The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.
The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.
Patent No.:
Date of Patent:
Sep. 11, 2018
Filed:
Dec. 06, 2013
Applicant:
The Boeing Company, Seal Beach, CA (US);
Inventors:
Brian Lee Muench, Huntington Beach, CA (US);
Morris Dahmen, Huntington Beach, CA (US);
Assignee:
THE BOEING COMPANY, Chicago, IL (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
C03B 29/00 (2006.01); B29C 65/00 (2006.01); B44C 1/165 (2006.01); B44C 1/17 (2006.01); B32B 37/00 (2006.01); C09J 5/04 (2006.01); B32B 5/32 (2006.01); C04B 35/488 (2006.01); B32B 3/30 (2006.01); B32B 7/12 (2006.01); B32B 18/00 (2006.01); B32B 37/12 (2006.01); C04B 37/00 (2006.01); F01D 11/24 (2006.01); F23R 3/00 (2006.01); F28F 3/12 (2006.01); C04B 38/00 (2006.01); F28F 21/04 (2006.01); C04B 111/28 (2006.01);
U.S. Cl.
CPC ...
B32B 5/32 (2013.01); B32B 3/30 (2013.01); B32B 7/12 (2013.01); B32B 18/00 (2013.01); B32B 37/1284 (2013.01); C04B 35/488 (2013.01); C04B 37/008 (2013.01); C04B 38/008 (2013.01); F01D 11/24 (2013.01); F23R 3/007 (2013.01); F28F 3/12 (2013.01); B32B 2250/02 (2013.01); B32B 2250/22 (2013.01); B32B 2605/18 (2013.01); C04B 2111/28 (2013.01); C04B 2237/341 (2013.01); C04B 2237/343 (2013.01); C04B 2237/36 (2013.01); C04B 2237/361 (2013.01); C04B 2237/368 (2013.01); C04B 2237/38 (2013.01); C04B 2237/385 (2013.01); C04B 2237/592 (2013.01); C04B 2237/62 (2013.01); C04B 2237/708 (2013.01); C04B 2237/72 (2013.01); C04B 2237/88 (2013.01); F05D 2240/11 (2013.01); F05D 2260/204 (2013.01); F05D 2300/514 (2013.01); F05D 2300/6033 (2013.01); F05D 2300/612 (2013.01); F23M 2900/05004 (2013.01); F23R 2900/00018 (2013.01); F28F 21/04 (2013.01); F28F 2275/025 (2013.01); Y02T 50/672 (2013.01); Y02T 50/675 (2013.01); Y10T 156/10 (2015.01); Y10T 428/24496 (2015.01);
Abstract
A method of forming a ceramic matrix composite component is provided. The method includes applying a first amount of adhesive across a surface of a release film, providing a first ceramic foam panel including a plurality of channels formed on a first side of the first ceramic foam panel, contacting the first ceramic foam panel and the release film such that adhesive transfers to the first side of the first ceramic foam panel, and coupling the first ceramic foam panel to a second ceramic foam panel.