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. 07, 2021

Filed:

Apr. 26, 2018
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

Jeffery L. Marcoe, Bellevue, WA (US);

Sahrudine Apdalhaliem, Seattle, WA (US);

Moushumi Shome, Kent, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B29C 61/06 (2006.01); B64C 3/48 (2006.01); B64C 3/52 (2006.01); B29C 70/88 (2006.01); B29B 11/16 (2006.01); B29C 70/32 (2006.01); B29C 70/22 (2006.01); B29C 70/30 (2006.01); B32B 15/08 (2006.01); F03G 7/06 (2006.01); H05K 1/05 (2006.01); H05K 1/16 (2006.01); B64C 3/44 (2006.01); B64C 27/72 (2006.01); B64C 3/54 (2006.01); B29C 53/82 (2006.01); B29K 71/00 (2006.01); B29K 267/00 (2006.01); B29L 31/30 (2006.01);
U.S. Cl.
CPC ...
B29C 61/0625 (2013.01); B29B 11/16 (2013.01); B29C 70/222 (2013.01); B29C 70/30 (2013.01); B29C 70/32 (2013.01); B29C 70/88 (2013.01); B32B 15/08 (2013.01); B64C 3/48 (2013.01); B64C 3/52 (2013.01); F03G 7/065 (2013.01); H05K 1/056 (2013.01); H05K 1/165 (2013.01); B29C 53/822 (2013.01); B29K 2071/00 (2013.01); B29K 2267/00 (2013.01); B29L 2031/3085 (2013.01); B32B 2250/02 (2013.01); B32B 2605/18 (2013.01); B64C 2003/445 (2013.01); B64C 2003/543 (2013.01); B64C 2027/7288 (2013.01); H05K 2201/0129 (2013.01); H05K 2201/0308 (2013.01); Y02T 50/30 (2013.01); Y02T 50/40 (2013.01);
Abstract

Systems and processes that integrate thermoplastic and shape memory alloy materials to form an adaptive composite structure capable of changing its shape. For example, the adaptive composite structure may be designed to serve as a multifunctional adaptive wing flight control surface. Other applications for such adaptive composite structures include in variable area fan nozzles, winglets, fairings, elevators, rudders, or other aircraft components having an aerodynamic surface whose shape is preferably controllable. The material systems can be integrated by means of overbraiding (interwoven) with tows of both thermoplastic and shape memory alloy materials or separate layers of each material can be consolidated (e.g., using induction heating) to make a flight control surface that does not require separate actuation.


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