Method for fabricating thermoplastic sandwich structural panel using thermoforming and compression molding

US10828822B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10828822-B2
Application numberUS-201815892920-A
CountryUS
Kind codeB2
Filing dateFeb 9, 2018
Priority dateAug 4, 2016
Publication dateNov 10, 2020
Grant dateNov 10, 2020

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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 method for making a structural sandwich panel includes the steps of positioning a first and second thermoplastic skin elements in overlying relationship with respect to a heated male and heated female die molds respectively. A first pressure reduction is applied between the first thermoplastic skin element and the heated male die mold and a second pressure reduction is applied between the second thermoplastic and the heated female die mold. A core panel element is positioned between the heated male die mold and the heated female die mold wherein the core panel element has a first adhesive on a first side and has a second adhesive on a second opposing side. The male and female die molds are closed and exert a pressure onto the core panel element to secure the first and second thermoplastic skin elements to the core panel element and form the core panel element.

First claim

Opening claim text (preview).

What is claimed: 1. A method for making a structural sandwich panel, comprising the steps of: positioning a first thermoplastic skin element in overlying relationship with respect to a heated male die mold of a matched die mold apparatus; applying a first pressure reduction between the first thermoplastic skin element and the heated male die mold forming the first thermoplastic skin element to a shape of the heated male die mold; positioning a second thermoplastic skin element in overlying relationship with respect to a heated female die mold of the matched die mold apparatus; applying a second pressure reduction between the second thermoplastic skin element and the heated female die mold forming the second thermoplastic skin element to a shape of the heated female die mold; positioning a core panel element between the heated male die mold and the heated female die mold wherein a first adhesive is positioned on a first side of the core panel element and a second adhesive is positioned on a second opposing side of the core panel element with the first side of the core panel element facing the first thermoplastic skin element and the second opposing side of the core panel element facing the second thermoplastic skin element; and closing the heated male and female die molds exerting a pressure onto the core panel element securing the first and second thermoplastic skin elements to the core panel element and further forming the first side of the core panel element to a shape corresponding to the shape of the heated male die mold and forming the second opposing side of the core panel element to a shape corresponding to the shape of the heated female die mold. 2. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the first thermoplastic skin element further includes securing the first thermoplastic skin element in a first frame assembly. 3. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the first thermoplastic skin element includes positioning the first thermoplastic skin element comprising at least one layer of material of a homogeneous construction comprising a resin of one of polyphenylsulfone, polyetherimide, polycarbonate, polyether ether ketone, acrylonitrile butadiene styrene, polyetherketoneketone or acrylic-polyvinyl chloride. 4. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the first thermoplastic skin element includes positioning the first thermoplastic skin element comprising at least one layer of material comprising a fiber reinforced resin wherein: the resin comprises one of polyphenylsulfone, polyetherimide, polycarbonate, polyether ether ketone, acrylonitrile butadiene styrene, polyetherketoneketone or acrylic-polyvinyl chloride and the fiber comprises one of fiberglass or carbon. 5. The method for making the structural sandwich panel of claim 1 , wherein the first thermoplastic skin element comprises construction of one to three layers. 6. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the first thermoplastic skin element further includes heating the first thermoplastic skin element to a temperature in a range which includes five hundred degrees Fahrenheit (500° F.) up to and including seven hundred degrees Fahrenheit (700° F.). 7. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the second thermoplastic skin element further includes securing the second thermoplastic skin in a second frame assembly. 8. The method for making the structural sandwich panel of claim 1 , the step of positioning the second thermoplastic skin element includes positioning the second thermoplastic skin element comprising at least one layer of material of a homogeneous construction comprising a resin of one of polyphenylsulfone, polyetherimide, polycarbonate, polyether ether ketone, acrylonitrile butadiene styrene, polyetherketoneketone or acrylic-polyvinyl chloride. 9. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the second thermoplastic skin element includes: positioning the second thermoplastic skin element comprising at least one layer of material comprising a fiber reinforced resin wherein: the resin comprises one of polyphenylsulfone, polyetherimide, polycarbonate, polyether ether ketone, acrylonitrile butadiene styrene, polyetherketoneketone or acrylic-polyvinyl chloride and the fiber comprises one of fiberglass or carbon. 10. The method for making the structural sandwich panel of claim 1 , wherein the second thermoplastic skin element comprises a construction of one layer up three layers. 11. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the second thermoplastic skin element further includes heating the second thermoplastic skin element to a temperature in a range which includes five hundred degrees Fahrenheit (500° F.) up to and including seven hundred degrees Fahrenheit (700° F.). 12. The method for making a structural sandwich panel of claim 1 , wherein the step of positioning the core panel element includes the step of positioning the core panel element constructed of one of aluminum, polypropylene, polycarbonate, polyethylene or fiber reinforced aramid core with thermoset phenolic resin. 13. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the core panel element includes the step of positioning the core panel element having a foam construction of one of an open or closed cell and one of polyethelene teraphalate, polyphenylsulfone, polyetherimide of polyvinyl chloride. 14. The method for making the structural sandwich panel of claim 1 , wherein the step of positioning the core panel element includes the step of positioning the core panel element with a first and second adhesive comprising one of a film or a liquid adhesive. 15. The method for making the structural sandwich panel of claim 1 , further includes a step of heating a male and female die molds to a temperature in a temperature range which includes two hundred and eighty degrees Fahrenheit (280° F.) up to and including three hundred and twenty degrees Fahrenheit (320° F.) resulting in the heated male die mold and the heated female die mold. 16. The method for making the structural sandwich panel of claim 1 , wherein the step of closing the heated male and female die molds includes the heated male and female die molds exerting a pressure in a range which includes fourteen pounds per square inch (14 psi) up to and including one hundred pounds per square inch (100 psi). 17. The method for making the structural sandwich panel of claim 1 , wherein: the step of applying a first pressure reduction between the first thermoplastic skin element and the heated male die mold and the step of applying a second pressure reduction between the second thermoplastic skin element and the heated female die mold each has a first time duration in a range which includes thirty (30) seconds up to and including sixty (60) seconds; and the step of closing the heated male and female die molds and exerting a pressure onto the core panel element has a second time duration in a range which includes thirty (30) seconds up to and including sixty (60) seconds. 18. The method for making the structural sandwich panel of claim 1 , further including at least one step of: positioning one of a gel or coating onto the heated male die mold prior to th

Assignees

Inventors

Classifications

  • Opening, closing or clamping means · CPC title

  • Twin sheet thermoforming, i.e. deforming two parallel opposing sheets or foils at the same time by using one common mould cavity and without welding them together during thermoforming (B29C51/267, B29C49/0691 take precedence) · CPC title

  • for making articles having hollow walls · CPC title

  • the preformed layer being a lining, e.g. shaped in the mould before compression moulding, or a preformed shell adapted to the shape of the mould · CPC title

  • of moulds or mould parts · CPC title

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What does patent US10828822B2 cover?
A method for making a structural sandwich panel includes the steps of positioning a first and second thermoplastic skin elements in overlying relationship with respect to a heated male and heated female die molds respectively. A first pressure reduction is applied between the first thermoplastic skin element and the heated male die mold and a second pressure reduction is applied between the sec…
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification B29C51/36. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Nov 10 2020 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 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).