Reconfigurable quadrotor with controlled rolling and turning

Patent metadata

Field	Value
Publication number	US-12384536-B2
Application number	US-202418406061-A
Country	US
Kind code	B2
Filing date	Jan 5, 2024
Priority date	Jan 5, 2024
Publication date	Aug 12, 2025
Grant date	Aug 12, 2025

Abstract

A quadrotor is proposed than can both fly and roll. The proposed robot employs passively reconfigurable structures to enable the rolling, tightly coupling the attitude of the robot to the rolling cage. The benefits are precise rolling and turning control as well as improved rolling efficiency. The passively reconfigurable structures are enabled by pre-stretched elastic springs to generate a nonlinear restoring torque. The robot leveraged the superior maneuverability in the rolling mode to take photos of the surroundings at different tilting and panning angles to construct a panoramic image. Besides, the results of the power measurements show a significant reduction in the cost of transport brought by at low speed, equating to a 15-fold extension in the operational range.

First claim

The invention claimed is:

1. An unmanned aerial vehicle, comprising:
a) a rolling structure adapted to roll on a surface;
b) a body mounted within the rolling structure; and
c) four propellers connected to the body;
wherein the body is coupled to the four propellers by a passively reconfigurable module, such that the unmanned aerial vehicle is adapted to be switched between a flying state and a rolling state; the passively reconfigurable module comprising four passively reconfigurable joints; each said passively reconfigurable joint connecting a respective one of the four propellers to the body; and
wherein in the rolling state, two of the four propellers are adapted to generate positive rolling torque and the other two of the four propellers are adapted to generate negative rolling torque.

2. The unmanned aerial vehicle of claim 1 , wherein the body is connected non-rotatably to the rolling structure.

3. The unmanned aerial vehicle of claim 2 , wherein the rolling structure comprises two wheels; the wheels connected respectively to two opposite ends of the body.

4. The unmanned aerial vehicle of claim 1 , wherein each said passively reconfigurable joint comprises:
d) a propeller arm pivotally coupled to the body at a revolute point; and
e) an elastic component with one end connected to or adjacent a free end of the propeller arm, and another end coupled to the body at a location away from the revolute point.

5. The unmanned aerial vehicle of claim 4 , wherein the elastic component is a coil spring which is pre-stretched, such that the unmanned aerial vehicle is in the rolling state when the propellers are not energized.

6. The unmanned aerial vehicle of claim 5 , wherein the coil spring is substantially parallel to the propeller arm when the unmanned aerial vehicle is in the flying state.

7. The unmanned aerial vehicle of claim 5 , wherein the coil spring and the propeller arm form two sides of a virtual triangle when the unmanned aerial vehicle is in the rolling state;
the revolute point located at a vertex of the triangle.

8. The unmanned aerial vehicle of claim 1 , wherein the four propellers are substantially aligned in a same plane when the unmanned aerial vehicle is in the flying state.

9. The unmanned aerial vehicle of claim 1 , wherein the four propellers consist of a first pair of the propellers and a second pair of the propellers; within each pair the two propellers are arranged oppositely such that they are in a substantially back-to-back configuration, when the unmanned aerial vehicle is in the rolling state; wherein propelling axes of the four propellers are substantially orthogonal to a rolling axis of the unmanned aerial vehicle in the rolling state.

10. The unmanned aerial vehicle of claim 4 , wherein each said passively reconfigurable joint further comprises a stopper coupled to the propeller arm; the stopper adapted to be urged against the body to prevent the propeller arm from moving beyond an angular limit.

11. The unmanned aerial vehicle of claim 3 , wherein a spanned area of the body and the four propellers, when the unmanned aerial vehicle is in the flying state, is smaller than an area defined by one said wheel.

12. The unmanned aerial vehicle of claim 1 , wherein the unmanned aerial vehicle switches from the rolling state to the flying state when generated thrusts by the propellers are greater than a predetermined threshold.

13. The unmanned aerial vehicle of claim 4 , wherein the propeller arm is connected to an end of an extension arm extending from the body; said another end of the elastic component connected to the extension arm at the location away from the revolute point.

14. The unmanned aerial vehicle of claim 13 , wherein the extension arm is fixedly connected to the body.

Assignees

• Univ City Hong Kong

Inventors

• Jia Huaiyuan
• Chirarattananon Pakpong
• Bai Songnan
• Ding Runze

Classifications

• B64U60/60

  with rolling cages · CPC title

• B64U30/293

  Foldable or collapsible rotors or rotor supports · CPC title

• B64U2101/00

  UAVs specially adapted for particular uses or applications · CPC title

• B64U10/14 Primary

  with four distinct rotor axes, e.g. quadcopters · CPC title

• B64U10/70

  Convertible aircraft, e.g. convertible into land vehicles · CPC title