Land all-terrain duct cross-domain robot and cross-domain method thereof

A robot and all-terrain technology, which is applied to manipulators, motor vehicles, and vehicles that can be converted into airplanes. It can solve the problems of difficult layout of the walking mechanism, easy crashes, and difficult cross-domain processes, etc., to achieve rapid change of flight direction, Reduce the complexity of the system, the effect of strong obstacle-crossing function

Pending Publication Date: 2020-04-10
CHANGCHUN INST OF TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] 1. The cross-domain process is relatively difficult, and the land take-off process is easy to realize, but the landing process is complicated and prone to crashes;
[0004] 2. For the flight function, the land walking function is added, an additional walking mechanism is added, the weight increases, and the flight difficulty increases;
[0005] 3. For the walking function, the power control of the aircraft is relatively complicated, the layout of the walking mechanism is difficult, and it is difficult to realize all-terrain movement

Method used

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  • Land all-terrain duct cross-domain robot and cross-domain method thereof
  • Land all-terrain duct cross-domain robot and cross-domain method thereof
  • Land all-terrain duct cross-domain robot and cross-domain method thereof

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Embodiment Construction

[0027] Such as figure 1 As shown, a land all-terrain ducted cross-domain robot includes control system I, power supply II, flight device III, wind guide mechanism IV, and mechanical legs V, wherein the mechanical legs V are evenly distributed around the flying device. The control system I controls the action of the flight device III, the wind guide mechanism IV and the mechanical leg V, and the power supply II supplies power for the control system I, the flight device III, the wind guide mechanism IV and the mechanical leg V.

[0028] The control system The control system I includes a control panel housing 9 and a placement platform 10 .

[0029] The power source II includes a placement platform 10 , a battery 11 and a battery fixing post 12 .

[0030] Such as figure 2 and image 3 As shown, the mechanical leg V is a connecting rod structure, including a steering gear fixing seat 1, a leg steering gear 2, a leg connecting rod 3, a leg transmission rod 4, a leg joint 5, a s...

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Abstract

Provided are a land all-terrain duct cross-domain robot and a cross-domain method thereof. The robot comprises a control system, a power source, a flight device, an air guide mechanism and mechanicallegs, and the mechanical legs are evenly distributed on the periphery of the flight device. The control system controls the flight device, the air guide mechanism and the mechanical legs to act, and the power supply supplies power to the control system, the flight device, the air guide mechanism and the mechanical legs. The air guide mechanism guides output airflow of a ducted fan to achieve flight control over the robot. Land operation and simple obstacle crossing functions are achieved through movement of two steering engines on the mechanical legs. The flight device lifts off through the relative movement of two blades on the motor so as to achieve the obstacle crossing function on complex terrains. The method has the characteristics that cross-domain operation in land and air space domains can be achieved and the requirement for reciprocating crossing is met. The executable capacity is improved, and related tasks of medium-and-long-distance complex road surface reconnaissance and rapid goods and materials delivery or transportation are achieved.

Description

technical field [0001] The invention belongs to the technical field of land cross-domain robots, and in particular relates to a land all-terrain ducted cross-domain robot and a cross-domain method thereof. Background technique [0002] The current land robot and aerial robot technologies are mature, but cross-domain robots are still difficult to design, mainly reflected in: [0003] 1. The cross-domain process is more difficult, and the land take-off process is easy to realize, but the landing process is complicated and prone to crashes; [0004] 2. For the flight function, the land walking function is added, an additional walking mechanism is added, the weight increases, and the flight difficulty increases; [0005] 3. For the walking function, the power control of the aircraft is relatively complicated, the layout of the walking mechanism is difficult, and it is difficult to realize all-terrain movement. Contents of the invention [0006] In view of the above problems,...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B60F5/02B62D57/032B25J11/00
CPCB60F5/02B62D57/032B25J11/00
Inventor 刘国松李明达王毅王泽宇李长雨刘鸿涛姜义门玉琢冀秉魁杨晓萍钟月曦
Owner CHANGCHUN INST OF TECH
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