CN213384714U

CN213384714U - Exploration unmanned aerial vehicle convenient to use

Info

Publication number: CN213384714U
Application number: CN202021902524.7U
Authority: CN
Inventors: 刘高森
Original assignee: Yunnan Gaoke Xinnong Technology Co ltd
Current assignee: Yunnan Gaoke Xinnong Technology Co ltd
Priority date: 2020-09-03
Filing date: 2020-09-03
Publication date: 2021-06-08
Anticipated expiration: 2030-09-03

Abstract

The utility model discloses an exploration unmanned aerial vehicle convenient to use, which comprises a bod, the front end and the equal fixedly connected with wing in rear end at organism both sides top, the bottom fixedly connected with camera of organism, the front end and the equal fixedly connected with loading board in rear end of organism both sides bottom. The utility model discloses a set up the loading board, supporting mechanism, the limiting plate, the fixed block, the slide bar, the sliding sleeve, first spring, the baffle-box, the second spring, the buffer board, the buffering post, the backup pad, the third spring, the spout, slider and slipmat mutually support, the improvement unmanned aerial vehicle shock attenuation effect of exploration has been reached, the advantage that the convenient to use person used, make unmanned aerial vehicle of exploration when descending, can effectually improve unmanned aerial vehicle's the buffering protective properties of exploration, simultaneously effectually carry out the shock attenuation to unmanned aerial vehicle of exploration, prevent to topple over the problem of breaking when unmanned aerial vehicle of exploration falls to the ground, unmanned aerial vehicle's of exploration life has been prolonged, the.

Description

Exploration unmanned aerial vehicle convenient to use

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is an exploration unmanned aerial vehicle convenient to use.

Background

The unmanned plane is called unmanned plane for short, and is called UAV in English for short, and is an unmanned plane operated by radio remote control equipment and a self-contained program control device, or autonomously, either completely or intermittently, by an on-board computer, a drone is often more suitable for tasks that are too "fool-, dirty-or dangerous" than a drone, which, depending on the field of application, the unmanned aerial vehicle can be divided into military use and civil use, the unmanned aerial vehicle is divided into a reconnaissance plane and a target drone, the unmanned aerial vehicle is applied to the industry in the civil use, the unmanned aerial vehicle is really just needed, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express delivery transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, electric power inspection, disaster relief, movie and television shooting, romantic manufacturing and the like at present, the application of the unmanned aerial vehicle is greatly expanded, and the developed countries are also actively expanding the industrial application and developing the unmanned aerial vehicle technology.

When carrying out the topography exploration, need use exploration unmanned aerial vehicle, present exploration unmanned aerial vehicle has following shortcoming: the existing unmanned aerial vehicle for exploration has poor damping effect, so that the unmanned aerial vehicle for exploration is easy to topple and break when falling to the ground due to poor damping effect, the service life of the unmanned aerial vehicle for exploration is shortened, and the unmanned aerial vehicle for exploration cannot meet the use requirements of users due to the use of inconvenient users.

SUMMERY OF THE UTILITY MODEL

Technical problem to be solved

Not enough to prior art, the utility model provides an exploration unmanned aerial vehicle convenient to use possesses the improvement and surveys unmanned aerial vehicle shock attenuation effect, and the advantage that the user of being convenient for used has solved current exploration unmanned aerial vehicle shock attenuation effect not good, leads to exploring unmanned aerial vehicle when descending, because the buffering shock attenuation is poor, causes to survey unmanned aerial vehicle to appear empting the problem of breaking easily when falling to the ground.

(II) technical scheme

In order to achieve the above object, the utility model provides a following technical scheme: an exploration unmanned aerial vehicle convenient to use comprises a machine body, wings are fixedly connected to the front end and the rear end of the tops of two sides of the machine body, a camera is fixedly connected to the bottom of the machine body, a bearing plate is fixedly connected to the front end and the rear end of the bottoms of two sides of the machine body, a supporting mechanism is arranged at the top of the bearing plate, limiting plates are fixedly connected to two sides of the bottom of the bearing plate, fixing blocks are fixedly connected to the top and the bottom of the inner side of each limiting plate, a sliding rod is fixedly connected to the inner side of each fixing block, a sliding sleeve is sleeved at the center of the surface of the sliding rod, a first spring is sleeved at the top and the bottom of the surface of the sliding rod, a buffer box is fixedly connected to the inner side of the sliding sleeve, second springs are fixedly connected to two sides of the top of the inner wall of the, the bottom of bumping post runs through to the bottom and the fixedly connected with backup pad of baffle-box, the equal fixedly connected with third spring in four corners at backup pad top, the top of third spring and the bottom fixed connection of baffle-box.

Preferably, the supporting mechanism comprises a supporting block, four corners of the outer side of the supporting block are fixedly connected with the center of the outer side of the machine body through bolts, a supporting column is fixedly connected with the center of the outer side of the supporting block, and the bottom of the supporting column is fixedly connected with the top of the bearing plate.

Preferably, the inner end of the first spring is fixedly connected with the outer side of the sliding sleeve, and the outer end of the first spring is fixedly connected with the inner side of the fixing block.

Preferably, the spout has all been seted up to the both sides of baffle-box inner wall, the inner chamber sliding connection of spout has the slider, the inboard outside fixed connection with the buffer board of slider.

Preferably, the bottom of the supporting plate is bonded with a non-slip mat, and the bottom of the non-slip mat is fixedly connected with a non-slip bump.

(III) advantageous effects

Compared with the prior art, the utility model provides an exploration unmanned aerial vehicle convenient to use possesses following beneficial effect:

1. the utility model discloses a set up the loading board, supporting mechanism, the limiting plate, the fixed block, the slide bar, the sliding sleeve, first spring, the baffle-box, the second spring, the buffer board, the buffering post, the backup pad, the third spring, the spout, slider and slipmat mutually support, the improvement unmanned aerial vehicle shock attenuation effect of exploration has been reached, the advantage that the convenient to use person used, make unmanned aerial vehicle of exploration when descending, can effectually improve unmanned aerial vehicle's of exploration buffering protective properties, simultaneously effectually carry out the shock attenuation to unmanned aerial vehicle of exploration, prevent to topple over the problem of breaking when unmanned aerial vehicle of exploration falls to the ground, unmanned aerial vehicle's life has been prolonged, the person of facilitating the use uses, user's.

2. The utility model discloses a set up supporting mechanism, play the fixed effect of support to the organism, through setting up the fixed block, the slide bar, sliding sleeve and first spring are mutually supported, to the baffle-box, cushion column and backup pad play the absorbing effect of buffering, through setting up the second spring, to the buffer board, cushion column and backup pad play the absorbing effect of buffering, through setting up the third spring, play the absorbing effect of buffering to backup pad and cushion column, through setting up spout and slider, play stable effect when removing to the buffer board, through setting up the slipmat, play skid-proof effect to the backup pad.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is an enlarged view of the sectional view of the internal structure of the buffer box of the present invention;

fig. 3 is a left side view structure diagram of the present invention.

In the figure: 1. a body; 2. an airfoil; 3. a camera; 4. a carrier plate; 5. a support mechanism; 51. a support block; 52. a support pillar; 6. a limiting plate; 7. a fixed block; 8. a slide bar; 9. a sliding sleeve; 10. a first spring; 11. a buffer tank; 12. a second spring; 13. a buffer plate; 14. a buffer column; 15. a support plate; 16. a third spring; 17. a chute; 18. a slider; 19. a non-slip mat.

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.

All the components of the present invention are general standard components or components known to those skilled in the art, and the structure and principle thereof can be known to those skilled in the art through technical manuals or through routine experimental methods.

Referring to fig. 1-3, a exploration unmanned aerial vehicle convenient to use comprises a machine body 1, wings 2 are fixedly connected to the front end and the rear end of the top of two sides of the machine body 1, a camera 3 is fixedly connected to the bottom of the machine body 1, a bearing plate 4 is fixedly connected to the front end and the rear end of the bottom of two sides of the machine body 1, a supporting mechanism 5 is arranged on the top of the bearing plate 4, a limiting plate 6 is fixedly connected to two sides of the bottom of the bearing plate 4, a fixing block 7 is fixedly connected to the top and the bottom of the inner side of the limiting plate 6, a sliding rod 8 is fixedly connected to the inner side of the fixing block 7, a sliding sleeve 9 is sleeved at the center of the surface of the sliding rod 8, a first spring 10 is sleeved on the top and the bottom of the surface of the sliding rod 8, a buffer box 11 is fixedly connected to the inner side of the sliding, the bottom of the buffer board 13 is fixedly connected with a buffer column 14, the bottom of the buffer column 14 penetrates to the bottom of the buffer box 11 and is fixedly connected with a support plate 15, four corners of the top of the support plate 15 are fixedly connected with third springs 16, the top of the third springs 16 is fixedly connected with the bottom of the buffer box 11, the support mechanism 5 comprises a support block 51, four corners of the outer side of the support block 51 are fixedly connected with the center of the outer side of the machine body 1 through bolts, a support column 52 is fixedly connected with the center of the outer side of the support block 51, the bottom of the support column 52 is fixedly connected with the top of the bearing board 4, the inner end of the first spring 10 is fixedly connected with the outer side of the sliding sleeve 9, the outer end of the first spring 10 is fixedly connected with the inner side of the fixed block 7, sliding grooves 17 are respectively arranged on two sides of the inner wall of the buffer box 11, the bottom of backup pad 15 is bonded and is connected with slipmat 19, the bottom fixedly connected with skid proof block of slipmat 19, through setting up supporting mechanism 5, play the fixed effect of support to organism 1, through setting up fixed block 7, slide bar 8, sliding sleeve 9 and first spring 10 are mutually supported, to baffle-box 11, cushion column 14 and backup pad 15 play the effect of buffering shock attenuation, through setting up second spring 12, to buffer plate 13, cushion column 14 and backup pad 15 play the effect of buffering shock attenuation, through setting up third spring 16, to backup pad 15 and cushion column 14 play the effect of buffering shock attenuation, through setting up spout 17 and slider 18, stable effect when moving to buffer plate 13, through setting up slipmat 19, play skid-proof effect to backup pad 15, through setting up loading board 4, supporting mechanism 5, limiting plate 6, fixed block 7, slide bar 8, sliding sleeve 9, First spring 10, buffer box 11, second spring 12, buffer board 13, cushion post 14, backup pad 15, third spring 16, spout 17, slider 18 and slipmat 19 mutually support, the improvement exploration unmanned aerial vehicle shock attenuation effect has been reached, the advantage that the person of being convenient for use used, make exploration unmanned aerial vehicle when descending, can effectual improvement exploration unmanned aerial vehicle's buffering protective properties, simultaneously effectual carry out the shock attenuation to exploration unmanned aerial vehicle, prevent to topple over the problem of breaking when exploration unmanned aerial vehicle falls to the ground, exploration unmanned aerial vehicle's life has been prolonged, the person of facilitating the use uses, user's user demand can be satisfied.

When the unmanned aerial vehicle is used, firstly, when the unmanned aerial vehicle body 1 falls to the ground, firstly, the anti-skid pad 19 and the support plate 15 vibrate, the anti-skid pad 19 plays an anti-skid role on the support plate 15, then the support plate 15 vibrates to buffer and absorb the support plate 15 through the third spring 16, simultaneously, the support plate 15 vibrates to drive the buffer column 14 to vibrate, the buffer column 14 vibrates to drive the buffer plate 13 to vibrate, the buffer plate 13 vibrates to drive the sliding block 18 to slide in the inner cavity of the sliding groove 17, so that the buffer plate 13 moves stably, simultaneously, the buffer plate 13 vibrates to buffer and absorb the vibration force of the buffer plate 13 through the second spring 12, simultaneously, the buffer box 11 vibrates to drive the sliding sleeve 9 to slide on the surface of the sliding rod 8, so that the buffer box 11 moves stably, simultaneously, the sliding sleeve 9 slides on the surface of the sliding rod 8, so that the sliding sleeve 9 performs elastic buffering and absorption on the first spring 10, convenient for the user to use.

The standard parts that use in this application file all can purchase from the market, and can order according to the record of description and attached drawing, the concrete connected mode of each part all adopts conventional means such as ripe bolt, rivet, welding among the prior art, machinery, part and equipment all adopt conventional model among the prior art, the control mode is come automatic control through the controller, the control circuit of controller can realize through the simple programming of technical staff in this field, belong to the common general knowledge in this field, and the utility model discloses mainly be used for protecting mechanical device, so the utility model discloses no longer explain in detail control mode and circuit connection.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an exploration unmanned aerial vehicle convenient to use, includes organism (1), its characterized in that: the aircraft engine body comprises an engine body (1), wherein wings (2) are fixedly connected to the front end and the rear end of the tops of the two sides of the engine body (1), a camera (3) is fixedly connected to the bottom of the engine body (1), a bearing plate (4) is fixedly connected to the front end and the rear end of the bottom of the two sides of the engine body (1), a supporting mechanism (5) is arranged at the top of the bearing plate (4), limiting plates (6) are fixedly connected to the two sides of the bottom of the bearing plate (4), fixing blocks (7) are fixedly connected to the top and the bottom of the inner side of each limiting plate (6), sliding rods (8) are fixedly connected to the inner sides of the fixing blocks (7), sliding sleeves (9) are arranged at the centers of the surfaces of the sliding rods (8), first springs (10) are sleeved at the tops and the bottoms of the surfaces of the sliding rods (8), a buffer box (11) is fixedly connected to the, the bottom fixedly connected with buffer board (13) of second spring (12), the bottom fixedly connected with cushion column (14) of buffer board (13), the bottom of cushion column (14) runs through to the bottom and the fixedly connected with backup pad (15) of baffle-box (11), the equal fixedly connected with third spring (16) in four corners at backup pad (15) top, the top of third spring (16) and the bottom fixed connection of baffle-box (11).

2. A prospecting drone ready for use according to claim 1, characterized in that: the supporting mechanism (5) comprises a supporting block (51), four corners of the outer side of the supporting block (51) are fixedly connected with the center of the outer side of the machine body (1) through bolts, a supporting column (52) is fixedly connected with the center of the outer side of the supporting block (51), and the bottom of the supporting column (52) is fixedly connected with the top of the bearing plate (4).

3. A prospecting drone ready for use according to claim 1, characterized in that: the inner end of the first spring (10) is fixedly connected with the outer side of the sliding sleeve (9), and the outer end of the first spring (10) is fixedly connected with the inner side of the fixed block (7).

4. A prospecting drone ready for use according to claim 1, characterized in that: spout (17) have all been seted up to the both sides of baffle-box (11) inner wall, the inner chamber sliding connection of spout (17) has slider (18), the inboard outside fixed connection with buffer board (13) of slider (18).

5. A prospecting drone ready for use according to claim 1, characterized in that: the bottom of the supporting plate (15) is connected with an anti-skid pad (19) in an adhesive mode, and the bottom of the anti-skid pad (19) is fixedly connected with an anti-skid bump.