CN218172615U - Unmanned aerial vehicle for surveying - Google Patents
Unmanned aerial vehicle for surveying Download PDFInfo
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- CN218172615U CN218172615U CN202221679441.5U CN202221679441U CN218172615U CN 218172615 U CN218172615 U CN 218172615U CN 202221679441 U CN202221679441 U CN 202221679441U CN 218172615 U CN218172615 U CN 218172615U
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Abstract
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle for survey, including unmanned aerial vehicle body and cloud platform, the lower surface and the cloud platform sliding connection of unmanned aerial vehicle body, the lower surface mounting of cloud platform has the camera, the last surface mounting of unmanned aerial vehicle body has four rotors, the unmanned aerial vehicle body is equipped with limit structure for the position of cloud platform, limit structure includes the screw rod, the screw rod rotates with the unmanned aerial vehicle body to be connected, opposite direction's screw thread is seted up to the arc surface at screw rod both ends, the equal threaded connection of arc surface at screw rod both ends has the pipe, the outer wall fixedly connected with connecting plate of pipe, one side fixedly connected with limiting plate of pipe is kept away from to the connecting plate, the vertical cross-section of limiting plate is right trapezoid, the inclined plane and the cloud platform sliding connection of limiting plate. This application has solved because unmanned aerial vehicle's fixed structure leads to the user can't install the problem of not unidimensional cloud platform on unmanned aerial vehicle.
Description
Technical Field
The application relates to the technical field of unmanned aerial vehicles, especially, relate to an unmanned aerial vehicle for surveying.
Background
Unmanned aerial vehicle is the unmanned aerial vehicle who utilizes radio remote control equipment and the program control device of self-contained to control, along with the development of science and technology, an unmanned aerial vehicle for surveying with the camera has appeared in the market, when using this kind of unmanned aerial vehicle, need install the camera on unmanned aerial vehicle with the help of the cloud platform, but because unmanned aerial vehicle's fixed structure, lead to the user can't install not unidimensional cloud platform on unmanned aerial vehicle, thereby unmanned aerial vehicle's application scope has been reduced, unmanned aerial vehicle's practicality has been reduced.
SUMMERY OF THE UTILITY MODEL
The purpose of this application is in order to solve to exist among the prior art because unmanned aerial vehicle's fixed structure leads to the user can't install the shortcoming of the cloud platform of unidimensional not on unmanned aerial vehicle, and the unmanned aerial vehicle is used in surveying that provides.
In order to achieve the purpose, the following technical scheme is adopted in the application: the utility model provides a survey and use unmanned aerial vehicle, includes unmanned aerial vehicle body and cloud platform, the lower surface and the cloud platform sliding connection of unmanned aerial vehicle body, the lower surface mounting of cloud platform has the camera, the last surface mounting of unmanned aerial vehicle body has four rotors, the unmanned aerial vehicle body is equipped with limit structure for the position of cloud platform, limit structure includes the screw rod, the screw rod rotates with the unmanned aerial vehicle body to be connected, opposite direction's screw thread has been seted up to the arc surface at screw rod both ends, the equal threaded connection of the arc surface at screw rod both ends has the pipe, the outer wall fixedly connected with connecting plate of pipe, one side fixedly connected with limiting plate of pipe is kept away from to the connecting plate, the vertical cross-section of limiting plate is right trapezoid, the inclined plane and the cloud platform sliding connection of limiting plate.
The effect that above-mentioned part reaches is: through setting up limit structure, reach and let the user can be spacing on the unmanned aerial vehicle body with not unidimensional cloud platform to enlarge the application scope of unmanned aerial vehicle body, make the unmanned aerial vehicle body have more the effect of practicality.
Preferably, the unmanned aerial vehicle body is for the equal fixedly connected with fixed plate in position of two limiting plates, the surface horizontal slip of fixed plate has run through the slide, slide and limiting plate fixed connection.
The effect that above-mentioned part reaches is: the limiting plate moves to drive the limiting plate to slide along the surface of the fixing plate, and at the moment, the fixing plate reaches the sliding path of the limiting sliding plate so as to limit the sliding path of the limiting plate, so that the limiting plate is prevented from rotating as much as possible.
Preferably, one end of the screw rod is fixedly connected with a pore plate, the inner wall of the pore plate is connected with two round rods in a sliding mode, and one ends, far away from the screw rod, of the two round rods are fixedly connected with a driving plate.
The effect that above-mentioned part reaches is: the drive plate rotates and can drive the round bar to rotate, the pore plate rotates and can drive the screw rod to rotate with the help of the round bar, and the drive plate achieves the effect of conveniently rotating the screw rod.
Preferably, the lateral wall fixedly connected with layer board of unmanned aerial vehicle body, the transversal "U" of personally submitting of layer board appears, the layer board size and the size looks adaptation of driving plate.
The effect that above-mentioned part reaches is: when the inner wall with the drive plate along the layer board slides in, the drive plate can drive the round bar and slide, and the round bar can be located the top of layer board this moment, and the layer board reaches the effect of restriction drive plate position.
Preferably, the unmanned aerial vehicle body all is equipped with protective structure for the position of four rotors, protective structure includes the backup pad, backup pad fixed connection is at the upper surface of unmanned aerial vehicle body, the surperficial sliding sleeve of backup pad has the cardboard, the cardboard is for the fixed position of rotor to be connected with the guard ring, the size of guard ring and the size looks adaptation of rotor.
The effect that above-mentioned part reaches does: through setting up protective structure, reach the in-process that flies at the unmanned aerial vehicle body, avoid the rotor to strike other objects as far as possible, lead to the condition of rotor damage to take place to rotor life's effect has been prolonged.
Preferably, the fixed surface of backup pad is connected with two rectangular plates, the last fixed surface of backup pad is connected with changes the board, the size of changeing the board and the size looks adaptation of backup pad, the cardboard is located between commentaries on classics board and the rectangular plate.
The effect that above-mentioned part reaches is: after the rotating plate and the supporting plate are staggered, the rotating plate and the rectangular plate reach the position of the limiting clamping plate and then limit the position of the protective ring.
In conclusion:
in this application, through setting up limit structure, reach and let the user can be spacing on the unmanned aerial vehicle body with not unidimensional cloud platform to enlarge the application scope of unmanned aerial vehicle body, make the unmanned aerial vehicle body have more the effect of practicality.
Drawings
FIG. 1 is a schematic perspective view of the present application;
FIG. 2 is a partial schematic structural view of the bottom left of FIG. 1 of the present application;
FIG. 3 is a schematic view of a portion of the structure shown in the right side of FIG. 2 of the present application;
FIG. 4 is an enlarged view taken at A of FIG. 2 of the present application;
fig. 5 is a partial structural schematic diagram of fig. 1 of the present application.
Illustration of the drawings: 1. an unmanned aerial vehicle body; 2. a holder; 3. a camera; 4. a rotor; 5. a limiting structure; 51. a screw; 52. a circular tube; 53. a connecting plate; 54. a limiting plate; 55. a fixing plate; 56. a slide plate; 57. an orifice plate; 58. a drive plate; 59. a support plate; 6. a protective structure; 61. a support plate; 62. clamping a plate; 63. a guard ring; 64. a rectangular plate; 65. and (6) rotating the plate.
Detailed Description
Referring to fig. 1 and 2, the present application provides a technical solution: the utility model provides an survey and use unmanned aerial vehicle, including unmanned aerial vehicle body 1 and cloud platform 2, the lower surface and the 2 sliding connection of cloud platform of unmanned aerial vehicle body 1, the lower surface mounting of cloud platform 2 has camera 3, the upper surface mounting of unmanned aerial vehicle body 1 has four rotors 4, unmanned aerial vehicle body 1 is equipped with limit structure 5 for the position of cloud platform 2, through setting up limit structure 5, it can be spacing on unmanned aerial vehicle body 1 with the 2 cloud platforms of equidimension to reach the user, thereby enlarge unmanned aerial vehicle body 1's application scope, make unmanned aerial vehicle body 1 have more the effect of practicality. Unmanned aerial vehicle body 1 all is equipped with protective structure 6 for the position of four rotors 4, through setting up protective structure 6, reaches the in-process that flies at unmanned aerial vehicle body 1, avoids rotor 4 to strike other objects as far as possible, leads to the condition emergence that rotor 4 damaged to rotor 4's effect has been prolonged.
The specific arrangement and function of the limit structures 5 and the protective structures 6 will be described in detail below.
Referring to fig. 2 and 3, in the present embodiment: limiting structure 5 includes screw rod 51, and screw rod 51 rotates with unmanned aerial vehicle body 1 to be connected, and opposite direction's screw thread has been seted up to the arc surface at screw rod 51 both ends. Circular tubes 52 are connected to the circular arc surfaces at the two ends of the screw 51 in a threaded manner, and when the screw 51 rotates, the screw drives the threads to drive the circular tubes 52 to move. The outer wall of the circular tube 52 is fixedly connected with a connecting plate 53, and the movement of the circular tube 52 drives the connecting plate 53 to move. One side of the connecting plate 53, which is far away from the circular tube 52, is fixedly connected with a limiting plate 54, and the movement of the connecting plate 53 drives the limiting plate 54 to move. The vertical section of the limit plate 54 is in a right trapezoid shape, and the inclined surface of the limit plate 54 is connected with the holder 2 in a sliding manner. Unmanned aerial vehicle body 1 is for the equal fixedly connected with fixed plate 55 in position of two limiting plates 54, and the surperficial horizontal slip of fixed plate 55 runs through there is slide 56, slide 56 and limiting plate 54 fixed connection, and limiting plate 54 removes the surperficial slip that can drive limiting plate 54 along fixed plate 55, and this moment fixed plate 55 reaches and restricts slide 56 slip path and then restrict limiting plate 54 slip path, prevents limiting plate 54 as far as possible and takes place rotatory effect.
Referring to fig. 3 and 4, specifically, an orifice plate 57 is fixedly connected to one end of the screw 51, and the rotation of the orifice plate 57 drives the screw 51 to rotate. The inner wall of the orifice plate 57 is slidably connected with two round rods, and the rotation of the round rods can drive the orifice plate 57 to rotate. One ends of the two round rods far away from the screw 51 are fixedly connected with a driving plate 58, and the driving plate 58 rotates to drive the round rods to rotate. Lateral wall fixedly connected with layer board 59 of unmanned aerial vehicle body 1, the transversal "U" shape of personally submitting of layer board 59, the size of layer board 59 and the size looks adaptation of drive plate 58, when the inner wall with drive plate 58 along layer board 59 slides, drive plate 58 can drive the round bar and slide, and the round bar can be located the top of layer board 59 this moment, and layer board 59 reaches the effect of restriction drive plate 58 position.
Referring to fig. 2 and 5, specifically, protective structure 6 includes a supporting plate 61, supporting plate 61 is fixedly connected to the upper surface of unmanned aerial vehicle body 1, the surface sliding sleeve of supporting plate 61 has a cardboard 62, cardboard 62 is fixedly connected with a protective ring 63 for the position of rotor 4, the size of protective ring 63 and the size of rotor 4 are adapted. Two rectangular plates 64 of fixed surface of backup pad 61 are connected with, and the last fixed surface of backup pad 61 is connected with changes board 65, changes the size of board 65 and backup pad 61's size looks adaptation, and cardboard 62 is located and changes between board 65 and the rectangular plate 64, and after changeing board 65 and backup pad 61 dislocation, changes board 65 and rectangular plate 64 and reaches the effect that limits cardboard 62 position and then limit guard ring 63 position.
Working principle, when needs use limit structure 5, put cloud platform 2 at the lower surface of unmanned aerial vehicle body 1, then remove drive plate 58, drive plate 58 removes the inner wall that can drive the round bar and insert orifice plate 57, then rotate drive plate 58, drive plate 58 rotates and can drive the round bar and rotate, orifice plate 57 rotates with the help of the round bar and can drive screw 51 and rotate, because opposite screw thread has been seted up to the arc surface at screw 51 both ends, consequently, screw 51 can drive two pipes 52 to the direction that is close to each other with the help of the screw thread when rotating, pipe 52 removes and can drive connecting plate 53 and remove, connecting plate 53 removes and can drive limiting plate 54 and remove, limiting plate 54 removes and can drive limiting plate 54 along the surface slip of fixed plate 55, fixed plate 55 reaches limiting slide 56 sliding path and then limiting plate 54 sliding path this moment, limiting plate 54 slides and can make the inclined plane of limiting plate 54 and cloud platform 2 contact, continue to rotate the drive plate 58 this moment and can make two limiting plates 54 extrude cloud platform 2 simultaneously, thereby reach the effect of limiting plate 2 position, and limiting plate 54 of right trapezoid structure reaches the effect that can restrict not unidimensional cloud platform 2 position.
After compressing tightly cloud platform 2, to the direction pulling drive plate 58 who keeps away from screw 51, drive plate 58 removes and can make round bar and orifice plate 57 break away from the contact, then slides in drive plate 58 along the inner wall of layer board 59, and drive plate 58 slides and can drive the round bar and slide, and the round bar can be located the top of layer board 59 this moment, and layer board 59 reaches the effect of restriction drive plate 58 position.
When needs use protective structure 6, along the surface of backup pad 61 to the direction slip cardboard 62 that is close to rectangular plate 64, cardboard 62 slides and can drive the retaining ring 63 and slide, rotate board 65 after cardboard 62 contacts with rectangular plate 64, after revolving board 65 misplaces with backup pad 61, revolving board 65 and rectangular plate 64 reach the effect that restricts cardboard 62 position and then restrict retaining ring 63 position, retaining ring 63 reaches the in-process of flying at unmanned aerial vehicle body 1 this moment, avoid rotor 4 to strike other objects as far as possible, the condition that leads to rotor 4 to damage takes place, thereby rotor 4 life's effect has been prolonged.
In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "connected," and "connected" are to be construed broadly, and may be, for example, fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meaning of the above terms in the present invention can be understood by those of ordinary skill in the art through specific situations.
Claims (6)
1. The utility model provides a survey and use unmanned aerial vehicle, includes unmanned aerial vehicle body (1) and cloud platform (2), its characterized in that: the lower surface and cloud platform (2) sliding connection of unmanned aerial vehicle body (1), the lower surface mounting of cloud platform (2) has camera (3), the last surface mounting of unmanned aerial vehicle body (1) has four rotors (4), unmanned aerial vehicle body (1) is equipped with limit structure (5) for the position of cloud platform (2), limit structure (5) include screw rod (51), screw rod (51) are rotated with unmanned aerial vehicle body (1) and are connected, opposite direction's screw thread is seted up to the arc surface at screw rod (51) both ends, the equal threaded connection of arc surface at screw rod (51) both ends has pipe (52), the outer wall fixedly connected with connecting plate (53) of pipe (52), one side fixedly connected with limiting plate (54) of pipe (52) are kept away from in connecting plate (53), the vertical cross-section of limiting plate (54) is right trapezoid, the inclined plane and cloud platform (2) sliding connection of limiting plate (54).
2. A unmanned aerial vehicle for surveying as claimed in claim 1, wherein: unmanned aerial vehicle body (1) is for the equal fixedly connected with fixed plate (55) in position of two limiting plate (54), the surperficial horizontal slip of fixed plate (55) has run through slide (56), slide (56) and limiting plate (54) fixed connection.
3. A unmanned aerial vehicle for surveying as claimed in claim 1, wherein: one end fixedly connected with orifice plate (57) of screw rod (51), the inner wall sliding connection of orifice plate (57) has two round bars, and the one end fixedly connected with drive plate (58) of screw rod (51) is kept away from to two round bars.
4. A unmanned aerial vehicle for surveying as claimed in claim 3, wherein: the lateral wall fixedly connected with layer board (59) of unmanned aerial vehicle body (1), the cross-section of layer board (59) personally submits "U" shape, the size of layer board (59) and the size looks adaptation of drive plate (58).
5. A survey drone according to claim 1, characterised in that: unmanned aerial vehicle body (1) all is equipped with protective structure (6) for the position of four rotors (4), protective structure (6) include backup pad (61), backup pad (61) fixed connection is at the upper surface of unmanned aerial vehicle body (1), the surperficial slip cap of backup pad (61) has cardboard (62), cardboard (62) are for the position fixedly connected with guard ring (63) of rotor (4), the size of guard ring (63) and the size looks adaptation of rotor (4).
6. A unmanned aerial vehicle for surveying of claim 5, wherein: the surface of the supporting plate (61) is fixedly connected with two rectangular plates (64), the upper surface of the supporting plate (61) is fixedly connected with a rotating plate (65), the size of the rotating plate (65) is matched with that of the supporting plate (61), and the clamping plate (62) is located between the rotating plate (65) and the rectangular plates (64).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221679441.5U CN218172615U (en) | 2022-06-30 | 2022-06-30 | Unmanned aerial vehicle for surveying |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202221679441.5U CN218172615U (en) | 2022-06-30 | 2022-06-30 | Unmanned aerial vehicle for surveying |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN218172615U true CN218172615U (en) | 2022-12-30 |
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ID=84611063
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202221679441.5U Active CN218172615U (en) | 2022-06-30 | 2022-06-30 | Unmanned aerial vehicle for surveying |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN218172615U (en) |
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2022
- 2022-06-30 CN CN202221679441.5U patent/CN218172615U/en active Active
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