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:
Nov. 10, 2020

Filed:

Nov. 14, 2018
Applicant:

Airbus Operations S.l., Madrid, ES;

Inventors:
Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16L 3/08 (2006.01); F16L 3/123 (2006.01); H02G 3/00 (2006.01); F16B 5/06 (2006.01); B29C 65/50 (2006.01); B29C 70/74 (2006.01); B29C 65/00 (2006.01); B29C 65/56 (2006.01); F16B 9/02 (2006.01); F16B 7/04 (2006.01); B29L 31/00 (2006.01); B29L 31/30 (2006.01); F16B 2/10 (2006.01);
U.S. Cl.
CPC ...
F16L 3/123 (2013.01); B29C 65/5014 (2013.01); B29C 65/5042 (2013.01); B29C 65/561 (2013.01); B29C 65/562 (2013.01); B29C 66/112 (2013.01); B29C 66/114 (2013.01); B29C 66/474 (2013.01); B29C 66/532 (2013.01); B29C 66/721 (2013.01); B29C 66/73751 (2013.01); B29C 70/74 (2013.01); F16B 5/0685 (2013.01); H02G 3/26 (2013.01); B29C 66/727 (2013.01); B29C 66/72143 (2013.01); B29C 66/7392 (2013.01); B29L 2031/3076 (2013.01); B29L 2031/737 (2013.01); F16B 2/10 (2013.01); F16B 7/0433 (2013.01); F16B 9/02 (2013.01);
Abstract

A composite structure () for an aircraft, having at least one insert () for receiving attachment devices, each insert () includes a core () having a major dimension and containing at least one through-hole (), and a composite strip arrangement formed by a first section () surrounding the core () and attached to said core () by an adhesive polymeric layer, and a second section () including at least one free end (). The first () and the second portion () of the composite strip arrangement are disposed over a first surface () of the composite structure (), such that the major dimension of the core () is positioned transversal to said first surface (a). The at least one insert () is co-cured with the composite structure ().


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