Methods and materials for forming in-situ cavities for silicon-based ceramic matrix composite components

US2016115086A1 · US · A1

Patent metadata
FieldValue
Publication numberUS-2016115086-A1
Application numberUS-201414893702-A
CountryUS
Kind codeA1
Filing dateApr 23, 2014
Priority dateMay 29, 2013
Publication dateApr 28, 2016
Grant date

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.

Methods and materials for forming in-situ features in a ceramic matrix composite component are described. The method of forming a ceramic matrix composite component with cooling features, comprises forming a preform tape, laying up said preform tape to a desired shape, placing a high-temperature resistant fugitive material insert of preselected geometry in the preform tape of the desired shape, compacting the preform tape of the desired shape, burning out the preform tape of the desired shape, melt infiltrating the desired shape, removing the high-temperature resistant insert to form the cooling features during one of the burning out or the melt infiltrating or following the burning out or the melt infiltrating.

First claim

Opening claim text (preview).

What is claimed is: 1 . A method of forming a ceramic matrix composite component with cooling features, comprising: forming a preform tape; laying up said preform tape to a desired shape; placing a high-temperature resistant fugitive material insert of preselected geometry in said preform tape of said desired shape; compacting said preform tape of said desired shape; burning out said preform tape of said desired shape; melt infiltrating said desired shape; and removing said high-temperature resistant insert to form said cooling features one of during or following one of said burning out or said melt infiltrating. 2 . The method of claim 1 , forming said high-temperature fugitive material resistant insert of one of boron nitride, silica, silicon oxide, boron nitride coated DAP polymer, Y 2 Si 2 O 7 rare earth oxides, boron nitride coated silicon oxide, carbon coated boron nitride, molybdenum wire, high refractories, or diamond powder. 3 . The method of claim 2 , said placing being by tape-cast placement, pre-formed tube placement, spraying, screen printing, rapid prototype polymer coated with boron nitride placement, and injection molding. 4 . The method of claim 1 , said removing being one of mechanical or chemical removal. 5 . The method of claim 1 , said removing being a chemical dissolution. 6 . The method of claim 1 , said removing occurring during said burning out or said melt infiltrating when said insert is formed of silicon oxide. 7 . The method of claim 1 , further comprising mechanically clearing said cooling features formed by said insert. 8 . The method of claim 1 , said melt infiltrating comprising inserting molten silicon at least 2600 degrees on said burned-out preform tape of preselected shape. 9 . The method of claim 1 , forming complex non-line of sight cooling features.

Assignees

Inventors

Classifications

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 US2016115086A1 cover?
Methods and materials for forming in-situ features in a ceramic matrix composite component are described. The method of forming a ceramic matrix composite component with cooling features, comprises forming a preform tape, laying up said preform tape to a desired shape, placing a high-temperature resistant fugitive material insert of preselected geometry in the preform tape of the desired shape,…
Who is the assignee on this patent?
Gen Electric
What technology area does this patent fall under?
Primary CPC classification C04B35/806. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Thu Apr 28 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).