CN217575622U - Unmanned aerial vehicle information acquisition transmission control system - Google Patents

Unmanned aerial vehicle information acquisition transmission control system Download PDF

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Publication number
CN217575622U
CN217575622U CN202221444626.8U CN202221444626U CN217575622U CN 217575622 U CN217575622 U CN 217575622U CN 202221444626 U CN202221444626 U CN 202221444626U CN 217575622 U CN217575622 U CN 217575622U
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CN
China
Prior art keywords
aerial vehicle
unmanned aerial
dead lever
bevel gear
threaded rod
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN202221444626.8U
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Chinese (zh)
Inventor
王若
谢群峰
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Huaihua Branch Of China Railway Guangzhou Bureau Group Co ltd
China Railway Guangzhou Group Co Ltd
Original Assignee
Huaihua Branch Of China Railway Guangzhou Bureau Group Co ltd
China Railway Guangzhou Group Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Huaihua Branch Of China Railway Guangzhou Bureau Group Co ltd, China Railway Guangzhou Group Co Ltd filed Critical Huaihua Branch Of China Railway Guangzhou Bureau Group Co ltd
Priority to CN202221444626.8U priority Critical patent/CN217575622U/en
Application granted granted Critical
Publication of CN217575622U publication Critical patent/CN217575622U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an unmanned aerial vehicle information acquisition transmission control system, including the unmanned aerial vehicle main part, the top of unmanned aerial vehicle main part inner chamber is connected with the second dead lever, the axle center of second dead lever is connected with the threaded rod, the outer wall connection of threaded rod has the thread bush, the bottom of thread bush is connected with camera device, second bevel gear is connected to the one end of threaded rod, the rear end of unmanned aerial vehicle main part inner chamber is connected with first dead lever, the axle center of first dead lever is connected with the connecting axle, the one end of connecting axle is connected with the motor, the other end of connecting axle is connected with first bevel gear, one side of first bevel gear is connected with the connecting rod, the one end of connecting rod is connected with the fan. The utility model discloses in, solved current unmanned aerial vehicle and carried out information acquisition and shoot the collection through the camera of bottom, current camera is fixed in unmanned aerial vehicle's bottom mostly, causes the problem that the bottom of camera damaged easily.

Description

Unmanned aerial vehicle information acquisition transmission control system
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an unmanned aerial vehicle information acquisition transmission control system.
Background
The unmanned plane is called as an unmanned plane for short, is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, is a general name of the unmanned aerial vehicle in practice, and can be defined as follows from the technical point of view: compared with manned aircrafts, the unmanned fixed wing aircraft has the advantages of small volume, low manufacturing cost, convenient use, low requirement on operational environment, strong battlefield viability and the like, and is widely used in the fields of aerial photography, agricultural plant protection, express transportation, disaster rescue, wild animal observation, news report, electric power inspection, movie shooting and the like.
At present, current unmanned aerial vehicle carries out information acquisition and shoots the collection through the camera of bottom, and current camera is fixed in unmanned aerial vehicle's bottom mostly, causes the bottom of camera to damage easily, and unmanned aerial vehicle long-time flight inside produces a large amount of heats simultaneously, and the radiating rate is comparatively slow.
SUMMERY OF THE UTILITY MODEL
The utility model aims at solving the shortcoming that exists among the prior art, and the unmanned aerial vehicle information acquisition transmission control system who proposes.
In order to achieve the above purpose, the utility model adopts the following technical scheme: including the unmanned aerial vehicle main part, the top of unmanned aerial vehicle main part inner chamber is connected with the second dead lever, the axle center of second dead lever is connected with the threaded rod, the outer wall connection of threaded rod has the thread bush, the bottom of thread bush is connected with camera device, the second bevel gear is connected to the one end of threaded rod, unmanned aerial vehicle main part inner chamber's rear end is connected with first dead lever, the axle center of first dead lever is connected with the connecting axle, the one end of connecting axle is connected with the motor, the other end of connecting axle is connected with first bevel gear, one side of first bevel gear is connected with the connecting rod, the one end of connecting rod is connected with the fan, the louvre has been seted up to one side of unmanned aerial vehicle main part, one side of louvre is equipped with the safety cover, one side of the inner chamber of louvre is connected with the third dead lever.
As a further description of the above technical solution:
the top of the inner cavity of the unmanned aerial vehicle body is fixedly connected with a second fixing rod, and the axis of the second fixing rod is rotatably connected with a threaded rod.
As a further description of the above technical solution:
the outer wall threaded connection of threaded rod has the thread bush, the bottom fixedly connected with camera device of thread bush, the second bevel gear is connected to the one end of threaded rod.
As a further description of the above technical solution:
the rear end of the inner cavity of the unmanned aerial vehicle body is connected with a first fixing rod, the axis of the first fixing rod is connected with a connecting shaft, and one end of the connecting shaft is connected with a motor.
As a further description of the above technical solution:
the other end of the connecting shaft is connected with a first bevel gear, one side of the first bevel gear is connected with a connecting rod, and the first bevel gear and the second bevel gear are meshed with each other.
As a further description of the above technical solution:
one end fixedly connected with fan of connecting rod, one side of the inner chamber of louvre is connected with the third dead lever, the connecting rod rotates to be connected in the axle center of third dead lever.
The utility model discloses following beneficial effect has: this unmanned aerial vehicle information acquisition transmission control system, through setting up the threaded rod, thread bush and first bevel gear isotructure can receive camera device in the inside of unmanned aerial vehicle main part, avoid the exposed outside of camera to cause the damage, can discharge a large amount of heats that unmanned aerial vehicle operation produced through setting up first bevel gear, fan and louvre isotructure, avoid the heat too high to cause the influence to inside electronic component.
Drawings
FIG. 1 is a schematic view of the present invention;
FIG. 2 is a partial schematic view of the structure of the present invention;
FIG. 3 is a schematic structural view of the present invention A;
fig. 4 is a schematic view of the structure of the present invention B.
Illustration of the drawings:
1. an unmanned aerial vehicle main body; 2. a camera device; 3. a threaded sleeve; 4. a motor; 5. a threaded rod; 6. a first bevel gear; 7. a second bevel gear; 8. a first fixing lever; 9. a second fixing bar; 10. a connecting shaft; 11. a connecting rod; 12. a third fixing bar; 13. a fan; 14. heat dissipation holes; 15. a protective cover.
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. 1-4, the present invention provides an embodiment: including unmanned aerial vehicle main part 1, the top of 1 inner chamber of unmanned aerial vehicle main part is connected with second dead lever 9, the axle center of second dead lever 9 is connected with threaded rod 5, the outer wall connection of threaded rod 5 has thread bush 3, the bottom of thread bush 3 is connected with camera device 2, second bevel gear 7 is connected to the one end of threaded rod 5, the rear end of 1 inner chamber of unmanned aerial vehicle main part is connected with first dead lever 8, the axle center of first dead lever 8 is connected with connecting axle 10, the one end of connecting axle 10 is connected with motor 4, the other end of connecting axle 10 is connected with first bevel gear 6, one side of first bevel gear 6 is connected with connecting rod 11, the one end of connecting rod 11 is connected with fan 13, louvre 14 has been seted up to one side of unmanned aerial vehicle main part 1, one side of louvre 14 is equipped with safety cover 15, one side of louvre 14's inner chamber is connected with third dead lever 12.
Specifically, the top fixedly connected with second dead lever 9 of 1 inner chamber of unmanned aerial vehicle main part, the axle center of second dead lever 9 is rotated and is connected with threaded rod 5, and second dead lever 9 is used for connecting threaded rod 5, and threaded rod 5 rotates and drives 3 removals of thread bush.
Specifically, the outer wall of the threaded rod 5 is in threaded connection with a threaded sleeve 3, the bottom of the threaded sleeve 3 is fixedly connected with a camera device 2, one end of the threaded rod 5 is connected with a second bevel gear 7, the threaded sleeve 3 moves under the rotation of the threaded rod 5, and the threaded sleeve 3 moves to drive the camera device 2 to move.
Specifically, the rear end of 1 inner chamber of unmanned aerial vehicle main part is connected with first dead lever 8, and the axle center of first dead lever 8 is connected with connecting axle 10, and the one end of connecting axle 10 is connected with motor 4, and motor 4 drives connecting axle pivot 10 and rotates, and first dead lever 8 is used for supporting connecting axle 10.
Specifically, the other end of the connecting shaft 10 is connected with a first bevel gear 6, one side of the first bevel gear 6 is connected with a connecting rod 11, the first bevel gear 6 and the second bevel gear 7 are meshed with each other, the first bevel gear 6 rotates to drive the fan 13 to rotate, and the second bevel gear 7 rotates to drive the threaded rod 5 to rotate.
Specifically, one end of the connecting rod 11 is fixedly connected with a fan 13, one side of an inner cavity of the heat dissipation hole 14 is connected with a third fixing rod 12, the connecting rod 11 is rotatably connected to the axis of the third fixing rod 12, the fan 13 rotates to discharge heat through the heat dissipation hole 14, and the third fixing rod 12 is used for supporting the connecting rod 11.
The working principle is as follows: driving motor 4 corotation, motor 4 drives connecting axle 10 and rotates, connecting axle 10 rotates and drives first bevel gear 6 and rotate, first bevel gear 6 rotates and drives connecting rod 11 and rotate, connecting rod 11 rotates and drives fan 13 and rotate, fan 13 rotates and discharges the heat through louvre 14, first bevel gear 6 rotates and drives second bevel gear 7 simultaneously and rotates, second bevel gear 7 rotates and drives threaded rod 5 and rotates, threaded rod 5 rotates and drives 3 rotating movement of thread bush, 3 removal of thread bush drive camera device 2 and move and reach the assigned position, drive first bevel gear 6 and rotate when motor 4 reversal, first bevel gear 6 drives second bevel gear 7 and rotates, second bevel gear 7 drives threaded rod 5 and rotates this moment, threaded rod 5 rotates and drives thread bush 3 and removes, it is inside to remove camera device 2 to unmanned aerial vehicle.
Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, those skilled in the art can still modify the technical solutions described in the foregoing embodiments or make equivalent substitutions for some technical features, and any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims (3)

1. The utility model provides an unmanned aerial vehicle information acquisition transmission control system, includes unmanned aerial vehicle main part (1), its characterized in that: the top of unmanned aerial vehicle main part (1) inner chamber is connected with second dead lever (9), the axle center of second dead lever (9) is connected with threaded rod (5), the outer wall connection of threaded rod (5) has thread bush (3), the bottom of thread bush (3) is connected with camera device (2), second bevel gear (7) is connected to the one end of threaded rod (5), the rear end of unmanned aerial vehicle main part (1) inner chamber is connected with first dead lever (8), the axle center of first dead lever (8) is connected with connecting axle (10), the one end of connecting axle (10) is connected with motor (4), the other end of connecting axle (10) is connected with first bevel gear (6), one side of first bevel gear (6) is connected with connecting rod (11), the one end of connecting rod (11) is connected with fan (13), unmanned aerial vehicle main part (1) has been seted up one side, one side of louvre (14) is equipped with safety cover (15), one side of the inner chamber of louvre (14) is connected with third dead lever (12).
2. The unmanned aerial vehicle information acquisition transmission control system of claim 1, wherein: the top fixedly connected with second dead lever (9) of unmanned aerial vehicle main part (1) inner chamber, the axle center of second dead lever (9) is rotated and is connected with threaded rod (5).
3. The unmanned aerial vehicle information acquisition transmission control system of claim 1, wherein: one end fixedly connected with fan (13) of connecting rod (11), connecting rod (11) rotate to be connected in the axle center of third dead lever (12).
CN202221444626.8U 2022-06-10 2022-06-10 Unmanned aerial vehicle information acquisition transmission control system Expired - Fee Related CN217575622U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN202221444626.8U CN217575622U (en) 2022-06-10 2022-06-10 Unmanned aerial vehicle information acquisition transmission control system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN202221444626.8U CN217575622U (en) 2022-06-10 2022-06-10 Unmanned aerial vehicle information acquisition transmission control system

Publications (1)

Publication Number Publication Date
CN217575622U true CN217575622U (en) 2022-10-14

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ID=83529097

Family Applications (1)

Application Number Title Priority Date Filing Date
CN202221444626.8U Expired - Fee Related CN217575622U (en) 2022-06-10 2022-06-10 Unmanned aerial vehicle information acquisition transmission control system

Country Status (1)

Country Link
CN (1) CN217575622U (en)

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CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20221014

CF01 Termination of patent right due to non-payment of annual fee