CN211457698U - Dust protected unmanned aerial vehicle carries satellite communication terminal controller - Google Patents

Abstract

The utility model discloses a dustproof unmanned aerial vehicle carries satellite communication terminal controller, including the mounting panel, the mounting panel bottom end bolt installs the machine box, the welding of machine box inside bottom has the support frame, support frame top end bolt installs the layer board, the utility model discloses a ventilation chamber that sets up through the inside both sides of machine box, air inlet and gas vent that can cooperate the machine box both ends surface to set up respectively accelerate the circulation face of gas to utilize the gas of high-speed flow to cool down the machine box, avoid the condition that traditional open heat dissipation leads to whole device inside entering dust to take place, through the fin of the inside both sides eye-splice installation of machine box, can cooperate the heat-conducting plate of fin one end bolt installation, cool down satellite communication module and information transmission control module, the fin that one end is located in ventilation chamber can improve the radiating effect of whole heat conduction and radiation structure simultaneously, the situation that the whole machine box is excessively sealed to cause poor heat dissipation effect is avoided.

Description

Dust protected unmanned aerial vehicle carries satellite communication terminal controller

Technical Field

The utility model relates to an unmanned aerial vehicle field specifically is a dust protected unmanned aerial vehicle carries satellite communication terminal control ware.

Background

An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Drones tend to be more suitable for tasks that are too "fool, dirty, or dangerous" than are manned aircraft. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + the industry application is really just needed by the unmanned aerial vehicle; at present, the unmanned aerial vehicle is applied to the fields of aerial photography, agriculture, plant protection, miniature self-timer, express transportation, disaster relief, wild animal observation, infectious disease monitoring, surveying and mapping, news reporting, power inspection, disaster relief, film and television shooting, romantic manufacturing and the like, the application of the unmanned aerial vehicle is greatly expanded, and developed countries actively expand industrial application and develop unmanned aerial vehicle technology.

The most main structure of unmanned aerial vehicle is exactly satellite communication terminal controller, and it is unmanned aerial vehicle's core, need rely on satellite communication terminal controller to receive and dispatch the satellite signal to control unmanned aerial vehicle work.

However, the existing unmanned airborne satellite communication terminal controller has the following disadvantages:

1. the existing unmanned aerial vehicle carries satellite communication terminal controller, because of need work for a long time, the radiating effect demand is mostly open heat dissipation, improves the radiating effect of unmanned aerial vehicle carries satellite communication terminal controller, and this kind of mode leads to a large amount of dusts to get into in the unmanned aerial vehicle carries satellite communication terminal controller easily to cause the damage to it.

2. The existing controller of the unmanned aerial vehicle-mounted satellite communication terminal has poor heat insulation effect, and easily causes mutual interference between equipment and the unmanned aerial vehicle due to temperature to influence respective work operation.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide a dustproof formula unmanned aerial vehicle carries satellite communication terminal controller, carry satellite communication terminal controller with current unmanned aerial vehicle in solving above-mentioned background art, work for a long time because of needs, the radiating effect demand, mostly be open heat dissipation, improve the radiating effect that unmanned aerial vehicle carried satellite communication terminal controller, this kind of mode leads to a large amount of dusts to get into in the unmanned aerial vehicle carries satellite communication terminal controller easily, thereby cause the damage to it, current unmanned aerial vehicle carries satellite communication terminal controller, thermal-insulated effect that separates is relatively poor, lead to easily because of temperature mutual interference between equipment and the unmanned aerial vehicle, influence respective work operation's problem.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides a dust protected unmanned aerial vehicle carries satellite communication terminal controller, includes the mounting panel, the quick-witted box is installed to mounting panel bottom bolt, the inside bottom welding of quick-witted box has the support frame, the layer board is installed to support frame top bolt, satellite communication module and information delivery control module are installed to layer board top bolt, data communication is connected between satellite communication module and the information delivery control module, the electronic condenser is installed to the inside top bolt of quick-witted box, the rotatory communication antenna of installing of machine box one end.

Preferably, the ventilation chamber has all been seted up to the inside both sides of machine box, air inlet and gas vent have been seted up respectively to machine box both ends surface, air inlet and gas vent all communicate each other with the ventilation intracavity portion, through the ventilation chamber of seting up in the inside both sides of machine box, can cooperate the air inlet and the gas vent of seting up respectively in machine box both ends surface, with higher speed gaseous circulation face to utilize the high-speed gaseous gas that flows to cool down the machine box, avoid the condition emergence that traditional open heat dissipation leads to the inside entering dust of whole device.

Preferably, the fin is installed to the inside both sides eye-splice of machine box, fin one end is located the ventilation cavity, the heat-conducting plate is installed to fin other end bolt, the heat-conducting plate supports respectively to lean on in satellite communication module and information transmission control module one side, through the fin of the inside both sides eye-splice installation of machine box, can cooperate the heat-conducting plate of fin one end bolt installation, to satellite communication module and information transmission control module cooling of dispelling the heat, the fin that one end is located the ventilation cavity simultaneously can improve whole heat conduction heat radiation structure's radiating effect, avoids whole machine box too sealed condition that leads to the radiating effect to be poor to take place.

Preferably, the tin piece division board is installed to the bolt between satellite communication module and the information transmission control module, drier storage box is installed to the inside bottom bolt of machine box, through the tin piece division board of bolt installation between satellite communication module and the information transmission control module, the insulating nature of usable tin piece division board and the function that separates the temperature are to satellite communication module and information transmission control module separation, avoid satellite communication module and information transmission control module during operation to influence each other and damage the condition that leads to the nearer together damage of another party's mounted position in one party and take place, install drier storage box through the inside bottom bolt of machine box, the additive drier, adsorb the liquid that condenses in the machine box, it takes place to avoid the condition that wets in the machine box and lead to electronic structure to damage.

Preferably, machine box inside inlays and has to separate the temperature intermediate layer, the liquid guide groove has been seted up on machine box surface, through the inside inlayed temperature intermediate layer that separates of machine box, can separate the temperature to whole machine box to avoid because of the high or low condition that leads to machine box inner structure to damage unable normal work takes place excessively of ambient temperature, through the liquid guide groove of seting up on machine box surface, can be with the liquid discharge of long-pending staying at machine box surface, avoid the liquid volume to stay on machine box surface, the condition that causes the corruption to the machine box takes place.

Preferably, the inside temperature insulating plate that inlays of mounting panel, the wiring hole has been seted up on the mounting panel surface, through the inside mosaic temperature insulating plate of mounting panel, can separate the temperature to the mounting panel to the condition that the temperature that avoids whole equipment work to produce and the temperature that unmanned aerial vehicle work produced influenced each other appears, through the wiring hole that the mounting panel surface was seted up, makes things convenient for carrying out being connected of power and job control pencil between whole equipment and the unmanned aerial vehicle.

The utility model provides a dust protected unmanned aerial vehicle carries satellite communication terminal controller possesses following beneficial effect:

(1) the utility model discloses a ventilation chamber that the inside both sides of machine box were seted up, air inlet and gas vent that can cooperate machine box both ends surface to set up respectively, gaseous circulation face accelerates, thereby utilize the gas of high-speed flow to cool down the machine box, avoid the condition emergence that traditional open heat dissipation leads to the inside entering dust of whole device, fin through the inside both sides eye-splice installation of machine box, can cooperate the heat-conducting plate of fin one end bolt installation, cool down the heat dissipation to satellite communication module and information transport control module, the fin that one end is located ventilation intracavity simultaneously can improve whole heat conduction heat radiation structure's radiating effect, avoid the too sealed condition that leads to the radiating effect poor to take place of whole machine box.

(2) The utility model discloses a tin piece division board of bolt installation between satellite communication module and the information transmission control module, the insulating nature of usable tin piece division board carries out the separation with the function that separates the temperature to satellite communication module and information transmission control module, avoid satellite communication module and information transmission control module during operation to influence each other and damage the condition that leads to the nearer together damage of another party's mounted position at one party and take place, install drier storage box through the inside bottom bolt of machine box, the addable drier, the liquid that condenses in the machine box adsorbs, the condition that leads to electronic structure to damage in avoiding the machine box to damp takes place.

(3) The utility model discloses an inside inlayed temperature intermediate layer that separates of machine box, can separate the temperature to whole machine box, thereby avoid taking place because of the too high or low condition that leads to the unable normal work of machine box inner structure damage of external temperature, the liquid guide groove of seting up through machine box surface, can be with the liquid discharge of long-pending staying machine box surface, avoid the liquid volume to stay machine box surface, the condition that causes the corruption to the machine box takes place, through the inside inlayed temperature insulating board of mounting panel, can separate the temperature to the mounting panel, thereby the condition that the temperature that avoids whole equipment work to produce and the temperature that unmanned aerial vehicle work produced influence each other appears, the wiring hole of seting up through the mounting panel surface, make things convenient for carrying out the connection of power and work control pencil between whole equipment and the unmanned aerial vehicle.

Drawings

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

FIG. 2 is a side view of the overall structure of the present invention;

FIG. 3 is a schematic view of the internal structure of the case of the present invention;

fig. 4 is a schematic view of the internal structure of the mounting plate of the present invention.

In the figure: 1. mounting a plate; 2. a case; 3. a communication antenna; 4. an air inlet; 5. an exhaust port; 6. a liquid guide groove; 7. a support frame; 8. a support plate; 9. a satellite communication module; 10. an information delivery control module; 11. a tin sheet separation plate; 12. an electronic condenser; 13. a communication antenna; 14. a thermal insulation interlayer; 15. a heat conducting plate; 16. a heat sink; 17. a ventilation cavity; 18. a thermal insulation plate; 19. and a wiring hole.

Detailed Description

The technical solution in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention.

As shown in fig. 1-4, the utility model provides a technical solution: the utility model provides a dust protected unmanned aerial vehicle carries satellite communication terminal controller, includes mounting panel 1, 1 bottom bolt of mounting panel installs a machine box 2, the inside bottom welding of machine box 2 has support frame 7, layer board 8 is installed to 7 top bolts of support frame, satellite communication module 9 and information transport control module 10 are installed to 8 top bolts of layer board, data communication is connected between satellite communication module 9 and the information transport control module 10, electronic condenser 12 is installed to 2 inside top bolts of machine box, 2 one end rotations of machine box are installed communication antenna 3.

Ventilation chamber 17 has all been seted up to the inside both sides of machine box 2, air inlet 4 and gas vent 5 have been seted up respectively to 2 both ends surfaces of machine box, air inlet 4 and gas vent 5 all communicate each other with ventilation chamber 17 is inside, through the ventilation chamber 17 of seting up in the inside both sides of machine box 2, can cooperate air inlet 4 and gas vent 5 that 2 both ends surfaces of machine box were seted up respectively, the circulation face of gas with higher speed to utilize the gas of high-speed flow to cool down machine box 2, avoid traditional open heat dissipation to lead to the inside condition of getting into the dust of whole device to take place.

The inside both sides eye-splice of machine box 2 installs fin 16, fin 16 one end is located ventilation chamber 17, heat-conducting plate 15 is installed to fin 16 other end bolt, heat-conducting plate 15 supports respectively and leans on in satellite communication module 9 and information delivery control module 10 one side, and through the fin 16 of the inside both sides eye-splice installation of machine box 2, can cooperate the heat-conducting plate 15 of the installation of fin 16 one end bolt, carries out the heat dissipation cooling to satellite communication module 9 and information delivery control module 10, and fin 16 that one end is located ventilation chamber 17 simultaneously can improve whole heat conduction heat radiation structure's radiating effect, avoids whole machine box 2 too sealed the poor condition of radiating effect to take place that leads to.

Tin piece division board 11 is installed to the bolt between satellite communication module 9 and the information transmission control module 10, drier storage box 13 is installed to the inside bottom bolt of machine box 2, through the tin piece division board 11 of bolt installation between satellite communication module 9 and the information transmission control module 10, usable tin piece division board 11's insulating nature and the function that separates the temperature are to satellite communication module 9 and information transmission control module 10 separation, avoid satellite communication module 9 and information transmission control module 10 during operation influence each other and damage the condition that leads to the nearer together damage of another party mounted position and take place in the side, install drier storage box 13 through the inside bottom bolt of machine box 2, the addable drier, adsorb the liquid that condenses in the machine box 2, it leads to the condition of electronic structure damage to take place to receive the tide in the machine box 2.

Machine 2 inside inlays and has to separate temperature intermediate layer 14, liquid guide groove 6 has been seted up on machine 2 surfaces, through machine 2 inside inlayed separate temperature intermediate layer 14, can separate the temperature to whole machine box 2 to avoid because of the high or condition emergence that leads to the unable normal work of machine 2 inner structure damage of low excessively of ambient temperature, liquid guide groove 6 of seting up through machine 2 surfaces can be with the liquid discharge of long-pending machine box 2 surfaces of staying, avoid the liquid volume to stay machine box 2 surfaces, the condition that causes the corruption to machine box 2 takes place.

The inside temperature insulating plate 18 that inlays of mounting panel 1, wiring hole 19 has been seted up on the mounting panel 1 surface, through the inside inlayed temperature insulating plate 18 of mounting panel 1, can separate the temperature to mounting panel 1 to the condition of the temperature that avoids the temperature that whole equipment work produced and unmanned aerial vehicle work to produce influences each other appears, through the wiring hole 19 that the mounting panel 1 surface was seted up, makes things convenient for carrying out being connected of power and work control pencil between whole equipment and the unmanned aerial vehicle.

It should be noted that, when working, the dustproof unmanned aerial vehicle carries the satellite communication terminal controller, through the electronic condenser 12 installed on the top bolt in the machine box 2, the internal structure of the machine box 2 can be cooled, the heat dissipation requirement of the equipment running for a long time is satisfied, meanwhile, through the communication antenna 3 installed by rotating one end of the machine box 2, the signal receiving and sending intensity of the satellite communication module 9 and the information transmission control module 10 in the whole machine box 2 can be enhanced, the condition that the sealed machine box 2 influences the information transmission of the satellite communication module 9 and the information transmission control module 10 is avoided, through the ventilation cavities 17 arranged on two sides in the machine box 2, the ventilation surface can be matched with the air inlet 4 and the air outlet 5 respectively arranged on the two end surfaces of the machine box 2, the circulation surface of the air is accelerated, thereby the machine box 2 is cooled by the high-speed flowing air, the condition that the dust enters the whole device due to the traditional open heat dissipation is avoided, the heat radiating fins 16 are installed through inserting and buckling at two sides in the machine box 2 and can be matched with the heat conducting plates 15 installed on the bolts at one ends of the heat radiating fins 16 to radiate and cool the satellite communication module 9 and the information transmission control module 10, meanwhile, the heat radiating fins 16 with one ends positioned in the ventilation cavities 17 can improve the heat radiating effect of the whole heat conducting and radiating structure, thereby avoiding the occurrence of poor heat radiating effect caused by over-sealing of the whole machine box 2, the satellite communication module 9 and the information transmission control module 10 can be separated by the tin sheet partition plate 11 installed between the satellite communication module 9 and the information transmission control module 10 through the bolts, the occurrence of mutual influence when the satellite communication module 9 and the information transmission control module 10 work and the occurrence of closer and same damage of the installation position of the other party caused by damage of the one party is avoided, the drying agent storage box 13 is installed on the bottom end in the machine box 2 through, a drying agent can be added to adsorb the liquid condensed in the case 2, thereby avoiding the electronic structure damage caused by the damp in the case 2, the whole case 2 can be insulated through the insulating interlayer 14 embedded in the case 2, thereby avoiding the situation that the internal structure of the machine box 2 is damaged and can not work normally due to overhigh or overlow external temperature, the liquid guide groove 6 arranged on the surface of the case 2 can discharge the liquid accumulated on the surface of the case 2, thereby avoiding the liquid volume remaining on the surface of the case 2, the case 2 is corroded, the mounting plate 1 can be insulated through the heat insulation plate 18 embedded in the mounting plate 1, thereby avoiding the mutual influence between the temperature generated by the work of the whole equipment and the temperature generated by the work of the unmanned aerial vehicle, through the wiring hole 19 that the mounting panel 1 surface was seted up, make things convenient for between whole equipment and the unmanned aerial vehicle to carry out being connected of power and work control pencil.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims (6)

1. The utility model provides a dust protected unmanned aerial vehicle carries satellite communication terminal control ware, includes mounting panel (1), its characterized in that: mounting panel (1) bottom bolt installs machine box (2), the inside bottom welding of machine box (2) has support frame (7), layer board (8) are installed to support frame (7) top bolt, satellite communication module (9) and information transmission control module (10) are installed to layer board (8) top bolt, data communication connection between satellite communication module (9) and information transmission control module (10), electronic condenser (12) are installed to the inside top bolt of machine box (2), communication antenna (3) are installed in machine box (2) one end rotation.

2. The dust-proof unmanned aerial vehicle carries satellite communication terminal controller of claim 1, characterized in that: ventilation chamber (17) have all been seted up to the inside both sides of machine box (2), air inlet (4) and gas vent (5) have been seted up respectively to machine box (2) both ends surface, air inlet (4) and gas vent (5) all communicate each other with ventilation chamber (17) inside.

3. The dust-proof unmanned aerial vehicle carries satellite communication terminal controller of claim 1, characterized in that: heat-dissipating fin (16) are installed to the inside both sides eye-splice of machine box (2), heat-dissipating fin (16) one end is located ventilation chamber (17), heat-conducting plate (15) are installed to heat-dissipating fin (16) other end bolt, heat-conducting plate (15) support respectively and lean on in satellite communication module (9) and information delivery control module (10) one side.

4. The dust-proof unmanned aerial vehicle carries satellite communication terminal controller of claim 1, characterized in that: tin sheet division board (11) are installed to the bolt between satellite communication module (9) and information transmission control module (10), drier storage box (13) are installed to the inside bottom bolt of machine box (2).

5. The dust-proof unmanned aerial vehicle carries satellite communication terminal controller of claim 1, characterized in that: a heat insulation interlayer (14) is embedded in the machine box (2), and a liquid guide groove (6) is formed in the surface of the machine box (2).

6. The dust-proof unmanned aerial vehicle carries satellite communication terminal controller of claim 1, characterized in that: the heat insulation plate (18) is embedded in the mounting plate (1), and the wiring hole (19) is formed in the surface of the mounting plate (1).

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