CN212332958U

CN212332958U - Laser fight unmanned aerial vehicle integrating control system and laser induction control system

Info

Publication number: CN212332958U
Application number: CN202021040535.9U
Authority: CN
Inventors: 蒋雄辉; 谢潮龙; 孙莹
Original assignee: Shanghai Aogen Uav Technology Co ltd
Current assignee: Shanghai Aogen Uav Technology Co ltd
Priority date: 2020-06-09
Filing date: 2020-06-09
Publication date: 2021-01-12
Anticipated expiration: 2030-06-09

Abstract

The utility model discloses an integrated control system and laser response control system's laser fight unmanned aerial vehicle, concretely relates to unmanned aerial vehicle technical field, including four rotor flight platforms, laser response control panel and unmanned aerial vehicle controller, the fixed cover in the four rotor flight platforms outside is equipped with the casing, the fixed protection machanism that is equipped with in casing bottom; the protection mechanism comprises a transverse plate, a plurality of columns are fixedly arranged between the transverse plate and the shell, an air cushion is arranged at the bottom of the transverse plate, and a plurality of connecting columns are fixedly arranged between the transverse plate and the air cushion. The utility model discloses a lug and ground contact, four rotor flight platform pass through the spliced pole and push down, and the plane contracts simultaneously about the air cushion, and the air in the air cushion is through a plurality of air vents outside discharge, is in same horizontal plane until lug and first pulley and second pulley, increases the area of contact on four rotor flight platform and ground from this, and the condition of bounce-back can not appear in the air cushion, and barrier propterty is good.

Description

Laser fight unmanned aerial vehicle integrating control system and laser induction control system

Technical Field

The embodiment of the utility model provides a relate to unmanned air vehicle technical field, concretely relates to integrated control system and laser induction control system's laser fight unmanned aerial vehicle.

Background

The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing radio remote control equipment and a self-contained program control device, and has the characteristics of high portability, simplicity in operation, flexibility in use and the like.

The prior art has the following defects: unmanned aerial vehicle is after participating in the project, and unmanned aerial vehicle because factors such as inertia lean forward easily or turn on one's side when descending, in order to reduce its probability of falling, its landing frame adopts the spring structure more for its shock attenuation, but the characteristic of spring makes unmanned aerial vehicle fall after, easily takes place to bounce back, and the protectiveness is relatively poor.

Therefore, the invention needs to invent a laser fight drone integrating a control system and a laser induction control system.

SUMMERY OF THE UTILITY MODEL

Therefore, the embodiment of the utility model provides an integrated control system and laser induction control system's laser fight unmanned aerial vehicle, through lug and ground contact, then four rotor flight platform passes through the spliced pole and pushes down, the plane contracts simultaneously about the air cushion, then the air in the air cushion is outwards discharged through a plurality of air vents, until the lug is in same horizontal plane with first pulley and second pulley, increase the area of contact on four rotor flight platform and ground from this, the condition of bounce-back can not appear in the air cushion, and barrier propterty is good, it adopts the spring structure for its shock attenuation more to fall the frame in order to solve prior art, but the characteristic of spring makes unmanned aerial vehicle fall behind, easily take place the bounce-back, the relatively poor problem of barrier propterty.

In order to achieve the above object, the embodiment of the present invention provides the following technical solutions: a laser fighting unmanned aerial vehicle integrating a control system and a laser induction control system comprises a four-rotor flight platform, a laser induction control panel and an unmanned aerial vehicle controller, wherein a shell is fixedly sleeved on the outer side of the four-rotor flight platform, and a protection mechanism is fixedly arranged at the bottom of the shell;

protection machanism includes the diaphragm, the diaphragm is established in the casing bottom, the fixed a plurality of cylinders that are equipped with between diaphragm and the casing, the diaphragm bottom is equipped with the air cushion, the fixed a plurality of spliced poles that are equipped with between diaphragm and the air cushion, a plurality of air vents have been seted up at the air cushion top, and is a plurality of the air vent is all established between a plurality of spliced poles, the inside a plurality of body of rod that is equipped with of air cushion, it is a plurality of the body of rod is all through pivot and air cushion swing joint, the body of rod is inside to be fixed to be equipped with two haulage ropes, two the haulage rope bottom all passes the body of rod and extends to body of rod bottom, the haulage rope.

Further, the vent hole top radius is smaller than the bottom radius.

Furthermore, both sides all are fixed around the diaphragm and are equipped with two supporting legs, two the supporting leg is all established in the air cushion outside, supporting leg one side is equipped with first pulley, first pulley is through pivot and supporting leg swing joint.

Furthermore, an inclined rod is fixedly arranged on the other side of the supporting leg, a second pulley is fixedly arranged at the bottom of the inclined rod, and the bottoms of the second pulley and the first pulley are located on the same horizontal line.

Further, the height of the plane where the bottoms of the second pulley and the first pulley are located is higher than that of the plane where the bump is located.

Further, a base frame is fixedly arranged inside the shell, an LED lamp bank is fixedly arranged at the bottom of the shell, and the LED lamp bank is arranged among the columns.

Further, laser response control panel is fixed to be established in the diaphragm bottom, laser response control panel establishes between a plurality of spliced poles, the fixed laser receiver that is equipped with of laser response control panel receiving end, the fixed casing one side of establishing of laser receiver, the fixed laser emitter that is equipped with of laser response control panel output, laser emitter establishes between diaphragm and air cushion, laser response control panel and LED banks electric connection.

Further, the unmanned aerial vehicle controller is in wireless connection with the laser induction control panel.

The embodiment of the utility model provides a have following advantage:

through lug and ground contact, then four rotor flight platform pass through the spliced pole and push down, and the plane contracts simultaneously about the air cushion, then the air in the air cushion outwards discharges through a plurality of air vents, is in same horizontal plane until lug and first pulley and second pulley, increases the area of contact on four rotor flight platform and ground from this, compares with prior art, and the condition of bounce-back can not appear in the air cushion, and barrier propterty is good.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below. It should be apparent that the drawings in the following description are merely exemplary, and that other embodiments can be derived from the drawings provided by those of ordinary skill in the art without inventive effort.

The structure, ratio, size and the like shown in the present specification are only used for matching with the content disclosed in the specification, so as to be known and read by people familiar with the technology, and are not used for limiting the limit conditions which can be implemented by the present invention, so that the present invention has no technical essential significance, and any structure modification, ratio relationship change or size adjustment should still fall within the scope which can be covered by the technical content disclosed by the present invention without affecting the efficacy and the achievable purpose of the present invention.

Fig. 1 is a top view of the overall structure provided by the present invention;

fig. 2 is a cross-sectional view of the overall structure provided by the present invention;

FIG. 3 is an enlarged view of the part A structure of FIG. 2 according to the present invention;

fig. 4 is an enlarged view of the part B structure of fig. 2 according to the present invention;

fig. 5 is a system diagram provided by the present invention;

in the figure: 1 four rotor flight platform, 2 cylinders, 3 diaphragm, 4 spliced poles, 5 air cushions, 6 air vents, the 7 body of rod, 8 haulage ropes, 9 lead block, 10 lugs, 11 supporting legs, 12 first pulleys, 13 down tube, 14 second pulleys, 15 casings, 16 bed frames, 17LED banks, 18 laser-induced control panel, 19 laser receiver, 20 laser emitter, 21 unmanned aerial vehicle controller.

Detailed Description

The present invention is described in terms of specific embodiments, and other advantages and benefits of the present invention will become apparent to those skilled in the art from the following disclosure. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to the attached drawings 1-5 in the specification, the laser fight unmanned aerial vehicle integrating the control system and the laser induction control system comprises a four-rotor flight platform 1, a laser induction control panel 18 and an unmanned aerial vehicle controller 21, wherein a shell 15 is fixedly sleeved on the outer side of the four-rotor flight platform 1, and a protection mechanism is fixedly arranged at the bottom of the shell 15;

protection machanism includes diaphragm 3, diaphragm 3 is established in casing 15 bottom, the fixed a plurality of cylinders 2 that are equipped with between diaphragm 3 and the

casing

15, 3 bottoms of diaphragm are equipped with air cushion 5, the fixed a plurality of spliced poles 4 that are equipped with between diaphragm 3 and the air cushion 5, a plurality of air vents 6 have been seted up at air cushion 5 top, and are a plurality of air vents 6 are all established between a plurality of spliced poles 4, the inside a plurality of body of rod 7 that is equipped with of air cushion 5, it is a plurality of the body of rod 7 is all through pivot and 5 swing joint of air cushion, the inside fixed two haulage ropes 8 that are equipped with of the body of rod 7, two 8 bottoms of haulage rope all pass the body of rod 7 and extend to body of rod 7 bottom, 8 bottom mounting of haulage rope is equipped with

lead block

9, 5.

Further, the radius of the top of the vent hole 6 is smaller than that of the bottom of the vent hole, so that the vent hole 6 can reduce the exhaust speed and improve the protection performance of the air cushion 5 when exhausting.

Further, both sides are all fixed and are equipped with two supporting legs 11 around the diaphragm 3, two supporting leg 11 all establishes in the air cushion 5 outside, supporting leg 11 one side is equipped with first pulley 12, first pulley 12 is through pivot and supporting leg 11 swing joint, and after certain degree can be put to gas in air cushion 5 through supporting leg 11, its cooperation air cushion 5 supports four rotor flight platform 1, improves the utility model discloses a stability.

Furthermore, an inclined rod 13 is fixedly arranged on the other side of the supporting leg 11, a second pulley 14 is fixedly arranged at the bottom of the inclined rod 13, the bottoms of the second pulley 14 and the first pulley 12 are located on the same horizontal line, and the inclined rod 13 and the supporting leg 11 are in a V-shaped structure, so that the possibility of side tilting is reduced to a certain extent.

Further, the height of the plane where the bottoms of the second pulley 14 and the first pulley 12 are located is higher than that of the plane where the bump 10 is located.

Further, casing 15 internal fixation is equipped with bed frame 16, the fixed LED banks 17 that is equipped with in casing 15 bottom, LED banks 17 establish between a plurality of cylinders 2, can strengthen through bed frame 16 the utility model discloses a fastness.

Further, laser response control panel 18 is fixed to be established in diaphragm 3 bottom, laser response control panel 18 is established between a plurality of spliced poles 4, the fixed laser receiver 19 that is equipped with of laser response control panel 18 receiving terminal, laser receiver 19 is fixed to be established in casing 15 one side, the fixed laser emitter 20 that is equipped with of laser response control panel 18 output end, laser emitter 20 is established between diaphragm 3 and air cushion 5, laser response control panel 18 and LED banks 17 electric connection.

Further, the unmanned aerial vehicle controller 21 is wirelessly connected with the laser sensing control panel 18.

The implementation scenario is specifically as follows: in the initial state, the lead block 9 contacts with the bottom of the inner cavity of the air cushion 5, then the rod body 7 inclines to prop open the inside of the air cushion 5, the air cushion 5 is filled with air, then the LED lamp group 17 is in the lightening state, when the utility model is put into practical use, after any one of the two four-rotor flying platforms 1 is hit by the laser emitter 20 in the fighting process, then the laser receiver 19 reacts the information to the laser induction control panel 18, then the laser induction control panel 18 closes the LED lamp group, the fighting is finished, then the user controls the utility model to descend downwards through the unmanned aerial vehicle controller 21, then the air cushion 5 contacts with the ground at first, the contact area between the supporting leg 11 and the ground is increased by the air cushion 5, the heeling probability of the utility model is reduced, at this moment, a plurality of convex blocks 10 at the bottom of the air cushion 5 can provide protection for the air cushion 5 to avoid the friction with the ground, the damage condition appears, the service life of the air cushion 5 is prolonged, then after the plurality of lugs 10 are contacted with the ground, the weight of the four-rotor flying platform 1 and the landing impact force exert pressure on the top surface of the air cushion 5, in addition, the lugs 10, the first pulley 12 and the second pulley 14 are not in a uniform horizontal plane, so the upper plane and the lower plane of the air cushion 5 are contracted together, then the air in the air cushion 5 is discharged through the plurality of vent holes 6, at the moment, the air in the vent holes 6 is blocked in air discharge speed due to the smaller radius of the tops of the plurality of vent holes 6, so the shock absorption performance of the utility model is improved, then the lugs 10, the first pulley 12 and the second pulley 14 are positioned in the same horizontal plane, the possibility of falling of the four-rotor flying platform 1 is reduced under the mutual cooperation of the three parts, the rebound condition of the air cushion can not appear, the protection performance is good, the embodiment specifically solves the problem that the spring structure, but the characteristic of spring makes unmanned aerial vehicle fall behind, easily takes place to bounce back, the relatively poor problem of protectiveness.

Although the invention has been described in detail with respect to the general description and the specific embodiments, it will be apparent to those skilled in the art that modifications and improvements can be made based on the invention. Therefore, such modifications and improvements are intended to be within the scope of the invention as claimed.

Claims

1. The utility model provides an integrated control system and laser-induced control system's laser fight unmanned aerial vehicle, includes four rotor flight platform (1), laser-induced control panel (18) and unmanned aerial vehicle controller (21), its characterized in that: a shell (15) is fixedly sleeved on the outer side of the four-rotor flight platform (1), and a protection mechanism is fixedly arranged at the bottom of the shell (15);

the protection mechanism comprises a transverse plate (3), the transverse plate (3) is arranged at the bottom of a shell (15), a plurality of cylinders (2) are fixedly arranged between the transverse plate (3) and the shell (15), an air cushion (5) is arranged at the bottom of the transverse plate (3), a plurality of connecting columns (4) are fixedly arranged between the transverse plate (3) and the air cushion (5), a plurality of air vents (6) are arranged at the top of the air cushion (5), the air vents (6) are arranged between the connecting columns (4), a plurality of rod bodies (7) are arranged inside the air cushion (5), the rod bodies (7) are movably connected with the air cushion (5) through rotating shafts, two traction ropes (8) are fixedly arranged inside the rod bodies (7), the bottoms of the two traction ropes (8) penetrate through the rod bodies (7) and extend to the bottoms of the rod bodies (7), and lead blocks (9) are fixedly arranged at the bottoms of the traction ropes (8), the bottom of the air cushion (5) is fixedly provided with a plurality of convex blocks (10).

2. The laser fighting unmanned aerial vehicle integrating the control system and the laser sensing control system according to claim 1, wherein: the radius of the top of the vent hole (6) is smaller than that of the bottom of the vent hole.

3. The laser fighting unmanned aerial vehicle integrating the control system and the laser sensing control system according to claim 1, wherein: diaphragm (3) front and back both sides all are fixed and are equipped with two supporting legs (11), two supporting leg (11) all establish in the air cushion (5) outside, supporting leg (11) one side is equipped with first pulley (12), first pulley (12) are through pivot and supporting leg (11) swing joint.

4. The laser fighting unmanned aerial vehicle integrating the control system and the laser sensing control system according to claim 3, wherein: the supporting leg (11) opposite side is fixed and is equipped with down tube (13), down tube (13) bottom is fixed and is equipped with second pulley (14), second pulley (14) and first pulley (12) bottom are located same water flat line.

5. The laser fighting unmanned aerial vehicle integrating the control system and the laser sensing control system according to claim 4, wherein: the height of the plane where the bottoms of the second pulley (14) and the first pulley (12) are positioned is higher than that of the plane where the bump (10) is positioned.

6. The laser fighting unmanned aerial vehicle integrating the control system and the laser sensing control system according to claim 1, wherein: the LED lamp is characterized in that a base frame (16) is fixedly arranged inside the shell (15), an LED lamp set (17) is fixedly arranged at the bottom of the shell (15), and the LED lamp set (17) is arranged among the columns (2).

7. The laser fighting unmanned aerial vehicle integrating the control system and the laser sensing control system according to claim 6, wherein: laser-induced control panel (18) are fixed to be established in diaphragm (3) bottom, laser-induced control panel (18) are established between a plurality of spliced poles (4), laser-induced control panel (18) receiving end is fixed and is equipped with laser receiver (19), laser receiver (19) are fixed to be established in casing (15) one side, laser-induced control panel (18) output end is fixed and is equipped with laser emitter (20), establish between diaphragm (3) and air cushion (5) laser emitter (20), laser-induced control panel (18) and LED banks (17) electric connection.

8. The integrated control system and laser induction control system's laser fight unmanned aerial vehicle of claim 7, characterized in that: unmanned aerial vehicle controller (21) and laser induction control panel (18) wireless connection.