CN117944922A - Unmanned aerial vehicle launches carrier loader - Google Patents
Unmanned aerial vehicle launches carrier loader Download PDFInfo
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- CN117944922A CN117944922A CN202410353422.0A CN202410353422A CN117944922A CN 117944922 A CN117944922 A CN 117944922A CN 202410353422 A CN202410353422 A CN 202410353422A CN 117944922 A CN117944922 A CN 117944922A
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- 229910052751 metal Inorganic materials 0.000 claims description 11
- 239000002184 metal Substances 0.000 claims description 11
- 210000001503 joint Anatomy 0.000 claims description 9
- 230000000149 penetrating effect Effects 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 5
- 229920005830 Polyurethane Foam Polymers 0.000 claims description 3
- 229910052782 aluminium Inorganic materials 0.000 claims description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 3
- 230000003028 elevating effect Effects 0.000 claims description 3
- 239000011496 polyurethane foam Substances 0.000 claims description 3
- 239000000126 substance Substances 0.000 claims description 2
- 238000013461 design Methods 0.000 abstract description 3
- 108010066114 cabin-2 Proteins 0.000 description 12
- 241000196324 Embryophyta Species 0.000 description 3
- 238000000034 method Methods 0.000 description 3
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- 230000007613 environmental effect Effects 0.000 description 2
- 238000012946 outsourcing Methods 0.000 description 2
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
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- 238000009413 insulation Methods 0.000 description 1
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- 235000009566 rice Nutrition 0.000 description 1
- 238000012546 transfer Methods 0.000 description 1
- 238000010792 warming Methods 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The invention relates to the technical field of unmanned aerial vehicle launching and carrying vehicles, in particular to an unmanned aerial vehicle launching and carrying vehicle. The problem of current unmanned aerial vehicle launches shelter volume on the carrier automobile body great, need use large-scale lifting device when shifting or changing, very inconvenient is solved. The utility model provides an unmanned aerial vehicle transmission carrier loader, includes frame and power supply system, the fixed surface of frame has shelter and fixing base, the top movable mounting of fixing base has unmanned aerial vehicle transmitter, unmanned aerial vehicle transmitter's front end is fixed with a plurality of rotatory connecting blocks, rotatory connecting block's both sides run through and rotate the grafting and have the location pivot, the both ends and the fixing base of location pivot are fixed, install lifting mechanism between the bottom surface of rotatory connecting block and the fixing base, install compressed gas holding vessel and gas compressor between shelter and the fixing base. The whole vehicle of the invention has scientific and reasonable overall design and overall layout of equipment and facilities, meets equipment requirements, and is convenient for the efficient implementation of unmanned aerial vehicle storage transportation and emission.
Description
Technical Field
The invention relates to the technical field of unmanned aerial vehicle launching and carrying vehicles, in particular to an unmanned aerial vehicle launching and carrying vehicle.
Background
The unmanned aerial vehicle is an unmanned aerial vehicle operated by using a radio remote control device and a self-provided program control device, or is operated by a vehicle-mounted computer completely or intermittently and autonomously, the unmanned aerial vehicle can be divided into independent unmanned aerial vehicles and clustered unmanned aerial vehicles according to different using modes, the clustered unmanned aerial vehicles are connected with each other through a signal network, the operation can be carried out together, the flying position can be replaced in real time, and dynamic graphic display can be carried out in the air by using the clustered unmanned aerial vehicles;
the cluster unmanned aerial vehicle comprises a plurality of unmanned aerial vehicles of specification size unanimity, because the quantity of cluster unmanned aerial vehicle is more so can not adopt single device to store and launch, need use centralized unmanned aerial vehicle to launch storage device to store or launch unmanned aerial vehicle.
However, the shelter volume on the existing unmanned aerial vehicle launching carrier body is large, and large-scale lifting equipment is required to be used during transfer or replacement, so that inconvenience is caused; therefore, the existing requirements are not met, and for this reason, an unmanned aerial vehicle launching carrier vehicle is provided.
Disclosure of Invention
The invention aims to provide an unmanned aerial vehicle launching carrier vehicle, which solves the problems that the shelter on the existing unmanned aerial vehicle launching carrier vehicle body is large in volume, large lifting equipment is required to be used during transferring or replacing, and the like in the prior art is very inconvenient.
In order to achieve the above purpose, the present invention provides the following technical solutions: the utility model provides an unmanned aerial vehicle launch vehicle, includes frame and power supply system, the fixed surface of frame has shelter lifting module and fixing base, detachable shelter is installed to the top of shelter lifting module, the top movable mounting of fixing base has unmanned aerial vehicle transmitter, unmanned aerial vehicle transmitter's front end is fixed with a plurality of rotatory connecting blocks, rotatory connecting block's both sides run through and rotate the grafting and have the location pivot, the both ends and the fixing base of location pivot are fixed, install elevating system between rotatory connecting block's bottom surface and the fixing base, install compressed gas holding tank and gas compressor between shelter and the fixing base, compressed gas holding tank and gas compressor are fixed on the frame surface and are connected through the gas pipeline between compressed gas holding tank and the gas compressor;
The shelter lifting module comprises a bearing plate, the bearing plate is fixed on the frame, three fixed screw rods are fixed in the bearing plate, a movable plate is slidably installed at one end of the bearing plate, three movable motors are fixed in the movable plate, a driving gear is fixed at the output shaft end of the movable motor, a sleeve gear is connected to one side of the driving gear in a meshed mode, an inner threaded sleeve is fixedly penetrated in the axial direction of the sleeve gear, the end of the fixed screw rod penetrates through the inner threaded sleeve in the axial direction of the inner threaded sleeve and is in threaded transmission with the inner threaded sleeve, a lifting plate is installed at one side of the movable plate, a supporting plate is connected to the end portion, far away from the movable plate, of the lifting plate, two rotatable supporting hydraulic rods are installed at the bottom surface of the supporting plate, two sliding supporting plates are installed below the lifting plate, two base plates are detachably installed on the upper surface of the sliding supporting plate, a plurality of linear arrangement movable anti-slip limiting elastic pieces are installed on the inner sides of the base plates, one end of the limiting elastic pieces is fixed with the base plates, two ends of the limiting elastic pieces are connected with the round base plates in a penetrating mode, and the round base plates are connected with two ends of the round base plates in a penetrating mode, and the round base plates are connected with the round anti-slip limiting rods.
Preferably, the butt joint axostylus axostyle is pegged graft in the lateral wall of lifting plate and the axis rotation of lifting plate around the butt joint axostylus axostyle, two symmetrical distribution's slip spout has all been seted up to the bottom surface of lifting plate and two slip backup pads, two the upper surface of slip backup pad all is fixed with the equipment slider, the inside at the slip spout of equipment slider slip joint, two auxiliary stay hydraulic stems have all been placed to the below of lifting plate and two slip backup pads detachable, the top of auxiliary stay hydraulic stem is pegged graft and is coniform at the slip spout inboard and bottom tip.
Preferably, the shelter includes six cabin boards and a plurality of equipment rivet, and the side of two adjacent cabin boards is laminated each other, and the outside of two adjacent cabin boards is covered and is had the outsourcing limit, and the interior layering is installed to the inboard of two adjacent cabin boards, and it has the PVC board to pack in the space between two adjacent cabin boards, cabin board and outsourcing limit, PVC board are all connected fixedly through the equipment rivet, the cabin board includes interior covering, metal skeleton, outer covering and foam board, the surface mounting of outer covering towards interior covering has metal skeleton, install the foam board between interior covering and the outer covering, and the foam board covers metal skeleton.
Preferably, the inner skin and the outer skin are made of t1.5mm antirust aluminum plates, surface base layers of the inner skin and the outer skin are subjected to chemical treatment, and the foam plates are made of rigid polyurethane foam.
Preferably, the top of shelter installs meteorological monitor and surveillance camera head, movable sealing door plant is installed to the rear side of shelter.
Preferably, the weather monitor is mounted on the left front side of the shelter, and the monitoring camera is mounted on the right rear side of the shelter.
Preferably, the main cabinet and the accessory box are arranged in the shelter, and a power distribution power supply, an uninterrupted power supply, a power taking motor control unit, a storage battery, a video monitoring module, a weather monitoring module and a transmitting control unit are arranged in the main cabinet.
Preferably, the video monitoring module is connected with the monitoring camera, and the weather monitoring module is connected with the weather monitor through a data line.
Preferably, the lifting mechanism is an industrial electric actuator and is provided with an onboard controller.
Preferably, the power supply system consists of a power supply lead-in cable, a power supply interface, an automobile power taking generator, a power distribution control unit, a UPS uninterrupted power supply and an in-automobile power supply cable.
Compared with the prior art, the invention has the beneficial effects that:
1. According to the invention, the internal thread sleeve is driven to rotate after the mobile motor is electrified, the internal thread sleeve drives the mobile plate to slide in the bearing plate, at the moment, the mobile plate drives the lifting plate and the supporting plate to extend out of the bearing plate, after the lifting plate and the supporting plate extend out completely, the two supporting hydraulic rods are rotated and vertical to the ground, the two supporting hydraulic rods are started to enable the movable end parts of the supporting hydraulic rods to contact with the ground and support the supporting plate, the two sliding supporting plates at the bottom of the lifting plate are unfolded in a sliding manner, the angles of the lifting plate and the two sliding supporting plates are adjusted, the end parts of the lowest sliding supporting plate are flush with the ground, the base plate is arranged on the surface of the sliding supporting plate, at the moment, the shelter is transferred to the surface of the lifting plate, the shelter is pushed to slide on the surface of the lifting plate and the surface of the two sliding supporting plates, the shelter is conveniently detached from the frame, the shelter is reversely rotated for half circle, the shelter located on the ground is pushed to the surface of the sliding supporting plate, the shelter is conveniently and rapidly conveyed to the frame, and the difficulty of movement and replacement of the shelter is reduced.
2. According to the invention, the anti-skid limiting elastic piece is arranged on the base plate, the anti-skid limiting elastic piece is shaped like a V, and one end of the anti-skid limiting elastic piece is in sliding connection with the base plate through the connecting round rod, so that when the fixed end part of the anti-skid limiting elastic piece is extruded, the other end of the anti-skid limiting elastic piece can slide, the anti-skid limiting elastic piece is deformed from the V to be straight, the sliding of a cabin on the base plate is not influenced, and when the movable end part of the anti-skid limiting elastic piece is extruded by hands, the other end of the anti-skid limiting elastic piece cannot move, and at the moment, the anti-skid limiting elastic piece can keep the V shape and cannot deform, so that the sliding of the square cabin can be blocked, and the safety of the square cabin in the process of transferring the square cabin from the ground to the surface of the frame is ensured.
3. The invention mainly comprises a frame, a shelter, a lifting mechanism, a weather monitor, a gas compressor, a compressed gas storage tank, a monitoring camera, a power supply system and the like, and has scientific and reasonable overall design of the whole vehicle and overall layout of equipment and facilities, meets equipment requirements, and is convenient for the efficient implementation of storage, transportation and emission of unmanned aerial vehicles.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a left side view of the frame of the present invention;
FIG. 3 is a right side view of the frame of the present invention;
FIG. 4 is a schematic view of the assembled structure of the deck and deck of the present invention;
FIG. 5 is a schematic view of the structure of the deck of the present invention;
FIG. 6 is a schematic view of a shelter lifting module according to the present invention;
FIG. 7 is a schematic diagram of a power supply system of the present invention;
FIG. 8 is a schematic view of the internal structure of the carrier plate according to the present invention;
fig. 9 is an enlarged view of the structure at a in fig. 8;
FIG. 10 is a schematic view of a sliding support plate according to the present invention;
fig. 11 is an enlarged view of the structure at B in fig. 10;
FIG. 12 is a structural cross-sectional view of the sliding support plate of the present invention;
Fig. 13 is an enlarged view of the structure at C in fig. 12;
Fig. 14 is an enlarged view of the structure at D in fig. 12.
In the figure: 1. a frame; 2. a shelter; 21. a deck; 211. an inner skin; 212. a metal skeleton; 213. an outer skin; 214. a foam board; 22. an outer wrapping edge; 23. a PVC plate; 24. assembling rivets; 25. an inner depression bar; 3. an unmanned aerial vehicle transmitter; 4. a fixing seat; 5. rotating the connecting block; 6. positioning a rotating shaft; 7. a weather monitor; 8. monitoring a camera; 9. a compressed gas storage tank; 10. a gas compressor; 11. a lifting mechanism; 12. a movable sealing door plate; 13. a shelter lifting module; 1301. a carrying plate; 1302. a moving plate; 1303. a lifting plate; 1304. a support plate; 1305. supporting a hydraulic rod; 1306. fixing a screw rod; 1307. a sliding support plate; 1308. an internally threaded sleeve; 1309. a sleeve gear; 1310. a drive gear; 1311. a moving motor; 1312. a butt joint shaft lever; 1313. a backing plate; 1314. an anti-slip limit elastic sheet; 1315. connecting round rods; 1316. an auxiliary support hydraulic rod; 1317. sliding chute; 1318. and assembling the sliding block.
Detailed Description
The following description of the embodiments of the present invention will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present invention, but not all embodiments.
As shown in fig. 1 to 3, an unmanned aerial vehicle launch vehicle, the surface mounting of frame 1 has shelter lifting module 13 and fixing base 4, detachable shelter 2 is installed to the top of shelter lifting module 13, the top movable mounting of fixing base 4 has unmanned aerial vehicle transmitter 3, the front end of unmanned aerial vehicle transmitter 3 is fixed with a plurality of rotatory connecting blocks 5, rotatory both sides of connecting block 5 run through the rotation and peg graft have location pivot 6, the both ends and the fixing base 4 of location pivot 6 are fixed, install elevating system 11 between the bottom surface and the fixing base 4 of rotatory connecting block 5, install compressed gas holding tank 9 and gas compressor 10 between shelter 2 and the fixing base 4, compressed gas holding tank 9 and gas compressor 10 are fixed at frame 1 surface and are connected through gas pipeline between compressed gas holding tank 9 and the gas compressor 10.
The shelter 2 comprises six deck boards 21 and a plurality of assembly rivets 24, the side edges of two adjacent deck boards 21 are mutually attached, the outer sides of two adjacent deck boards 21 are covered with outer edges 22, inner layering 25 is arranged on the inner sides of two adjacent deck boards 21, PVC boards 23 are filled in gaps between two adjacent deck boards 21, the deck boards 21 are fixedly connected with the outer edges 22 and the PVC boards 23 through the assembly rivets 24, gaps at the attaching positions of the side edges of two adjacent deck boards 21 are sealed by the outer edges 22 and the PVC boards 23, gaps between the deck boards 21 and the deck boards 21 are filled by the PVC boards 23, and the integral tightness of the shelter 2 after the deck boards 21 are assembled into the shelter 2 is ensured.
The weather monitor 7 and the surveillance camera 8 are installed at the top of shelter 2, and movable sealing door plant 12 is installed to the rear side of shelter 2, and weather monitor 7 is installed in the left front side of shelter 2, and surveillance camera 8 is installed in the right rear side of shelter 2, and the staff can get into shelter 2 inside after opening movable sealing door plant 12 and overhaul the maintenance, and weather monitor 7, surveillance camera 8 can real-time supervision shelter 2 outside weather condition and surrounding environment information.
The main cabinet and the accessory box are arranged in the shelter 2, a power distribution power supply, an uninterrupted power supply, a power taking motor control unit, a storage battery, a video monitoring module, a weather monitoring module and an emission control unit are arranged in the main cabinet, and the video monitoring module is connected with the monitoring camera 8 and the weather monitoring module and the weather monitor 7 through data lines.
The lifting mechanism 11 is an industrial electric actuator and is provided with an onboard controller, the electric actuator has faster response and higher predictability, does not drift when in power failure, is quicker and simpler to install relative to a hydraulic or pneumatic system, requires fewer components than the hydraulic or pneumatic system, occupies small volume, simultaneously has environmental adaptability, and can work and store in complex environments.
As shown in fig. 4 and 5, the cabin board 21 includes an inner skin 211, a metal skeleton 212, an outer skin 213 and a foam board 214, the surface of the outer skin 213 facing the inner skin 211 is fixed with the metal skeleton 212, the foam board 214 is installed between the inner skin 211 and the outer skin 213, the foam board 214 covers the metal skeleton 212, the inner skin 211 and the outer skin 213 are made of t1.2mm rust-proof aluminum plates, the surface base layers of the inner skin 211 and the outer skin 213 are chemically treated, the foam board 214 is made of rigid polyurethane foam, the cabin board 21 is assembled in a splicing way by adopting a non-bridge structure, the outer skin 213 is used as a broken heat bridge, the heat preservation, heat insulation and airtight performance of the cabin 2 are better realized, the structural strength of the cabin 2 is ensured, the internal structure of the cabin 21 is not damaged, the whole cabin 2 formed by the metal skeleton 212 and the foam board 214 serving as a main body is light, and manual movement can be performed.
As shown in fig. 6 and 8 to 14, the shelter lifting module 13 comprises a bearing plate 1301, wherein the bearing plate 1301 is fixed on a frame 1, three fixing screw rods 1306 are fixed in the bearing plate 1301, one end of the bearing plate 1301 is slidably provided with a moving plate 1302, three moving motors 1311 are fixed in the moving plate 1302, the output shaft ends of the moving motors 1311 are fixed with driving gears 1310, one side of each driving gear 1310 is connected with a sleeve gear 1309 in a meshed manner, an internal thread sleeve 1308 is fixed in an axial penetrating manner of each sleeve gear 1309, the end part of each fixing screw rod 1306 penetrates through the internal thread sleeve 1308 along the axial direction of the internal thread sleeve 1308 and is in threaded transmission with the internal thread sleeve 1308, one side of the moving plate 1302 is provided with a lifting plate 1303, the end part of the lifting plate 1303 far away from the moving plate 1302 is connected with a supporting plate 1304, the bottom surface of the supporting plate 1304 is provided with two rotatable supporting hydraulic rods 1305, two sliding support plates 1307 which are arranged in a sliding manner are arranged below the lifting plate 1303, two base plates 1313 are detachably arranged on the upper surfaces of the two sliding support plates 1307, a plurality of linearly arranged movable anti-slip limit elastic sheets 1314 are arranged on the inner side of the base plates 1313, one end of each anti-slip limit elastic sheet 1314 is fixed with the base plate 1313, the other end of each anti-slip limit elastic sheet 1314 is inserted and connected with a connecting round rod 1315 in a penetrating manner, the two sliding support plates 1307 at the bottom of the lifting plate 1303 are slidably unfolded, the angles of the lifting plate 1303 and the two sliding support plates 1307 are adjusted, the end parts of the lowest sliding support plates 1307 are flush with the ground, the base plates 1313 are arranged on the surfaces of the sliding support plates 1307, at the moment, the square cabin 2 is transferred to the surfaces of the lifting plate 1303 and the two sliding support plates 1307 are pushed to slide on the surfaces of the lifting plate 1303, the square cabin 2 is conveniently detached from the frame 1, on the contrary, the backing plate 1313 is arranged on the surface of the sliding support plate 1307 in a half-circle rotating way, and then the shelter 2 positioned on the ground is pushed to the surface of the sliding support plate 1307, so that the shelter 2 can be conveniently and rapidly carried to the frame 1, and the difficulty in moving and replacing the shelter 2 is reduced;
The surface that movable plate 1302 and backup pad 1304 and lifting plate 1303 contacted all is fixed with the butt joint axostylus axostyle 1312, the butt joint axostylus axostyle 1312 is pegged graft in the lateral wall of lifting plate 1303 and lifting plate 1303 can rotate around the axis of butt joint axostylus axostyle 1312, two symmetrically distributed's slip spout 1317 have all been seted up to lifting plate 1303 and the bottom surface of two slip backup pads 1307, the upper surface of two slip backup pads 1307 all is fixed with equipment slider 1318, equipment slider 1318 slip joint is inside slip spout 1317, two auxiliary stay hydraulic stem 1316 have all been dismantled to the below of lifting plate 1303 and two slip backup pads 1307, the top of auxiliary stay hydraulic stem 1316 is pegged graft in slip spout 1317 inboard and the bottom tip is coniform, utilize the auxiliary stay hydraulic stem 1316 that the bottom is coniform to fix subaerial, and the top joint of auxiliary stay hydraulic stem 1316 is in slip spout 1317, lifting plate 1303 and two slip backup pads 1307 are supported from the bottom, and do not influence lifting plate 1303 and two slip backup pads 1307 and carry out the angle modulation, guarantee that shelter 2 is in the process of the slip of lifting cabin 1307 and two sides 1307, and the safety of shelter 2 can not be collapsed because of the transportation under the lifting cabin 2.
As shown in fig. 7, the power supply system is composed of a power supply lead-in cable, a power supply interface, an automobile power taking generator, a power distribution control unit, a UPS uninterrupted power supply and an in-car power supply cable, when the urban power supply and parking work, the urban power supply is connected from a power supply wall box through 30 rice market power cables, and the quality detection is carried out on the input power supply after overvoltage, overcurrent, electric leakage, grounding and lightning protection detection are carried out through the power distribution control unit; after the input preference is carried out by the power distribution control unit, electric power supply output is carried out, one path of alternating current 220V output is output to the air compressor, one path of alternating current 220V output is output to the UPS uninterrupted power source, the UPS uninterrupted power source output line is respectively used for working of alternating current 220V power source task system equipment by the power distribution control unit, the power supply preference sequence carries out power supply control according to the sequence of mains supply, a power taking generator set, a generator set and a UPS uninterrupted storage battery pack, uninterrupted power supply of the control equipment is realized, the power distribution control unit simultaneously reserve one path of alternating current 220V output, one path of UPS uninterrupted 220V power source output, and the UPS uninterrupted storage battery pack supplies power: when no commercial power and vehicle-mounted silence exists, when no alternating current power supply is used for supplying power, the UPS uninterrupted storage battery is used for emergency power supply, the power supply time is not less than 30 minutes, the power distribution control unit can convert the alternating current power supply into 24V direct current power supply, one path of power supply is used for illumination in a cabin and outside the cabin, one path of power supply is used for warming of an indoor fan heater, and the other path of power supply is used for 24V power supply for standby.
Working principle: when the cabin 2 needs to be transferred or replaced, firstly, a mobile motor 1311 is electrified and drives an internal thread sleeve 1308 to rotate, the internal thread sleeve 1308 drives a mobile plate 1302 to slide in a bearing plate 1301, at the moment, the mobile plate 1302 drives a lifting plate 1303 and a supporting plate 1304 to extend out of the bearing plate 1301, after the lifting plate 1303 and the supporting plate 1304 extend out completely, two supporting hydraulic rods 1305 rotate and are perpendicular to the ground, the two supporting hydraulic rods 1305 are started to enable the movable end parts of the supporting hydraulic rods 1305 to be in contact with the ground and support the supporting plate 1304, then two sliding supporting plates 1307 at the bottom of the lifting plate 1303 are slidably unfolded, the angles of the lifting plate 1303 and the two sliding supporting plates 1307 are adjusted, the end parts of the lowest sliding supporting plate 1307 are flush with the ground, a base plate 1313 is arranged on the surface of the sliding supporting plate 1307, at the moment, the cabin 2 is transferred to the surface of the lifting plate 1303, the cabin 2 is pushed to slide on the surface of the lifting plate 1303 and the surface of the two sliding supporting plates 1307, the cabin 2 is conveniently detached from the frame 1, and the difficulty of pushing the sliding cabin 2 is quickly pushed to the surface of the sliding supporting plate 1307, and the cabin 2 is quickly replaced on the surface of the frame 1301;
The personnel drive the vehicle to move, the weather monitor 7 can monitor external environmental factors in real time in the moving process, the monitoring camera 8 monitors the surrounding environment in real time, the video site of the monitoring camera 8 of the personnel and the weather factor analysis of the weather monitor 7 select proper positions to stop the frame 1, then the whole power supply of the launching vehicle can be connected, the lifting mechanism 11 is electrified and started after the power supply is connected, the movable end part of the lifting mechanism 11 pushes the unmanned aerial vehicle emitter 3 to move upwards, at the moment, the unmanned aerial vehicle emitter 3 can drive the rotary connecting block 5 to rotate around the axis of the positioning rotating shaft 6, at the moment, the angle of the unmanned aerial vehicle emitter 3 can be changed, after the unmanned aerial vehicle emitter 3 reaches the transmitting angle, the personnel can open the cabin cover behind the unmanned aerial vehicle emitter 3, the unmanned aerial vehicle monitoring system is characterized in that the unmanned aerial vehicle monitoring system is outwards transmitted by an unmanned aerial vehicle transmitter 3, workers can enter a shelter 2 after the unmanned aerial vehicle is outwards transmitted, the transmitted unmanned aerial vehicle is monitored in real time by a host cabinet and an accessory box inside the shelter 2, after the unmanned aerial vehicle is completely patrolled, the transmitted unmanned aerial vehicle is recycled into the unmanned aerial vehicle transmitter 3, the unmanned aerial vehicle monitoring system is formed by adopting a vehicle-mounted technology and mainly comprises a frame 1, a shelter 2, a lifting mechanism 11, a weather monitor 7, a gas compressor 10, a compressed gas storage tank 9, a monitoring camera 8, a power supply system and the like, and the overall design of the whole unmanned aerial vehicle is scientific and reasonable, the overall layout of equipment and facilities is scientific and reasonable, the equipment requirements are met, and the unmanned aerial vehicle is convenient to store, transport and the efficient implementation of the transmission.
It will be evident to those skilled in the art that the invention is not limited to the details of the foregoing illustrative embodiments, and that the present invention may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Claims (10)
1. The utility model provides an unmanned aerial vehicle launches carrier loader, includes frame (1) and power supply system, its characterized in that: a shelter lifting module (13) and a fixing seat (4) are fixed on the surface of the frame (1), and a detachable shelter (2) is arranged above the shelter lifting module (13);
The shelter lifting module (13) comprises a bearing plate (1301), the bearing plate (1301) is fixed on a frame (1), three fixed screw rods (1306) are fixed inside the bearing plate (1301), one end of the bearing plate (1301) is slidably provided with a moving plate (1302), three moving motors (1311) are fixed inside the moving plate (1302), the output shaft ends of the moving motors (1311) are fixed with driving gears (1310), one side of each driving gear (1310) is in meshed connection with a sleeve gear (1309), the axial direction of each sleeve gear (1309) penetrates through and is fixedly provided with an internal screw sleeve (1308), the end parts of the fixed screw rods (1306) penetrate through the internal screw sleeve (1308) along the axial direction of the internal screw sleeve (1308) and are in threaded transmission with the internal screw sleeve (1308), one side of each moving plate (1302) is provided with a lifting plate (1303), the end parts of the lifting plates (1303) are far away from the moving plates (1302) and are connected with supporting plates (1304), the bottom surfaces of the supporting plates (1304) are provided with two rotatable supporting hydraulic rods (1309), the two supporting plates (1307) are slidably provided with two base plates (1307), the anti-slip limiting elastic piece (1314) capable of moving in a linear arrangement is arranged on the inner side of the base plate (1313), one end of the anti-slip limiting elastic piece (1314) is fixed with the base plate (1313), the other end of the anti-slip limiting elastic piece (1314) is inserted into a connecting round rod (1315) in a penetrating mode, and two end portions of the connecting round rod (1315) are in sliding connection with the base plate (1313).
2. The unmanned aerial vehicle launch vehicle of claim 1, wherein: the utility model discloses a movable plate, including movable plate (1302), backup pad, lifting plate (1303), bearing plate (1304), bearing plate (1303), butt joint axostylus axostyle (1312) are all fixed with on the surface that movable plate (1302) and backup pad (1304) contacted with lifting plate (1303), butt joint axostylus axostyle (1312) are pegged graft in the lateral wall of lifting plate (1303) and lifting plate (1303) can be rotated around the axis of butt joint axostylus axostyle (1312), two symmetrically distributed's slip spout (1317) have all been seted up to the bottom surface of lifting plate (1303) and two slip backup pads (1307), two the upper surface of slip backup pad (1307) all is fixed with equipment slider (1318), equipment slider (1318) slip joint is inside slip spout (1317), two auxiliary support hydraulic stem (1316) have all been dismantled to the below of lifting plate (1303) and two slip backup pads (1307), the top of auxiliary support hydraulic stem (1316) is pegged graft in slip spout (1317) inboard and the bottom tip is the cone.
3. The unmanned aerial vehicle launch vehicle of claim 2, wherein: the square cabin (2) comprises six cabin plates (21) and a plurality of assembly rivets (24), the side edges of two adjacent cabin plates (21) are mutually attached, the outer sides of two adjacent cabin plates (21) are covered with outer wrapping edges (22), inner layering (25) are installed on the inner sides of two adjacent cabin plates (21), PVC plates (23) are filled in gaps between two adjacent cabin plates (21), the cabin plates (21) are fixedly connected with the outer wrapping edges (22) and the PVC plates (23) through the assembly rivets (24), the cabin plates (21) comprise inner skin (211), metal frameworks (212), outer skin (213) and foam plates (214), the surfaces of the outer skin (213) facing the inner skin (211) are fixedly provided with the metal frameworks (212), the foam plates (214) are installed between the inner skin (211) and the outer skin (213), and the foam plates (214) cover the metal frameworks (212).
4. A launch vehicle for an unmanned aerial vehicle according to claim 3, wherein: and the inner skin (211) and the outer skin (213) are made of t1.2mm antirust aluminum plates, surface base layers of the inner skin (211) and the outer skin (213) are subjected to chemical treatment, and the foam plates (214) are made of hard polyurethane foam.
5. The unmanned aerial vehicle launch vehicle of claim 1, wherein: unmanned aerial vehicle transmitter (3) are movably mounted above fixing base (4), the front end of unmanned aerial vehicle transmitter (3) is fixed with a plurality of rotatory connecting blocks (5), the both sides of rotatory connecting block (5) run through and rotate and peg graft have location pivot (6), the both ends and the fixing base (4) of location pivot (6) are fixed, install elevating system (11) between the bottom surface and fixing base (4) of rotatory connecting block (5), install compressed gas holding vessel (9) and gas compressor (10) between shelter (2) and fixing base (4), compressed gas holding vessel (9) and gas compressor (10) are fixed on frame (1) surface and are connected through gas piping between compressed gas holding vessel (9) and gas compressor (10).
6. The unmanned aerial vehicle launch vehicle of claim 5, wherein: weather monitor (7) and surveillance camera head (8) are installed at the top of shelter (2), movable sealing door plant (12) are installed to the rear side of shelter (2), weather monitor (7) are installed in the left front side of shelter (2), surveillance camera head (8) are installed in the right rear side of shelter (2).
7. The unmanned aerial vehicle launch vehicle of claim 1, wherein: the power supply system is characterized in that a main cabinet and an accessory box are arranged in the square cabin (2), and a power distribution power supply, an uninterruptible power supply, a power taking motor control unit, a storage battery, a video monitoring module, a weather monitoring module and a transmitting control unit are arranged in the main cabinet.
8. The unmanned aerial vehicle launch vehicle of claim 6, wherein: the video monitoring module is connected with the monitoring camera (8), and the weather monitoring module is connected with the weather monitor (7) through data lines.
9. The unmanned aerial vehicle launch vehicle of claim 5, wherein: the lifting mechanism (11) is an industrial electric actuator and is provided with an on-board controller.
10. The unmanned aerial vehicle launch vehicle of claim 1, wherein: the power supply system consists of a power supply lead-in cable, a power supply interface, an automobile power taking generator, a power distribution control unit, a UPS uninterrupted power supply and an in-automobile power supply cable.
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| CN202410353422.0A CN117944922A (en) | 2024-03-27 | 2024-03-27 | Unmanned aerial vehicle launches carrier loader |
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| CN202410353422.0A CN117944922A (en) | 2024-03-27 | 2024-03-27 | Unmanned aerial vehicle launches carrier loader |
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