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:
Dec. 17, 2019
Filed:
Oct. 19, 2016
Applicant:
Rohr, Inc., Chula Vista, CA (US);
Inventor:
Christian Soria, La Mesa, CA (US);
Assignee:
Rohr, Inc., Chula Vista, CA (US);
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 29/00 (2006.01); B32B 7/12 (2006.01); B32B 37/06 (2006.01); B32B 3/12 (2006.01); B32B 37/10 (2006.01); B32B 37/12 (2006.01); B32B 37/14 (2006.01); B29C 70/68 (2006.01); B32B 37/18 (2006.01); B29C 70/30 (2006.01); B32B 5/26 (2006.01); B32B 15/04 (2006.01); B32B 15/08 (2006.01); B32B 15/12 (2006.01); B32B 27/08 (2006.01); B32B 27/10 (2006.01); B32B 27/12 (2006.01); B32B 29/02 (2006.01); B32B 1/00 (2006.01); B32B 3/08 (2006.01); B32B 3/18 (2006.01);
U.S. Cl.
CPC ...
B64D 29/00 (2013.01); B29C 70/30 (2013.01); B29C 70/68 (2013.01); B32B 1/00 (2013.01); B32B 3/08 (2013.01); B32B 3/12 (2013.01); B32B 3/18 (2013.01); B32B 5/26 (2013.01); B32B 7/12 (2013.01); B32B 15/043 (2013.01); B32B 15/08 (2013.01); B32B 15/12 (2013.01); B32B 27/08 (2013.01); B32B 27/10 (2013.01); B32B 27/12 (2013.01); B32B 29/02 (2013.01); B32B 37/06 (2013.01); B32B 37/10 (2013.01); B32B 37/12 (2013.01); B32B 37/14 (2013.01); B32B 37/144 (2013.01); B32B 37/18 (2013.01); B32B 2250/40 (2013.01); B32B 2260/021 (2013.01); B32B 2260/046 (2013.01); B32B 2307/10 (2013.01); B32B 2307/102 (2013.01); B32B 2307/54 (2013.01); B32B 2307/546 (2013.01); B32B 2307/732 (2013.01); B32B 2605/18 (2013.01);
Abstract
Aspects of the disclosure are directed to a panel configured for use on an aircraft nacelle, comprising: a first skin, a second skin, a first core portion coupled to the first skin and the second skin, a second core portion coupled to the first skin and the second skin, and an insert coupled to the first skin, the second skin, the first core portion, and the second core portion, the insert forming a corner fitting between the first core portion and the second core portion.