitized file describes a unitary deflection member comprising a plurality of regularly spaced protuberances extending from said reinforcing member, at least two of said protuberances being 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. 12 . The method for making a unitary deflection member of claim 8 , 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. 13 . The method for making a unitary deflection member of claim 12 , 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. 14 . The method for making a unitary deflection member of claim 12 , 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. 15 . A method for making a unitary deflection member, the method comprising the steps of: a. providing 3-D printer apparatus; b. providing at least one material for the unitary deflection member, 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 and at least one protuberance having transition portions and forming portions; d. optionally, 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. 16 . The method for making a unitary deflection member of claim 15 , 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. 17 . The method for making a unitary deflection member of claim 15 , wherein the digitized file describes a unitary deflection member comprising a plurality of regularly spaced protuberance

Assignees

Inventors

Classifications

  • Processes of additive manufacturing · CPC title

  • Products made by additive manufacturing · CPC title

  • Cellulose series · CPC title

  • Substantially impermeable for transferring fibrous webs · CPC title

  • by fluid jet · CPC title

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What does patent US2016354979A1 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 Thu Dec 08 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).