CN211033062U - Simple unmanned aerial vehicle for camera shooting - Google Patents
Simple unmanned aerial vehicle for camera shooting Download PDFInfo
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- CN211033062U CN211033062U CN201922098869.5U CN201922098869U CN211033062U CN 211033062 U CN211033062 U CN 211033062U CN 201922098869 U CN201922098869 U CN 201922098869U CN 211033062 U CN211033062 U CN 211033062U
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- top cover
- camera
- aerial vehicle
- unmanned aerial
- rotor wing
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Abstract
The utility model discloses a simple unmanned aerial vehicle for camera shooting, which comprises a frame, four rotor wing mechanisms, a control panel, a top cover, a camera and a return device, wherein the frame comprises a central fixed seat and extension arms, the rear end of each extension arm is respectively provided with a rotor wing mounting seat, and the extension arms are provided with triangular through holes; the rotor wing mechanism is arranged on the rotor wing mounting seat; the control panel and the top cover are both detachably arranged on the central fixed seat; the top cover is internally provided with an accommodating cavity, the front end of the top cover is provided with an extending hole, and the upper surface of the rear end of the top cover is provided with a threading hole; the camera is arranged in the accommodating cavity; the return device comprises a return circuit board and a signal wire connected to the return circuit board. Therefore, the unmanned aerial vehicle is formed by integrally mounting the four rotor wing mechanisms, the control panel, the camera and the return device on the rack and the top cover; this frame overall structure is simple to seted up a plurality of heavy through-holes that subtract, alleviateed the fuselage load, made unmanned aerial vehicle structure compacter, the flight is more nimble.
Description
Technical Field
The utility model relates to an unmanned vehicles field technique especially indicates a simple and easy type is made a video recording and is used unmanned aerial vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle for short, and is also called as UAV in English, and is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, the unmanned aerial vehicle has the characteristics of simple operation and stable and easy flight, and can be carried with various loads to complete various complex tasks, and the unmanned aerial vehicle has wide application in various fields such as photography, pesticide spraying, fire prevention and disaster relief, communication, public security and counter terrorism, drug and smuggling and the like. A drone generally includes a housing assembly and a wing assembly fixedly connected to the housing to provide flight power. The circuit board of the existing unmanned aerial vehicle is usually arranged in a side-by-side mode, and each part is free of weight reduction design, so that the whole structure of the unmanned aerial vehicle is complex, the unmanned aerial vehicle is large in size, heavy in weight and poor in flexibility, stability is poor, long lenses and narrow and small range shooting cannot be carried out, and the shooting application environment is limited. Therefore, should have unmanned aerial vehicle now and improve to solve above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
In view of the above, the present invention provides a simplified unmanned aerial vehicle for camera shooting, which is formed by integrally mounting four rotor wing mechanisms, a control panel, a camera and a return device on a frame and a top cover; this frame is by the integrative continuous formation that links to each other of central fixing base and four extension arms, and frame overall structure is simple to seted up a plurality of heavy through-holes that subtract, alleviateed the fuselage load, made unmanned aerial vehicle structure compacter, the flight is more nimble.
In order to achieve the above purpose, the utility model adopts the following technical scheme:
a simple unmanned aerial vehicle for camera shooting comprises a frame, four rotor wing mechanisms, a control panel for controlling the rotor wing mechanisms to operate, a top cover, a camera and a return device for returning images shot by the camera, wherein the frame comprises a central fixed seat and extension arms extending outwards from four corners of the central fixed seat, a rotor wing mounting seat is arranged at the rear end of each extension arm respectively, and a triangular through hole for reducing the weight of the frame is formed at the joint of each extension arm and the central fixed seat; the four rotor wing mechanisms are correspondingly arranged on the rotor wing installation seats of the four extension arms; the control board is detachably arranged on the central fixed seat; the top cover is detachably arranged on the central fixed seat and covers the control panel, an accommodating cavity for accommodating the camera and the return device is arranged in the top cover, a stretching hole for stretching the camera is formed in the upper part of the front end of the top cover, and a threading hole is formed in the upper surface of the rear end of the top cover; the rear end of the camera is arranged in the accommodating cavity of the top cover, and the front end of the camera extends out of the extending hole; the return device comprises a return circuit board and a signal wire connected to the return circuit board, the return circuit board is connected with the camera, and the signal wire extends out of the threading hole of the top cover.
As a preferred embodiment: the rotor wing mechanism comprises a motor and blades arranged at the shaft end of the motor, and two connecting bolts are connected between the blades and the shaft end of the motor side by side.
As a preferred embodiment: the central fixing seat comprises a central frame body and a plurality of reinforcing ribs connected in the central frame body, and a plurality of through holes are formed between the reinforcing ribs and the central frame body in a surrounding manner.
As a preferred embodiment: among the four extension arms, two extension arms at the same side are transitionally connected in an arc shape along the edge of the central fixed seat.
As a preferred embodiment: protruding the stretching respectively in center framework both sides is provided with one and is used for carrying out spacing convex part to the control panel, is provided with the locating pin corresponding the control panel both ends on the convex part.
As a preferred embodiment: the rotor wing installation seat of each extension arm is respectively provided with two positioning columns for fixing the rotor wing mechanism, and the rotor wing mechanism is fixed on the two positioning columns.
As a preferred embodiment: the extension arm is from the center fixed seat to keeping away from the direction of center fixed seat and is the transition from wide to narrow.
As a preferred embodiment: the central fixing seat is provided with a fixing column for fixing the top cover, the two sides of the top cover are respectively provided with a fixing part, and the fixing parts are installed on the fixing column.
Compared with the prior art, the utility model has obvious advantages and beneficial effects, and specifically, according to the technical scheme, the unmanned aerial vehicle is formed by integrally installing four rotor wing mechanisms, a control panel, a camera and a return device on the frame and the top cover; the frame is formed by integrally connecting a central fixed seat and four extension arms, the frame is simple in integral structure, and a plurality of weight-reducing through holes are formed while the structural strength is ensured, so that the weight of the frame is reduced, and the load of a machine body is further reduced; make unmanned aerial vehicle structure compacter, the flight is more nimble, can adapt to different shooting scenes and shooting environment.
To more clearly illustrate the structural features and effects of the present invention, the following detailed description is given with reference to the accompanying drawings and specific embodiments.
Drawings
Fig. 1 is a schematic perspective view of the unmanned aerial vehicle of the present invention;
fig. 2 is a perspective view of the unmanned aerial vehicle according to another perspective of the present invention;
fig. 3 is a schematic view of the three-dimensional structure of the unmanned aerial vehicle with the top cover opened;
FIG. 4 is a perspective view of the combination of the frame and the rotor mechanism of the present invention;
fig. 5 is a perspective view of the frame and the rotor mechanism of the present invention with another view angle.
The attached drawings indicate the following:
10. frame 11, central fixing seat
111. Center frame 112 and reinforcing ribs
113. Through hole 114, convex part
115. Locating pin 116, edge
12. Extension arm 121, triangular through hole
13. Rotor wing mounting seat 131 and positioning column
14. Fixed column 20 and rotor wing mechanism
21. Motor 22, blade
23. Connecting bolt 30 and control panel
40. Top cover 41 and fixing part
42. Accommodating chamber 43, extension hole
44. Threading hole 50 and camera
60. Pass-back device 61 and pass-back circuit board
62. And a signal line.
Detailed Description
The utility model discloses as shown in fig. 1 to 5, a simple and easy type is made a video recording and is used unmanned aerial vehicle, including frame 10, four rotor mechanisms 20, control rotor mechanism 20 moving control panel 30, top cap 40, camera 50 and be used for the passback device 60 with the image passback that the camera 50 was made a video recording, wherein:
the rack 10 comprises a central fixed seat 11 and extension arms 12 extending outwards from four corners of the central fixed seat 11, a rotor wing mounting seat 13 is arranged at the rear end of each extension arm 12, and a triangular through hole 121 for reducing the weight of the rack 10 is arranged at the joint of each extension arm 12 and the central fixed seat 11 (the triangular shape can improve the stability); the four rotor mechanisms 20 are correspondingly arranged on the rotor mounting seats 13 of the four extension arms 12; the control board 30 is detachably mounted on the central fixing seat 11; the top cover 40 is detachably mounted on the central fixing seat 11 (the central fixing seat 11 is provided with a fixing column 14 for fixing the top cover 40, two sides of the top cover 40 are respectively provided with a fixing part 41, the fixing parts 41 are mounted on the fixing column 14), and the top cover covers the control panel 30, the top cover 40 is internally provided with an accommodating cavity 42 for accommodating the camera 50 and the pass-back device 60, the upper part of the front end of the top cover 40 is provided with a protruding hole 43 for the camera 50 to extend out, and the upper surface of the rear end of the top cover 40 is provided with a threading hole 44; the central fixing base 11 includes a central frame 111 and a plurality of ribs 112 connected to the central frame 111, and a plurality of through holes 113 are formed between the plurality of ribs 112 and the central frame 111. Protruding portions 114 for limiting the control board 30 are respectively protruded from two sides of the central frame 111, positioning pins 115 are disposed on the protruding portions 114 corresponding to two ends of the control board 30, and the control board 30 is fixed on the central fixing base 11 by the positioning pins 115. Among the four extension arms 12, two extension arms 12 on the same side are transitionally connected in an arc shape along the edge 116 of the central fixing seat 11. Two positioning posts 131 for fixing the rotor mechanism 20 are respectively disposed on the rotor mounting base 13 of each extension arm 12, and the rotor mechanism 20 is fixed on the two positioning posts 131. In addition, each extension arm 12 is by central fixing base 11 to keeping away from central fixing base direction and is by wide to narrow transition, makes 10 centrobaries of frame be located central point and puts, improves unmanned aerial vehicle focus stability to do benefit to unmanned aerial vehicle's controlling.
The rotor wing mechanism 20 comprises a motor 21 and a blade 22 mounted at the shaft end of the motor 21, two connecting bolts 23 are connected between the shaft ends of the blade 22 and the motor 21 side by side, and the two connecting bolts 23 can better prevent the blade 22 from slipping relative to the shaft end of the motor 21 relative to one connecting bolt.
The rear end of the camera 50 is arranged in the containing cavity 42 of the top cover 40, and the front end thereof extends out of the extending hole 43; the return device 60 includes a return circuit board 61 and a signal line 62 connected to the return circuit board 61, the return circuit board 61 is connected to the camera 50, and the signal line 62 extends from the threading hole 44 of the top cover 40.
The utility model is mainly designed in that the unmanned aerial vehicle is formed by integrally installing four rotor wing mechanisms, a control panel, a camera and a return device on a rack and a top cover; the frame is formed by integrally connecting a central fixed seat and four extension arms, the frame is simple in integral structure, and a plurality of weight-reducing through holes are formed while the structural strength is ensured, so that the weight of the frame is reduced, and the load of a machine body is further reduced; make unmanned aerial vehicle structure compacter, the flight is more nimble, can adapt to different shooting scenes and shooting environment.
The above description is only a preferred embodiment of the present invention, and is not intended to limit the technical scope of the present invention, so that any slight modification, equivalent change and modification made by the technical spirit of the present invention to the above embodiments are all within the scope of the technical solution of the present invention.
Claims (8)
1. The utility model provides a simple and easy type is made a video recording and is used unmanned aerial vehicle which characterized in that: the aircraft comprises a rack, four rotor wing mechanisms, a control panel for controlling the rotor wing mechanisms to operate, a top cover, a camera and a return device for returning an image shot by the camera, wherein the rack comprises a central fixing seat and extension arms extending outwards from four corners of the central fixing seat, the rear end of each extension arm is respectively provided with a rotor wing mounting seat, and a triangular through hole for reducing the weight of the rack is arranged at the joint of each extension arm and the central fixing seat; the four rotor wing mechanisms are correspondingly arranged on the rotor wing installation seats of the four extension arms; the control board is detachably arranged on the central fixed seat; the top cover is detachably arranged on the central fixed seat and covers the control panel, an accommodating cavity for accommodating the camera and the return device is arranged in the top cover, a stretching hole for stretching the camera is formed in the upper part of the front end of the top cover, and a threading hole is formed in the upper surface of the rear end of the top cover; the rear end of the camera is arranged in the accommodating cavity of the top cover, and the front end of the camera extends out of the extending hole; the return device comprises a return circuit board and a signal wire connected to the return circuit board, the return circuit board is connected with the camera, and the signal wire extends out of the threading hole of the top cover.
2. The simplified unmanned aerial vehicle for camera shooting according to claim 1, characterized in that: the rotor wing mechanism comprises a motor and blades arranged at the shaft end of the motor, and two connecting bolts are connected between the blades and the shaft end of the motor side by side.
3. The simplified unmanned aerial vehicle for camera shooting according to claim 1, characterized in that: the central fixing seat comprises a central frame body and a plurality of reinforcing ribs connected in the central frame body, and a plurality of through holes are formed between the reinforcing ribs and the central frame body in a surrounding manner.
4. The simplified unmanned aerial vehicle for camera shooting according to claim 1, characterized in that: among the four extension arms, two extension arms at the same side are transitionally connected in an arc shape along the edge of the central fixed seat.
5. The simplified unmanned aerial vehicle for camera shooting according to claim 3, wherein: protruding the stretching respectively in center framework both sides is provided with one and is used for carrying out spacing convex part to the control panel, is provided with the locating pin corresponding the control panel both ends on the convex part.
6. The simplified unmanned aerial vehicle for camera shooting according to claim 1, characterized in that: the rotor wing installation seat of each extension arm is respectively provided with two positioning columns for fixing the rotor wing mechanism, and the rotor wing mechanism is fixed on the two positioning columns.
7. The simplified unmanned aerial vehicle for camera shooting according to claim 1, characterized in that: the extension arm is from the center fixed seat to keeping away from the direction of center fixed seat and is the transition from wide to narrow.
8. The simplified unmanned aerial vehicle for camera shooting according to claim 1, characterized in that: the central fixing seat is provided with a fixing column for fixing the top cover, the two sides of the top cover are respectively provided with a fixing part, and the fixing parts are installed on the fixing column.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922098869.5U CN211033062U (en) | 2019-11-29 | 2019-11-29 | Simple unmanned aerial vehicle for camera shooting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922098869.5U CN211033062U (en) | 2019-11-29 | 2019-11-29 | Simple unmanned aerial vehicle for camera shooting |
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| Publication Number | Publication Date |
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| CN211033062U true CN211033062U (en) | 2020-07-17 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201922098869.5U Active CN211033062U (en) | 2019-11-29 | 2019-11-29 | Simple unmanned aerial vehicle for camera shooting |
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| CN (1) | CN211033062U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112212881A (en) * | 2020-12-14 | 2021-01-12 | 成都飞航智云科技有限公司 | Flight navigator based on big dipper is used |
-
2019
- 2019-11-29 CN CN201922098869.5U patent/CN211033062U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112212881A (en) * | 2020-12-14 | 2021-01-12 | 成都飞航智云科技有限公司 | Flight navigator based on big dipper is used |
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