CN212125519U - Aerial survey unmanned aerial vehicle aircraft - Google Patents
Aerial survey unmanned aerial vehicle aircraft Download PDFInfo
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- CN212125519U CN212125519U CN202020543782.4U CN202020543782U CN212125519U CN 212125519 U CN212125519 U CN 212125519U CN 202020543782 U CN202020543782 U CN 202020543782U CN 212125519 U CN212125519 U CN 212125519U
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Abstract
The utility model discloses an aerial survey unmanned aerial vehicle aircraft, including unmanned aerial vehicle main part, cradling piece and bottom plate, the below both sides of unmanned aerial vehicle main part all are provided with the bottom plate, the both sides of unmanned aerial vehicle main part all are provided with the flabellum, and the outside of flabellum is provided with the bearer bar, the below mid-mounting of unmanned aerial vehicle main part has driving motor, and driving motor's below installs the pivot, the below of pivot is provided with the camera, and the outside of camera is provided with transparent guard shield, and the bolt has all been run through to the both sides of transparent guard shield simultaneously, the cradling piece is installed respectively in unmanned aerial vehicle main part below both sides, and the below of cradling piece is provided with the frame, the threaded hole has been seted up on the inboard surface of cradling piece. The utility model discloses, be convenient for protect flight fan blade, flight fan blade is difficult to be drawn into debris such as leaf, and is convenient for highly adjust the support to make this aerial survey unmanned aerial vehicle can adapt to different topography.
Description
Technical Field
The utility model relates to a relevant technical field of aerial survey unmanned aerial vehicle specifically is an aerial survey unmanned aerial vehicle aircraft.
Background
Aerial survey unmanned aerial vehicle is the powerful supplement of traditional aerial photogrammetry means, has characteristics such as flexible, high-efficient quick, meticulous accuracy, the operating cost is low, application scope is wide, production cycle is short, has obvious advantage in the aspect of the quick acquisition of small region and flight difficult area high resolution image, along with unmanned aerial vehicle and digital camera technical development, the digital aerial photography technique based on unmanned aerial vehicle platform has shown its unique advantage.
But the aerial survey unmanned aerial vehicle that uses at present is not convenient for protect the flight flabellum, leads to the flight flabellum to be drawn into debris such as leaf easily, and is not convenient for adjust the height of support to make this aerial survey unmanned aerial vehicle can not adapt to different topography.
For this reason, an aerial survey unmanned aerial vehicle aircraft is proposed.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a aerial survey unmanned aerial vehicle aircraft is convenient for protect the flight flabellum, and the flight flabellum is difficult to be drawn into debris such as leaf, and is convenient for highly adjust the support to make this aerial survey unmanned aerial vehicle can adapt to different topography, with the problem of proposing in solving above-mentioned background art.
In order to achieve the above object, the utility model provides a following technical scheme: an aerial survey unmanned aerial vehicle aircraft comprises an unmanned aerial vehicle main body, a support rod and bottom plates, wherein the bottom plates are arranged on two sides below the unmanned aerial vehicle main body;
the unmanned aerial vehicle comprises an unmanned aerial vehicle body and is characterized in that fan blades are arranged on two sides of the unmanned aerial vehicle body, a protection frame is arranged on the outer side of each fan blade, a driving motor is mounted in the middle of the lower portion of the unmanned aerial vehicle body, a rotating shaft is mounted below the driving motor, a camera is arranged below the rotating shaft, a transparent protection cover is arranged on the outer side of the camera, and bolts penetrate through two sides of the transparent protection cover;
the support rods are respectively installed on two sides below the main body of the unmanned aerial vehicle, an outer frame is arranged below the support rods, threaded holes are formed in the inner side surfaces of the support rods, and threaded rods penetrate through the threaded holes;
the bottom plate is installed in the below of frame, and the below of bottom plate is fixed with the spring, and the support base is installed to the below of spring simultaneously.
According to the undulation height of topography, the frame lengthens to adjust the whole length of cradling piece and frame, so that this aerial survey unmanned aerial vehicle can adapt to different topography, then pass the threaded rod in the frame screw-in threaded hole, so that fix cradling piece and frame.
Preferably, the diameter of flabellum is less than the diameter of bearer bar, and the bearer bar sets up with the axis symmetry of unmanned aerial vehicle main part.
The protective frame outside the fan blades can protect the fan blades and prevent the fan blades from rolling up the leaves and being damaged in the flying process.
Preferably, the driving motor and the camera form a rotating structure through a rotating shaft, and the rotating shaft and the camera are vertically distributed.
The driving motor drives the camera to rotate through the rotating shaft, so that the shooting angle is adjusted.
Preferably, the width of the transparent shield is greater than that of the camera, and the transparent shield has a square structure.
The transparent guard shield in the camera outside can play the guard action to the camera.
Preferably, the support rod is movably connected with the outer frame, and the diameter of the support rod is smaller than that of the outer frame.
The frame lengthens to adjust the overall length of cradling piece and frame, so that this aerial survey unmanned aerial vehicle can adapt to different topography.
Preferably, the threaded rod is in threaded connection with the support rod through threaded holes, and the threaded holes are distributed on the support rod at equal intervals.
The threaded rod is screwed into the threaded hole through the outer frame so as to fix the support rod and the outer frame.
Preferably, the bottom plate passes through the spring and constitutes elevation structure with the support base, and the spring sets up with the axis symmetry that supports the base.
When aerial survey unmanned aerial vehicle descends, support base contact ground can make the spring compression to play absorbing effect.
Compared with the prior art, the beneficial effects of the utility model are that:
1. the utility model discloses, through being provided with frame and threaded rod, according to the undulation height of topography, lengthen the frame to adjust the overall length of cradling piece and frame, so that this aerial survey unmanned aerial vehicle can adapt to different topography, then pass the threaded rod the frame and twist threaded hole, so that fix cradling piece and frame.
2. The utility model discloses, through being provided with the bearer bar, at the in-process of flight, the bearer bar in the flabellum outside can play the guard action to the flabellum, prevents that the flabellum from rolling up the leaf impaired at the in-process of flight.
3. The utility model discloses, through being provided with the spring and supporting the base, when aerial survey unmanned aerial vehicle descends, support base contact ground and can make the spring compression to play absorbing effect.
Drawings
Fig. 1 is a schematic view of the front cross-sectional structure of the present invention;
FIG. 2 is a schematic top view of the present invention;
fig. 3 is an enlarged schematic view of a portion a in fig. 1 according to the present invention.
In the figure: 1. an unmanned aerial vehicle main body; 2. a fan blade; 3. a protective frame; 4. a drive motor; 5. a rotating shaft; 6. A camera; 7. a transparent shield; 8. a bolt; 9. a support rod; 10. an outer frame; 11. a threaded hole; 12. A threaded rod; 13. a base plate; 14. a spring; 15. and a base is supported.
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. 1-3, the present invention provides a technical solution: an aerial survey unmanned aerial vehicle aircraft is shown in fig. 1 and 2 and comprises an unmanned aerial vehicle main body 1, a support rod 9 and a bottom plate 13, wherein the bottom plate 13 is arranged on two sides below the unmanned aerial vehicle main body 1;
as shown in fig. 1 and 2, fan blades 2 are arranged on both sides of an unmanned aerial vehicle main body 1, a protective frame 3 is arranged on the outer side of each fan blade 2, a driving motor 4 is arranged in the middle of the lower portion of the unmanned aerial vehicle main body 1, a rotating shaft 5 is arranged below the driving motor 4, a camera 6 is arranged below the rotating shaft 5, a transparent shield 7 is arranged on the outer side of the camera 6, and bolts 8 penetrate through both sides of the transparent shield 7;
as shown in fig. 1 and 3, the support rods 9 are respectively installed at two sides below the main body 1 of the unmanned aerial vehicle, an outer frame 10 is arranged below the support rods 9, a threaded hole 11 is formed in the inner side surface of the support rods 9, and a threaded rod 12 penetrates through the threaded hole 11;
as shown in fig. 1, a base plate 13 is installed below the outer frame 10, and a spring 14 is fixed below the base plate 13, while a support base 15 is installed below the spring 14.
Through adopting above-mentioned scheme, according to the undulation height of topography, lengthen frame 10 to adjust the overall length of cradling piece 9 and frame 10, so that this aerial survey unmanned aerial vehicle can adapt to the topography of difference, then pass frame 10 screw-in screw hole 11 with threaded rod 12 in, so that fix cradling piece 9 and frame 10.
Specifically, as shown in fig. 1 and 2, the diameter of flabellum 2 is less than the diameter of protective frame 3, and protective frame 3 sets up with the axis symmetry of unmanned aerial vehicle main part 1.
Through adopting above-mentioned scheme, the fender bracket 3 in the flabellum 2 outside can play the guard action to flabellum 2, when using the device, prevents that flabellum 2 from rolling up the leaf impaired at the in-process of flight.
Specifically, as shown in fig. 1, the driving motor 4 and the camera 6 form a rotating structure through a rotating shaft 5, and the rotating shaft 5 and the camera 6 are vertically distributed.
Through adopting above-mentioned scheme, driving motor 4 can drive camera 6 through pivot 5 and rotate, when using the device to adjust shooting angle.
Specifically, as shown in fig. 1 and 3, the width of the transparent shield 7 is larger than that of the camera 6, and the transparent shield 7 has a square structure.
By adopting the scheme, the transparent shield 7 on the outer side of the camera 6 can protect the camera 6, and the device is extremely convenient to use.
Specifically, as shown in fig. 1, the support rod 9 is movably connected to the outer frame 10, and the diameter of the support rod 9 is smaller than that of the outer frame 10.
Through adopting above-mentioned scheme, lengthen frame 10 to adjust the overall length of cradling piece 9 and frame 10, when using the device, so that this aerial survey unmanned aerial vehicle can adapt to different topography.
Specifically, as shown in fig. 1, the threaded rod 12 is in threaded connection with the support rod 9 through a threaded hole 11, and the threaded holes 11 are distributed on the support rod 9 at equal intervals.
By adopting the scheme, the threaded rod 12 is threaded into the threaded hole 11 through the outer frame 10, so that the support rod 9 and the outer frame 10 can be fixed when the device is used.
Specifically, as shown in fig. 1, the bottom plate 13 and the supporting base 15 form a lifting structure through a spring 14, and the spring 14 is symmetrically disposed about a central axis of the supporting base 15.
Through adopting above-mentioned scheme, when aerial survey unmanned aerial vehicle descends, support 15 contact ground and can make spring 14 compress, when using the device to play absorbing effect.
The working principle is as follows: firstly, a power supply is started, the outer frame 10 is elongated according to the relief height of the terrain, so that the overall length of the support rod 9 and the outer frame 10 is adjusted, so that the aerial survey unmanned aerial vehicle can adapt to different terrains, then the threaded rod 12 penetrates through the outer frame 10 and is screwed into the threaded hole 11, so that the support rod 9 and the outer frame 10 are fixed, in the flight process, the protective frame 3 outside the fan blade 2 can protect the fan blade 2, the fan blade 2 is prevented from being wound on leaves and damaged in the flight process, when the shooting angle of the camera 6 needs to be adjusted, the driving motor 4 is started, the driving motor 4 can drive the camera 6 to rotate through the rotating shaft 5, so that the shooting angle is adjusted, the transparent shield 7 outside the camera 6 can protect the camera 6, when the aerial survey unmanned aerial vehicle descends, the supporting base 15 contacts the ground, so that the spring 14 is compressed, thereby play absorbing effect, wherein 4 models of driving motor are: 50KTYZ has just so accomplished this aerial survey unmanned aerial vehicle aircraft's use, the utility model relates to an electrical property technique is prior art.
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 (7)
1. An aerial survey unmanned aerial vehicle aircraft which characterized in that: the unmanned aerial vehicle comprises an unmanned aerial vehicle main body (1), a support rod (9) and a bottom plate (13), wherein the bottom plate (13) is arranged on each of two sides below the unmanned aerial vehicle main body (1);
the unmanned aerial vehicle is characterized in that fan blades (2) are arranged on two sides of the unmanned aerial vehicle main body (1), a protection frame (3) is arranged on the outer side of each fan blade (2), a driving motor (4) is installed in the middle of the lower portion of the unmanned aerial vehicle main body (1), a rotating shaft (5) is installed below the driving motor (4), a camera (6) is arranged below the rotating shaft (5), a transparent shield (7) is arranged on the outer side of the camera (6), and meanwhile, bolts (8) penetrate through two sides of the transparent shield (7);
the support rods (9) are respectively installed on two sides below the unmanned aerial vehicle main body (1), an outer frame (10) is arranged below the support rods (9), threaded holes (11) are formed in the inner side surfaces of the support rods (9), and threaded rods (12) penetrate through the threaded holes (11);
the bottom plate (13) is arranged below the outer frame (10), a spring (14) is fixed below the bottom plate (13), and a supporting base (15) is arranged below the spring (14).
2. An aerial survey drone aircraft according to claim 1, characterised in that: the diameter of flabellum (2) is less than the diameter of bearer bar (3), and bearer bar (3) set up with the axis symmetry of unmanned aerial vehicle main part (1).
3. An aerial survey drone aircraft according to claim 1, characterised in that: the driving motor (4) and the camera (6) form a rotating structure through the rotating shaft (5), and the rotating shaft (5) and the camera (6) are vertically distributed.
4. An aerial survey drone aircraft according to claim 1, characterised in that: the width of the transparent shield (7) is larger than that of the camera (6), and the transparent shield (7) is of a square structure.
5. An aerial survey drone aircraft according to claim 1, characterised in that: the support rod (9) is movably connected with the outer frame (10), and the diameter of the support rod (9) is smaller than that of the outer frame (10).
6. An aerial survey drone aircraft according to claim 1, characterised in that: threaded rod (12) are threaded connection through threaded hole (11) and cradling piece (9), and threaded hole (11) are equidistant distribution on cradling piece (9).
7. An aerial survey drone aircraft according to claim 1, characterised in that: the bottom plate (13) and the supporting base (15) form a lifting structure through a spring (14), and the spring (14) is symmetrically arranged with the central axis of the supporting base (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020543782.4U CN212125519U (en) | 2020-04-14 | 2020-04-14 | Aerial survey unmanned aerial vehicle aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020543782.4U CN212125519U (en) | 2020-04-14 | 2020-04-14 | Aerial survey unmanned aerial vehicle aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN212125519U true CN212125519U (en) | 2020-12-11 |
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ID=73687406
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020543782.4U Active CN212125519U (en) | 2020-04-14 | 2020-04-14 | Aerial survey unmanned aerial vehicle aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN212125519U (en) |
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2020
- 2020-04-14 CN CN202020543782.4U patent/CN212125519U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230523 Address after: 515800 No.8 East Jiangbei Road, Guangyi Longtian, Chenghai District, Shantou City, Guangdong Province Patentee after: SHANTOU HELICUTE MODEL AIRCRAFT INDUSTRIAL Co.,Ltd. Address before: 211700 Moxiangyuan Community, Xuyi County, Huai'an City, Jiangsu Province Patentee before: Yang Hong |