CN214566151U - A unmanned aerial vehicle structure for water ring survey and drawing - Google Patents
A unmanned aerial vehicle structure for water ring survey and drawing Download PDFInfo
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- CN214566151U CN214566151U CN202120155752.0U CN202120155752U CN214566151U CN 214566151 U CN214566151 U CN 214566151U CN 202120155752 U CN202120155752 U CN 202120155752U CN 214566151 U CN214566151 U CN 214566151U
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- unmanned aerial
- aerial vehicle
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- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 title claims abstract description 33
- 238000009434 installation Methods 0.000 claims abstract description 25
- 235000017166 Bambusa arundinacea Nutrition 0.000 claims abstract description 12
- 235000017491 Bambusa tulda Nutrition 0.000 claims abstract description 12
- 241001330002 Bambuseae Species 0.000 claims abstract description 12
- 235000015334 Phyllostachys viridis Nutrition 0.000 claims abstract description 12
- 239000011425 bamboo Substances 0.000 claims abstract description 12
- 238000013507 mapping Methods 0.000 claims abstract description 9
- 230000001681 protective effect Effects 0.000 claims abstract description 7
- 230000009189 diving Effects 0.000 claims description 8
- 238000004804 winding Methods 0.000 claims description 3
- 238000005188 flotation Methods 0.000 claims 1
- 238000004891 communication Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 241000196324 Embryophyta Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 238000010422 painting Methods 0.000 description 1
- 239000003643 water by type Substances 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle structure for water ring survey and drawing, including unmanned aerial vehicle main part, arc pole, chassis, connecting rod, first step motor and screw, unmanned aerial vehicle main part and arc pole fixed connection, arc pole and chassis welded connection, unmanned aerial vehicle main part and connecting rod fixed connection, the connecting rod is kept away from the one end and the first step motor fixed connection of unmanned aerial vehicle main part, the output and the screw fixed connection of first step motor, the bottom fixed mounting of unmanned aerial vehicle main part has an installation section of thick bamboo, the bottom detachable of an installation section of thick bamboo installs showy mechanism, be equipped with protective airbag on the chassis, showy mechanism includes barrel, connecting plate, fixed plate and outer cursory ring. The utility model discloses in, through when surveying and mapping on water again, the installation of floating mechanism before using, then fly unmanned aerial vehicle on water, then descend the surface of water and can make its stable on the surface of water, when the executable flight task, can be quick dismantle floating mechanism get off, make things convenient for the unmanned aerial vehicle multiple condition to use.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle structure for water ring survey and drawing.
Background
A drone is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device. Unmanned aerial vehicles are of a wide variety and mainly comprise fixed-wing unmanned aerial vehicles, flapping-wing unmanned aerial vehicles, multi-rotor unmanned aerial vehicles and the like. Because control simple, the reliability is high to do not need the runway alright with VTOL, can hover in the air after taking off, consequently for fixed wing unmanned aerial vehicle and flapping wing unmanned aerial vehicle, many rotor unmanned aerial vehicle use more extensively. Many rotor unmanned aerial vehicle usually has more than 3 rotors, and its maneuverability can be realized through torsion and the rotational speed that changes different rotors. Common many rotor unmanned aerial vehicle, like four rotors, six rotors and eight rotor unmanned aerial vehicle, by the wide application in fields such as movie & TV aerial photography, safety monitoring, agricultural plant protection and electric power patrol line. Present unmanned aerial vehicle is when survey and drawing on water, has the accident that takes place probably, leads to unmanned aerial vehicle can not move to drop into in the water, sink to the bottom, hardly drag for out, also have empty amphibious unmanned aerial vehicle in addition at present, can be used for shooting the water environment condition of the following certain degree of depth of surface of water through waterproof camera, but this kind of amphibious unmanned aerial vehicle need stable floating mechanism, has certain heavy burden when it carries out the flight task and disturbs. Therefore, the person skilled in the art provides a structure of a drone for water ring mapping to solve the problems set forth in the background above.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide an unmanned aerial vehicle structure for water ring survey and drawing to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides an unmanned aerial vehicle structure for water ring survey and drawing, includes unmanned aerial vehicle main part, arc pole, chassis, connecting rod, first step motor and screw, the unmanned aerial vehicle main part with arc pole fixed connection, the arc pole with chassis welded connection, the unmanned aerial vehicle main part with connecting rod fixed connection, the connecting rod is kept away from the one end of unmanned aerial vehicle main part with first step motor fixed connection, the output of first step motor with screw fixed connection, the bottom fixed mounting of unmanned aerial vehicle main part has an installation section of thick bamboo, the bottom detachable of an installation section of thick bamboo installs showy mechanism, be equipped with protective airbag on the chassis.
As a further aspect of the present invention: the floating mechanism comprises a barrel, a connecting plate, a fixing plate and an outer floating ring, the barrel is connected with the connecting plate in a welding mode, the connecting plate is fixedly connected with the fixing plate, the fixing plate is fixedly connected with the outer floating ring, the inner side of the outer floating ring is provided with a middle floating ring, the middle floating ring is fixedly connected with the fixing plate, the inner side of the middle floating ring is provided with an inner floating ring, the inner floating ring is fixedly connected with the fixing plate, and the outer side of the barrel is fixedly provided with a limiting rod.
As a further aspect of the present invention: the installation cylinder is internally provided with a movable ring in a sliding manner, a spring is fixedly installed between the movable ring and the installation cylinder, a first sliding groove is formed in the installation cylinder, a second sliding groove is formed in the communication position of the first sliding groove and the installation cylinder, and a third sliding groove is formed in the communication position of the second sliding groove and the installation cylinder.
As a further aspect of the present invention: be equipped with the casing in the installation section of thick bamboo, the casing with the unmanned aerial vehicle main part passes through bolt fixed connection, there is second step motor through bolt fixed mounting in the casing, the output fixed mounting of second step motor has the axis of rotation, the axis of rotation is kept away from the one end of second step motor with the casing rotates to be connected, the external fixed surface cover of axis of rotation is equipped with the sleeve, the winding has the dive area on the sleeve, the dive area is kept away from telescopic one end fixedly connected with connecting band, the connecting band is kept away from the one end in dive area is connected with the counter weight.
As a further aspect of the present invention: the bottom end of the counterweight is fixedly provided with a waterproof camera, the bottom end of the waterproof camera is fixedly embedded with a camera, an auxiliary plate is fixedly arranged in the second stepping motor, and the diving belt penetrates through the inside of the auxiliary plate.
As a further aspect of the present invention: an open slot is formed in the auxiliary plate, and a ball is movably embedded in the open slot.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses in, through flying unmanned aerial vehicle on water then descend to the surface of water, rotate through second step motor, drive the axis of rotation and rotate to the sleeve takes place to rotate, makes the dive area move down and lets the connecting band move down, thereby counter weight, waterproof camera body and camera move down and fall in the aquatic, make the camera measurable condition of painting the aquatic.
2. The utility model discloses in when will surveying and mapping above the surface of water, protective airbag plays under the unexpected circumstances and prevents that unmanned aerial vehicle from sinking submarine, when flying the task, can be quick dismantle the showy mechanism get off, make things convenient for the multiple condition of unmanned aerial vehicle to use.
Drawings
Fig. 1 is a schematic structural view of the present invention;
fig. 2 is a top view of the present invention in fig. 1;
FIG. 3 is a view showing an internal structure of the mounting barrel of FIG. 1 according to the present invention;
fig. 4 is a schematic structural view of the mounting cylinder of fig. 3 according to the present invention;
fig. 5 is a plan view of the auxiliary plate of fig. 3 according to the present invention.
In the figure: 1. an unmanned aerial vehicle main body; 2. an arc rod; 3. a chassis; 4. a connecting rod; 5. a first stepper motor; 6. A propeller; 7. mounting the cylinder; 8. a floating mechanism; 9. a barrel; 10. a connecting plate; 11. a fixing plate; 12. An outer buoyant ring; 13. a middle floating ring; 14. an inner floating ring; 15. a movable ring; 16. a spring; 17. a first chute; 18. a second chute; 19. a third chute; 20. a limiting rod; 21. a housing; 22. a second stepping motor; 23. a rotating shaft; 24. a sleeve; 25. a submarine belt; 26. a connecting belt; 27. a counterweight device; 28. A waterproof camera body; 29. a camera; 30. an auxiliary plate; 31. an open slot; 32. a ball bearing; 33. and (4) protecting the air bag.
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.
Referring to fig. 1 to 5, in an embodiment of the present invention, an unmanned aerial vehicle structure for water ring mapping includes an unmanned aerial vehicle main body 1, an arc rod 2, a bottom frame 3, a connecting rod 4, a first step motor 5 and a propeller 6, the unmanned aerial vehicle main body 1 is fixedly connected to the arc rod 2, the arc rod 2 is welded to the bottom frame 3, the unmanned aerial vehicle main body 1 is fixedly connected to the connecting rod 4, one end of the connecting rod 4 away from the unmanned aerial vehicle main body 1 is fixedly connected to the first step motor 5, an output end of the first step motor 5 is fixedly connected to the propeller 6, a mounting cylinder 7 is fixedly mounted at a bottom end of the unmanned aerial vehicle main body 1, a floating mechanism 8 is detachably mounted at a bottom end of the mounting cylinder 7, a protective airbag 33 is disposed on the bottom frame 3, the protective airbag 33 is filled with air, but the bottom frame 3 has a limited volume, so that it is not enough to serve as a stable support function, and is only used to ensure that the unmanned aerial vehicle main body 1 does not sink under an accident situation, in addition, the protective air bag 33 can play a certain protection role when flying on the ground and falling.
When needs float on the surface of water and survey and drawing, through the quick bottom of installing in installation section of thick bamboo 7 of 8 floating mechanism, can be quick when carrying out the flight dismantle 8 floating mechanism get off, make things convenient for the unmanned aerial vehicle multiple condition to use.
Wherein, the floating mechanism 8 comprises a cylinder 9 and a connecting plate 10, the mounting structure comprises a fixing plate 11 and an outer floating ring 12, a barrel 9 is welded with the connecting plate 10, the connecting plate 10 is fixedly connected with the fixing plate 11, the fixing plate 11 is fixedly connected with the outer floating ring 12, the inner side of the outer floating ring 12 is provided with a middle floating ring 13, the middle floating ring 13 is fixedly connected with the fixing plate 11, the inner side of the middle floating ring 13 is provided with an inner floating ring 14, the inner floating ring 14 is fixedly connected with the fixing plate 11, the outer side of the barrel 9 is fixedly provided with a limiting rod 20, a movable ring 15 slides in the mounting barrel 7, a spring 16 is fixedly arranged between the movable ring 15 and the mounting barrel 7, the mounting barrel 7 is provided with a first sliding groove 17, the mounting barrel 7 is provided with a second sliding groove 18 communicated with the first sliding groove 17, the mounting barrel 7 is provided with a third sliding groove 19 communicated with the second sliding groove 18, and the number of the second sliding groove 18 and the third sliding groove 19 are two symmetrically distributed on the inner wall of the mounting barrel 7; the quick installation mode of floating mechanism 8 and installation section of thick bamboo 7 does: imbed in installation section of thick bamboo 7 through barrel 9, barrel 9 acts on movable ring 15, and movable ring 15 slides in installation section of thick bamboo 7, and movable ring 15 extrudees spring 16, and gag lever post 20 slides in first spout 17 simultaneously, and rotatory barrel 9 of back makes gag lever post 20 slide in second spout 18, and the third spout 19 is slided in to gag lever post 20, accomplishes quick installation.
The unmanned aerial vehicle comprises an unmanned aerial vehicle main body 1, a mounting barrel 7, a shell 21, a second stepping motor 22, a rotating shaft 23, a waterproof camera 28, a camera 29 (such as an FS01A-2 model) and an auxiliary plate 30, wherein the shell 21 is fixedly connected with the unmanned aerial vehicle main body 1 through bolts, the second stepping motor 22 is fixedly installed in the shell 21 through bolts, the rotating shaft 23 is fixedly installed at the output end of the second stepping motor 22, one end, far away from the second stepping motor 22, of the rotating shaft 23 is rotatably connected with the shell 21, a sleeve 24 is fixedly sleeved on the outer surface of the rotating shaft 23, a diving belt 25 is wound on the sleeve 24, one end, far away from the sleeve 24, of the diving belt 25 is fixedly connected with a connecting belt 26, one end, far away from the diving belt 25, of the connecting belt 26 is connected with the counterweight 27, the bottom end of the counterweight 27 is fixedly installed with the waterproof camera 28, the bottom end of the waterproof camera 28 is fixedly embedded with the camera 29 (such as the FS01A-2 model), the auxiliary plate 30 is fixedly installed in the second stepping motor 22, and the diving belt 25 penetrates through the auxiliary plate 30; the unmanned aerial vehicle flies to the water, the second stepping motor 22 rotates to drive the rotating shaft 23 to rotate, the sleeve 24 rotates to enable the diving belt 25 to move downwards, the connecting belt 26 moves downwards, the counterweight 27, the waterproof camera 28 and the camera 29 move downwards and fall into the water, the camera 29 can detect the situation in the water, the shell 21 is provided with a through hole for arranging a cable so as to be electrically connected with a controller (the unmanned aerial vehicle can carry out remote control operation, at present, a plurality of prior art schemes are provided, so that the detailed description is not needed) in the unmanned aerial vehicle main body 1 and a battery, the movement stroke and data transmission of the second stepping motor 22 are controlled, wherein the cable connected with the waterproof camera 28 is coiled (similar to a telephone line), so that the cable can automatically curl when the waterproof camera 28 descends, extends and ascends, and away from the rotation shaft 23 at the position where the housing 21 is disposed, no winding occurs).
Can dismantle the bolt of being connected with unmanned aerial vehicle main part 1 on the casing 21 in addition to wholly change casing 21 and inside part, survey and drawing parts such as sonar can be replaced waterproof camera body 28 according to the demand of difference, in order to realize detecting under water.
Wherein, the auxiliary plate 30 is provided with an open slot 31, and a ball 32 is movably embedded in the open slot 31; the balls 32 are used to assist the up and down movement of the submersible belt 25.
The utility model discloses a process is: the equipment is arranged according to actual needs, for example, when the flying mission on the water surface and the ground is carried out, the floating mechanism 8 arranged can be quickly disassembled to carry out the flying mission; when carrying out the survey and drawing under the waters, can install floating mechanism 8 fast and fly unmanned aerial vehicle to water and utilize floating mechanism 8 to realize the stable stop at the surface of water, rotate through second step motor 22, drive axis of rotation 23 and rotate to sleeve 24 takes place to rotate, makes diving belt 25 move down, makes connecting band 26 move down, thereby counter weight 27, waterproof camera 28 and camera 29 move down in the aquatic, makes the measurable condition of drawing the aquatic of camera 29.
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 (6)
1. The utility model provides an unmanned aerial vehicle structure for water ring survey and drawing, includes unmanned aerial vehicle main part (1), arc pole (2), chassis (3), connecting rod (4), first step motor (5) and screw (6), unmanned aerial vehicle main part (1) with arc pole (2) fixed connection, arc pole (2) with chassis (3) welded connection, unmanned aerial vehicle main part (1) with connecting rod (4) fixed connection, connecting rod (4) are kept away from the one end of unmanned aerial vehicle main part (1) with first step motor (5) fixed connection, the output of first step motor (5) with screw (6) fixed connection, its characterized in that: the bottom fixed mounting of unmanned aerial vehicle main part (1) has an installation section of thick bamboo (7), the bottom detachable of an installation section of thick bamboo (7) installs flotation mechanism (8), be equipped with protective air bag (33) on chassis (3).
2. The drone structure for water ring mapping according to claim 1, characterized in that: float mechanism (8) including barrel (9), connecting plate (10), fixed plate (11) and outer cursory ring (12), barrel (9) with connecting plate (10) welded connection, connecting plate (10) with fixed plate (11) fixed connection, fixed plate (11) with outer cursory ring (12) fixed connection, the inboard of outer cursory ring (12) is equipped with well cursory ring (13), well cursory ring (13) with fixed plate (11) fixed connection, the inboard of well cursory ring (13) is equipped with interior cursory ring (14), interior cursory ring (14) with fixed plate (11) fixed connection, the outside fixed mounting of barrel (9) has gag lever post (20).
3. The drone structure for water ring mapping according to claim 1, characterized in that: the installation cylinder (7) is internally provided with a movable ring (15) in a sliding manner, the movable ring (15) is fixedly arranged between the installation cylinder (7) and provided with a spring (16), the installation cylinder (7) is provided with a first sliding groove (17), the installation cylinder (7) is provided with a second sliding groove (18) communicated with the first sliding groove (17), and the installation cylinder (7) is provided with a second sliding groove (19) communicated with the second sliding groove (18).
4. The drone structure for water ring mapping according to claim 1, characterized in that: be equipped with casing (21) in installation section of thick bamboo (7), casing (21) with unmanned aerial vehicle main part (1) passes through bolt fixed connection, there is second step motor (22) through bolt fixed mounting in casing (21), the output fixed mounting of second step motor (22) has axis of rotation (23), axis of rotation (23) are kept away from the one end of second step motor (22) with casing (21) rotate to be connected, the external fixed surface cover of axis of rotation (23) is equipped with sleeve (24), the winding has dive area (25) on sleeve (24), dive area (25) are kept away from the one end fixedly connected with connecting band (26) of sleeve (24), connecting band (26) are kept away from the one end of dive area (25) is connected with counterweight (27).
5. The drone structure for water ring mapping according to claim 4, characterized in that: the bottom end of the counterweight device (27) is fixedly provided with a waterproof camera body (28), the bottom end of the waterproof camera body (28) is fixedly embedded with a camera (29), an auxiliary plate (30) is fixedly arranged in the second stepping motor (22), and the diving belt (25) penetrates through the inside of the auxiliary plate (30).
6. The drone structure for water ring mapping according to claim 5, characterized in that: an opening groove (31) is formed in the auxiliary plate (30), and a ball (32) is movably embedded in the opening groove (31).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120155752.0U CN214566151U (en) | 2021-01-20 | 2021-01-20 | A unmanned aerial vehicle structure for water ring survey and drawing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120155752.0U CN214566151U (en) | 2021-01-20 | 2021-01-20 | A unmanned aerial vehicle structure for water ring survey and drawing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214566151U true CN214566151U (en) | 2021-11-02 |
Family
ID=78370078
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120155752.0U Expired - Fee Related CN214566151U (en) | 2021-01-20 | 2021-01-20 | A unmanned aerial vehicle structure for water ring survey and drawing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214566151U (en) |
-
2021
- 2021-01-20 CN CN202120155752.0U patent/CN214566151U/en not_active Expired - Fee Related
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20211102 |