WO2019041069A1

WO2019041069A1 - Flying robot

Info

Publication number: WO2019041069A1
Application number: PCT/CN2017/099210
Authority: WO
Inventors: 刘哲
Original assignee: 刘哲
Priority date: 2017-08-27
Filing date: 2017-08-27
Publication date: 2019-03-07

Abstract

A flying robot, comprising a flying robot body and a damping device body (9). Both left and right sides of the damping device body (9) are equipped with a chest fixing plate (1) and a back fixing plate (4), and an arm fixing column (2) is fixed to the middle of the front side of the chest fixing plate (1); a signal transmitter (101) is provided at the top of the left inner side of the chest fixing plate (1), and a parachute notch (102) is provided in the middle of the inner side of the chest fixing plate (1). The flying robot is provided with an arm stretchable column (3) and a head stretchable column (7); the top of the left side of the arm stretchable column (3) is movably connected to the top of the right side of the arm fixing column (2), and the head stretchable column (7) is movably connected to a head fixing column (8). Because the arm stretchable column (3) and the arm fixing column (2) are stretchable leftwards and rightwards, and the head fixing column (8) and the head stretchable column (7) are stretchable leftwards and rightwards, the damping device can be well and stably worn by any robots of different body shapes, and the applicability is improved.

Description

Flying robot

Technical field

The invention relates to the technical field of flying robots, in particular to a flying robot with a shock absorbing function.

Background technique

A robot is a machine that automatically performs work. It can accept human command, run pre-programmed procedures, or act on principles that are based on artificial intelligence techniques. Its mission is to assist or replace human work, such as production, construction, or other dangerous work. As the times progress, robotic disassembly equipment also increases.

Existing flying robots cannot effectively use the surrounding environment to save energy, and cannot provide safety protection during the fall, and cannot flexibly control the shock absorbing equipment.

Summary of the invention

It is an object of the present invention to provide a flying robot that solves the problem of the above-mentioned background art that cannot effectively utilize the surrounding environment for energy saving, provides safety protection during a fall, and cannot flexibly control a shock absorbing device.

In order to achieve the above object, the present invention provides the following technical solution: a flying robot comprising a flying robot body and a damping device body disposed on the flying robot body, wherein the front and rear chest fixing plates are mounted on the left and right sides of the damping device body a rear fixing plate, and an arm fixing column is fixed in a front middle portion of the front chest fixing plate, a signal transmitter is disposed at a top left inner side of the front chest fixing plate, and a parachute slot is disposed at an inner side of the front chest fixing plate. A fixing strap is installed in the middle of the front surface of the parachute slot, and a buckle base is fixed in the middle of the left side of the parachute slot. A buckle is fixed in the middle of the left side of the buckle base, and the ring buckle is disposed with a plurality of even distributions. a steel belt with a parachute fixed to the left side of the steel belt, an arm telescopic column fixed in the middle of the front side of the rear fixing column, and the inside of the fixing column a plurality of uniformly distributed elastic telescopic columns and elastic telescopic column bases are disposed, the opposite sides of the fixing columns are fixed with gravity plates, and the top ends of the front chest fixing plates are provided with two head fixing columns, the back Two head telescopic columns are fixed to the top end of the fixing column, and a solar panel is installed in the middle of the right side of the back fixing column. The four corners of the solar panel are fixed with a fixing nut.

Preferably, the left end of the arm telescopic column is movably connected with the right end of the arm fixing column, and the head telescopic column is movably connected with the head fixing column.

Preferably, the elastic telescopic column and the elastic telescopic column base are movably connected, and the elastic telescopic column and the elastic telescopic column base are embedded in the back fixing plate.

Preferably, the gravity plate covers the rear side of the back fixing plate, and the weight of the gravity plate is 9 kg.

Preferably, the right side of the parachute is fixedly connected to the left side of the buckle by a steel wire band.

Compared with the prior art, the invention has the beneficial effects that the flying robot is provided with an arm telescopic column and a head telescopic column, and the left end of the arm telescopic column is movably connected with the right top end of the arm fixing column, and the head The telescopic column is movably connected to the head fixing column. Because the arm telescopic column and the arm fixing column are telescopic, the head fixing column and the head telescopic column are telescopic to the left and right, so that any robot of different sizes can wear the shock absorbing device well and stably. The utility model has the advantages of improving the practicability, and the elastic telescopic column, the elastic telescopic column and the elastic telescopic column base are movably connected, and the elastic telescopic column and the elastic telescopic column base are embedded in the back fixing plate, and the elasticity is passed during the flight of the robot. The telescopic column and the elastic telescopic column base telescope will buffer the impact force in the air, avoiding the impact force being too large, causing the parts of the shock absorbing device to be dislocated, improving the safety, setting the gravity plate, the gravity plate covering and the back side of the back fixing plate And the weight of the gravity plate is 9kg, because the gravity plate is disposed on the back fixing plate, so that the quality of the back fixing plate exceeds the front chest solid The plate allows the backing plate to land first when the robot is dropped, and the impact force is reduced as much as possible through the buffer column. The parachute is set. The right side of the parachute is fixedly connected to the left side of the buckle by the steel wire band, because the front chest fixing plate A parachute is installed in the middle, and when the terminal finds that the robot is malfunctioning, the robot's parachute is opened in time to minimize the damage of the robot falling, thereby improving safety.

DRAWINGS

Figure 1 is a schematic view of the overall structure of the present invention;

Figure 2 is a cross-sectional view showing the structure of the front chest fixing plate of the present invention;

Figure 3 is a cross-sectional view showing the structure of the back fixing plate of the present invention;

4 is a schematic view showing a partial structure of a parachute slot of the present invention;

FIG. 5 is a schematic structural diagram of a structure of a signal transmitter module according to the present invention.

In the picture: 1, front chest fixed plate, 101, signal transmitter, 102, parachute slot, 103, fixed belt, 104, buckle base, 105, buckle, 106, wire belt, 107, parachute, 2, arm Fixed column, 3, arm telescopic column, 4, back fixed plate, 401, elastic telescopic column, 402, elastic telescopic column base, 403, gravity plate, 5, solar panel, 6, fixing nut, 7, head telescopic column 8, the head fixed column, 9, the main body of the damping device.

Detailed ways

The technical solutions in the embodiments of the present invention are clearly and completely described in the following with reference to the accompanying drawings in the embodiments of the present invention. It is obvious that the described embodiments are only a part of the embodiments of the present invention, but not all embodiments. All other embodiments obtained by a person of ordinary skill in the art based on the embodiments of the present invention without creative efforts are within the scope of the present invention.

Referring to FIG. 1-5, the present invention provides a technical solution: a flying robot includes a flying robot body (not shown) and a damping device body disposed on the flying robot body, and the damping device body includes 1. a front chest Fixed plate, 101, signal transmitter, 102, parachute slot, 103, fixed strap, 104, buckle base, 105, buckle, 106, wire belt, 107, parachute, 2, arm fixed column, 3, arm telescopic Column, 4, back fixed plate, 401, elastic telescopic column, 402, elastic telescopic column base, 403, gravity plate, 5, solar panel, 6, fixing nut, 7, head telescopic column, 8, head fixing column 9. The main body of the shock absorbing device is provided with a front chest fixing plate 1 on both left and right sides of the main body 9 of the damping device The back fixing plate 4 is fixed to the front surface of the front chest fixing plate 1 with an arm fixing column 2, and the top left inner side of the front chest fixing plate 1 is provided with a signal transmitter 101, and the inner side of the front chest fixing plate 1 is provided A parachute slot 102 is disposed, and a fixing strap 103 is disposed in a front surface of the parachute slot 102, and a buckle base 104 is fixed in a middle of a left side of the parachute slot 102, and a middle of the left side of the buckle base 104 is fixed The buckle 105 is disposed, and the buckle 105 is provided with a plurality of evenly distributed steel belts 106. The left side of the steel belt 106 is fixed with a parachute 107, and a parachute 107 is disposed. The right side of the parachute 107 passes through the steel belt 106 and the buckle 105. The left side is fixedly connected, because the parachute 107 is installed in the front chest fixing plate 1, and when the terminal finds that the robot is faulty, the robot's parachute 107 is opened in time to minimize the damage of the robot falling, thereby improving safety, and the back is fixed. An arm telescopic column 3 is fixed in the middle of the front surface of the column 4, and a plurality of uniformly distributed elastic telescopic columns 401 and an elastic telescopic column base 402 are disposed inside the fixing column 4, and an elastic telescopic column 401 is disposed. The telescopic column 401 and the elastic telescopic column base 402 are movably connected, and the elastic telescopic column 401 and the elastic telescopic column base 402 are embedded in the back fixing plate 4, and the elastic telescopic column 401 and the elastic telescopic column are passed during the flight of the robot. The base 402 expands and contracts to cushion the impact force in the air, avoiding the impact force being too large, causing the parts of the shock absorbing device body 9 to be misaligned, and improving the safety. The opposite side of the fixed column 4 is fixed with the gravity plate 403, and the gravity plate 403 is disposed. The gravity plate 403 covers the rear side of the back fixing plate 4, and the weight of the gravity plate 403 is 9 kg, because the gravity plate 403 is disposed on the back fixing plate 4, so that the mass of the back fixing plate 4 exceeds the front chest fixing plate. 1. When the robot is dropped, the back fixing plate 4 can be grounded first, and the impact force is relieved as much as possible by buffering. The top of the front chest fixing plate 1 is provided with two head fixing columns 8, the back The top end of the fixed column 4 is fixed with two head telescopic columns 7 , and the arm telescopic column 3 and the head telescopic column 7 are disposed, and the left end of the arm telescopic column 3 is movably connected with the right top end of the arm fixing column 2, and Head telescopic column 7 The head fixing column 8 is movably connected, because the arm telescopic column 3 and the arm fixing column 2 are retracted to the left and right, and the head fixing column 8 and the head telescopic column 7 are retracted to the left and right, so that any robot of different sizes can wear the shock absorbing body well and stably. The apparatus main body 9 is improved in practicality, and the solar panel 5 is installed in the middle of the right side of the back fixing column 4, and the fixing edges are fixed to the four corners of the solar panel 5. 6.

Working principle: First, the user puts the main body of the shock absorbing device on the body of the flying robot, and sets the arm telescopic column 3 and the head telescopic column 7, the left end of the arm telescopic column 3 and the right end of the arm fixing column 2 The movable connection, and the head telescopic column 7 and the head fixing column 8 are movably connected, because the arm telescopic column 3 and the arm fixing column 2 are retracted to the left and right, and the head fixing column 8 and the head telescopic column 7 are retracted to the left and right to achieve any body shape. The robot can wear the shock absorbing device body 9 well and stably, and the utility model is improved. Then, when the flying robot is flying under the sunlight, the back fixing plate 4 can effectively convert the solar energy into electric energy for use by the flying robot. The flight cost is saved. Next, a gravity plate 403 is provided, and the gravity plate 403 covers the rear side of the back fixing plate 4, and the weight of the gravity plate 403 is 9 kg because the gravity plate 403 is disposed on the back fixing plate 4, so that The mass of the back fixing plate 4 exceeds that of the front chest fixing plate 1, so that when the robot is dropped, the back fixing plate 4 can be grounded first, and the impact force is relieved as much as possible by buffering, and then the drop is set. The umbrella 107, the right side of the parachute 107 is fixedly connected to the left side of the buckle 105 by the steel belt 106, because the parachute 107 is installed in the front chest fixing plate 1, and when the terminal finds that the robot is malfunctioning, the robot's parachute 107 is opened in time to minimize The damage of the robot falling, thereby improving the safety, thereby completing the working process of the main body 9 of the damping device.

While the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art The scope of the invention is defined by the appended claims and their equivalents.

Claims

A flying robot, comprising: a flying robot body and a damping device body (9) disposed on the flying robot body, wherein the left and right sides of the damping device body (9) are mounted with a chest fixing plate ( 1) and a back fixing plate (4), and an arm fixing column (2) is fixed in the front of the front side of the front chest fixing plate (1), and a signal transmitter is disposed at the top left inner side of the front chest fixing plate (1) (101), and a parachute slot (102) is disposed in the middle of the inner side of the front chest fixing plate (1), and a fixing belt (103) and a parachute slot (102) are installed in the front surface of the parachute slot (102). A buckle base (104) is fixed in the middle of the left side, a buckle (105) is fixed in the middle of the left side of the buckle base (104), and the buckle (105) is provided with a plurality of evenly distributed steel belts (106). a left side of the steel belt (106) is fixed with a parachute (107), and an arm telescopic column (3) is fixed in the middle of the front side of the back fixing column (4), and the inside of the fixing column (4) is provided with a plurality of a uniformly distributed elastic telescopic column (401) and an elastic telescopic column base (402), the opposite side of the fixing column (4) is fixed with a gravity plate (403), the front chest solid The top end of the plate (1) is provided with two head fixing columns (8), and the top end of the back fixing column (4) is fixed with two head telescopic columns (7), and the back fixing column (4) A solar panel (5) is mounted in the middle of the right side, and fixing nuts (6) are fixed to the four corners of the solar panel (5).
A flying robot according to claim 1, characterized in that the left end of the arm telescopic column (3) is movably connected to the right top end of the arm fixing column (2), and the head telescopic column (7) It is movably connected to the head fixing column (8).
The flying robot according to claim 1, wherein the elastic telescopic column (401) and the elastic telescopic column base (402) are movably connected, and the elastic telescopic column (401) and the elastic telescopic column base (402) are provided. They are all embedded in the back fixing plate (4).
A flying robot according to claim 1, wherein said gravity plate (403) covers the rear side of the back fixing plate (4), and the weight of the gravity plate is 9 kg.
A flying robot according to claim 1, characterized in that the right side of the parachute (107) is fixedly connected to the left side of the buckle (105) by a steel belt (106).
A flying robot according to claim 1, characterized in that the parachute (107) is movably embedded in the parachute slot (102).
A flying robot according to claim 1, wherein said flying robot damping device further comprises receiving means for opening the parachute 107 upon receiving the parachute enabling command.