CN213566447U - Traffic investigation is with shooting unmanned aerial vehicle - Google Patents
Traffic investigation is with shooting unmanned aerial vehicle Download PDFInfo
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- CN213566447U CN213566447U CN202022187296.6U CN202022187296U CN213566447U CN 213566447 U CN213566447 U CN 213566447U CN 202022187296 U CN202022187296 U CN 202022187296U CN 213566447 U CN213566447 U CN 213566447U
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Abstract
The utility model discloses a traffic investigation is with shooing unmanned aerial vehicle, which comprises a bod, the bottom of organism is by both sides all install the supporting legs, and the bottom of organism is by the middle-end and install the dead lever, the top of organism is by four corners all install the fixed block, four the top of fixed block all installs the rotation axis, and the both sides of rotation axis all install the wing, one side of dead lever is installed the bull stick, and one side of bull stick installs the camera, the four corners of organism all installs bracing piece two, and the four corners of organism is by both sides all install two bracing pieces one, the top of two bracing pieces one and bracing piece two is installed the safety cover, and the inboard of safety cover is installed a plurality of spring one; the utility model discloses can reduce the vibrations when unmanned aerial vehicle descends to contact the ground when using at unmanned aerial vehicle descending for the descending is more stable, can protect the wing when flight simultaneously and can also reduce the vibration that the unmanned aerial vehicle collision brought.
Description
Technical Field
The utility model belongs to the unmanned aerial vehicle field specifically is a traffic investigation is with shooting unmanned aerial vehicle.
Background
With the rapid development of economic science and technology in China, vehicles are rapidly increased, urban traffic jam is increasingly severe, traffic accidents are frequent, law enforcement vehicles cannot enter accident points in time to conduct field command work due to jam, command efficiency is low, traffic jam can be greatly reduced and accidents can be rapidly solved by monitoring traffic in real time through a traffic detection unmanned aerial vehicle.
The existing shooting unmanned aerial vehicle for traffic investigation has certain defects when in use, and the existing shooting unmanned aerial vehicle for traffic investigation cannot absorb shock when the unmanned aerial vehicle lands and contacts the ground when in use, so that other parts are easily damaged and the landing is unstable; the existing shooting unmanned aerial vehicle for traffic investigation can not protect wings when in use and can also reduce the vibration caused by collision of the unmanned aerial vehicle, so that the unmanned aerial vehicle is protected, the requirement of a user can not be met, and certain influence is brought to the reality.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a shooting unmanned aerial vehicle for traffic investigation, which effectively solves the problem that the existing shooting unmanned aerial vehicle for traffic investigation cannot absorb shock when the unmanned aerial vehicle lands and contacts the ground, thereby easily damaging other parts and having unstable landing; the vibration that can also reduce the unmanned aerial vehicle collision and bring when can not protect the wing when flying with shooting unmanned aerial vehicle when using to current traffic investigation to protect unmanned aerial vehicle's technical problem.
The purpose of the utility model can be realized by the following technical scheme:
the shooting unmanned aerial vehicle for traffic investigation comprises a machine body, wherein supporting legs are arranged on the bottom of the machine body close to two sides, a fixing rod is arranged on the bottom of the machine body close to the middle end, fixing blocks are arranged on the top of the machine body close to four corners, rotating shafts are arranged on the tops of the four fixing blocks, wings are arranged on two sides of each rotating shaft, a rotating rod is arranged on one side of each fixing rod, and a camera is arranged on one side of each rotating rod;
the four corners of the machine body are respectively provided with a second supporting rod, two first supporting rods are respectively arranged at the two sides of the four corners of the machine body, the tops of the first supporting rods and the second supporting rods are respectively provided with a protective cover, and the inner side of each protective cover is provided with a plurality of first springs;
the supporting legs include the montant, the thread bush is installed in the bottom outside of montant, and the bottom inboard of montant installs spring two, the horizontal pole is installed to the bottom of thread bush, and the bottom inboard of horizontal pole leans on to install spring three, the snubber block is installed to the bottom of spring three, and the bottom of snubber block is provided with the slipmat.
As a further scheme of the utility model, the bottom both sides fixed connection of organism is in the top of montant, and the fixed top of dead lever is connected in the bottom of organism, and the top of organism leans on four corners and four fixed block fixed connection.
As a further aspect of the present invention, the top of the fixed block is movably connected to the bottom of the rotating shaft, and the two sides of the rotating shaft are fixedly connected to the opposite sides of the two wings.
As a further aspect of the present invention, the outside fixed connection of one side of the rotating rod is inside one side of the camera, and the outside rotation of the other side of the rotating rod is connected inside one side of the fixing rod.
As a further scheme of the utility model, the outside of safety cover all is provided with silica gel, and the inboard both ends of safety cover and the both sides fixed connection of spring one, and the both sides of bracing piece one and bracing piece two respectively fixed connection in one side of safety cover and the side of organism.
As a further scheme of the utility model, the top and the bottom of spring two are fixed connection respectively in the bottom of montant and the top of horizontal pole, and the top and the bottom of thread bush are fixed connection respectively in the bottom of montant and the top of horizontal pole, and the top of upper end and snubber block are leaned on to the top of top and snubber block in the bottom inboard of horizontal pole in the roof of spring three and bottom fixed connection respectively, and the bottom fixed connection of snubber block is in the top of slipmat.
The utility model has the advantages that:
the utility model discloses a set up spring two and spring three cooperation snubber blocks and slipmat, supporting legs bottom contact ground, ground can have recoil force to unmanned aerial vehicle, cushion through spring two that sets up between horizontal pole and the montant, prevent that the vibration that the recoil force brought from makes other parts of unmanned aerial vehicle damage, the spring three that sets up at the snubber block top also can cushion the recoil force simultaneously, the snubber block bottom sets up the slipmat and makes the landing more stable simultaneously;
through setting up bracing piece one and bracing piece two cooperation spring one and safety cover, support through setting up two bracing pieces one and bracing piece two pairs of safety covers, the safety cover protects the wing when unmanned aerial vehicle collides with other objects aloft, can not make the wing damage cause unmanned aerial vehicle to fall, the safety cover inboard is provided with a plurality of spring one simultaneously for carry out the shock attenuation to unmanned aerial vehicle when the collision, prevent that the vibration from causing the influence for unmanned aerial vehicle's balance.
Drawings
FIG. 1 is a sectional view of the overall structure of the present invention;
fig. 2 is a top view of the machine body of the present invention;
FIG. 3 is a top sectional view of the protective cover of the present invention;
fig. 4 is a side sectional view of the supporting leg of the present invention.
In the figure: 1. a body; 2. supporting legs; 3. fixing the rod; 4. a fixed block; 5. a rotating shaft; 6. an airfoil; 7. a first supporting rod; 8. a protective cover; 9. a threaded sleeve; 10. a damper block; 11. a rotating rod; 12. a camera; 13. a second supporting rod; 14. a first spring; 15. a second spring; 16. a third spring; 17. a non-slip mat; 18. a vertical rod; 19. a cross bar.
Detailed Description
The technical solution of the present invention will be described clearly and completely with reference to the following embodiments, and it should be understood that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
As shown in fig. 1-4, a shooting unmanned aerial vehicle for traffic investigation comprises a machine body 1, wherein supporting legs 2 are respectively installed at the bottom of the machine body 1 close to two sides, a fixing rod 3 is installed at the bottom of the machine body 1 close to the middle end, fixing blocks 4 are respectively installed at the top of the machine body 1 close to four corners, rotating shafts 5 are respectively installed at the tops of the four fixing blocks 4, wings 6 are respectively installed at two sides of each rotating shaft 5, a rotating rod 11 is installed at one side of each fixing rod 3, and a camera 12 is installed at one side of each rotating rod 11;
four corners of the machine body 1 are respectively provided with a second support rod 13, two first support rods 7 are respectively arranged at two sides of the four corners of the machine body 1, protective covers 8 are arranged at the tops of the first support rods 7 and the second support rods 13, and a plurality of first springs 14 are arranged on the inner sides of the protective covers 8;
supporting legs 2 include montant 18, and threaded sleeve 9 is installed in the bottom outside of montant 18, and the bottom inboard of montant 18 installs spring two 15, and horizontal pole 19 is installed to the bottom of threaded sleeve 9, and the bottom inboard of horizontal pole 19 leans on to install spring three 16, and snubber block 10 is installed to the bottom of spring three 16, and the bottom of snubber block 10 is provided with slipmat 17.
Bottom both sides fixed connection of organism 1 is in the top of montant 18, and the top of dead lever 3 fixing is connected in the bottom of organism 1, and organism 1's top leans on four corners and 4 fixed connection of four fixed blocks, and montant 18 sets up and supports ground when fixed connection makes things convenient for unmanned aerial vehicle to descend.
The top of the fixed block 4 is movably connected with the bottom of the rotating shaft 5, and two sides of the rotating shaft 5 are fixedly connected with the opposite sides of the two wings 6.
One side of the rotating rod 11 is fixedly connected to the inside of one side of the camera 12, and the other side of the rotating rod 11 is rotatably connected to the inside of one side of the fixing rod 3.
The outside of safety cover 8 all is provided with silica gel, and the inboard both ends of safety cover 8 and the both sides fixed connection of spring 14, and the both sides of bracing piece 7 and bracing piece two 13 respectively fixed connection in one side of safety cover 8 and the side of organism 1, vibration caused the damage for the unmanned aerial vehicle part when setting up silica gel and spring 14 reduction collision.
The top and the bottom of the second spring 15 are respectively and fixedly connected to the bottom of the vertical rod 18 and the top of the cross rod 19, the top and the bottom of the threaded sleeve 9 are respectively and fixedly connected to the bottom of the vertical rod 18 and the top of the cross rod 19, the top plate and the bottom of the third spring 16 are respectively and fixedly connected to the inner side of the bottom of the cross rod 19 and close to the upper end and the top of the shock absorption block 10, and the bottom of the shock absorption block 10 is fixedly connected to the top of the non-slip mat.
A shooting unmanned aerial vehicle for traffic investigation, when using, firstly start the unmanned aerial vehicle through the outer MC6A controller, the rotating shaft 5 drives the wing 6 to rotate, under the effect of lifting, the unmanned aerial vehicle body 1 lifts off, the bottom of the body 1 is fixedly connected with a fixed rod 3 and one side of the body is fixed by a camera 12 through a rotating rod 11, the rotating rod 11 rotates to drive the camera 12 to rotate, thereby carrying out traffic investigation shooting, when the unmanned aerial vehicle descends, the bottom of a supporting leg 2 contacts the ground, the ground can have recoil force to the unmanned aerial vehicle, the shock is buffered through a spring II 15 arranged between a cross bar 19 and a vertical bar 18, the vibration caused by the recoil force can be prevented from damaging other parts of the unmanned aerial vehicle, meanwhile, a spring III 16 arranged at the top of a shock absorption block 10 can also buffer the recoil force, meanwhile, a non-slip mat 17 arranged at the bottom of the shock absorption block 10 can make the descending more stable, a protective cover 8 is supported, when unmanned aerial vehicle collides with other objects aloft, the protective cover 8 protects the wings 6, so that the wings 6 are not damaged to cause the unmanned aerial vehicle to fall, and meanwhile, the inner side of the protective cover 8 is provided with a plurality of springs 14, so that the unmanned aerial vehicle is damped when colliding, and the influence on the balance of the unmanned aerial vehicle caused by vibration is prevented.
The utility model discloses a set up spring two 15 and spring three 16 cooperation snubber block 10 and slipmat 17, 2 bottoms of supporting legs contact ground, ground can have recoil force to unmanned aerial vehicle, cushion through spring two 15 that sets up between horizontal pole 19 and montant 18, prevent that the vibration that the recoil force brought from making other parts of unmanned aerial vehicle damage, spring three 16 that the top of snubber block 10 set up can cushion the recoil force too simultaneously, the setting of 10 bottoms of snubber blocks has slipmat 17 to make the landing more stable simultaneously; through setting up bracing piece one 7 and bracing piece two 13 cooperation spring one 14 and safety cover 8, support safety cover 8 through setting up two bracing pieces one 7 and bracing piece two 13, safety cover 8 protects wing 6 when unmanned aerial vehicle collides with other objects aloft, can not make wing 6 damage cause unmanned aerial vehicle to fall, 8 inboards of safety cover are provided with a plurality of spring one 14 simultaneously, make when colliding carry out the shock attenuation to unmanned aerial vehicle, prevent that the vibration from leading to the fact the influence for unmanned aerial vehicle's balance.
The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.
Claims (6)
1. The utility model provides a traffic investigation is with shooing unmanned aerial vehicle which characterized in that: the airplane wing fixing device comprises an airplane body (1), supporting legs (2) are mounted on the bottom of the airplane body (1) by means of two sides, a fixing rod (3) is mounted on the bottom of the airplane body (1) by means of the middle end, fixing blocks (4) are mounted on the top of the airplane body (1) by means of four corners, rotating shafts (5) are mounted on the tops of the four fixing blocks (4), wings (6) are mounted on the two sides of each rotating shaft (5), a rotating rod (11) is mounted on one side of each fixing rod (3), and a camera (12) is mounted on one side of each rotating rod (11);
two support rods II (13) are mounted at four corners of the machine body (1), two support rods I (7) are mounted at two sides of the four corners of the machine body (1), protective covers (8) are mounted at the tops of the two support rods I (7) and the support rods II (13), and a plurality of springs I (14) are mounted on the inner sides of the protective covers (8);
the supporting legs (2) include montant (18), thread bush (9) are installed in the bottom outside of montant (18), and the bottom inboard of montant (18) installs spring two (15), horizontal pole (19) are installed to the bottom of thread bush (9), and the bottom inboard of horizontal pole (19) leans on to install spring three (16), snubber block (10) are installed to the bottom of spring three (16), and the bottom of snubber block (10) is provided with slipmat (17).
2. The photographing unmanned aerial vehicle for traffic investigation of claim 1, wherein: the bottom both sides fixed connection of organism (1) is in the top of montant (18), and the top of dead lever (3) fixed is connected in the bottom of organism (1), and the top of organism (1) leans on four corners and four fixed block (4) fixed connection.
3. The photographing unmanned aerial vehicle for traffic investigation of claim 1, wherein: the top of the fixed block (4) is movably connected with the bottom of the rotating shaft (5), and two sides of the rotating shaft (5) are fixedly connected to the opposite sides of the two wings (6).
4. The photographing unmanned aerial vehicle for traffic investigation of claim 1, wherein: the outer portion of one side of the rotating rod (11) is fixedly connected to the inner portion of one side of the camera (12), and the outer portion of the other side of the rotating rod (11) is rotatably connected to the inner portion of one side of the fixing rod (3).
5. The photographing unmanned aerial vehicle for traffic investigation of claim 1, wherein: the outside of safety cover (8) all is provided with silica gel, and the inboard both ends of safety cover (8) and the both sides fixed connection of spring (14), and the both sides of bracing piece (7) and bracing piece two (13) fixed connection respectively in one side of safety cover (8) and the side of organism (1).
6. The photographing unmanned aerial vehicle for traffic investigation of claim 1, wherein: the top and the bottom of spring two (15) are fixed connection respectively in the bottom of montant (18) and the top of horizontal pole (19), and the top and the bottom of thread bush (9) are fixed connection respectively in the bottom of montant (18) and the top of horizontal pole (19), and the roof and the bottom of spring three (16) are fixed connection respectively and lean on the top of upper end and snubber block (10) in the bottom inboard of horizontal pole (19), and the bottom fixed connection of snubber block (10) is in the top of slipmat (17).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022187296.6U CN213566447U (en) | 2020-09-29 | 2020-09-29 | Traffic investigation is with shooting unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022187296.6U CN213566447U (en) | 2020-09-29 | 2020-09-29 | Traffic investigation is with shooting unmanned aerial vehicle |
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| CN213566447U true CN213566447U (en) | 2021-06-29 |
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| CN202022187296.6U Active CN213566447U (en) | 2020-09-29 | 2020-09-29 | Traffic investigation is with shooting unmanned aerial vehicle |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114524087A (en) * | 2022-02-28 | 2022-05-24 | 北京博瑞翔伦科技发展有限公司 | Unmanned aerial vehicle detection interference system's unmanned aerial vehicle protective structure |
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2020
- 2020-09-29 CN CN202022187296.6U patent/CN213566447U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114524087A (en) * | 2022-02-28 | 2022-05-24 | 北京博瑞翔伦科技发展有限公司 | Unmanned aerial vehicle detection interference system's unmanned aerial vehicle protective structure |
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