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.

Date of Patent:
Sep. 01, 2026

Filed:

Jul. 10, 2020
Applicant:

Boeing Ace Collateral Agent, Llc, Arlington, VA (US);

Inventor:

Edward Barnes, Palo Alto, CA (US);

Assignee:

Boeing Ace Collateral Agent, LLC, Arlington, VA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 1/06 (2006.01); B29C 70/34 (2006.01); B29K 307/04 (2006.01); B29K 309/08 (2006.01); B29L 31/30 (2006.01); B32B 5/02 (2006.01); B32B 17/02 (2006.01); B32B 27/12 (2006.01); B32B 37/10 (2006.01); B64C 1/00 (2006.01); B64F 5/10 (2017.01);
U.S. Cl.
CPC ...
B64C 1/068 (2013.01); B29C 70/342 (2013.01); B32B 5/02 (2013.01); B32B 17/02 (2013.01); B32B 27/12 (2013.01); B32B 37/10 (2013.01); B64F 5/10 (2017.01); B29K 2307/04 (2013.01); B29K 2309/08 (2013.01); B29L 2031/3082 (2013.01); B32B 2260/023 (2013.01); B32B 2260/046 (2013.01); B32B 2262/101 (2013.01); B32B 2262/106 (2013.01); B32B 2307/202 (2013.01); B32B 2605/18 (2013.01); B64C 2001/0072 (2013.01);
Abstract

An aircraft body section comprises a first layer of composite material, a first group of conductive traces, a second layer of composite material, and a first group of conductive connectors. The first layer of composite material has an upper surface and a lower surface, with the lower surface forming an exterior surface of a body of the aircraft. The first group of conductive traces are formed on the upper surface of the first layer of composite material. The second layer of composite material is positioned on the first layer of composite material and has an upper surface and a lower surface, with the upper surface forming an interior surface of a body of the aircraft. The first group of conductive connectors is formed on the upper surface of the second layer of composite material and is configured to provide electrical connection from external conductors to the conductive traces.


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