Laminates of polysilazane and carbon fiber reinforced polymer

US11365705B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11365705-B2
Application numberUS-201816170966-A
CountryUS
Kind codeB2
Filing dateOct 25, 2018
Priority dateOct 25, 2018
Publication dateJun 21, 2022
Grant dateJun 21, 2022

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

Disclosed are laminates comprising a carbon fiber reinforced polymer sheet and a layer of polysilazane and methods for producing such laminates.

First claim

Opening claim text (preview).

What is claimed is: 1. A laminate comprising a sheet of carbon fiber reinforced polymer (CFRP), the sheet having a first side and a second side opposite the first side and at least one of the first side and the second side of the sheet is in electrical communication with a metal cellular core or a metal alloy cellular core; and a layer of polysilazane covering one or both of the first side and the second side of the sheet of CFRP, wherein the sheet of CFRP contains multiple perforations and at least one of the perforations extends entirely through the sheet, wherein the perforations include sidewalls and the sidewalls of the perforations are coated with polysilazane. 2. A laminate according to claim 1 , wherein the perforations have a diameter of from about 0.75 (0.03 in) to about 1.5 mm (0.06 in). 3. A laminate according to claim 2 , wherein the layer of polysilazane has a thickness of from about 1-10 μm. 4. A laminate according to claim 3 , wherein the perforations cover from about 5-20% of the first side of the sheet. 5. A laminate according to claim 4 , wherein the polysilazane is an inorganic polysilazane, an organic polysilazane, or a mixture thereof. 6. A laminate according to claim 5 , wherein the sheet of CFRP comprises exposed carbon fibers. 7. A laminate according to claim 6 , wherein the metal cellular core comprises aluminum. 8. A laminate according to claim 1 , wherein the sheet of CFRP comprises exposed carbon fibers. 9. A aircraft engine thrust reverser comprising a laminate according to claim 1 . 10. An aircraft engine thrust reverser according to claim 9 , wherein the metal cellular core comprises aluminum. 11. An aircraft engine thrust reverser according to claim 9 , wherein the perforations have a diameter of from about 0.75 (0.03 in) to about 1.5 mm (0.06 in). 12. An aircraft engine thrust reverser according to claim 11 , wherein the layer of polysilazane has a thickness of from about 1-10 μm. 13. A structure comprising a sheet of carbon fiber reinforced polymer (CFRP) coated with a discrete layer of a polysilazane, the sheet having a first side and a second side opposite the first side; a metal cellular core or a metal alloy cellular core in electrical communication with at least one of the first side and the second side of the sheet; and wherein the layer of polysilazane covers one or both of the first side and the second side of the sheet of CFRP, wherein the sheet of CFRP contains multiple perforations and at least one of the perforations extends entirely through the sheet, wherein the perforations include sidewalls and the sidewalls of the perforations are coated with polysilazane. 14. A structure according to claim 13 , wherein the perforations have a diameter of from about 0.75 (0.03 in) to about 1.5 mm (0.06 in). 15. A structure according to claim 14 , wherein the layer of polysilazane has a thickness of from about 1-10 μm. 16. A structure according to claim 15 , wherein the perforations cover from about 5-20% of the first side of the sheet. 17. A structure according to claim 16 , wherein the sheet of CFRP comprises exposed carbon fibers. 18. A structure according to claim 17 , wherein the metal cellular core or metal alloy cellular core comprises aluminum. 19. A structure according to claim 13 , wherein the perforations have a diameter of from about 1 mm (0.04 in) to about 1.25 mm (0.05 in). 20. A structure according to claim 14 , wherein the layer of polysilazane has a thickness of from about 2-3 μm.

Assignees

Inventors

Classifications

  • in which all the silicon atoms are connected by linkages other than oxygen atoms · CPC title

  • with only one layer of a composition containing a polymer binder (with more layers C08J7/042) · CPC title

  • Synthetic resin · CPC title

  • using interposed adhesives or interposed materials with bonding properties · CPC title

  • Water vapor barrier · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US11365705B2 cover?
Disclosed are laminates comprising a carbon fiber reinforced polymer sheet and a layer of polysilazane and methods for producing such laminates.
Who is the assignee on this patent?
Boeing Co
What technology area does this patent fall under?
Primary CPC classification F02K1/827. Mapped technology areas include Mechanical Engineering.
When was this patent published?
Publication date Tue Jun 21 2022 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).