Panel structure
US-9688050-B2 · Jun 27, 2017 · US
US10647083B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10647083-B2 |
| Application number | US-201715628055-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 20, 2017 |
| Priority date | Jun 18, 2004 |
| Publication date | May 12, 2020 |
| Grant date | May 12, 2020 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A panel structure and a method of forming the panel structure are disclosed. The panel structure typically includes at least one panel associated with a material. The panel structure has been found particularly advantageous for use as an interior panel of an airplane.
Opening claim text (preview).
What is claimed is: 1. An interior panel structure of a transportation vehicle, comprising: a first panel formed at least partially of a plastic material; a second panel formed at least partially of a porous material, the second panel being an outer panel that is closer to a body of the transportation vehicle than the first panel while the first panel is closer to an interior cabin of the transportation vehicle; and an activatable material intermediate the first panel and the second panel, the activatable material softens, expands, and cures upon exposure to heat; wherein a volume is defined between the first panel and the second panel and wherein the activatable material when activated, fills from about 5% to about 90% of the volume, and wherein the interior panel structure, when assembled and in use, provides at least one functional attribute selected from reinforcement, baffling, sound absorption, sound attenuation, baffling or sealing. 2. The interior panel structure as in claim 1 , wherein the transportation vehicle is an airplane and the body of the transportation vehicle is a fuselage of the airplane. 3. The interior panel structure as in claim 1 , wherein the activatable material is part of a composite that includes a support having a plurality of openings. 4. The interior panel structure as in claim 1 , wherein the activatable material is epoxy-based. 5. The interior panel structure as in claim 1 , wherein the activatable material is a thermoset, a thermoplastic or a combination thereof. 6. The interior panel structure as in claim 1 , wherein the activatable material is adhered to either the first panel or the second panel. 7. The interior panel structure as in claim 1 , wherein the first panel is formed of an epoxy/glass composite. 8. The interior panel structure as in claim 1 , wherein space is formed between the activatable material when activated and the first panel. 9. The interior panel structure as in claim 3 , wherein the support is a honeycomb structure located between the first and second panel. 10. The interior panel structure as in claim 9 , wherein expansion of the activatable material provides adhesion between at least one of the panels and the support. 11. The interior panel structure as in claim 1 , wherein the activatable material when activated has a compressive strength of about 1.5 MPa or greater. 12. A method of forming an interior panel structure of a transportation vehicle, comprising: providing a first panel formed at least partially of a plastic material, the first panel being an inner panel at least partially defining an interior cabin of the transportation vehicle; providing a second panel formed at least partially of a porous material, the second panel being an outer panel that is closer to a body of the transportation vehicle than the first panel; locating an activatable material that softens, expands, and cures upon exposure to heat and a support intermediate the first panel and the second panel; and exposing the activatable material to an elevated temperature for activating the activatable material to expand and form a foam whereby the interior panel structure, when assembled and in use, provides a functional attribute selected from reinforcement, baffling, sound absorption, sound attenuation, baffling or sealing to the panel structure, wherein a volume is defined between the first panel and the second panel and wherein the activatable material when activated, fills from about 5% to about 90% of the volume. 13. The method as in claim 12 , wherein a volume is defined between the first panel and the second panel and wherein the foam, the support or both fill at least about 15% of the volume but less than about 75% of the volume. 14. The method as in claim 12 , wherein the first panel is formed of an epoxy/glass composite. 15. The method as in claim 12 , wherein, upon expansion, the activatable material expands to a volume that is at least 500% greater than its original unexpanded volume. 16. The method as in claim 12 , wherein the support is a honeycomb structure located between the first and second panel having a plurality of openings for receiving the activatable material. 17. The method as in claim 16 , wherein a plurality of spaces are formed between the foam in each of the plurality of openings and the first panel. 18. The method as in claim 12 , wherein a plurality of spaces are formed between the activatable material when activated and the first panel. 19. The method as in claim 12 , wherein expansion of the activatable material provides adhesion between at least one of the panels and the support.
Insulating · CPC title
Containers; Receptacles · CPC title
foamed in situ · CPC title
Walls, e.g. building panels · CPC title
Dimensional properties · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.