CN213057511U - Fire control unmanned aerial vehicle of utensil investigation function - Google Patents

Fire control unmanned aerial vehicle of utensil investigation function Download PDF

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Publication number
CN213057511U
CN213057511U CN202021518393.2U CN202021518393U CN213057511U CN 213057511 U CN213057511 U CN 213057511U CN 202021518393 U CN202021518393 U CN 202021518393U CN 213057511 U CN213057511 U CN 213057511U
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China
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wall
aerial vehicle
unmanned aerial
recess
damping spring
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CN202021518393.2U
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Chinese (zh)
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刘运鸿
刘志斌
钟群
姜海云
王文
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Changsha Bosun Intelligent Fire Technology Co ltd
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Changsha Bosun Intelligent Fire Technology Co ltd
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Abstract

The utility model discloses a utensil investigation function's fire control unmanned aerial vehicle, which comprises a bod, a pedestal, anticollision piece and two grip blocks, two supporting legs have all been welded to the both sides of bottom of the body outer wall, and the bottom welding of supporting leg has the buffing pad, set up the recess that is equidistance structural distribution on the outer wall at base top, and the inside sliding connection of recess has the support column that is connected with the buffing pad, the welding has the first damping spring who is connected with the support column on the inner wall of recess bottom, and the support column has cup jointed the second damping spring on being located the outside outer wall of recess. The utility model discloses first damping spring and second damping spring can have the effect of buffer protection to it when unmanned aerial vehicle falls to the ground, can avoid unmanned aerial vehicle directly to fall to subaerial production vibrations and cause the damage to internals, have prolonged unmanned aerial vehicle's life, can prevent to rise on blade and the driving motor striking wall, and damping spring can alleviate the impact force that the crash bar hit on the wall.

Description

Fire control unmanned aerial vehicle of utensil investigation function
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to a fire control unmanned aerial vehicle of utensil investigation function.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, the unmanned aerial vehicle is a general name of the unmanned aerial vehicle actually, and the unmanned aerial vehicle can be defined from the technical point of view as follows: compared with manned aircraft, the unmanned fixed wing aircraft has the advantages of small volume, low manufacturing cost, convenient use, low requirement on the operational environment, strong battlefield viability and the like.
Current unmanned aerial vehicle does not install damping device mostly, and unmanned aerial vehicle produces the vibration when descending to ground, leads to unmanned aerial vehicle inside part and equipment to cause the damage to do not have the function of anticollision, lead to damaging after making the wing pole receive the striking with the blade that rises easily, consequently, the fire control unmanned aerial vehicle who needs to design an utensil investigation function solves above-mentioned problem urgently.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the fire control unmanned aerial vehicle of a utensil investigation function that proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
the utility model provides a fire control unmanned aerial vehicle of investigation function, includes organism, base, anticollision piece and two grip blocks, two supporting legs have all been welded to the both sides of bottom of the body outer wall, and the bottom welding of supporting leg has the buffing pad, set up the recess that is equidistance structural distribution on the outer wall at base top, and the inside sliding connection of recess has the support column that is connected with the buffing pad, the welding has the first damping spring who is connected with the support column on the inner wall of recess bottom, and the support column is located and has cup jointed the second damping spring on the outside outer wall of recess.
Furthermore, the spacing groove has all been seted up to the both sides of base top outer wall, and two otic placodes, two have all been welded to the both sides of buffer base bottom outer wall rotate through the bearing on the outer wall of the adjacent one side of otic placode and are connected with the connecting rod, and the other end that the otic placode was kept away from to the connecting rod rotates through the pivot and is connected with the spacing wheel of slip in spacing inslot portion.
Further, install four wing bars that are equidistant structure and distribute through the bolt on the lateral wall of organism, and the other end that the body was kept away from to the wing bar installs driving motor through the bolt, two ascending blades are installed through the bolt to the output at driving motor top.
Furthermore, the outer wall of the driving motor, which is far away from the other side of the wing rod, is provided with an anti-collision rod through a bolt, the outer wall of one side, adjacent to the anti-collision rod and the anti-collision block, of the anti-collision rod is provided with a spring groove, and the inner wall of one side, adjacent to the spring groove, of the spring groove is welded with a buffer spring.
Further, install the camera and put in the frame through the bolt on the outer wall of bottom of the body respectively, and put in and be connected with the bottom plate through the pivot rotation on the outer wall of frame bottom, the welding has the stay cord on the outer wall of bottom plate one side, and the top of stay cord is provided with the lantern ring.
Furthermore, put in and rotate through the pivot on the outer wall of frame one side and be connected with the semi-ring, and the lantern ring cup joints the outside at the semi-ring, put in and be provided with the electro-magnet on the frame is close to one side outer wall of semi-ring, and the bottom of semi-ring is provided with the iron plate that adsorbs mutually with the electro-magnet.
Furthermore, all be connected with the supporting rod through the pivot rotation on the outer wall of putting in frame and the adjacent one side of grip block, and all weld on the outer wall of grip block both sides has two protruding poles, horizontal adjacent two the rubber circle has been cup jointed to the outside of protruding pole.
The utility model has the advantages that:
1. through buffer seat, base, recess, support column, first damping spring, second damping spring, spacing groove and the spacing wheel that sets up, first damping spring and second damping spring can have the effect of buffer protection to it when unmanned aerial vehicle falls to the ground, can avoid unmanned aerial vehicle directly to fall to subaerial production vibrations and cause the damage to internals, have prolonged unmanned aerial vehicle's life.
2. Through the crash bar, the crash block and the buffer spring which are arranged, the rising blade and the driving motor can be prevented from colliding with the wall, the buffer spring can relieve the impact force of the crash bar on colliding with the wall, and then the machine body, the driving motor and the rising blade are protected.
3. Through the putting in frame, stay cord, the lantern ring, electro-magnet, iron plate, grip block and the rubber circle that sets up, the rubber circle can be fixed article, and when the electro-magnet was kept away from with the iron plate, because the action of gravity makes article between two grip blocks automatic put in, it is more convenient to use.
Drawings
Fig. 1 is a schematic view of a three-dimensional structure of a fire-fighting unmanned aerial vehicle with a detection function provided by the present invention;
fig. 2 is a schematic view of a damping structure of a fire-fighting unmanned aerial vehicle with a detection function provided by the utility model;
fig. 3 is a schematic structural view of a throwing frame of a fire-fighting unmanned aerial vehicle with a detection function provided by the utility model;
fig. 4 is a schematic view of an anti-collision structure of a fire-fighting unmanned aerial vehicle with a detection function provided by the utility model;
fig. 5 is the utility model provides a fire control unmanned aerial vehicle's of utensil investigation function stay cord fixed knot constructs the schematic diagram.
In the figure: 1 organism, 2 cushion blocks, 3 bases, 4 grooves, 5 support columns, 6 first damping springs, 7 second damping springs, 8 limit grooves, 9 lug plates, 10 connecting rods, 11 limit wheels, 12 support legs, 13 wing rods, 14 driving motors, 15 bumper bars, 16 bumper blocks, 17 damping springs, 18 spring grooves, 19 putting frames, 20 bottom plates, 21 pull ropes, 22 rising blades, 23 half rings, 24 lantern rings, 25 electromagnets, 26 iron blocks, 27 cameras, 28 clamping rods, 29 clamping blocks, 30 convex rods and 31 rubber rings.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. 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.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When a component is referred to as being "connected" to another component, it can be directly connected to the other component or intervening components may also be present. When a component is referred to as being "disposed on" another component, it can be directly on the other component or intervening components may also be present. The terms "vertical," "horizontal," "left," "right," and the like as used herein are for illustrative purposes only.
Unless defined otherwise, all technical and scientific terms used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. The terminology used in the description of the invention herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. As used herein, the term "and/or" includes any and all combinations of one or more of the associated listed items.
Please refer to fig. 1 to 5 simultaneously, a fire control unmanned aerial vehicle of investigation function, which comprises a bod 1, a pedestal 3, anticollision piece 16 and two grip blocks 29, two supporting legs 12 have all been welded to the both sides of 1 bottom outer wall of organism, and the bottom welding of supporting leg 12 has buffer seat 2, set up the recess 4 that is equidistance structural distribution on the outer wall at base 3 top, and the inside sliding connection of recess 4 has the support column 5 that is connected with buffer seat 2, the welding has the first damping spring 6 that is connected with support column 5 on the inner wall of recess 4 bottom, and support column 5 has cup jointed second damping spring 7 on being located the outside outer wall of recess 4, first damping spring 6 and second damping spring 7 can weaken the impact force that unmanned aerial vehicle produced when falling to ground, have shock attenuation protection's function to unmanned aerial vehicle.
Further, spacing groove 8 has all been seted up to the both sides of 3 top outer walls of base, and two otic placodes 9 have all been welded to the both sides of 2 bottom outer walls of cushion socket, it is connected with connecting rod 10 to rotate through the bearing on the outer wall of two adjacent one sides of otic placode 9, and connecting rod 10 keeps away from the other end of otic placode 9 and is connected with the spacing wheel 11 that slides in spacing groove 8 inside through the pivot rotation, spacing wheel 11 has spacing function to it when enabling cushion socket 2 to remove, skew when can preventing unmanned aerial vehicle from falling to the ground.
Further, four wing rods 13 which are distributed in an equidistant structure are installed on the outer side wall of the machine body 1 through bolts, a driving motor 14 is installed at the other end, far away from the machine body 1, of the wing rods 13 through bolts, two ascending blades 22 are installed at the output end of the top of the driving motor 14 through bolts, the type of the driving motor 14 is X-TEAM2212, and the driving motor 14 can be fixed through the wing rods 13.
Further, the crash bar 15 is installed on the outer wall of the driving motor 14 far away from the other side of the wing rod 13 through a bolt, the spring groove 18 is formed in the outer wall of one side, adjacent to the crash bar 15 and the crash block 16, the buffer spring 17 is welded on the inner wall of one side, adjacent to the spring groove 18, the impact force of the crash bar 15 and the crash block 16 can be weakened through the buffer spring 17, and the unmanned aerial vehicle can be protected in an all-around mode.
Further, install camera 27 and put in frame 19 through the bolt on the outer wall of organism 1 bottom respectively, and put in and be connected with bottom plate 20 through the pivot rotation on the outer wall of frame 19 bottom, the welding has stay cord 21 on the outer wall of bottom plate 20 one side, and the top of stay cord 21 is provided with lantern ring 24, and camera 27 can be to investigation on the spot, can in time discover conflagration and survey the real-time condition of fire control.
Furthermore, put in on the outer wall of frame 19 one side and rotate through the pivot and be connected with semi-ring 23, and lantern ring 24 cup joints the outside at semi-ring 23, puts in and is provided with electro-magnet 25 on the outer wall of frame 19 one side near semi-ring 23, and semi-ring 23's bottom is provided with the iron plate 26 that adsorbs mutually with the electro-magnet, and when iron plate 26 adsorbs on electro-magnet 25, can fix bottom plate 20.
Further, the clamping rods 28 are rotatably connected to the outer walls of the adjacent sides of the releasing frame 19 and the clamping block 29 through rotating shafts, the two convex rods 30 are welded to the outer walls of the two sides of the clamping block 29, the rubber rings 31 are sleeved outside the two transversely adjacent convex rods 30, the rubber rings 31 can fix released articles, and the articles can be prevented from falling in the air.
The working principle is as follows: when the fire-fighting unmanned aerial vehicle with the investigation function is used, articles to be thrown are placed between two clamping blocks 29, rubber rings 31 are sleeved on two transversely adjacent convex rods, the rubber rings 31 can fix the articles, when the unmanned aerial vehicle runs, the buffer springs 17 can prevent the driving motor 14 and the ascending blades 22 from impacting the wall surface, meanwhile, the impact force received by the anti-collision blocks 16 and the anti-collision rods 15 can be relieved, the unmanned aerial vehicle can be further protected, when the articles need to be thrown, a button of the electromagnet 25 is controlled to be turned off on the ground, the pull rope 21 drives the lantern ring 24 and the iron block to fall down after the gravity of the articles is received, the iron block 26 is separated from the electromagnet 25, at the moment, the bottom plate 20 inclines, the articles can be thrown due to falling of the gravity, meanwhile, the on-site investigation can be carried out through the camera 27, the fire can be timely discovered when the unmanned aerial vehicle falls to the ground, first damping spring 6 and second damping spring 7 can have certain cushioning effect to base 3 and cushion 2, can weaken unmanned aerial vehicle and fall to the impact force that ground made the production to avoid the unmanned aerial vehicle internals to receive the condition of damage behind the impact force, can prolong unmanned aerial vehicle's life.
The above, only be the concrete implementation of the preferred embodiment of the present invention, but the protection scope of the present invention is not limited thereto, and any person skilled in the art is in the technical scope of the present invention, according to the technical solution of the present invention and the utility model, the concept of which is equivalent to replace or change, should be covered within the protection scope of the present invention.

Claims (7)

1. The utility model provides a fire control unmanned aerial vehicle of investigation function, includes organism (1), base (3), anticollision piece (16) and two grip blocks (29), its characterized in that, two supporting legs (12) have all been welded to the both sides of organism (1) bottom outer wall, and the bottom welding of supporting leg (12) has buffer seat (2), set up recess (4) that are equidistance structural distribution on the outer wall at base (3) top, and the inside sliding connection of recess (4) has support column (5) that are connected with buffer seat (2), the welding has first damping spring (6) that are connected with support column (5) on the inner wall of recess (4) bottom, and support column (5) are located and cup jointed second damping spring (7) on the outer wall of recess (4) outside.
2. The unmanned fire fighting vehicle with the detection function according to claim 1, wherein the base (3) is provided with a limiting groove (8) on both sides of the top outer wall, the buffer base (2) is welded with two ear plates (9) on both sides of the bottom outer wall, the outer wall on the adjacent side of the two ear plates (9) is rotatably connected with a connecting rod (10) through a bearing, and the other end of the connecting rod (10) far away from the ear plates (9) is rotatably connected with a limiting wheel (11) sliding in the limiting groove (8) through a rotating shaft.
3. The fire-fighting unmanned aerial vehicle with the detection function is characterized in that four wing rods (13) which are distributed in an equidistant structure are mounted on the outer side wall of the machine body (1) through bolts, a driving motor (14) is mounted at the other end, far away from the machine body (1), of each wing rod (13) through a bolt, and two lifting blades (22) are mounted at the output end of the top of the driving motor (14) through bolts.
4. The unmanned fire fighting vehicle with the detection function according to claim 3, wherein the outer wall of the driving motor (14) on the other side away from the wing rod (13) is provided with an anti-collision rod (15) through a bolt, the outer walls of the anti-collision rod (15) and the anti-collision block (16) on the adjacent sides are provided with spring grooves (18), and the inner wall of the spring groove (18) on the adjacent side is welded with a buffer spring (17).
5. The unmanned fire fighting vehicle with the investigation function according to claim 1, wherein the outer wall of the bottom of the machine body (1) is provided with a camera (27) and a throwing frame (19) through bolts, the outer wall of the bottom of the throwing frame (19) is rotatably connected with a bottom plate (20) through a rotating shaft, the outer wall of one side of the bottom plate (20) is welded with a pull rope (21), and the top end of the pull rope (21) is provided with a lantern ring (24).
6. The unmanned fire fighting vehicle with the investigation function according to claim 5, wherein the outer wall of one side of the throwing frame (19) is rotatably connected with a half ring (23) through a rotating shaft, a sleeve ring (24) is sleeved outside the half ring (23), the outer wall of one side of the throwing frame (19) close to the half ring (23) is provided with an electromagnet (25), and the bottom end of the half ring (23) is provided with an iron block (26) adsorbed with the electromagnet.
7. The unmanned fire fighting vehicle with the investigation function according to claim 5, wherein the outer walls of the adjacent sides of the throwing frame (19) and the clamping block (29) are rotatably connected with clamping rods (28) through rotating shafts, the outer walls of the two sides of the clamping block (29) are welded with two convex rods (30), and the outer parts of the two transversely adjacent convex rods (30) are sleeved with rubber rings (31).
CN202021518393.2U 2020-07-28 2020-07-28 Fire control unmanned aerial vehicle of utensil investigation function Active CN213057511U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202021518393.2U CN213057511U (en) 2020-07-28 2020-07-28 Fire control unmanned aerial vehicle of utensil investigation function

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202021518393.2U CN213057511U (en) 2020-07-28 2020-07-28 Fire control unmanned aerial vehicle of utensil investigation function

Publications (1)

Publication Number Publication Date
CN213057511U true CN213057511U (en) 2021-04-27

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ID=75577994

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202021518393.2U Active CN213057511U (en) 2020-07-28 2020-07-28 Fire control unmanned aerial vehicle of utensil investigation function

Country Status (1)

Country Link
CN (1) CN213057511U (en)

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