CN213620246U

CN213620246U - Many rotors environmental monitoring unmanned aerial vehicle

Info

Publication number: CN213620246U
Application number: CN202022632728.XU
Authority: CN
Inventors: 张磊
Original assignee: Hainan Bolos Control Technology Co ltd
Current assignee: Hainan Bolos Control Technology Co ltd
Priority date: 2020-11-13
Filing date: 2020-11-13
Publication date: 2021-07-06
Anticipated expiration: 2030-11-13

Abstract

The utility model belongs to the environmental monitoring field specifically is a many rotors environmental monitoring unmanned aerial vehicle, including the flight control computer, the bottom fixed mounting of flight control computer has monitor probe, the top surface fixedly connected with ejector pin of flight control computer, the fixed bearing ring that is equipped with of cover in top of ejector pin, the outer wall fixedly connected with of bearing ring strengthens the fan piece, the flight control computer is the rectangle. This many rotor environmental monitoring unmanned aerial vehicle, through four supports of flight control computer outer wall and driving motor's setting, can drive four driving motor simultaneously and provide power to the device, can also increase the stability of the device when increasing the device power, the setting of fan piece and ejector pin is strengthened at the flight control computer top in the cooperation, can be in the air impact force that the balanced wind speed brought to the device around, the stability of the device has been increased, the relatively poor problem of current device list rotor stability has been solved.

Description

Many rotors environmental monitoring unmanned aerial vehicle

Technical Field

The utility model relates to an environmental monitoring field specifically is a many rotors environmental monitoring unmanned aerial vehicle.

Background

Unmanned aerial vehicle is called unmanned aerial vehicle for short, it is the unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to control, or by vehicle-mounted computer completely or intermittently independently operate, unmanned aerial vehicle according to the application field, can be divided into military use and civilian use, for military use, unmanned aerial vehicle divide into reconnaissance aircraft and target drone, civilian use, unmanned aerial vehicle civilian use aspect, is the real just-needed of unmanned aerial vehicle.

In civilian aspect, general unmanned aerial vehicle is used for monitoring the environment, and such unmanned aerial vehicle generally is single rotor unmanned aerial vehicle, and the volume is less, and this kind of unmanned aerial vehicle is great owing to small consequently receiving external environment influence factor, leads to its stability relatively poor, therefore monitoring effect is also relatively poor.

For solving above-mentioned problem, provide a many rotor environmental monitoring unmanned aerial vehicle in this application.

SUMMERY OF THE UTILITY MODEL

Objects of the invention

For solving the technical problem who exists among the background art, the utility model provides a many rotors environmental monitoring unmanned aerial vehicle has the characteristics that can stabilize the high efficiency and carry out the monitoring to the environment.

(II) technical scheme

For solving the technical problem, the utility model provides a many rotor environmental monitoring unmanned aerial vehicle, including the flight control computer, the bottom fixed mounting of flight control computer has monitor, the top surface fixedly connected with ejector pin of flight control computer, the fixed bearing ring that is equipped with in top of ejector pin, the outer wall fixedly connected with of bearing ring strengthens the fan piece, the flight control computer is the rectangle, the outer wall fixedly connected with support of flight control computer, the outer end fixed mounting of support has driving motor, driving motor's output is the pivot, the top fixed mounting of pivot has the bearing piece, and the outer wall fixed mounting who accepts the piece has four drive fan pieces that the position is relative.

Preferably, the flight control computer and the monitoring probe are fixedly connected through a sleeve screwing mechanism.

Preferably, the rotating sleeve mechanism is composed of a round sleeve, a rotating ball and a connecting rod, a monitoring probe is fixedly mounted on the outer wall of the round sleeve, the outer end of the connecting rod is fixedly mounted on the bottom surface of the flight control computer, and the rotating ball can freely rotate on the inner side of the connecting rod.

Preferably, the bottom surface of the flight control computer is fixedly connected with a fixing rod, and the bottom end of each adjacent fixing rod is fixedly provided with a bottom plate.

Preferably, the number of the fixed rods is four, the four fixed rods are arranged at four opposite positions outside the monitoring probe, and a convex lens sheet is fixedly arranged between the adjacent fixed rods.

Preferably, the convex lens plate is a rectangular frame, and a protective frame is fixedly mounted on the inner side of the convex lens plate.

Preferably, four brackets which are opposite in position and have the same specification are fixedly installed on the outer wall of the flight control computer.

The above technical scheme of the utility model has following profitable technological effect:

1. through the setting of four supports of flight control computer outer wall and driving motor, can drive four driving motor simultaneously and provide power to the device, can also increase the stability of the device when increasing the device power, flight control computer top is strengthened the setting of fan piece and ejector pin in the cooperation, can be in the impact force that air speed brought to the device around the aerial equilibrium, increased the device's stability, solved the relatively poor problem of current device list rotor stability.

2. Through the setting of flight control computer bottom plate, can increase the area of contact of the device and bottom surface through the bottom plate, the setting of convex lens piece between the adjacent dead lever on the cooperation can provide certain protective capacities to monitor probe in the air, avoids partly not having the bright flier impact monitor probe in the air and leads to the condition emergence that monitoring effect is poor.

3. Through the setting of rotating the cover mechanism between flight control computer and the monitor, can follow the monitoring demand and adjust monitor's shooting angle, the setting of the inboard protective frame of cooperation epirelief lens piece can also increase definition and the shooting scope when shooing to a certain extent, has increased the device's monitoring effect.

Drawings

Fig. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic structural view of the monitoring probe of the present invention;

FIG. 3 is a front view of the present invention;

fig. 4 is a schematic structural view of the rotating sleeve mechanism of the present invention.

Reference numerals:

in the figure: 1. a flight control computer; 2. a support; 3. a drive motor; 4. a rotating shaft; 5. a bearing ring; 6. a top rod; 7. strengthening the fan blade; 8. a bearing block; 9. driving the fan blade; 10. fixing the rod; 11. a base plate; 12. a lenticular sheet; 13. a protective frame; 14. monitoring the probe; 15. a sleeve rotating mechanism; 151. a round sleeve; 152. rotating the ball; 153. a connecting rod.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention will be described in detail with reference to the accompanying drawings. It should be understood that the description is intended to be illustrative only and is not intended to limit the scope of the present invention. Moreover, in the following description, descriptions of well-known structures and techniques are omitted so as to not unnecessarily obscure the concepts of the present invention.

As shown in fig. 1-4, the utility model provides a many rotor environmental monitoring unmanned aerial vehicle, including flight control computer 1, flight control computer 1's bottom fixed mounting has monitoring probe 14, flight control computer 1's top surface fixedly connected with ejector pin 6, the fixed cover in top of ejector pin 6 is equipped with bearing ring 5, bearing ring 5's outer wall fixedly connected with strengthens fan 7, flight control computer 1 is the rectangle, flight control computer 1's outer wall fixedly connected with support 2, support 2's outer end fixed mounting has driving motor 3, driving motor 3's output is pivot 4, the top fixed mounting of pivot 4 has the piece 8 that holds, and the outer wall fixed mounting who holds piece 8 has four drive fan 9 that the position is relative.

In this embodiment, it should be noted that the flight control computer 1 and the monitoring probe 14 are fixedly connected through a sleeve screwing mechanism 15; the setting of rotating sleeve mechanism 15 is convenient for flight control computer 1 to adjust the shooting angle of monitor probe 14, and then is convenient for shoot different position environment as required, and the side has increased the device to the shooting effect of environment.

In this embodiment, the rotating mechanism 15 is composed of a circular sleeve 151, a rotating ball 152, and a connecting rod 153, the monitoring probe 14 is fixedly mounted on the outer wall of the circular sleeve 151, the outer end of the connecting rod 153 is fixedly mounted on the bottom surface of the flight control computer 1, and the rotating ball 152 can freely rotate inside the connecting rod 153.

In this embodiment, it should be noted that the bottom surface of the flight control computer 1 is fixedly connected with a fixing rod 10, and the bottom end of the adjacent fixing rod 10 is fixedly provided with a bottom plate 11; the setting of bottom plate 11 can increase the area of contact with the bottom surface when the device falls to the ground, and then increased the stability when the device falls to the ground, avoided falling to the ground to make because with the ground area of contact undersize and lead to the condition appearance that the device overturns.

In this embodiment, it should be noted that there are four fixing rods 10, four fixing rods 10 are arranged at four opposite positions outside the monitoring probe 14, and a convex lens 12 is fixedly installed between adjacent fixing rods 10; the arrangement of the convex lens 12 can provide certain protection capability for the monitoring probe 14, and further, the situation that part of unknown flying objects impact the monitoring probe 14 to cause poor monitoring effect can be avoided in the air.

In this embodiment, the convex lens sheet 12 is a rectangular frame, and the protection frame 13 is fixedly mounted on the inner side of the convex lens sheet 12; the setting of protective frame 13 can provide the protective capacities for monitor probe 14 on the one hand, and on the other hand can increase monitor probe 14 and to the definition and the scope of surrounding environment shooting, has increased the shooting effect of device.

In this embodiment, it should be noted that four brackets 2 with the same specification and opposite positions are fixedly mounted on the outer wall of the flight control computer 1; the four supports 2 with the same specification are convenient for driving the driving motor 3 and the driving fan blade 9 to rotate simultaneously, and the device is convenient to operate.

The utility model discloses a theory of operation and use flow: drive motor 3 through four support 2 outer ends earlier drives drive fan 9 simultaneously and provides power to the device, when the device was in flight in the air, the air current around the device can be balanced to the enhancement fan 7 of flight control computer 1 top, and then can effectively increase the device's stability, flight control computer 1 makes monitor 14 carry out all-round rotation through drive swivel cover mechanism 15 according to the demand simultaneously, and then reach the effect of carrying out high-efficient shooting to the surrounding environment, simultaneously monitor 14 outside convex lens piece 12 and protective frame 13 can increase its definition of shooting for monitor 14 when protecting, finally, after the shooting was accomplished, make the bottom plate 11 of flight control computer 1 bottom surface contact with the bottom surface at first, can.

It is to be understood that the above-described embodiments of the present invention are merely illustrative of or explaining the principles of the invention and are not to be construed as limiting the invention. Therefore, any modification, equivalent replacement, improvement and the like made without departing from the spirit and scope of the present invention should be included in the protection scope of the present invention. Further, it is intended that the appended claims cover all such variations and modifications as fall within the scope and boundaries of the appended claims or the equivalents of such scope and boundaries.

Claims

1. A multi-rotor environment monitoring unmanned aerial vehicle is characterized by comprising a flight control computer (1), a monitoring probe (14) is fixedly arranged at the bottom of the flight control computer (1), the top surface of the flight control computer (1) is fixedly connected with a mandril (6), the top end of the mandril (6) is fixedly sleeved with a bearing ring (5), the outer wall of the bearing ring (5) is fixedly connected with a reinforcing fan blade (7), the flight control computer (1) is rectangular, the outer wall of the flight control computer (1) is fixedly connected with a bracket (2), a driving motor (3) is fixedly arranged at the outer end of the bracket (2), the output end of the driving motor (3) is a rotating shaft (4), a bearing block (8) is fixedly arranged at the top end of the rotating shaft (4), and four driving fan blades (9) which are opposite in position are fixedly arranged on the outer wall of the bearing block (8).

2. A multi-rotor environment monitoring unmanned aerial vehicle according to claim 1, wherein the flight control computer (1) and the monitoring probe (14) are fixedly connected through a swivel mechanism (15).

3. A multi-rotor environment monitoring unmanned aerial vehicle according to claim 2, wherein the rotating sleeve mechanism (15) is composed of a round sleeve (151), a rotating ball (152) and a connecting rod (153), the outer wall of the round sleeve (151) is fixedly provided with the monitoring probe (14), the outer end of the connecting rod (153) is fixedly arranged on the bottom surface of the flight control computer (1), and the rotating ball (152) can freely rotate on the inner side of the connecting rod (153).

4. The unmanned aerial vehicle for monitoring environment with multiple rotors as claimed in claim 1, wherein the flight control computer (1) is fixedly connected with fixing rods (10) on the bottom surface, and a bottom plate (11) is fixedly mounted at the bottom end of the adjacent fixing rods (10).

5. A multi-rotor environment monitoring unmanned aerial vehicle according to claim 4, wherein the number of the fixing rods (10) is four, four fixing rods (10) are arranged at four opposite positions outside the monitoring probe (14), and a convex lens sheet (12) is fixedly installed between adjacent fixing rods (10).

6. A multi-rotor environment monitoring unmanned aerial vehicle according to claim 5, wherein the convex lens (12) is a rectangular frame, and a protective frame (13) is fixedly mounted on the inner side of the convex lens (12).

7. A multi-rotor environment monitoring unmanned aerial vehicle according to claim 1, wherein four opposite brackets (2) with the same specification are fixedly installed on the outer wall of the flight control computer (1).