CN219077517U - Novel unmanned aerial vehicle shoots device - Google Patents
Novel unmanned aerial vehicle shoots device Download PDFInfo
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- CN219077517U CN219077517U CN202222390591.0U CN202222390591U CN219077517U CN 219077517 U CN219077517 U CN 219077517U CN 202222390591 U CN202222390591 U CN 202222390591U CN 219077517 U CN219077517 U CN 219077517U
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, and discloses a novel unmanned aerial vehicle shooting device, which comprises an unmanned aerial vehicle main body and further comprises: an imaging device: the shooting device is arranged below the unmanned aerial vehicle main body; and (2) base: the base is arranged on the outer side of the unmanned aerial vehicle main body; and (3) machine leaves: the machine blade is arranged on the base; and a protection module: the protection module is arranged on the unmanned aerial vehicle main body and comprises a protection plate, a drainage groove is formed in the outer wall of the protection plate, a rotating groove is formed in the lower portion of the inner wall of the protection plate, a cooling fan located in the middle of the rotating groove is connected in the middle of the inner wall of the protection plate, and the light supplementing assembly is capable of conducting shooting work at any angle by rotating the rotation assembly in a rotating shaft through the rotation plate in the opening inner wall of the top of a main control machine through the position adjusting plate.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a novel unmanned aerial vehicle shooting device.
Background
The unmanned plane is called as an unmanned plane for short, is a unmanned plane operated by using radio remote control equipment and a self-provided program control device, or is operated completely or intermittently and autonomously by a vehicle-mounted computer, and has wide application range, low cost and higher efficiency; no risk of casualties; the method has the advantages of strong survivability, good maneuvering characteristics, convenient use, extremely important function in modern war and wider prospect in civil field.
The existing unmanned aerial vehicle device is not enough:
first, current unmanned aerial vehicle device is rotatory through the wing when using, is unmanned aerial vehicle and takes off and then pass through electronic signal, and control camera shoots work for unmanned aerial vehicle operating time's instability for unmanned aerial vehicle can shoot work in evening sometimes, but the sky is dim this moment, leads to unmanned aerial vehicle unable shooting clearly, influences its work efficiency.
Secondly, current unmanned aerial vehicle device can meet rainwater strong wind weather sometimes when using for unmanned aerial vehicle receives strong wind and rain water influence, has reduced its work efficiency of shooing, and the rainwater can influence shooting work simultaneously.
Disclosure of Invention
In order to overcome the above-mentioned drawbacks of the prior art, the present utility model provides a novel unmanned aerial vehicle shooting device, so as to solve the problems existing in the above-mentioned background art.
The utility model provides the following technical scheme: novel unmanned aerial vehicle shoots device, and the base is installed in the four corners of unmanned aerial vehicle main part, and drive connection organic leaf, its characterized in that on the base: further comprises:
an imaging device: the shooting device is arranged below the unmanned aerial vehicle main body;
and a protection module: the protection module is installed in unmanned aerial vehicle main part, the protection module includes the guard plate, the water drainage tank has been seted up to the outer wall of guard plate, the rotation groove has been seted up to the inner wall below of guard plate, be connected with in the middle of the inner wall of guard plate and be located radiator fan in the middle of the rotation groove.
Further, the unmanned aerial vehicle main part includes the main control computer, the top of main control computer is connected with the power storehouse, be connected with the support frame in the middle of the top of main control computer, the top of support frame is connected with the holding ring.
Further, the shooting device comprises a rotating ring, the winding displacement hole has been seted up in the middle of the top of rotating ring, the outer wall connection of rotating ring has the locating plate, the below of rotating ring is connected with the fixed plate, one side of fixed plate is connected with the pivot, one side of pivot is connected with rotating assembly, rotating assembly is provided with the opening, and fixed assembly is installed to this opening part, fixed assembly's the place ahead is connected with shooting assembly, shooting assembly's outer wall connection has the light filling subassembly, and the size of rotating ring and main control machine top open-ended size looks adaptation, and the quantity of light filling subassembly is four, and four light filling subassemblies evenly distributed are shooting assembly's outer wall.
Further, the size of the rotating groove is matched with that of the supporting frame, the number of the water draining grooves is eight, and the eight water draining grooves are uniformly distributed on the outer wall of the protection plate.
Further, the number of the power bins is four, and the four power bins are uniformly distributed above the main control computer.
The utility model has the technical effects and advantages that:
1. according to the utility model, the shooting device is arranged, the positioning plate rotates on the inner wall of the opening at the top of the main control machine, and the rotating assembly rotates on the rotating shaft, so that the light supplementing assembly can perform shooting work at any angle, when the night work is performed, the four light supplementing assemblies are started to supplement light for shooting of the shooting assembly, and meanwhile, the light of the light supplementing assembly can provide positioning information for the personnel on the top surface, so that the comfort of a user and the work applicability of the unmanned aerial vehicle are improved.
2. According to the utility model, the protection module is arranged, when the unmanned aerial vehicle works in windy days of rainwater, the windy rainwater can blow on the outer surface of the protection plate, the rainwater can flow along the drainage groove, meanwhile, the windy rainwater can generate power when blowing to the drainage groove, so that the rotation groove of the inner wall of the bottom of the protection plate rotates along the support ring, the cooling fan of the inner wall of the bottom of the protection plate is driven to rotate, the shooting device and the winding displacement thereof are subjected to heat dissipation treatment, the working temperature of the shooting device is reduced, meanwhile, the influence of the windy rainwater and the rainwater on the unmanned aerial vehicle is reduced by the rotating protection plate, and the working efficiency of the unmanned aerial vehicle is increased.
Drawings
Fig. 1 is a schematic diagram of the overall structure of the present utility model.
Fig. 2 is a schematic diagram of a main body structure of the unmanned aerial vehicle of the present utility model.
Fig. 3 is a schematic view of a photographing device according to the present utility model.
Fig. 4 is a schematic structural diagram of a protection module according to the present utility model.
The reference numerals are: 1. an unmanned aerial vehicle main body; 101. a main control machine; 102. a power supply bin; 103. a support; 104. a support ring; 2. a photographing device; 201. a rotating ring; 202. a wire arrangement hole; 203. a positioning plate; 204. a fixing plate; 205. a rotating shaft; 206. a rotating assembly; 207. a fixing assembly; 208. a shooting assembly; 209. a light supplementing component; 3. a base; 4. a machine blade; 5. a protection module; 501. a protection plate; 502. a drainage channel; 503. a rotating groove; 504. a heat radiation fan.
Detailed Description
The following description will be made in detail, with reference to the drawings, of the present utility model, wherein the configurations of the configurations described in the following embodiments are merely examples, and the novel unmanned aerial vehicle photographing device according to the present utility model is not limited to the configurations described in the following embodiments, and all other embodiments obtained by a person skilled in the art without making any inventive effort are within the scope of the present utility model.
Referring to fig. 1 to 4, the present utility model provides a novel unmanned aerial vehicle photographing device, wherein a base 3 is installed at four corners of an unmanned aerial vehicle main body 1, and an organic leaf 4 is connected to the base 3 in a driving manner, and the novel unmanned aerial vehicle photographing device further comprises:
photographing device 2: the photographing device 2 is installed below the unmanned aerial vehicle body 1;
protection module 5: the protection module 5 is installed on the unmanned aerial vehicle main part 1, the protection module 5 includes guard plate 501, water drainage tank 502 has been seted up to the outer wall of guard plate 501, the rotation groove 503 has been seted up to the inner wall below of guard plate 501, be connected with the radiator fan 504 that is located in the middle of the rotation groove 503 in the middle of the inner wall of guard plate 501, install the motor in the base 3, make unmanned aerial vehicle take off work through motor drive machine leaf 4, unmanned aerial vehicle can blow at the surface of guard plate 501 in the heavy wind weather during operation of rainwater, the rainwater can flow along water drainage tank 502, can produce power when the heavy wind blows water drainage tank 502 simultaneously, and then make the rotation groove 503 of guard plate 501 bottom inner wall rotate along support ring 104, and then drive the radiator fan 504 of guard plate 501 bottom inner wall and rotate, carry out the heat dissipation to shooting device 2 and winding displacement, the temperature of shooting device 2 during operation has been reduced, rotatory guard plate 501 has reduced the influence of heavy wind and rainwater to unmanned aerial vehicle, unmanned aerial vehicle's work efficiency has been increased.
Preferably, unmanned aerial vehicle main part 1 includes host computer 101, and the top of host computer 101 is connected with power storehouse 102, and the top intermediate junction of host computer 101 has support 103, and the top of support 103 is connected with support ring 104, provides the working electric quantity to unmanned aerial vehicle through power storehouse 102, through support ring 104 and the movable joint of rotating groove 503, makes its and support ring 104 firmly movable joint through the self weight of guard plate 501 and subassembly, has increased the joint stability between guard plate 501 and the support ring 104.
Preferably, the shooting device 2 comprises a rotating ring 201, a winding displacement hole 202 is formed in the middle of the upper portion of the rotating ring 201, a positioning plate 203 is connected to the outer wall of the rotating ring 201, a fixing plate 204 is connected to the lower portion of the rotating ring 201, a rotating shaft 205 is connected to one side of the fixing plate 204, a rotating assembly 206 is connected to one side of the rotating shaft 205, an opening is formed in the rotating assembly 206, a fixing assembly 207 is arranged at the opening, a shooting assembly 208 is connected to the front of the fixing assembly 207, a light supplementing assembly 209 is connected to the outer wall of the shooting assembly 208, shooting work is performed through the light supplementing assembly 209, the working range of the light supplementing assembly 209 is increased through the shooting assembly 208, the inner wall of the opening of the top of the main control machine 101 is rotated through the positioning plate 203, and the rotating assembly 206 rotates on the rotating shaft 205, so that the light supplementing assembly 209 can perform shooting work at any angle.
Preferably, the size of the rotating groove 503 is matched with the size of the supporting frame 103, the number of the water draining grooves 502 is eight, the eight water draining grooves 502 are uniformly distributed on the outer wall of the protection plate 501, and the eight water draining grooves 502 enable rainwater to be uniformly dispersed on the surface of the protection plate 501, meanwhile, the contact area between the outer surface of the protection plate 501 and high wind is increased, and then the heat dissipation speed of the heat dissipation fan 504 is increased.
Preferably, the number of the power bins 102 is four, the four power bins 102 are uniformly distributed above the main control computer 101, and the power is simultaneously supplied through the four power bins 102, so that the working time of the unmanned aerial vehicle is prolonged.
Preferably, the size of the rotating ring 201 is matched with the size of the opening above the main control computer 101, the number of the light supplementing components 209 is four, the four light supplementing components 209 are uniformly distributed on the outer wall of the shooting component 208, when the unmanned aerial vehicle works at night, the four light supplementing components 209 are started to supplement light for shooting of the shooting component 208, and meanwhile, the light of the light supplementing components 209 can also provide positioning information for the top surface personnel, so that the comfort level of a user and the working applicability of the unmanned aerial vehicle are improved.
The working principle of the utility model is as follows: the user steadily puts unmanned aerial vehicle subaerial earlier, then control the work of leaf 4, make unmanned aerial vehicle start the work of taking off, wait that unmanned aerial vehicle flies to suitable height time, through positioning plate 203 at main control computer 101 open top inner wall rotation, rotating assembly 206 rotates on pivot 205, make light filling assembly 209 can carry out arbitrary angle and shoot work, at night during operation, through starting four light filling assemblies 209, carry out the light filling to shooting assembly 208's shooting, light filling assembly 209's illumination also can provide location information for the top surface personnel simultaneously, user's comfort level and unmanned aerial vehicle's work suitability have been increased, when meetting big weather, the rainwater strong wind can blow the surface at guard plate 501, the rainwater can flow along water drainage tank 502, can produce power when simultaneously big wind blows water drainage tank 502, and then make guard plate 501 bottom inner wall's rotating tank 503 rotate along holding ring 104, and then drive guard plate 501 bottom inner wall's radiator fan 504 rotates, carry out the heat dissipation to shooting device 2 and row line, the temperature of shooting device 2 during operation has been reduced, rotatory guard plate and the work applicability of the same time can provide location information for the top surface personnel, the rainwater has been increased, the rainwater has been blown down at the surface of guard plate 501, the surface of the unmanned aerial vehicle has been increased, the surface has been more evenly spread to the rainwater, the rainwater has been increased, and the surface of the unmanned aerial vehicle has been more evenly spread the surface has been passed through the weather has been increased, and has been increased the surface of the guard plate 501.
The last points to be described are: first, in the description of the present application, it should be noted that, unless otherwise specified and defined, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be mechanical or electrical, or may be a direct connection between two elements, and "upper," "lower," "left," "right," etc. are merely used to indicate relative positional relationships, which may be changed when the absolute position of the object being described is changed;
secondly: in the drawings of the disclosed embodiments, only the structures related to the embodiments of the present disclosure are referred to, and other structures can refer to the common design, so that the same embodiment and different embodiments of the present disclosure can be combined with each other under the condition of no conflict;
finally: the foregoing description of the preferred embodiments of the utility model is not intended to limit the utility model to the precise form disclosed, and any such modifications, equivalents, and alternatives falling within the spirit and principles of the utility model are intended to be included within the scope of the utility model.
Claims (5)
1. Novel unmanned aerial vehicle shoots device, including unmanned aerial vehicle main part (1), base (3) are installed in the four corners of unmanned aerial vehicle main part (1), and drive connection organic leaf (4), its characterized in that on base (3): further comprises:
imaging device (2): the shooting device (2) is arranged below the unmanned aerial vehicle main body (1);
protection module (5): the protection module (5) is installed on the unmanned aerial vehicle main body (1), the protection module (5) includes guard plate (501), water drainage tank (502) have been seted up to the outer wall of guard plate (501), rotation groove (503) have been seted up to the inner wall below of guard plate (501), be connected with in the middle of the inner wall of guard plate (501) and be located radiator fan (504) in the middle of rotation groove (503).
2. The novel unmanned aerial vehicle shooting device according to claim 1, wherein: unmanned aerial vehicle main part (1) include main control computer (101), the top of main control computer (101) is connected with power storehouse (102), be connected with support frame (103) in the middle of the top of main control computer (101), the top of support frame (103) is connected with holding ring (104).
3. The novel unmanned aerial vehicle shooting device according to claim 2, wherein: the shooting device (2) comprises a rotating ring (201), a wire arrangement hole (202) is formed in the middle of the upper portion of the rotating ring (201), a positioning plate (203) is connected to the outer wall of the rotating ring (201), a fixing plate (204) is connected to the lower portion of the rotating ring (201), a rotating shaft (205) is connected to one side of the fixing plate (204), a rotating assembly (206) is connected to one side of the rotating shaft (205), an opening is formed in the rotating assembly (206), a fixing assembly (207) is arranged at the opening, a shooting assembly (208) is connected to the front of the fixing assembly (207), a light supplementing assembly (209) is connected to the outer wall of the shooting assembly (208), the size of the rotating ring (201) is matched with the size of the opening in the upper portion of the main control machine (101), the number of the light supplementing assemblies (209) is four, and the four light supplementing assemblies (209) are evenly distributed on the outer wall of the shooting assembly (208).
4. The novel unmanned aerial vehicle shooting device according to claim 2, wherein: the size of the rotating groove (503) is matched with the size of the supporting frame (103), the number of the drainage grooves (502) is eight, and the eight drainage grooves (502) are uniformly distributed on the outer wall of the protection plate (501).
5. The novel unmanned aerial vehicle shooting device according to claim 2, wherein: the number of the power bins (102) is four, and the four power bins (102) are uniformly distributed above the main control computer (101).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222390591.0U CN219077517U (en) | 2022-09-08 | 2022-09-08 | Novel unmanned aerial vehicle shoots device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202222390591.0U CN219077517U (en) | 2022-09-08 | 2022-09-08 | Novel unmanned aerial vehicle shoots device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219077517U true CN219077517U (en) | 2023-05-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202222390591.0U Active CN219077517U (en) | 2022-09-08 | 2022-09-08 | Novel unmanned aerial vehicle shoots device |
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| Country | Link |
|---|---|
| CN (1) | CN219077517U (en) |
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2022
- 2022-09-08 CN CN202222390591.0U patent/CN219077517U/en active Active
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