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CN-224225340-U - Unmanned aerial vehicle is with land empty control conversion control equipment

CN224225340UCN 224225340 UCN224225340 UCN 224225340UCN-224225340-U

Abstract

The utility model discloses land-air control conversion control equipment for an unmanned aerial vehicle, which is applied to the technical field of unmanned aerial vehicle equipment and comprises a bottom baffle, wherein a left side plate is welded on the left side of the bottom baffle, a right side plate is welded on the right side of the bottom baffle, a threaded column is welded at the bottom of the bottom baffle, a threaded cylinder is connected with the surface of the threaded column in a threaded manner, a chassis is welded at the bottom of the threaded cylinder, a first motor is bolted to one end of the front of the chassis, the output end of the first motor is fixedly connected with a rotating rod through a coupler, a rotating gear is sleeved at one end of the rotating rod, a second motor is bolted to the back of the bottom of the chassis, the output end of the second motor is fixedly connected with a rotating rod through the coupler in an adhesive and fixed connection mode, a ground mobile device is arranged on the unmanned aerial vehicle, and the unmanned aerial vehicle can be conveniently installed and used for different sizes, and the unmanned aerial vehicle falls into the ground.

Inventors

  • LIU QIN
  • WU CHENGXIN
  • PENG JING
  • KE YAO

Assignees

  • 湖南汽车工程职业学院

Dates

Publication Date
20260512
Application Date
20250625

Claims (8)

  1. 1. The land-air control conversion control equipment for the unmanned aerial vehicle comprises a bottom baffle (1) and is characterized in that a left side plate (2) is welded on the left side of the bottom baffle (1), a right side plate (3) is welded on the right side of the bottom baffle (1), a threaded column (4) is welded on the bottom of the bottom baffle (1), a threaded cylinder (5) is connected with the surface of the threaded column (4) in a threaded manner, a chassis (6) is welded on the bottom of the threaded cylinder (5), a first motor (7) is bolted to one end of the front of the chassis (6), a rotating rod (8) is fixedly connected to the output end of the first motor (7) through a coupler, a rotating gear (9) is sleeved to one end of the rotating rod (8), a second motor (10) is bolted to the back of the bottom of the chassis (6), and a rotating rod (11) is fixedly connected to the output end of the second motor (10) through a coupler.
  2. 2. The land-air control switching control device for unmanned aerial vehicle according to claim 1, wherein the left side plate (2) is connected with a left side binding belt (12) by sewing.
  3. 3. The land-air control switching control device for the unmanned aerial vehicle according to claim 1, wherein the right side plate (3) is connected with a right side binding belt (13) in a sewing way.
  4. 4. The land-air control switching control device for the unmanned aerial vehicle according to claim 1, wherein the surface of the rotating gear (9) is meshed with a booster gear (14).
  5. 5. The land-air control switching control equipment for the unmanned aerial vehicle of claim 4, wherein the T-shaped rod (15) is welded at the bottom of the booster gear (14).
  6. 6. A land-air control switching control apparatus for unmanned aerial vehicle as set forth in claim 5, wherein said T-bar (15) is bolted at both ends with steering tires (16).
  7. 7. The land-air control conversion control equipment for the unmanned aerial vehicle according to claim 1, wherein the surface of the rotary rod (11) is sleeved with a belt (17), the inner wall of the back of the belt (17) is sleeved with an auxiliary rod (18), and two ends of the auxiliary rod (18) are bolted with power tires (19).
  8. 8. The land-air control conversion control equipment for the unmanned aerial vehicle according to claim 1, wherein an auxiliary shaft (20) is connected below the front booster gear of the chassis (6) in a bolt mode, and the inner wall of the auxiliary shaft (20) is connected with the surface of the T-shaped rod (15) in a sliding sleeve mode.

Description

Unmanned aerial vehicle is with land empty control conversion control equipment Technical Field The utility model belongs to the technical field of unmanned aerial vehicle equipment, and particularly relates to land-air control conversion control equipment for an unmanned aerial vehicle. Background With the development of unmanned aerial vehicle technology and the continuous expansion of application fields thereof, unmanned aerial vehicles have been widely applied to a plurality of industries including, but not limited to, agricultural monitoring, disaster assessment, geographical mapping, security monitoring, express delivery service and the like. However, conventional unmanned aerial vehicles are typically only operable in the air, and this limitation limits their application to some extent. For example, in urban environments, it can be very difficult to find suitable take-off and landing sites due to dense buildings, staggered wires, etc., and, as such, unmanned aerial vehicles may be challenging to take-off and land in places where the terrain is complex or where obstacles are numerous. Most unmanned aerial vehicles on the market adopt manual operation to adjust the conversion when land-air conversion for in use very inconvenient, when installing land-air equipment additional, because land-air equipment is different manufacturers face different products independent designs mostly, cause land-air equipment unable to install on different unmanned aerial vehicles, consequently, in order to solve above-mentioned problem, we propose a land-air control conversion control equipment for unmanned aerial vehicle. Disclosure of utility model The utility model aims at a land-air control conversion control device for an unmanned aerial vehicle, and has the advantages that an adhesive tape mode is adopted, different unmanned aerial vehicle models are installed in a portable mode, and a land tire device is arranged, so that the control action on the ground is facilitated. The technical aim of the utility model is achieved through the following technical scheme that the land-air control conversion control equipment for the unmanned aerial vehicle comprises a bottom baffle, wherein a left side plate is welded on the left side of the bottom baffle, a right side plate is welded on the right side of the bottom baffle, a threaded column is welded on the bottom of the bottom baffle, a threaded cylinder is connected on the surface of the threaded column in a threaded manner, a chassis is welded on the bottom of the threaded cylinder, a first motor is bolted to one end of the front of the chassis, the output end of the first motor is fixedly connected with a rotating rod through a coupler, one end of the rotating rod is sleeved with a rotating gear, a second motor is bolted to the back of the bottom of the chassis, and the output end of the second motor is fixedly connected with a rotating rod through the coupler. By means of the technical scheme, the unmanned aerial vehicle is conveniently placed and placed, binding belts are arranged on two sides of the left side plate and the right side plate to fix the unmanned aerial vehicle, a threaded column is arranged at the bottom of the bottom baffle plate, the surface of the threaded column and the inner wall of the threaded cylinder are fixedly installed, the rotating rod starts to drive the rotating gear to provide rotating power by starting the first motor, the power-assisted gear is driven to drive the steering tire to rotate, the second motor is started to drive the rotating rod, the rotating rod drives the belt to operate, the auxiliary rod rotates along with the belt to provide power, and the power tire moves. The utility model is further arranged that the left side of the left side plate is connected with a left side binding belt in a sewing way. By adopting the technical scheme, the unmanned aerial vehicle is fixed by arranging the left binding belt and placing the unmanned aerial vehicle into the left side plate and the right side plate. The utility model is further arranged that the right side of the right side plate is connected with a right side binding belt in a sewing way. By adopting the technical scheme, the right side plate is arranged, and after the unmanned aerial vehicle is put in, the right side binding belt and the left side binding belt are adjusted to be bonded, so that the unmanned aerial vehicle is fixed. The utility model is further arranged that the surface of the rotating gear is meshed with a booster gear. By adopting the technical scheme, the booster gear is arranged, and after the rotating gear operates, the booster gear operates to provide rotating force. The utility model further provides that the bottom of the booster gear is welded with a T-shaped rod. By adopting the technical scheme, after the power-assisted gear is driven by the rotating gear, the power-assisted gear drives the T-shaped rod to adjust the rotation angle through the T-shaped ro