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:
Apr. 23, 2019

Filed:

Mar. 21, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Jeffery Lee Marcoe, Bellevue, WA (US);

Marc Rollo Matsen, Seattle, WA (US);

Waeil M. Ashmawi, Bellevue, WA (US);

Jaime C. Garcia, Kent, WA (US);

Sahrudine Apdalhaliem, Seattle, WA (US);

John B. Moser, Bonney Lake, WA (US);

Brett I. Lyons, Seattle, WA (US);

Moushumi Shome, Kent, WA (US);

Kay Y. Blohowiak, Issaquah, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B32B 1/08 (2006.01); B32B 5/02 (2006.01); B29C 70/46 (2006.01); B29C 33/52 (2006.01); B29C 70/20 (2006.01); D04C 1/06 (2006.01); B29C 35/08 (2006.01);
U.S. Cl.
CPC ...
B32B 1/08 (2013.01); B29C 33/52 (2013.01); B29C 70/205 (2013.01); B29C 70/462 (2013.01); B32B 5/024 (2013.01); D04C 1/06 (2013.01); B29C 2035/0811 (2013.01); B32B 2262/106 (2013.01); B32B 2605/08 (2013.01); B32B 2605/12 (2013.01); B32B 2605/18 (2013.01);
Abstract

Manufacturing a thermoplastic composite tubular structure embedded with a first load fitting comprising the steps of braiding a first plurality of inner layers of thermoplastic composite material around a soluble, expandable mandrel. A first load fitting is positioned on the first plurality of inner layers of thermoplastic composite material. A second plurality of outer layers of thermoplastic composite material is braided around the first load fitting and the mandrel so as to form an overbraided mandrel embedded with the first load fitting. The overbraided mandrel is installed into a matched tooling assembly and heated at a specified heating profile in order to consolidate the first plurality of inner layers of thermoplastic composite material and the second plurality of outer layers of thermoplastic composite material with the first load fitting so as to form a thermoplastic composite tubular structure embedded with the first load fitting. A second load fitting may be positioned on the first plurality of inner layers of thermoplastic composite material.


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