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. 25, 2023

Filed:

Jul. 09, 2020
Applicant:

Jilin University, Jilin, CN;

Inventors:

Zhihui Zhang, Jilin, CN;

Zhenglei Yu, Jilin, CN;

Xiaolong Zhang, Jilin, CN;

Wei Yan, Jilin, CN;

Yanlong Shao, Jilin, CN;

Yunhong Liang, Jilin, CN;

Qingping Liu, Jilin, CN;

Qingquan Zhang, Jilin, CN;

Yuting Liu, Jilin, CN;

Assignee:

Jilin University, Changchun, CN;

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64C 3/38 (2006.01); B33Y 10/00 (2015.01); B33Y 50/02 (2015.01); B33Y 70/00 (2020.01); B33Y 80/00 (2015.01); B29C 64/118 (2017.01); B29C 64/393 (2017.01); B64C 3/18 (2006.01); B64C 39/00 (2023.01); B64C 39/02 (2023.01); B29L 31/30 (2006.01); B64U 10/40 (2023.01); B64U 30/12 (2023.01);
U.S. Cl.
CPC ...
B64C 3/38 (2013.01); B29C 64/118 (2017.08); B29C 64/393 (2017.08); B33Y 10/00 (2014.12); B33Y 50/02 (2014.12); B33Y 70/00 (2014.12); B33Y 80/00 (2014.12); B64C 3/187 (2013.01); B64C 39/003 (2013.01); B64C 39/024 (2013.01); B29L 2031/3085 (2013.01); B64U 10/40 (2023.01); B64U 30/12 (2023.01);
Abstract

A rigid-flexible coupled unmanned aerial vehicle (UAV) morphing wing and an additive manufacturing method thereof are disclosed. A shape memory alloy (SMA) strip/wire for controlling the wing upward deformation and an SMA strip/wire for controlling the wing downward deformation are arranged alternately, and a plurality of reinforcing ribs are arranged at intervals on the SMA strips/wires for controlling the wing upward deformation and the SMA strips/wires for controlling the wing downward deformation. The SMA strips/wires for controlling the wing upward deformation and the SMA strips/wires for controlling the wing downward deformation are arranged on a flexible substrate, and are wrapped with an insulating covering. The SMA strips/wires for controlling the wing upward deformation and the SMA strips/wires for controlling the wing downward deformation each are provided with an electric heating element.


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