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US 12,498,186 B2Granted
Transpirational cooling panel
AssigneeThe Boeing Company
InventorRobert A. DiChiara, Jr.
Life of this patent
Estimating the term…
Abstract
A transpirational cooling panel comprises a porous ceramic matrix composite layer and a porous high-temperature fabric layer. A machined ceramic fiber batting is located between the porous ceramic matrix composite layer and the porous high-temperature fabric layer. A ceramic stitching joins the porous ceramic matrix composite layer and the porous high-temperature fabric layer through the machined ceramic fiber batting.
Claims13
A method of manufacturing a transpirational cooling panel, the method comprising
- saturating one or more layers of a precursor ceramic fiber batting material with a polymer solution;
- compressing the precursor ceramic fiber batting material comprising the polymer solution;
- evaporating solvent from the precursor ceramic fiber batting material to form a ceramic batting/polymer intermediate;
- machining the ceramic batting/polymer intermediate;
- placing a ceramic fabric layer adjacent to the machined ceramic batting/polymer intermediate;
- placing a porous high-temperature fabric layer adjacent to the machined ceramic batting/polymer intermediate on an opposite side of the machined ceramic batting/polymer intermediate as the ceramic fabric layer;
- stitching the ceramic fabric layer to the porous high-temperature fabric layer through the machined ceramic batting/polymer intermediate using a ceramic thread to form a pre-panel structure;
- heating the pre-panel structure to remove the polymer from within the machined ceramic batting/polymer intermediate after stitching the pre-panel structure;
- forming a ceramic matrix composite skin that incorporates the ceramic fabric layer of the pre-panel structure, by
- adding a solution comprising a suspension of ceramic particles and an organic component to the ceramic fabric layer of the pre-panel structure,
- applying a first heating cycle to cure the organic component in the ceramic fabric layer, and
- applying a second heating cycle to sinter the ceramic particles and to remove the organic component cured thereby forming pores in the ceramic matrix composite skin;
- and
- coupling the porous high-temperature fabric layer to a carrier panel including one or more openings configured to pass cooling air.
11 more elements
Dependencies are inferred from the claim text.