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:
Feb. 27, 2024

Filed:

Oct. 27, 2022
Applicant:

Embraer S.a., São José dos Campos, BR;

Inventors:

Paulo Anchieta da Silva, São José dos Campos, BR;

Fabio Santos da Silva, São José dos Campos, BR;

Danillo Cafaldo dos Reis, São José dos Campos, BR;

Assignee:

EMBRAER S.A., São José Dos Campos, BR;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B22F 10/20 (2021.01); B64C 23/06 (2006.01); B33Y 70/00 (2020.01); B33Y 80/00 (2015.01); F03G 7/06 (2006.01); C21D 6/00 (2006.01); B22F 10/28 (2021.01); B22F 12/90 (2021.01); B22F 10/64 (2021.01); B64C 3/18 (2006.01);
U.S. Cl.
CPC ...
B64C 23/065 (2013.01); B33Y 70/00 (2014.12); B33Y 80/00 (2014.12); B64C 23/072 (2017.05); C21D 6/004 (2013.01); F03G 7/06 (2013.01); B22F 10/20 (2021.01); B22F 10/28 (2021.01); B22F 10/64 (2021.01); B22F 12/90 (2021.01); B22F 2301/15 (2013.01); B64C 3/185 (2013.01); C21D 2201/01 (2013.01); Y02T 50/10 (2013.01);
Abstract

Thermally configurable structural elements (e.g., aircraft components such as an aircraft winglet spar) capable of assuming at least first and second structural configurations are provided whereby the structural element includes an integral actuation mechanism may be formed of sintered shape memory alloy (SMA) particles and sintered non-SMA particles formed by an additive layer manufacturing (ALM) process, such as 3D printing. The ALM process thereby provides by at least one thermally configurable region, and at least one non-thermally configurable region which is unitarily contiguous with the at least one thermally configurable region. The at least one thermally configurable region is capable of assuming at least first and second positional orientations in response to the presence or absence of a thermal input to thereby cause the structural element to assume the at least first and second structural configurations, respectively.


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