Control terminal applied to C-band unmanned aerial vehicle communication link

Abstract

The utility model relates to the technical field of unmanned aerial vehicle communication, and discloses a control terminal applied to a C-band unmanned aerial vehicle communication link, which comprises a main body mechanism and an auxiliary mechanism, the auxiliary mechanism is located at the outer end of the main body mechanism, and the main body mechanism comprises a machine body, a machine cover, an observation window, a main machine and a dust removal assembly. The machine cover is movably installed on the outer side of the machine body, the observation window is fixedly arranged at the inner end of the machine cover, the main machine is fixedly installed in the machine body, the dust removal assembly is movably installed in the machine body and comprises an auxiliary bin, a dust suction pump and a dust collection box, and the auxiliary bin is fixedly installed on the outer side of the machine body. The dust suction pump is fixedly installed in the auxiliary bin. According to the control terminal applied to the C-band unmanned aerial vehicle communication link, a main body mechanism is installed, a servo motor is started, and a ball screw is driven to rotate, so that a ball nut and a dust suction port move up and down, and a dust suction pump sucks dust in a vehicle body into a dust collection box for storage through the dust suction port and a dust guide pipe; and the safety of the device is effectively improved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicle communication, in particular to a control terminal applied to a C-band unmanned aerial vehicle communication link. Background Art

[0002] C-band UAV data link communication system, description: C-band UAV data link is a system for LOS (line of sight) air-to-air and air-to-ground real-time two-way communication, transmitting manned / unmanned system command and control data on an electronic warfare (EW) protected ground system with high reliability requirements, and receiving telemetry and high data rate real-time video data. Surveillance data from manned and unmanned aerial vehicle sensors are compressed in H.264 format and transmitted to the ground control station via a long-range C-band data link. UAV remote control data is transmitted in real time from the ground control station to the UAV flight computer. The system consists of an air data terminal (ADT) and a ground data terminal (GDT).

[0003] The existing patent CN205707368U proposes a mainframe cabin for unmanned aerial vehicles. The utility model is composed of side panels and a bottom plate, and is characterized in that: the side panels and the bottom plate are both made of aviation aluminum, the side panels are vertically arranged on the bottom plate, and the side panels are U-shaped structures surrounded by the first long side panel, the short side panel, and the second long side panel in sequence, and the short side panel is perpendicular to the first and second long side panels; the bottom plate is a rectangular structure, and together with the side panels thereon, it forms a rectangular parallelepiped frame structure with an upward opening and a short side opening; a number of equidistant long strip grooves are respectively provided on the side panels and the bottom plate. Compared with the prior art, the utility model has the characteristics of simple structure, easy processing and forming, strong heat dissipation capacity, strong anti-interference ability, etc., under the premise of meeting the requirements of light weight and installation and use with multiple components, which effectively improves the comprehensive use performance of the mainframe cabin for unmanned aerial vehicles and meets market demand.

[0004] However, compared with the prior art, the existing patent CN205707368U has the characteristics of simple structure, easy processing and forming, strong heat dissipation capacity, strong anti-interference ability, etc. under the premise of light weight and installation and use with multiple components, which effectively improves the comprehensive performance of the main engine compartment for drones and meets market demand. However, when the drone is flying at high altitudes, it may be subject to greater wind resistance, and dust mixed in the wind passes through the cabin and enters the interior of the main engine, which may affect the normal operation of the main engine over time. Utility Model Content

[0005] 1. Technical issues to be resolved

[0006] The purpose of the utility model is to provide a control terminal for a C-band UAV communication link, so as to solve the problem mentioned in the above background technology that when the UAV is flying at high altitude, it may be subject to large wind resistance, and the wind mixed with dust passes through the cabin and enters the interior of the host, which may affect the normal operation of the host over time.

[0007] (II) Technical solution

[0008] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: a control terminal applied to a C-band UAV communication link, comprising a main mechanism and an auxiliary mechanism, wherein the auxiliary mechanism is located at the outer end of the main mechanism, and the main mechanism comprises a machine body, a machine cover, an observation window, a main body and a dust removal assembly, wherein the machine cover is movably mounted on the outer side of the machine body, the observation window is fixedly arranged at the inner end of the machine cover, the main body is fixedly mounted on the inside of the machine body, and the dust removal assembly is movably mounted on the inside of the machine body; the dust removal assembly comprises a sub-bin, a dust suction pump and a dust collecting box, wherein the sub-bin is fixedly mounted on the outer side of the machine body, the dust suction pump is fixedly mounted on the inside of the sub-bin, and the dust collecting box is fixedly mounted on the lower end of the dust suction pump.

[0009] Preferably, the dust removal assembly also includes a dust guide pipe, a servo motor, a ball screw, a ball nut, a dust suction port and a heat dissipation window. The dust guide pipe is fixedly installed in the middle of the machine body and the auxiliary compartment. The servo motor is started to drive the ball screw to rotate, causing the ball nut and the dust suction port to move up and down.

[0010] Preferably, the servo motor is fixedly mounted on the inner end of the machine body, the ball screw is movably mounted on the upper end of the servo motor, and the dust suction pump sucks the dust inside the machine body into the dust collecting box through the dust suction port and the dust guide pipe for storage.

[0011] Preferably, the ball nut is movably mounted on the outer end of the ball screw, the dust suction port is fixedly mounted on the outer end of the ball nut, and the heat dissipation window 1 is fixedly arranged on the left side of the machine body. The arrangement of the heat dissipation window 1 facilitates the heat dissipation inside the auxiliary compartment, thereby effectively improving the safety of the device.

[0012] Preferably, the auxiliary mechanism includes a semiconductor refrigerator, a temperature controller, a condenser, a ventilation net, a motor, a fan and a heat dissipation window. The semiconductor refrigerator is fixedly installed at the upper end of the dust box, and the semiconductor refrigerator cools the condenser through the temperature controller.

[0013] Preferably, the temperature controller is fixedly installed on the right side of the semiconductor refrigerator, the condenser is fixedly installed on the right side of the temperature controller, and the ventilation net is fixedly arranged on the right side of the condenser. The motor is started to drive the fan to rotate and generate wind.

[0014] Preferably, the motor is fixedly mounted on the left side of the inner end of the auxiliary compartment, the fan is movably mounted on the right end of the motor, and the heat dissipation window 2 is fixedly arranged at the outer end of the auxiliary compartment. Wind passes through the condenser to form cold air, which is blown toward the main unit through the ventilation net to dissipate heat. Excess heat inside the body can be discharged from the heat dissipation window 2, which effectively improves the safety of the device.

[0015] Compared with the prior art, the beneficial effects of the utility model are:

[0016] 1. The control terminal applied to the communication link of the C-band UAV is installed on the main body, the servo motor is started, and the ball screw is driven to rotate, so that the ball nut and the dust suction port move up and down. The dust suction pump sucks the dust inside the body into the dust collection box through the dust suction port and the dust guide pipe for storage. The setting of the heat dissipation window facilitates the heat dissipation inside the auxiliary compartment, which effectively improves the safety of the device;

[0017] 2. The control terminal used for the C-band UAV communication link installs auxiliary mechanisms. The semiconductor refrigerator cools the condenser through the temperature controller. The motor starts and drives the fan to rotate to generate wind. The wind passes through the condenser to form cold wind, which is blown to the host through the ventilation net to dissipate heat. The excess heat inside the body can be discharged from the second heat dissipation window, which effectively improves the safety of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] Figure 1 It is a schematic diagram of the three-dimensional structure of the utility model;

[0019] Figure 2 This is a schematic diagram of the cross-sectional structure of the utility model;

[0020] Figure 3 It is a schematic diagram of a partial cross-section of the three-dimensional structure of the dust removal component of the utility model;

[0021] Figure 4 It is a schematic diagram of the partial cross-section of the three-dimensional structure of the dust removal component of the utility model.

[0022] In the figure: 1. Main mechanism; 101. Machine body; 102. Machine cover; 103. Observation window; 104. Main body; 105. Dust removal assembly; 1051. Auxiliary compartment; 1052. Dust suction pump; 1053. Dust collection box; 1054. Dust guide tube; 1055. Servo motor; 1056. Ball screw; 1057. Ball nut; 1058. Dust suction port; 1059. Heat dissipation window one; 2. Auxiliary mechanism; 201. Semiconductor refrigerator; 202. Temperature controller; 203. Condenser; 204. Ventilation net; 205. Motor; 206. Fan; 207. Heat dissipation window two. DETAILED DESCRIPTION

[0023] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0024] See also Figure 1-Figure 4 The utility model provides a technical solution: a control terminal for a C-band UAV communication link, comprising a main body 1 and an auxiliary body 2, the auxiliary body 2 is located at the outer end of the main body 1, the main body 1 comprises a body 101, a cover 102, an observation window 103, a main body 104 and a dust removal component 105, the cover 102 is movably mounted on the outer side of the body 101, the observation window 103 is fixedly arranged at the inner end of the cover 102, the main body 104 is fixedly mounted inside the body 101, and the dust removal component 105 is movably mounted inside the body 101; the dust removal component 105 comprises an auxiliary compartment 1051, a dust suction pump 1052 and a dust collection box 1053, the auxiliary compartment 1051 is fixedly mounted on the outer side of the body 101, the dust suction pump 105 2 is fixedly installed inside the auxiliary bin 1051, the dust box 1053 is fixedly installed at the lower end of the dust suction pump 1052, the dust removal assembly 105 also includes a dust guide pipe 1054, a servo motor 1055, a ball screw 1056, a ball nut 1057, a dust suction port 1058 and a heat dissipation window 1059, the dust guide pipe 1054 is fixedly installed in the middle of the machine body 101 and the auxiliary bin 1051, the servo motor 1055 is fixedly installed at the inner end of the machine body 101, the ball screw 1056 is movably installed at the upper end of the servo motor 1055, the ball nut 1057 is movably installed at the outer end of the ball screw 1056, the dust suction port 1058 is fixedly installed at the outer end of the ball nut 1057, and the heat dissipation window 1059 is fixedly set on the left side of the machine body 101.

[0025] The auxiliary mechanism 2 includes a semiconductor refrigerator 201, a temperature controller 202, a condenser 203, a ventilation net 204, a motor 205, a fan 206 and a heat dissipation window 207. The semiconductor refrigerator 201 is fixedly installed at the upper end of the dust box 1053, the temperature controller 202 is fixedly installed on the right side of the semiconductor refrigerator 201, the condenser 203 is fixedly installed on the right side of the temperature controller 202, the ventilation net 204 is fixedly set on the right side of the condenser 203, the motor 205 is fixedly installed on the left side of the inner end of the auxiliary compartment 1051, the fan 206 is movably installed on the right end of the motor 205, and the heat dissipation window 207 is fixedly set at the outer end of the auxiliary compartment 1051. When using the control device for the C-band UAV communication link When the terminal is in operation, the servo motor 1055 starts and drives the ball screw 1056 to rotate, so that the ball nut 1057 and the dust suction port 1058 move up and down, and the dust suction pump 1052 sucks the dust inside the body 101 into the dust box 1053 through the dust suction port 1058 and the dust guide pipe 1054 for storage. The setting of the heat dissipation window 1059 facilitates the heat dissipation inside the auxiliary compartment 1051. The semiconductor refrigerator 201 cools the condenser 203 through the temperature controller 202. The motor 205 starts and drives the fan 206 to rotate to generate wind. The wind passes through the condenser 203 to form cold wind, which is blown to the main unit through the ventilation net 204 to dissipate heat. The excess heat inside the body 101 can be discharged from the heat dissipation window 207.

[0026] Working principle: When using the control terminal applied to the C-band UAV communication link, the servo motor 1055 is started, driving the ball screw 1056 to rotate, so that the ball nut 1057 and the dust suction port 1058 move up and down, and the dust suction pump 1052 sucks the dust inside the body 101 into the dust box 1053 through the dust suction port 1058 and the dust guide tube 1054 for storage. The setting of the heat dissipation window 1059 facilitates the heat dissipation inside the auxiliary compartment 1051. The semiconductor refrigerator 201 cools the condenser 203 through the temperature controller 202. The motor 205 is started and drives the fan 206 to rotate to generate wind. The wind passes through the condenser 203 to form cold wind, which is blown to the main unit through the ventilation net 204 to dissipate heat. Excess heat inside the body 101 can be discharged from the heat dissipation window 207.

[0027] Finally, it should be noted that the above content is only used to illustrate the technical solution of the utility model, rather than to limit the protection scope of the utility model. Simple modifications or equivalent substitutions of the technical solution of the utility model by ordinary technicians in this field do not deviate from the essence and scope of the technical solution of the utility model.

Claims

1. A control terminal for a C-band UAV communication link, comprising a main mechanism (1) and an auxiliary mechanism (2), characterized in that: The auxiliary mechanism (2) is located at the outer end of the main mechanism (1); the main mechanism (1) comprises a machine body (101), a machine cover (102), an observation window (103), a main body (104) and a dust removal component (105); the machine cover (102) is movably mounted on the outer side of the machine body (101); the observation window (103) is fixedly arranged at the inner end of the machine cover (102); the main body (104) is fixedly mounted inside the machine body (101); and the dust removal component (105) is movably mounted inside the machine body (101); The dust removal component (105) comprises an auxiliary bin (1051), a dust suction pump (1052) and a dust collection box (1053); the auxiliary bin (1051) is fixedly mounted on the outside of the machine body (101); the dust suction pump (1052) is fixedly mounted inside the auxiliary bin (1051); and the dust collection box (1053) is fixedly mounted at the lower end of the dust suction pump (1052).

2. A control terminal for a C-band UAV communication link according to claim 1, characterized in that: The dust removal assembly (105) further comprises a dust guide pipe (1054), a servo motor (1055), a ball screw (1056), a ball nut (1057), a dust suction port (1058) and a heat dissipation window (1059); the dust guide pipe (1054) is fixedly mounted in the middle of the machine body (101) and the auxiliary compartment (1051).

3. A control terminal for a C-band UAV communication link according to claim 2, characterized in that: The servo motor (1055) is fixedly mounted on the inner end of the machine body (101), and the ball screw (1056) is movably mounted on the upper end of the servo motor (1055).

4. A control terminal for a C-band UAV communication link according to claim 3, characterized in that: The ball nut (1057) is movably mounted on the outer end of the ball screw (1056), the dust suction port (1058) is fixedly mounted on the outer end of the ball nut (1057), and the heat dissipation window (1059) is fixedly arranged on the left side of the machine body (101).

5. A control terminal for a C-band UAV communication link according to claim 4, characterized in that: The auxiliary mechanism (2) comprises a semiconductor refrigerator (201), a temperature controller (202), a condenser (203), a ventilation net (204), a motor (205), a fan (206) and a second heat dissipation window (207); the semiconductor refrigerator (201) is fixedly mounted on the upper end of the dust box (1053).

6. A control terminal for a C-band UAV communication link according to claim 5, characterized in that: The temperature controller (202) is fixedly installed on the right side of the semiconductor refrigerator (201), the condenser (203) is fixedly installed on the right side of the temperature controller (202), and the ventilation net (204) is fixedly arranged on the right side of the condenser (203).

7. A control terminal for a C-band UAV communication link according to claim 6, characterized in that: The motor (205) is fixedly mounted on the left side of the inner end of the auxiliary compartment (1051), the fan (206) is movably mounted on the right end of the motor (205), and the second heat dissipation window (207) is fixedly arranged on the outer end of the auxiliary compartment (1051).

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