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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.:

US 10611454 B1

PDFFull Text
Date of Patent:
Apr. 07, 2020

Filed:

Mar. 06, 2017

Aircraft cabin panel and method of manufacturing the same

Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Russ Raynal LeBlanc, Kirkland, WA (US);

Chris Gren McInelly, Stanwood, WA (US);

Andrew Anthony Pillar, Camano Island, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:

Armstrong Teasdale LLP

Primary Examiner:

Monica A Huson

Int. Cl.
CPC ...
B64C 1/06 (2006.01); B32B 3/12 (2006.01); B32B 3/26 (2006.01); B32B 3/30 (2006.01); B32B 7/12 (2006.01); B32B 3/04 (2006.01); B32B 5/02 (2006.01); B32B 5/26 (2006.01); B32B 27/12 (2006.01); B32B 27/10 (2006.01); B32B 29/06 (2006.01); B32B 29/02 (2006.01); B32B 37/02 (2006.01); B32B 37/12 (2006.01); B33Y 10/00 (2015.01); B33Y 40/00 (2020.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
B64C 1/066 (2013.01); B32B 3/04 (2013.01); B32B 3/12 (2013.01); B32B 3/263 (2013.01); B32B 3/30 (2013.01); B32B 5/02 (2013.01); B32B 5/26 (2013.01); B32B 7/12 (2013.01); B32B 27/10 (2013.01); B32B 27/12 (2013.01); B32B 29/02 (2013.01); B32B 29/06 (2013.01); B32B 37/02 (2013.01); B32B 37/12 (2013.01); B33Y 10/00 (2014.12); B33Y 40/00 (2014.12); B33Y 80/00 (2014.12); B32B 2250/24 (2013.01); B32B 2255/02 (2013.01); B32B 2255/10 (2013.01); B32B 2255/12 (2013.01); B32B 2260/023 (2013.01); B32B 2260/028 (2013.01); B32B 2260/046 (2013.01); B32B 2262/0269 (2013.01); B32B 2262/101 (2013.01); B32B 2262/106 (2013.01); B32B 2305/024 (2013.01); B32B 2305/076 (2013.01); B32B 2305/08 (2013.01); B32B 2313/04 (2013.01); B32B 2315/085 (2013.01); B32B 2377/00 (2013.01); B32B 2386/00 (2013.01); B32B 2605/18 (2013.01);
Abstract

An interior panel for use in an aircraft cabin includes an inner core including a first surface and an opposing second surface. The interior panel also includes a first honeycomb layer coupled to the first surface and a second honeycomb layer coupled to the second surface. The inner core includes an integral forming tool configured to shape the first honeycomb layer and the second honeycomb layer. The interior panel also includes a first skin layer coupled to the first honeycomb layer and a second skin layer coupled to the second honeycomb layer.

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