A multi-application scenario high-throughput satellite antenna data terminal

Abstract

The present invention provides a high-throughput satellite antenna data terminal for multiple application scenarios, including a first main body, a second main body, and a camera. A satellite antenna is provided inside the first main body. The second main body includes a fixed shell, a circuit board, a storage battery, a floating assembly, an air pump, and two power devices. The satellite antenna, the camera, the storage battery, the air pump, and the two power devices are respectively electrically connected to the circuit board. A wireless transmission module for connecting external devices is provided on the circuit board. The two power devices can be unfolded outward to be flush with the horizontal plane, and the air pump can pump gas into the floating assembly so that the floating assembly can be extended to adapt to the water surface environment. The present invention has the function of amphibious travel and can adapt to various terrain environments; an air pump is used to extend the floating assembly to increase the contact area with the water surface; a telescopic arm is used to meet the smooth driving requirements for different terrains; the solar panel is embedded in the upper cover plate to achieve both shading and power generation, which is beneficial to improving the collection of electric energy.

Description

Technical Field

[0001] The present invention relates to the technical field of satellite antennas, and particularly to a high-throughput satellite antenna data terminal for multiple application scenarios. Background Art

[0002] A satellite antenna is a metal parabolic surface that is responsible for reflecting satellite signals into the feeder and low-noise block converter located at the focal point. The function of a satellite antenna is to collect weak signals transmitted by satellites and remove noise as much as possible. Most antennas are usually parabolic in shape, and some multi-focus antennas are composed of a spherical surface and a parabolic surface. The satellite signal is concentrated at its focal point after being reflected by the parabolic antenna.

[0003] Iridium satellite communication, as a widespread communication method with global coverage, compared with other communication methods, is not restricted by unstable factors such as weather, altitude, ionosphere, and distance. It can ensure the signal strength of data communication anywhere and has a very wide range of applicable occasions. It is particularly suitable for application in remote and underdeveloped areas such as the ocean, mountains, deserts, isolated islands, glaciers, and polar regions, and becomes an auxiliary communication function for oil exploration, industrial control, geological survey, engineering survey, scientific expedition, marine environmental monitoring, disaster monitoring and forecasting, maritime emergency rescue, ship safety alarm system, disaster relief, emergency handling, emergency rescue command, etc.

[0004] An unmanned ship is a fully automatic surface robot that can sail on the water according to a preset task without remote control, relying on precise satellite positioning and its own sensors. The uses of domestic unmanned ships are mostly for surveying, hydrology, and water quality monitoring. An amphibious unmanned ship is also one of them. Because an amphibious ship has excellent performance in traveling smoothly on water and land, it can cross mountains and rivers, and traverse rivers, lakes, and seas without restriction. Therefore, it can play a huge role in various professional fields such as military, transportation, disaster relief, and exploration.

[0005] For workers engaged in geological survey, engineering survey, scientific expedition, and marine environmental monitoring, accessing the Internet in the wild is extremely difficult. The survey data and photos they collect can only be stored on the devices they carry (mobile phones, cameras, laptops, or external hard drives). After collecting a certain amount of survey data and photos, they can only return to the nearest rest station for storage transfer. This wastes a lot of time and energy for round trips, with low efficiency and being time-consuming and laborious.

[0006] Therefore, it is necessary to propose a high-throughput satellite antenna data terminal for multiple application scenarios to solve the above problems. Summary of the Invention

[0007] To solve the above problems, the present invention proposes a multi-application scenario high-throughput satellite antenna data terminal to solve the above problems.

[0008] The present invention is realized through the following technical solutions:

[0009] The present invention proposes a multi-application scenario high-throughput satellite antenna data terminal, including a first main body, a second main body, and a camera. The first main body and the camera are both fixedly connected above the second main body. The camera is located on one side of the first main body. A satellite antenna is provided inside the first main body. The second main body includes a fixed shell, a circuit board, a battery, a floating component, an air pump, and two power devices for providing traveling power. A first placement cavity is provided inside the fixed shell. The circuit board, the battery, and the air pump are all fixedly accommodated in the placement cavity. The floating component is fixedly connected to the bottom of the fixed shell and is connected and communicated with the air pump. The two power devices are respectively fixedly connected to both sides of the fixed shell. The satellite antenna, the camera, the battery, the air pump, and the two power devices are all electrically connected to the circuit board respectively. A wireless transmission module for connecting external devices is provided on the circuit board. The two power devices can be unfolded outward to be flush with the horizontal plane, and the air pump can pump gas into the floating component so that the floating component can be stretched out to adapt to the water surface environment.

[0010] Further, the floating component includes a first floating block, two sliding blocks, and two second floating blocks. The first floating block is fixedly connected to the bottom of the fixed shell. A sliding cavity is provided inside the first floating block. The two sliding blocks are symmetrically arranged and slidably accommodated in the sliding cavity. An air duct is provided on the first floating block. The air duct is communicated with the sliding cavity and is located between the two sliding blocks. The air duct penetrates the surface of the fixed shell and extends into the first placement cavity and is connected and communicated with the air pump. The two second floating blocks are respectively fixed on the outer sides of the two sliding blocks and are symmetrically arranged.

[0011] Further, a plurality of first guide plates arranged in sequence are provided on the first floating block, and all the first guide plates face downward.

[0012] Furthermore, the power device includes two telescopic arms, two rotating wheel groups, two first driving devices, two fixings, a waterproof pipe, and a third floating block. The two telescopic arms, the two rotating wheel groups, and the two first driving devices are all electrically connected to the circuit board. The two fixings are symmetrically arranged and respectively fixedly connected to the fixed shell. The two first driving devices are respectively fixedly connected to the two fixings and are symmetrically arranged. One end of the two telescopic arms is respectively fixedly connected to the rotating shafts of the two first driving devices, and the other ends of the two telescopic arms are respectively fixedly connected to the two rotating wheel groups. Both ends of the third floating block are respectively fixedly connected to the two telescopic arms. The waterproof pipes are respectively sleeved on the two first driving devices and fixedly connected to the fixed shell and are communicated with the first placement cavity.

[0013] Furthermore, a plurality of second guide plates are provided on the third floating block, and the plurality of second guide plates are arranged in sequence.

[0014] Furthermore, the telescopic arm includes a first telescopic rod, a second driving device, and a second telescopic rod. The first telescopic rod is provided with a sliding groove, the second driving device is fixedly received in the sliding groove, the second telescopic rod is partially received in the sliding groove and is slidably connected to the first telescopic rod and is threadedly connected to the rotating shaft of the first driving device, and one end of the second telescopic rod is fixedly connected to the rotating wheel group.

[0015] Furthermore, the rotating wheel group includes a fixed block, a third driving device, an amphibious wheel, a seal, and a waterproof shell. The third driving device is electrically connected to the circuit board. The fixed block is provided with a placement groove. The third driving device is partially accommodated in the placement groove and passes through the fixed block. The rotating shaft of the third driving device is fixedly connected to the amphibious wheel. The seal is mounted on the fixed block and abuts against the telescopic arm. The waterproof shell is fixedly connected to the fixed block and covers the third driving device.

[0016] Furthermore, the amphibious wheel includes a rotating wheel and an impeller, the rotating wheel is provided with a first mounting groove, the impeller is partially accommodated in the first mounting groove, and the impeller is provided with a plurality of toggle plates with an inclined angle and uniformly distributed circumferentially.

[0017] Furthermore, the air pump is provided with an air valve and a ventilation pipe, the air valve is electrically connected to the circuit board, the air valve is connected and conducted to the ventilation pipe, and the air valve is connected and conducted to the air outlet of the air pump.

[0018] Further, the first main body includes a protective shell, two fourth driving devices, two upper covers, two solar panels, and two shielding components. A second placement cavity and two fixed positions are provided in the protective shell. The two fixed positions are respectively accommodated in the second placement cavity and are symmetrically arranged. The satellite antenna is fixedly accommodated in the second placement cavity. The two fourth driving devices are respectively fixedly connected to the two fixed positions. The rotating shafts of the two fourth driving devices are respectively provided with rotating rods. The two upper covers are respectively fixedly connected to the two rotating rods and are symmetrically arranged. The two upper covers are respectively provided with second mounting grooves. The two solar panels are respectively accommodated in the two second mounting grooves. The two shielding components are respectively rotatably connected to both sides of the protective shell and partially shield the upper covers. The shielding components include a shielding plate, an elastic member and a limiting member. A locking position and a connecting position are provided on the protective shell. The shielding plate is rotatably connected to the connecting position. One end of the elastic member is fixedly connected to the shielding plate, and the other end of the elastic member is fixedly connected to the limiting member. A clamping groove is provided on the locking position, and the limiting member is fixedly accommodated in the clamping groove.

[0019] Beneficial effects of the present invention:

[0020] 1. The present invention has the function of amphibious travel; when traveling on land, the two power devices are arranged vertically, and the ends of the power devices are rotating wheels that are in contact with the ground, and the rotating wheels provide the present invention with driving power. When traveling on the water surface, the two power devices can be unfolded outward to be flush with the horizontal plane, and the air pump can pump gas into the floating assembly so that the floating assembly can be stretched to adapt to the water surface environment. At this time, the rotating wheels provide the present invention with driving power on water. The present invention is adaptable to various terrain environments and helps field exploration workers to perform data transmission work;

[0021] 2. An air pump is used to extend the floating component to increase the contact area with the water surface; when entering the water, the two power devices can be expanded outward to be flush with the horizontal plane, and at this time the circuit board sends a start command to the air pump, the air pump is turned on, the floating component is inflated, and the two sliding blocks respectively drive the two second floating blocks to extend outward. At this time, the buoyancy of the bottom of the present invention becomes balanced, so that the present invention is not easy to capsize after entering the water, which is conducive to the present invention moving on the water surface;

[0022] 3. The telescopic arm is used to meet the needs of stable driving on different terrains; when driving on mountain roads or uneven roads, each telescopic arm can automatically adjust the height according to the degree of concavity or convexity of the road surface to ensure the stable driving of the present invention and prevent overturning due to excessive bumps during driving;

[0023] 4. The solar panels are embedded in the upper cover plate to achieve both shielding and power generation; when the present invention is in motion, the two upper cover plates are closed to shield the satellite antenna and prevent foreign objects from falling in. At the same time, the solar panels can also generate electricity, which is beneficial to improving the collection of electric energy and is environmentally friendly and green;

[0024] In summary, the present invention has the function of amphibious travel, can adapt to various terrain environments, and helps field exploration workers with data transmission work; an air pump is used to extend the floating component to increase the contact area with the water surface, which is beneficial for the present invention to travel on the water surface; a telescopic arm is used to meet the demand for stable travel on different terrains, ensuring the stable travel of the present invention and preventing it from tipping over due to excessive jolting during travel; the solar panels are embedded in the upper cover plate to achieve both shielding and power generation, which is beneficial to improving the collection of electric energy and is environmentally friendly and green. BRIEF DESCRIPTION OF THE DRAWINGS

[0025] Figure 1 is an exploded view of the multi-application scenario high-throughput satellite antenna data terminal of the present invention;

[0026] Figure 2 is a cross-sectional view of the multi-application scenario high-throughput satellite antenna data terminal of the present invention;

[0027] Figure 3 is a schematic diagram of the multi-application scenario high-throughput satellite antenna data terminal of the present invention when used on land;

[0028] Figure 4 is another cross-sectional view of the multi-application scenario high-throughput satellite antenna data terminal of the present invention;

[0029] Figure 5 is a schematic diagram of the multi-application scenario high-throughput satellite antenna data terminal of the present invention when used on the water surface;

[0030] Figure 6 is a schematic diagram of the multi-application scenario high-throughput satellite antenna data terminal of the present invention when the floating component is extended;

[0031] Figure 7 is an overall schematic diagram of the multi-application scenario high-throughput satellite antenna data terminal of the present invention;

[0032] Figure 8 is Figure 1 a partially enlarged schematic diagram of label A;

[0033] Figure 9 is Figure 1 a partially enlarged schematic diagram of label B;

[0034] Figure 10 is Figure 2 a partially enlarged schematic diagram of label C. Detailed implementation mode

[0035] In order to more clearly and completely illustrate the technical solution of the present invention, the present invention will be further described below with reference to the accompanying drawings.

[0036] Please refer to Figures 1-10 , the present invention provides a high-throughput satellite antenna data terminal for multiple application scenarios, including a first main body 1, a second main body 2, and a camera 3. The first main body 1 and the camera 3 are both fixedly connected above the second main body 2, and the camera 3 is located on one side of the first main body 1. A satellite antenna 11 is provided inside the first main body 1. The second main body 2 includes a fixed shell 21, a circuit board 22, a storage battery 23, a floating assembly 24, an air pump 25, and two power devices 26 for providing traveling power. A first placement cavity 211 is provided inside the fixed shell 21. The circuit board 22, the storage battery 23, and the air pump 25 are all fixedly received in the placement cavity 211. The floating assembly 24 is fixedly connected to the bottom of the fixed shell 21 and is connected and communicated with the air pump 25. The two power devices 26 are respectively fixedly connected to both sides of the fixed shell 21. The satellite antenna 11, the camera 3, the storage battery 23, the air pump 25, and the two power devices 26 are all electrically connected to the circuit board 22. A wireless transmission module for connecting external devices is provided on the circuit board 22. The two power devices 26 can be unfolded outward to be flush with the horizontal plane, and the air pump 25 can pump gas into the floating assembly 24 so that the floating assembly 24 can be stretched to adapt to the water surface environment.

[0037] In this embodiment:

[0038] The first main body 1 is used for signal transmission and converting solar energy into electric energy to charge the storage battery 23;

[0039] The satellite antenna 11 is used for receiving satellite signals and transmitting them back to the circuit board 22;

[0040] The second main body 2 is used to provide a stable support structure for the camera 3 and the first main body 1, and is also the core area of the present invention;

[0041] The fixed shell 21 is used to provide a placement and fixation structure for the circuit board 22, the storage battery 23, the floating assembly 24, the air pump 25, and the two power devices 26. The frame of the fixed shell 21 is made of aviation aluminum, and its peripheral panel is made of polyethylene material;

[0042] The circuit board 22 is the main control board of the present invention, which is provided with a wireless transmission module, a data processing module, a driving module, an imaging module, a gyroscope, and a charging module. The data processing module is electrically connected to the wireless transmission module, the driving module, the imaging module, the charging module, and the gyroscope respectively. The data processing module is used to process the data information transmitted back by the imaging module and the gyroscope. The driving module is electrically connected to the first driving device 263, the second driving device 2612, the third driving device 2622, the fourth driving device 13, and the air pump 25 respectively. The imaging module is electrically connected to the camera 3. The charging module is electrically connected to the solar panel and the interface of the external wiring. The gyroscope monitors the balance of the present invention at all times. The wireless transmission module is used for wireless connection with the user's device, and a decoder is provided in the wireless transmission module;

[0043] The storage battery 23 is a lithium battery, which is used to provide power for the circuit board and each electrical device;

[0044] The floating component 24 is used to provide buoyancy for the present invention;

[0045] The air pump 25 is used to supply air to the floating component 24 so that the floating component 24 can be stretched out. The air pump 25 can also pump out air. When the air inside the floating component 24 is pumped out, it will shrink and recover;

[0046] The power device 26 is used to provide driving force for the present invention;

[0047] The camera 3 is used to obtain images of the external environment and transmit the image information back to the imaging module. The imaging module then converts the image into data information and transmits it back to the data processing module. The data processing module then calculates the external environment according to the information and combines the image recognition algorithm, and then issues corresponding driving instructions to the driving module;

[0048] Specifically, when driving on land, the two power devices 26 are vertically arranged, and the ends of the power devices 26 are the rotating wheel sets 262 and are in contact with the ground. The rotating wheel sets 262 provide driving force for the present invention to travel. When driving into the water surface, the two power devices 26 can be unfolded outward to be flush with the horizontal plane, and the air pump 25 can pump gas into the floating component 24 so that the floating component 24 can be stretched out to adapt to the water surface environment. At this time, the rotating wheel sets 262 provide driving force for the present invention to travel on the water. The present invention adapts to various terrain environments and helps to assist field exploration workers in data transmission work;

[0049] When entering the water, the two power devices 26 can be unfolded outward to be flush with the horizontal plane. At this time, the circuit board 22 issues a start command to the air pump 25, and the air pump 25 is turned on. The floating component 24 is inflated, and the two sliding blocks 242 drive the two second floating blocks 243 to extend outward respectively. At this time, the buoyancy received by the bottom of the present invention becomes balanced, making the present invention not prone to roll over after entering the water, which is beneficial to the present invention to travel on the water surface.

[0050] Furthermore, the floating component 24 includes a first floating block 241, two sliding blocks 242, and two second floating blocks 243. The first floating block 241 is fixedly connected to the bottom of the fixed shell 21. A sliding cavity 2411 is provided inside the first floating block 241. The two sliding blocks 242 are symmetrically arranged and slidably received in the sliding cavity 2411. An air duct 2412 is provided on the first floating block 241. The air duct 2412 is in communication with the sliding cavity 2411 and is located between the two sliding blocks 242. The air duct 2412 penetrates the surface of the fixed shell 21 and extends into the first placement cavity 211 and is connected and communicated with the air pump 25. The two second floating blocks 243 are respectively fixed to the outside of the two sliding blocks 242 and are symmetrically arranged; A plurality of first guide plates 2413 arranged in sequence are provided on the first floating block 243, and all the plurality of first guide plates 2413 face downward.

[0051] In this embodiment:

[0052] The first floating block 241 is used to provide buoyancy for the present invention;

[0053] The sliding cavity 2411 is used to provide a sliding space for the two sliding blocks 242;

[0054] The air duct 2412 is used to provide a channel for introducing the gas pumped out by the air pump 25 into the sliding cavity 2411;

[0055] The first guide plate 2413 is used to provide a guiding structure for the part of the first floating block 241 that sinks into the water, preventing the present invention from rotating randomly in the water;

[0056] There are 2 sliding blocks 242 in total, which are used to assist the first floating block 241 to contact the water surface, thereby increasing the force-bearing area of the buoyancy, so that the present invention travels smoothly on the water surface;

[0057] The second floating block 243 is used to increase the buoyancy of the sliding block 242;

[0058] Specifically, after the air pump 25 fills the gas into the air duct 2412, the gas is introduced into the sliding cavity 2411. The two sliding blocks 242 are located on both sides of the air outlet of the air duct 2412. After the gas flows out, it pushes the two sliding blocks 242 outward to slide and expand. When the invention lands on land, the air pump 25 drives in the reverse direction to extract the gas from the sliding cavity 2411. At this time, the two sliding blocks 242 are pushed by the atmospheric pressure to contract and return to their original positions. A part of the air duct 2412 extends into the sliding cavity 2411, so as to distinguish the central positions of the two sliding blocks 242. When the sliding blocks 242 slide and contract to return to their original positions, they will not slide excessively.

[0059] Furthermore, the power device 26 includes two telescopic arms 261, two rotating wheel groups 262, two first driving devices 263, two fixing members 264, a waterproof pipe 265, and a third floating block 266. The two telescopic arms 261, the two rotating wheel groups 262, and the two first driving devices 263 are all electrically connected to the circuit board 22. The two fixing members 264 are symmetrically arranged and respectively fixedly connected to the fixed shell 21. The two first driving devices 263 are respectively fixedly connected to the two fixing members 264 and are symmetrically arranged. One end of the two telescopic arms 261 is respectively fixedly connected to the rotating wheels of the two first driving devices 263. The second guide plates 2661 are arranged in sequence; the telescopic arm 261 includes a first telescopic rod 2611, a second driving device 2612, and a second telescopic rod 2613; the first telescopic rod 2611 is provided with a sliding groove, and the second driving device 2612 is provided with a second guide plate 2661; the ... The second driving device 2612 is fixedly received in the sliding groove, the second telescopic rod 2613 is partially received in the sliding groove and is slidably connected to the first telescopic rod 2611 and is threadedly connected to the rotating shaft of the first driving device 263, one end of the second telescopic rod 2613 is fixedly connected to the rotating wheel group 262; the rotating wheel group 262 includes a fixed block 2621, a third driving device 2622, an amphibious wheel 2623, a sealing member 2624, and a waterproof shell 2625, the third driving device 2622 is electrically connected to the circuit board 22, the fixed block 2621 is provided with a placement groove 26211, and the third driving device 2622 is partially received in the sliding groove. The third driving device 2622 is placed in the groove 26211 and passes through the fixed block 2621. The rotating shaft of the third driving device 2622 is fixedly connected to the amphibious wheel 2623. The sealing member 2624 is sleeved on the fixed block 2621 and abuts against the telescopic arm 261. The waterproof shell 2625 is fixedly connected to the fixed block 2621 and shields the third driving device 2622. The amphibious wheel 2623 includes a rotating wheel 26231 and an impeller 26232. The rotating wheel 26231 is provided with a first mounting groove. The impeller 26232 is partially accommodated in the first mounting groove. The impeller 26232 is provided with a plurality of toggle plates 102 with an inclined angle and uniformly distributed circumferentially.

[0060] In this embodiment:

[0061] The telescopic arm 261 is used to provide a structure for the present invention that can freely adjust the height, and can also cooperate with the gyroscope on the circuit board 22 to enhance the balance performance of the present invention;

[0062] The first telescopic rod 2611 is used to provide a fixed structure for the second driving device 2612;

[0063] The sliding groove is used to provide a sliding space for the second telescopic rod 2613;

[0064] The second driving device 2612 is a stepping motor, which is used to drive the second telescopic rod 2613 to extend and retract back and forth;

[0065] The second telescopic rod 2613 is used to drive the rotating wheel group 262 to telescopic movement;

[0066] The rotating wheel set 262 is used to provide the present invention with driving force;

[0067] The fixing block 2621 is used to provide a stable fixing structure for the third driving device 2622;

[0068] The placement groove 26211 is used to provide a space for placing the third driving device 2622;

[0069] The third driving device 2622 is a DC reduction motor, which is used to drive the amphibious wheel 2623 to rotate;

[0070] The amphibious wheel 2623 is used to rotate and drive the present invention to move forward;

[0071] The rotating wheel 26231 is a rubber wheel, which is used to rotate and drive the present invention to move on land;

[0072] The first mounting groove is used to provide a fixed placement space for the impeller 26232;

[0073] The impeller 26232 is made of polyethylene material and is used to assist the rotating wheel 26231 to wave the water surface and drive the present invention to move on the water surface;

[0074] The shifting plate 102 is used to provide a structure for the impeller 26232 to shift the water surface;

[0075] The sealing member 2624 is made of a soft material (silicone, soft glue, soft rubber), and is used to seal the gap between the second telescopic rod 2613 and the first telescopic rod 2611;

[0076] The waterproof housing 2625 is used to provide a waterproof structure for the third driving device 2622;

[0077] The first driving device 263 is a large torque DC reduction motor, there are two of them, used to drive the telescopic arm 261 to rotate;

[0078] The fixing member 264 is used to provide a connection structure for the first driving device 263 to be fixed on the fixing housing 21;

[0079] The waterproof pipe 265 is used to provide a waterproof structure for the connection line between the first driving device 263 and the circuit board 22;

[0080] The third floating block 266 is used to increase the buoyancy of the present invention. When the telescopic arm 261 rotates to be parallel to the horizontal plane, the third floating block 266 is also parallel to the horizontal plane, which increases the contact area between the present invention and the water surface, thereby enhancing the balance of the present invention when traveling on water.

[0081] The second guide plate 2661 is used to provide a guiding structure for the third floating block 266 to prevent the present invention from spinning on the water surface.

[0082] Specifically, when traveling on a mountain road or an uneven road surface, each telescopic arm 261 can automatically adjust its height according to the degree of depression or convexity of the road surface to ensure the smooth travel of the present invention and prevent it from tipping over due to excessive jolting during travel.

[0083] When the present invention travels on land, the gyroscope on the circuit board 22 can continuously monitor the balance situation during its travel. If the tilt angle in one direction is greater than the preset value, the data processing module acquires this angle and calculates the lifting height required for the return angle, and sends the corresponding driving instruction to the driving module. The driving module then sends an operation instruction to the corresponding second driving device 2612 (or multiple second driving devices 2612 can also run separately), and the second driving device 2612 will drive the second telescopic rod 2613 to slide up or down to maintain the balance of the present invention.

[0084] When the present invention travels on water, the telescopic arm 261 contracts to the shortest size. At this time, the seal 2624 blocks the gap between the second telescopic rod 2613 and the first telescopic rod 2611, and the telescopic arm 261 will not let water in. Then the circuit board 22 issues an operation instruction to the driving module, and the driving module issues a driving instruction to the third driving device 2622. The third driving device 2622 rotates to drive the amphibious wheel 2623 to rotate. At this time, the impeller 26232 rotates to stir the water surface to provide driving force for the present invention to move forward.

[0085] Furthermore, the air pump 25 is provided with an air valve 251 and an air vent pipe 252. The air valve 251 is electrically connected to the circuit board 22, the air valve 251 is connected and conducted with the air vent pipe 252, and the air valve 251 is connected and conducted with the air outlet of the air pump 25.

[0086] In this embodiment:

[0087] The air valve 251 is an electromagnetic valve, which is used to block the inflow of air and also seal the gas in the sliding cavity 2411.

[0088] The air vent pipe 252 is used to provide a channel for the gas pumped by the air pump 25 to flow into the air guide pipe 2412.

[0089] Further, the first body 1 includes a protective case 12, two fourth driving devices 13, two upper cover plates 14, two solar panels 15, and two shielding components 16. A second placement cavity 121 and two fixing positions 122 are provided inside the protective case 12. The two fixing positions 122 are respectively received in the second placement cavity 121 and are symmetrically arranged. The satellite antenna 11 is fixedly received in the second placement cavity 121. The two fourth driving devices 13 are respectively fixedly connected to the two fixing positions 122. Rotating rods 131 are provided on the rotating shafts of the two fourth driving devices 13. The two upper cover plates 14 are respectively fixedly connected to the two rotating rods 131 and are symmetrically arranged. Second mounting grooves 141 are provided on the two upper cover plates 14. The two solar panels 15 are respectively received in the two second mounting grooves 141. The two shielding components 16 are respectively rotatably connected to both sides of the protective case 12 and partially shield the upper cover plates 14. The shielding component 16 includes a shielding plate 161, an elastic member 162, and a limiting member 163. A locking position 123 and a connecting position 124 are provided on the protective case 12. The shielding plate 161 is rotatably connected to the connecting position 124. One end of the elastic member 162 is fixedly connected to the shielding plate 161, and the other end of the elastic member 162 is fixedly connected to the limiting member 163. A clamping groove 1231 is provided on the locking position 123. The limiting member 163 is fixedly received in the clamping groove 1231.

[0090] In this embodiment:

[0091] The protective case 12 is used to provide a placement space for the fourth driving device 13 and the satellite antenna 11;

[0092] The second placement cavity 121 is used to provide a placement space for the satellite antenna 11 and the fourth driving device 13;

[0093] The fixing position 122 is used to provide a supporting structure for the fourth driving device 13. A bearing is provided on the fixing position 122. The end of the rotating rod 131 away from the fourth driving device 13 is fixedly connected to the inner ring of the bearing;

[0094] The locking position 123 is used to lock the limiting member 163;

[0095] The clamping groove 1231 is used to provide a placement space for the limiting member 163;

[0096] The connecting position 124 is used to provide a structure for the protective case 12 to be rotatably connected to the shielding plate 161;

[0097] The fourth driving device 13 is a stepping motor, which is used to drive the upper cover plate 14 to rotate and open or close;

[0098] The rotating rod 131 is used to provide a clamping structure for the upper cover plate 14;

[0099] The upper cover plate 14 is used to provide a stable mounting structure for the solar panel 15 and also to provide a shielding structure for the satellite antenna;

[0100] The second mounting groove 141 is used to provide a space for placing the solar cell panel 15;

[0101] The solar panel 15 is used to convert sunlight into electrical energy and transmit it to the circuit board 22, which then charges the storage battery 23;

[0102] The shielding component 16 is used to shield the position on the protective shell 12 reserved for the upper cover plate 14 to rotate;

[0103] The shielding plate 161 is used to shield the upper cover plate 14;

[0104] The elastic member 162 is a spring, which is used to provide a resilience for the reset of the shielding plate 161. Clamping columns are provided at both ends of the elastic member 162. The shielding plate 161 is provided with a first clamping groove, and the limiting member 163 is provided with a second clamping groove. The clamping column at one end of the elastic member 162 is received in the first clamping groove, and the clamping column at the other end of the elastic member 162 is received in the second clamping groove.

[0105] The limiting member 163 is used to limit the torsion degree of the elastic member 162 away from the end of the shielding plate 161, so that the shielding plate 161 can be rotated and reset;

[0106] Specifically, when the present invention is in motion, the two upper covers 14 are closed to shield the satellite antenna 11 to prevent foreign objects from falling in. At the same time, the solar panel 15 can also generate electricity, which is beneficial to improve the collection of electric energy and is green and environmentally friendly.

[0107] When receiving satellite signals, the two fourth driving devices 13 rotate respectively to drive the upper cover plate 14 to open, and at this time the satellite antenna 11 can receive satellite signals.

[0108] In summary, the present invention has the function of amphibious travel, adapts to various terrain environments, and helps field exploration workers to perform data transmission work; an air pump is used to extend the floating component to increase the contact area with the water surface, which is beneficial for the present invention to travel on the water surface; a telescopic arm is used to adapt to the smooth driving requirements of different terrains, to ensure the smooth driving of the present invention, and to prevent overturning due to excessive bumps during driving; the solar cell panel is embedded in the upper cover plate to provide both shielding and power generation, which is beneficial to improving the collection of electrical energy and is green and environmentally friendly.

[0109] Of course, the present invention may have many other implementations. Based on this implementation, other implementations obtained by ordinary technicians in this field without any creative work are all within the scope of protection of the present invention.

Claims

1. A multi-application scenario high-throughput satellite antenna data terminal, characterized in that, It includes a first main body, a second main body, and a camera. The first main body and the camera are both fixedly connected above the second main body. The camera is located on one side of the first main body. A satellite antenna is provided inside the first main body. The second main body includes a fixed housing, a circuit board, a storage battery, a floating assembly, an air pump, and two power devices for providing traveling power. A first placement cavity is provided inside the fixed housing. The circuit board, the storage battery, and the air pump are all fixedly received in the placement cavity. The floating assembly is fixedly connected to the bottom of the fixed housing and is connected and communicated with the air pump. The two power devices are respectively fixedly connected to both sides of the fixed housing. The satellite antenna, the camera, the storage battery, the air pump, and the two power devices are all electrically connected to the circuit board respectively. A wireless transmission module for connecting external devices is provided on the circuit board. The two power devices can be unfolded outward to be flush with the horizontal plane, and the air pump can pump gas into the floating assembly so that the floating assembly can be stretched out to adapt to the water surface environment; The floating assembly includes a first floating block, two sliding blocks, and two second floating blocks. The first floating block is fixedly connected to the bottom of the fixed housing. A sliding cavity is provided inside the first floating block. The two sliding blocks are symmetrically arranged and slidably received in the sliding cavity. An air duct is provided on the first floating block. The air duct is communicated with the sliding cavity and is located between the two sliding blocks. The air duct penetrates the surface of the fixed housing and extends into the first placement cavity and is connected and communicated with the air pump. The two second floating blocks are respectively fixed to the outer sides of the two sliding blocks and are symmetrically arranged; A plurality of first guide plates arranged in sequence are provided on the first floating block, and all the first guide plates face downward; The power device includes two telescopic arms, two rotating wheel sets, two first driving devices, two fixing members, a waterproof pipe, and a third floating block. The two telescopic arms, the two rotating wheel sets, and the two first driving devices are all electrically connected to the circuit board. The two fixing members are symmetrically arranged and are respectively fixedly connected to the fixed housing. The two first driving devices are respectively fixedly connected to the two fixing members and are symmetrically arranged. One ends of the two telescopic arms are respectively fixedly connected to the rotating shafts of the two first driving devices. The other ends of the two telescopic arms are respectively fixedly connected to the two rotating wheel sets. The two ends of the third floating block are respectively fixedly connected to the two telescopic arms. The waterproof pipe is respectively sleeved on the two first driving devices and is fixedly connected to the fixed housing and is communicated with the first placement cavity.

2. The multi-application scenario high-throughput satellite antenna data terminal according to claim 1, characterized in that, A plurality of second guide plates are provided on the third floating block, and the plurality of second guide plates are arranged in sequence.

3. The multi-application scenario high-throughput satellite antenna data terminal according to claim 1, wherein The telescopic arm includes a first telescopic rod, a second driving device, and a second telescopic rod. A sliding groove is provided inside the first telescopic rod. The second driving device is fixedly accommodated in the sliding groove. The second telescopic rod is partially accommodated in the sliding groove, slidably connected to the first telescopic rod, and threadedly connected to the rotating shaft of the first driving device. One end of the second telescopic rod is fixedly connected to the rotating wheel set.

4. The multi-application scenario high-throughput satellite antenna data terminal according to claim 1, characterized in that, The rotating wheel set includes a fixed block, a third driving device, an amphibious wheel, a sealing member, and a waterproof housing. The third driving device is electrically connected to the circuit board. A placement groove is provided on the fixed block. The third driving device is partially accommodated in the placement groove and penetrates through the fixed block. The rotating shaft of the third driving device is fixedly connected to the amphibious wheel. The sealing member is sleeved on the fixed block and abuts against the telescopic arm. The waterproof housing is fixedly connected to the fixed block and shields the third driving device.

5. The multi-application scenario high-throughput satellite antenna data terminal according to claim 4, wherein The amphibious wheel includes a rotating wheel and an impeller. A first installation groove is provided on the rotating wheel. The impeller is partially accommodated in the first installation groove. The impeller is provided with a plurality of deflecting plates having an inclined angle and circumferentially evenly distributed.

6. The multi-application scenario high-throughput satellite antenna data terminal according to claim 1, characterized in that, The air pump is provided with an air valve and a ventilation pipe. The air valve is electrically connected to the circuit board. The air valve is connected and communicated with the ventilation pipe, and the air valve is connected and communicated with the air outlet of the air pump.

7. The multi-application scenario high-throughput satellite antenna data terminal according to claim 1, wherein The first main body includes a protective shell, two fourth driving devices, two upper covers, two solar panels, and two shielding components. A second placement cavity and two fixing positions are provided inside the protective shell. The two fixing positions are respectively accommodated in the second placement cavity and are symmetrically arranged. The satellite antenna is fixedly accommodated in the second placement cavity. The two fourth driving devices are respectively fixedly connected to the two fixing positions. Rotating rods are provided on the rotating shafts of the two fourth driving devices. The two upper covers are respectively fixedly connected to the two rotating rods and are symmetrically arranged. Second installation grooves are provided on the two upper covers. The two solar panels are respectively accommodated in the two second installation grooves. The two shielding components are respectively rotatably connected to both sides of the protective shell and partially shield the upper covers. The shielding component includes a shielding plate, an elastic member, and a limiting member. Locking positions and connecting positions are provided on the protective shell. The shielding plate is rotatably connected to the connecting position. One end of the elastic member is fixedly connected to the shielding plate, and the other end of the elastic member is fixedly connected to the limiting member. A clamping groove is provided on the locking position, and the limiting member is fixedly accommodated in the clamping groove.

Images