Crossing machine for shooting

Abstract

The utility model provides a crossing machine for shooting, which belongs to the technical field of unmanned aerial vehicles and comprises a machine body, a heat dissipation assembly and a multicolor adjusting lamp. A cover plate is arranged at the top of the machine body; a bottom plate is mounted at the bottom of the machine body; the ventilation holes are formed in the surface of the outer side plate, when the crossing machine flies, air flow quickly passes through the ventilation holes to take away heat in the machine body, the installation hole is formed in the middle of the machine body, the axial flow cooling fan is installed in the installation hole, and when external air flow enters the machine body, the axial flow cooling fan can cool the air flow. The axial flow cooling fan drives airflow to penetrate through the aircraft body and exhaust the airflow from the exhaust duct formed in the bottom of the bottom plate, so that the airflow can cool the interior in the flying process, the cooling effect is achieved, and the situation that normal operation is affected by too high temperature in the aircraft body is avoided.

Description

Technical Field

[0001] The utility model relates to the technical field of drones, in particular to a racing quadcopter for shooting. Background Technique

[0002] The unmanned aerial vehicle, abbreviated as UAV, is an unpiloted aircraft controlled by radio remote control equipment and self-prepared program control devices. The airframe of traditional models includes a fuselage and a bottom plate. The bottom plate is fixed below the fuselage, and the camera is fixed on the fuselage. It needs to pass through the fuselage and then connect to the electrical components carried on the bottom plate. It is impossible to completely separate the camera from the fuselage, and the antenna also needs to pass through the fuselage, making it impossible to completely separate the antenna from the fuselage. Its structure is complex, which is not convenient for mass production and maintenance. Among them, a racing quadcopter with the application number "CN202322558860.4", the bottom plate of the racing quadcopter of the utility model is detachably fixed below the protective frame, and a cavity is formed by the cooperation between the bottom plate and the protective frame; the camera and the antenna are arranged on the bottom plate and at least partially accommodated in the cavity, and the protective frame is provided with a first avoidance hole for avoiding the camera and a second avoidance hole for avoiding the antenna. Therefore, the camera and the antenna of the racing quadcopter can be completely separated from the fuselage, with a simple structure, convenient for assembly, mass production and maintenance. However, there is still room for improvement in the flight process of this racing quadcopter: the heat sink is arranged in the heat dissipation through hole, so that the external air flow cannot quickly circulate inside the fuselage, thereby reducing the heat dissipation and easily causing the temperature to be too high, affecting the working stability. Moreover, the UAV does not have a flight prompt during the flight process, making it impossible for the operator to view the position of the UAV. Content of the Utility Model

[0003] The purpose of the utility model is to provide a racing quadcopter for shooting, so as to solve the problems raised in the above background technique that the heat sink is arranged in the heat dissipation through hole, so that the external air flow cannot quickly circulate inside the fuselage, thereby reducing the heat dissipation and easily causing the temperature to be too high, affecting the working stability, and the UAV does not have a flight prompt during the flight process, making it impossible for the operator to view the position of the UAV.

[0004] To achieve the above purpose, the utility model provides the following technical solution: A racing quadcopter for shooting, including an airframe, a heat dissipation component and a multi-color adjustable lamp;

[0005] Among them: a cover plate is provided on the top of the airframe, a bottom plate is installed at the bottom of the airframe, and outer side plates are provided on both sides of the airframe;

[0006] The heat dissipation component includes a plurality of ventilation holes opened on the surface of the outer side plate, an installation hole is opened in the middle of the airframe, an axial flow cooling fan is installed inside the installation hole, and an exhaust duct is opened at the bottom of the bottom plate corresponding to the axial flow cooling fan;

[0007] An installation groove is opened on the inner wall of the outer side plate, and a multi-color adjustable lamp is installed inside the installation groove.

[0008] As a preferred solution of the present utility model: On both sides of the fuselage, armrests are fixedly installed. One end of each armrest is fixedly installed with a connecting arm part. Connecting holes are formed on the surface of the connecting arm part. A rotor motor is installed through the connecting holes formed on the surface.

[0009] As a preferred solution of the present utility model: At one end of the top of the cover plate, a hinge seat is installed. A camera external mounting bracket is provided on the top of the hinge seat. The camera external mounting bracket is connected to the hinge seat.

[0010] As a preferred solution of the present utility model: A placement seat is installed inside the fuselage, and a battery pack is placed inside the placement seat.

[0011] As a preferred solution of the present utility model: A receiving antenna is fixedly installed at the front end of the fuselage.

[0012] As a preferred solution of the present utility model: Reinforcing ribs are installed on the surface of the armrests.

[0013] Compared with the prior art, the beneficial effects of the present utility model are:

[0014] (1) A number of ventilation holes are formed on the surface of the outer side plate. When the drone is flying, the airflow quickly passes through the ventilation holes to take away the heat inside the fuselage. An installation hole is formed in the middle of the fuselage. An axial flow cooling fan is installed inside the installation hole. When the external airflow enters the inside of the fuselage, the axial flow cooling fan drives the airflow to pass through the fuselage and is discharged from the exhaust duct formed at the bottom of the bottom plate, so that the airflow can dissipate heat inside during flight, achieving the effect of cooling and avoiding the internal temperature of the fuselage being too high to affect normal operation.

[0015] (2) Installation grooves are formed on the inner wall of the outer side plate. The multi-color adjustable lights are installed inside the installation grooves, which reduces the space occupation. At the same time, multi-color adjustable lights are also provided at the bottom of the armrests. The multi-color adjustable lights are lit during flight to facilitate the operator to observe the flight position of the drone. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 is the overall structural schematic diagram of the present utility model;

[0017] Figure 2 is the split structural schematic diagram of the present utility model;

[0018] Figure 3 is the structural schematic diagram of the heat dissipation component of the present utility model;

[0019] Figure 4 is the structural schematic diagram of the installation of the rotor motor of the present utility model.

[0020] In the figure: 1, body; 2, cover plate; 3, bottom plate; 4, outer side plate; 41, mounting groove; 5, heat dissipation component; 51, ventilation hole; 52, mounting hole; 53, axial flow cooling fan; 54, exhaust air duct; 6, multi-color adjustable lamp; 7, machine arm; 8, connecting arm part; 9, connecting hole; 10, rotor motor; 11, hinge seat; 12, camera mounting bracket; 13, placing seat; 14, battery pack; 15, receiving antenna; 16, reinforcing rib. Detailed implementation mode

[0021] To make the purpose, technical solution and advantages of the embodiments of the present utility model clearer, the technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Obviously, the described embodiments are part of the embodiments of the present utility model, rather than all of the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative work shall fall within the protection scope of the present utility model.

[0022] Please refer to Figures 1 - 4 , a racing quadcopter for shooting, comprising: a body 1, a heat dissipation component 5 and a multi-color adjustable lamp 6; a cover plate 2 is provided on the top of the body 1, a bottom plate 3 is installed at the bottom of the body 1, and outer side plates 4 are provided on both sides of the body 1;

[0023] Please refer to Figure 3 , the heat dissipation component 5 includes a plurality of ventilation holes 51 opened on the surface of the outer side plate 4, a mounting hole 52 is opened in the middle of the body 1, an axial flow cooling fan 53 is installed inside the mounting hole 52, and an exhaust air duct 54 is opened at the bottom of the bottom plate 3 corresponding to the axial flow cooling fan 53.

[0024] During specific use: a plurality of ventilation holes 51 are opened on the surface of the outer side plate 4. When the racing quadcopter is flying, the airflow quickly passes through the ventilation holes 51 to take away the heat inside the body 1. A mounting hole 52 is opened in the middle of the body 1, and an axial flow cooling fan 53 is installed inside the mounting hole 52. When the external airflow enters the body 1, the axial flow cooling fan 53 drives the airflow to pass through the body 1 and exhausts the airflow through the exhaust air duct 54 opened at the bottom of the bottom plate 3, so that the airflow can dissipate heat inside during flight, achieving the effect of cooling and avoiding the internal temperature of the body 1 being too high to affect normal operation.

[0025] Please refer to Figure 2 , Figure 3 , a mounting groove 41 is opened on the inner wall of the outer side plate 4, and a multi-color adjustable lamp 6 is installed inside the mounting groove 41.

[0026] During specific use: an installation groove 41 is formed in the inner wall of the outer plate 4, and the multi-color adjustable lamp 6 is installed inside the installation groove 41, which reduces the space occupation. At the same time, the multi-color adjustable lamp 6 is also provided at the bottom of the arm 7. During flight, the multi-color adjustable lamp 6 is lit to facilitate the operator to observe the flight position of the racing drone.

[0027] Please refer to Figure 4 , both sides of the fuselage 1 are fixedly installed with arms 7. One end of the arm 7 is fixedly installed with a connecting arm part 8. A connecting hole 9 is formed on the surface of the connecting arm part 8. The connecting arm part 8 is installed with a rotor motor 10 through the connecting hole 9 formed on the surface.

[0028] During specific use: both sides of the fuselage 1 are fixedly installed with arms 7. One end of the arm 7 is installed with a connecting arm part 8. A connecting hole 9 is formed on the surface of the connecting arm part 8. The rotor motor 10 is installed on the connecting arm part 8 through the connecting hole 9. The rotor motor 10 facilitates providing driving force for flight. The connection method using the connecting hole 9 is convenient for subsequent disassembly and maintenance.

[0029] Please refer to Figure 2 , one end of the top of the cover plate 2 is installed with a hinge seat 11. A camera mounting bracket 12 is provided on the top of the hinge seat 11. The camera mounting bracket 12 is connected to the hinge seat 11.

[0030] During specific use: the cover plate 2 is connected to the hinge seat 11 at the top. The camera mounting bracket 12 is connected to the hinge seat 11 at the top. It is convenient to install a shooting camera through the camera mounting bracket 12.

[0031] Please refer to Figure 2 , Figure 3 , a placement seat 13 is installed inside the fuselage 1. A battery pack 14 is placed inside the placement seat 13.

[0032] During specific use: the placement seat 13 is installed inside the fuselage 1. The battery pack 14 is placed inside the placement seat 13, which is convenient to provide power support for electronic components through the battery pack 14.

[0033] Please refer to Figure 1 , a receiving antenna 15 is fixedly installed at the front end of the fuselage 1.

[0034] During specific use: the receiving antenna 15 installed at the front end of the fuselage 1 is convenient for receiving command signals sent by ground operators to realize the control of the racing drone.

[0035] Please refer to Figure 1 , a reinforcing rib 16 is installed on the surface of the arm 7.

[0036] During specific use: the reinforcing rib 16 is installed on the surface of the arm 7. The reinforcing rib 16 is convenient for improving the structural strength of the arm 7.

[0037] A number of ventilation holes 51 are provided on the surface of the outer plate 4. When the drone is flying, the airflow quickly passes through the ventilation holes 51 to take away the heat inside the fuselage 1. An installation hole 52 is provided in the middle of the fuselage 1, and an axial flow cooling fan 53 is installed inside the installation hole 52. When the external airflow enters the fuselage 1, the axial flow cooling fan 53 drives the airflow to pass through the fuselage 1 and discharges the airflow from the exhaust duct 54 provided at the bottom of the bottom plate 3, so that the airflow can dissipate heat inside during flight, achieving the effect of cooling and avoiding the internal temperature of the fuselage 1 being too high to affect normal operation.

[0038] The content not described in detail in this specification belongs to the prior art well-known to those skilled in the art. Although the present invention has been described in detail with reference to the foregoing embodiments, for those skilled in the art, they can still modify the technical solutions described in the foregoing embodiments, or perform equivalent replacements for some of the technical features. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.

Claims

1. A through-copter for shooting, characterized in that, Comprising: A fuselage (1), a cover plate (2) is provided at the top of the fuselage (1), a bottom plate (3) is installed at the bottom of the fuselage (1), and outer side plates (4) are provided on both sides of the fuselage (1); A heat dissipation component (5), the heat dissipation component (5) includes a plurality of ventilation holes (51) opened on the surface of the outer side plate (4), an installation hole (52) is opened in the middle of the fuselage (1), and an axial flow cooling fan (53) is installed inside the installation hole (52), and a ventilation duct (54) is opened at the bottom of the bottom plate (3) corresponding to the axial flow cooling fan (53); A multi-color adjustable lamp (6), an installation groove (41) is opened on the inner wall of the outer side plate (4), and the multi-color adjustable lamp (6) is installed inside the installation groove (41).

2. The FPV drone for shooting according to claim 1, wherein: Both sides of the fuselage (1) are fixedly installed with machine arms (7), one end of the machine arm (7) is fixedly installed with a connecting arm part (8), a connecting hole (9) is opened on the surface of the connecting arm part (8), and a rotor motor (10) is installed through the connecting hole (9) opened on the surface of the connecting arm part (8).

3. A through-plane camera for shooting according to claim 1, characterized in that: One end of the top of the cover plate (2) is installed with a hinge seat (11), a camera mounting bracket (12) is provided on the top of the hinge seat (11), and the camera mounting bracket (12) is connected to the hinge seat (11).

4. A through-camera for shooting according to claim 3, characterized in that: A placement seat (13) is installed inside the fuselage (1), and a battery pack (14) is placed inside the placement seat (13).

5. A through-camera for shooting according to claim 1, characterized in that: A receiving antenna (15) is fixedly installed at the front end of the fuselage (1).

6. A through-camera for shooting according to claim 2, characterized in that: Reinforcing ribs (16) are installed on the surface of the machine arm (7).

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