Rigid-flexible coupled UAV morphing wing and additive manufacturing method thereof

Patent metadata

Field	Value
Publication number	US-11634208-B2
Application number	US-202016924812-A
Country	US
Kind code	B2
Filing date	Jul 9, 2020
Priority date	Sep 4, 2019
Publication date	Apr 25, 2023
Grant date	Apr 25, 2023

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.

First claim

The invention claimed is:

1. A rigid-flexible coupled UAV morphing wing, comprising SMA strips/wires for controlling the wing upward deformation, SMA strips/wires for controlling the wing downward deformation, reinforcing ribs, a flexible substrate, an insulating covering, an SMA polymer composite strip for controlling the wingtip downward deformation, an SMA polymer composite strip for controlling the wingtip upward deformation, SMA springs for controlling the wing backward deformation, and SMA springs for controlling the wing forward deformation; wherein
the SMA strips/wires for controlling the wing upward deformation and the SMA strips/wires 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 the flexible substrate, and are wrapped with the insulating covering;
the SMA polymer composite strip for controlling the wingtip downward deformation and the SMA polymer composite strip for controlling the wingtip upward deformation are arranged in the flexible substrate of an wingtip, with the SMA polymer composite strip for controlling the wingtip upward deformation on an outer side and the SMA polymer composite strip for controlling the wingtip downward deformation on an inner side; the SMA spring for controlling the wing backward deformation and the SMA spring for controlling the wing forward deformation are arranged alternately, and are located on the flexible substrate; the SMA spring for controlling the wing backward deformation and the SMA spring for controlling the wing forward deformation are connected between two reinforcing ribs located at the wing root; and
the SMA strips/wires for controlling the wing upward deformation, the SMA strips/wires for controlling the wing downward deformation, the flexible substrate, the SMA polymer composite strip for controlling the wingtip downward deformation, the SMA polymer composite strip for controlling the wingtip upward deformation, the SMA spring for controlling the wing backward deformation, and the SMA spring for controlling the wing forward deformation each are provided with an electric heating element.

2. The rigid-flexible coupled UAV morphing wing according to claim 1 , wherein the SMA is nickel titanium alloy.

3. The rigid-flexible coupled UAV morphing wing according to claim 1 , wherein a material of the flexible substrate is polyether ether ketone; and a polymer material is polyether ether ketone.

4. An additive manufacturing method for the rigid-flexible coupled UAV morphing wing according to claim 1 , comprising the following steps:
a. building a 3D model of a UAV morphing wing skeleton:
using computer aided design software to build the 3D model of the UAV morphing wing skeleton;
b. fabricating a rigid and high-strength SMA skeleton:
b1: selecting SMA strips/wires and springs according to a size of the UAV morphing wing model, and training deformation characteristics of the SMA strips/wires and springs through a high-temperature furnace;
c. building a 3D model of a flexible and low-strength polymer shape memory material substrate:
using computer-aided design and manufacturing software to build the flexible and low-strength polymer shape memory material filler model and generate an STL file;
d. performing slicing processing on the flexible and low-strength polymer shape memory material filler model:
using a computer program to analyze the STL file of the model to generate two-dimensional slices and obtain contour information;
e. making preparation before printing:
e1: determining a location of the rigid and high-strength SMA skeleton, and setting up the SMA skeleton;
f. using additive manufacturing to print flexible and low-strength polymer shape memory materials to complete fabrication of the UAV morphing wing:
f1: using a 3D printing nozzle to print the flexible and low-strength polymer shape memory materials on a printing substrate according to a printing path, to form a substrate base;
f2: during the printing process, setting up the high-strength SMA skeleton on the substrate base; f3: printing the flexible and low-strength polymer shape memory materials layer by layer
based on the 3D substrate model, to form the UAV morphing wing after cooling and solidification.

Assignees

• Univ Jilin

Inventors

• Zhang Zhihui
• Yu Zhenglei
• Zhang Xiaolong
• Yan Wei
• Shao Yanlong
• Liang Yunhong
• Liu Qingping
• Zhang Qingquan
• Liu Yuting

Classifications

• B64U30/12

  Variable or detachable wings, e.g. wings with adjustable sweep · CPC title

• B33Y70/00

  Materials specially adapted for additive manufacturing · CPC title

• B29L2031/3085

  Wings · CPC title

• B29C64/118 Primary

  using filamentary material being melted, e.g. fused deposition modelling [FDM] · CPC title

• B64C3/187

  Ribs · CPC title