CN220221178U

CN220221178U - Vehicle-mounted rotor unmanned aerial vehicle modularization hangar

Info

Publication number: CN220221178U
Application number: CN202321779504.9U
Authority: CN
Inventors: 李勇; 甘建业; 付强; 李阳东; 杨贤明
Original assignee: Dewiver Intelligent Equipment Group Co ltd
Current assignee: Dewiver Intelligent Equipment Group Co ltd
Priority date: 2023-07-07
Filing date: 2023-07-07
Publication date: 2023-12-22
Anticipated expiration: 2033-07-07

Abstract

The utility model discloses a vehicle-mounted rotor unmanned aerial vehicle modularized hangar, which comprises a hangar module and a screw lifting module, wherein the hangar module comprises a hangar main frame and a hangar shell, a hatch is arranged at the top of the hangar main frame, a mounting window is arranged on the hangar main frame, a reinforcing rib is arranged in the mounting window, the hangar shell is matched and mounted in the mounting window, and a diversion head for diversion of air in running is arranged at the front end of the hangar main frame; the top of the main frame of the hangar is provided with a sliding cabin door which is in sliding connection with the main frame of the hangar, and the main frame of the hangar is internally provided with a cabin door driving assembly; screw rod lifting module sets up in the hangar body frame, and screw rod lifting module includes place platform, screw rod lifting assembly and screw rod drive assembly, is equipped with the foot rest fixed slot on the place platform, simplifies hangar structure, makes it be applicable to and carries on the vehicle, has unmanned aerial vehicle to emit the function simultaneously, has solved present unmanned aerial vehicle hangar and has had hangar structure complicacy, is unsuitable for loading the problem on the vehicle.

Description

Vehicle-mounted rotor unmanned aerial vehicle modularization hangar

Technical Field

The utility model relates to the technical field of unmanned aerial vehicle transportation, in particular to a vehicle-mounted rotor unmanned aerial vehicle modularized hangar.

Background

With the development of unmanned aerial vehicle technology, the field of unmanned aerial vehicle application is also increasing, for example: photography, field inspection, high altitude fire fighting, etc. The wide application of unmanned aerial vehicles in these fields also represents a rapid development of unmanned aerial vehicle technology, but the transportation problem of unmanned aerial vehicles is followed.

Some small-size unmanned aerial vehicle can directly use quick-witted case just portability, and some great unmanned aerial vehicle then do not have suitable on-vehicle equipment and carry, though now there is the unmanned aerial vehicle hangar, current unmanned aerial vehicle hangar structure is complicated, and its main effect is fixed point to be released and withdraw unmanned aerial vehicle to be used for transporting unmanned aerial vehicle on loading the vehicle.

The application number is: CN202222038006.0, publication No. CN218324173U discloses an unmanned aerial vehicle warehouse, which comprises a box body, wherein a plurality of cabin boards are arranged on the box body at intervals and have different orientations, openings are arranged at positions of the box body corresponding to the cabin boards, the cabin boards are in sliding connection with the box body, the cabin boards can extend out of the box body or retract into the box body from the corresponding openings, and the cabin boards bear the unmanned aerial vehicle when extending out of the box body; the two ends of the cabin board are respectively a connecting end and a free end; when the cabin board extends out of the box body, the box body stops the connecting end at the opening, and the free end is positioned outside the box body and far away from the connecting end; the thickness of the cabin board is gradually reduced from the connecting end to the free end, and the problem that the structure of the cabin board is complex and the cabin board is not suitable for being loaded on a vehicle still exists in the technology.

Disclosure of Invention

Based on the above, the utility model provides a vehicle-mounted rotor unmanned aerial vehicle modularized hangar, which simplifies the hangar structure, is suitable for being carried on a vehicle, has an unmanned aerial vehicle releasing function, and solves the problems that the hangar has a complex structure and is not suitable for being carried on the vehicle.

The technical scheme of the utility model is as follows:

the utility model provides a vehicle-mounted rotor unmanned aerial vehicle modularization hangar, includes hangar module and screw rod elevating module, the hangar module includes hangar body frame and hangar casing, hangar body frame top is equipped with the hatch that is used for unmanned aerial vehicle to come in and go out, it has a plurality of installation windows to open on the hangar body frame, all be equipped with the strengthening rib in the installation window, the vertical setting of strengthening rib is in the installation window, the hangar casing cooperation is installed in the installation window, and can dismantle with the hangar body frame and be connected, hangar body frame front end is equipped with the water conservancy diversion head that is used for the air in the water conservancy diversion driving;

the top of the main frame of the hangar is provided with two sliding cabin doors for closing or opening a hatch on the top of the main frame of the hangar, the sliding cabin doors are in sliding connection with the main frame of the hangar, and a cabin door driving assembly for driving the sliding cabin doors to open or close is arranged in the main frame of the hangar;

the screw lifting module is arranged in the hangar main frame and comprises a placing platform, a screw lifting assembly and a screw driving assembly, wherein the screw lifting assembly is matched with the placing platform and used for driving the placing platform to ascend or descend, and the screw driving assembly is used for driving the screw lifting assembly, and a foot rest fixing groove used for fixing a foot rest of the unmanned aerial vehicle is formed in the placing platform.

Preferably, the main frame of the hangar comprises a bottom frame body, a front frame body, a rear frame body and a left frame body and a right frame body, wherein the front frame body and the rear frame body are arranged on the front side and the rear side of the bottom frame body, the left frame body and the right frame body are arranged on the left side and the right side of the bottom frame body, the bottoms of the front frame body, the rear frame body, the left frame body and the right frame body are respectively detachably connected with the bottom frame body, and the mounting windows are respectively arranged on the front frame body, the rear frame body, the left frame body and the right frame body.

Preferably, sliding guide rails are arranged at the tops of the front side frame body and the rear side frame body in the main frame of the hangar, each sliding guide rail comprises a sliding rail and two sliding connecting blocks which are arranged at two ends of the sliding rail and are in sliding connection with the sliding rail, two ends of the sliding rail are respectively contacted with the left side frame body and the right side frame body, and the sliding cabin doors are respectively fixedly connected with the sliding connecting blocks.

Preferably, the cabin door driving assembly comprises a driving motor arranged in the main frame of the machine base and positioned on the right side frame body and a transmission assembly connected with the driving motor, and the output end of the driving motor is arranged towards the top of the main frame of the machine base.

Preferably, the transmission assembly comprises a first bidirectional threaded rod arranged at the upper end of the front side frame body, a second bidirectional threaded rod arranged at the upper end of the rear side frame body, a first transmission rod and a second transmission rod, wherein one ends of the first transmission rod and the second transmission rod are connected with the output end of the driving motor through a first corner gear box, the other end of the first transmission rod is connected with one end of the first bidirectional threaded rod through a second corner gear box, the other end of the first bidirectional threaded rod is rotationally connected with a first rotation mounting seat, the first rotation mounting seat is arranged on the left side frame body, the other end of the second transmission rod is connected with one end of the second bidirectional threaded rod through a third corner gear box, the other end of the second bidirectional threaded rod is connected with a second rotation mounting seat, the second rotation mounting seat is arranged on the left side frame body, the first bidirectional threaded rod and the second bidirectional threaded rod are respectively matched with sliding guide rails arranged on the front side frame body and the rear side frame body, two ends of the first bidirectional threaded rod are respectively provided with first thread connecting blocks, the first thread connecting blocks are respectively matched with two sliding connection threaded rods arranged on the front side frame body and the two sliding connection blocks, and the second thread connecting blocks are respectively arranged on the two sliding connection blocks.

Preferably, the first bidirectional threaded rod and the second bidirectional threaded rod are respectively provided with a positive thread and a negative thread which are arranged from the middle part to the two ends, the positive thread on the first bidirectional threaded rod corresponds to the negative thread on the second bidirectional threaded rod, and the negative thread on the first bidirectional threaded rod corresponds to the positive thread on the second bidirectional threaded rod.

Preferably, the screw lifting assembly comprises four threaded rotating rods and a gear reverser arranged at the bottom of the threaded rotating rods, a fixed threaded block and a fixed installation block are matched on the threaded rotating rods, one end of the fixed threaded block is in threaded fit with the threaded rotating rods, the other end of the fixed threaded block is arranged at the bottom of the placement platform, one end of the fixed installation block is arranged at the top of the threaded rotating rods and is in rotary connection with the threaded rotating rods, and the other end of the fixed installation block is arranged on a main frame of the hangar.

Preferably, the screw driving assembly comprises a rotating motor and a first gear reversing box, the first gear reversing box is connected with the driving end of the rotating motor, a first rotating rod and a second rotating rod are connected to the first gear reversing box, a second gear reversing box is arranged at one end, close to the left side frame, of the bottom frame, a third gear reversing box is arranged at one end, close to the right side frame, of the bottom frame, the first rotating rod and the second rotating rod are respectively connected with the second gear reversing box and the third gear reversing box, two third rotating rods are connected to the second gear reversing box, the third rotating rods are respectively connected with the gear reversing box, two fourth rotating rods are connected to the third gear reversing box, and the fourth rotating rods are respectively connected with the gear reversing box.

Preferably, two of the threaded rotating rods are arranged in the main frame of the machine base and close to one end of the left side frame, the other two threaded rotating rods are arranged in the main frame of the machine base and close to one end of the right side frame, the third rotating rods are respectively connected with the gear reverser at the bottom of the threaded rotating rod close to one end of the left side frame, and the fourth rotating rods are respectively connected with the gear reverser at the bottom of the threaded rotating rod close to one end of the right side frame.

Preferably, the placement platform is square, the threaded rotating rods are respectively arranged at one ends of the left side frame body and the right side frame body of the placement platform, and the number of the threaded rotating rods positioned at the left side frame body and the right side frame body is two.

Compared with the prior art, the utility model has the beneficial effects that:

compared with the traditional unmanned aerial vehicle hangar, the unmanned aerial vehicle modularized hangar disclosed by the utility model has the advantages that the structure is divided into the hangar module and the screw lifting module, so that the structure is simplified, and meanwhile, the unmanned aerial vehicle releasing and withdrawing function is still realized; when the unmanned aerial vehicle is used, the hangar module and the screw lifting module can be matched and installed on a vehicle, the unmanned aerial vehicle is placed on the placing platform, and meanwhile, the foot rest of the unmanned aerial vehicle is positioned in the foot rest fixing groove, so that the unmanned aerial vehicle cannot shake easily, and the problem that the unmanned aerial vehicle collides with the inner wall of the hangar in the transportation process is solved; be equipped with a plurality of installing window on the hangar body frame, all be equipped with the strengthening rib in the installing window for the hangar body frame has better stability, is difficult for taking place to warp, and the hangar body frame front end is equipped with the water conservancy diversion head that is used for the air in the water conservancy diversion to travel, makes the vehicle produce when traveling at high speed air resistance dispersion, makes the hangar be difficult for taking place to warp, through simplifying the hangar structure, makes it be suitable for to carry on the vehicle, and the hangar also has unmanned aerial vehicle and discharges the function simultaneously, has solved that present unmanned aerial vehicle hangar has the hangar structure complicated, is unsuitable for loading the problem on the vehicle.

Drawings

Fig. 1 is a schematic structural diagram of a modular hangar of a vehicular rotorcraft unmanned aerial vehicle according to an embodiment of the present utility model;

fig. 2 is a schematic partial structure of a modular hangar of a vehicular rotorcraft unmanned aerial vehicle according to an embodiment of the present utility model;

FIG. 3 is a schematic view of the structure of the main frame of the hangar and the screw lifting module according to the embodiment of the utility model;

FIG. 4 is a schematic view of a door drive assembly and sliding guide according to an embodiment of the present utility model;

FIG. 5 is a schematic view of a second configuration of a hatch drive assembly and a sliding rail according to an embodiment of the utility model;

FIG. 6 is a schematic view of a screw lifting module according to an embodiment of the present utility model;

reference numerals illustrate:

10-hangar module, 11-hatch, 100-hangar main frame, 101-bottom frame body, 102-front frame body, 103-rear frame body, 104-left frame body, 105-right frame body, 110-hangar housing, 120-mounting window, 121-reinforcing rib, 122-triangular fixing piece, 130-diversion head, 140-sliding hatch, 150-hatch driving component, 151-driving motor, 152-driving component, 153-first bidirectional threaded rod, 154-second bidirectional threaded rod, 155-first driving rod, 156-second driving rod, 157-first corner gear box, 158-second corner gear box, 159-third corner gear box, 160-sliding guide rail, 161-sliding track, 162-sliding connection blocks, 170-first rotation installation seats, 171-second rotation installation seats, 172-first thread connection blocks, 173-second thread connection blocks, 20-screw lifting modules, 200-placing platforms, 201-foot rest fixing grooves, 210-screw lifting assemblies, 220-screw driving assemblies, 221-rotation motors, 222-first gear reversing boxes, 223-first rotation rods, 224-second rotation rods, 225-second gear reversing boxes, 226-third gear reversing boxes, 227-third rotation rods, 228-fourth rotation rods, 230-thread rotation rods, 231-fixed thread blocks, 232-fixed installation blocks and 233-gear reversers.

Detailed Description

Embodiments of the present utility model will be described in detail below with reference to the accompanying drawings.

Examples:

as shown in fig. 1 to 6, in order to solve the above-mentioned problems, the present embodiment discloses a vehicle-mounted rotor unmanned aerial vehicle modularized hangar, which comprises a hangar module 10 and a screw lifting module 20, wherein the hangar module 10 comprises a hangar main frame 100 and a hangar housing 110, a hatch 11 for the unmanned aerial vehicle to come in and go out is provided at the top of the hangar main frame 100, a plurality of mounting windows 120 are provided on the hangar main frame 100, reinforcing ribs 121 are provided in the mounting windows 120, the reinforcing ribs 121 are vertically provided in the mounting windows 120, the hangar housing 110 is mounted in the mounting windows 120 in a matching manner and is detachably connected with the hangar main frame 100, and a flow guiding head 130 for guiding the air in running is provided at the front end of the hangar main frame 100;

the top of the main frame 100 of the hangar is provided with two sliding hatches 140 for closing or opening the hatch 11 at the top of the main frame 100 of the hangar, the sliding hatches 140 are in sliding connection with the main frame 100 of the hangar, and the main frame 100 of the hangar is internally provided with a hatch driving assembly 150 for driving the sliding hatches 140 to open or close;

the screw lifting module 20 is arranged in the hangar main frame 100, the screw lifting module 20 comprises a placing platform 200, a screw lifting assembly 210 which is matched with the placing platform 200 and used for driving the placing platform 200 to lift or descend, and a screw driving assembly 220 which is used for driving the screw lifting assembly 210, and a foot rest fixing groove 201 used for fixing the foot rest of the unmanned aerial vehicle is arranged on the placing platform 200.

Compared with the traditional unmanned aerial vehicle hangar, the unmanned aerial vehicle modularized hangar disclosed by the utility model has the advantages that the structure is divided into the hangar module 10 and the screw lifting module 20, so that the structure is simplified, and meanwhile, the unmanned aerial vehicle releasing and withdrawing function is still realized; when the unmanned aerial vehicle is used, the hangar module 10 and the screw lifting module 20 can be matched and installed on a vehicle, the unmanned aerial vehicle is placed on the placing platform 200, and meanwhile, the foot rest of the unmanned aerial vehicle is positioned in the foot rest fixing groove 201, so that the unmanned aerial vehicle cannot shake easily, and the problem that the unmanned aerial vehicle collides with the inner wall of the hangar in the transportation process and is damaged is solved; the machine base main frame 100 is provided with a plurality of mounting windows 120, and the mounting windows 120 are internally provided with reinforcing ribs 121, so that the machine base main frame 100 has better stability and is not easy to deform, and the front end of the machine base main frame 100 is provided with a flow guide head 130 for guiding air in running, so that air resistance generated by a vehicle in high-speed running is dispersed, and the machine base is not easy to deform; the sliding cabin door 140 is driven to be opened through the cabin door driving assembly 150, the screw lifting assembly 210 is driven through the screw driving assembly 220, and the placing platform 200 is driven, so that the opening of the sliding cabin door 140 and the lifting of the placing platform 200 can be completed only by arranging two driving components, the overall structure of the unmanned aerial vehicle hangar is simplified, the hangar is suitable for being carried on a vehicle through simplifying the hangar structure, meanwhile, the hangar also has an unmanned aerial vehicle discharging function, and the problems that the hangar is complex in structure and unsuitable for being carried on the vehicle in the prior unmanned aerial vehicle hangar are solved.

As shown in fig. 1 to 3, in order to facilitate the installation and disassembly of the main frame 100 of the hangar and also facilitate the installation of the hangar on a vehicle, the present embodiment is modified on the basis of the above embodiment, and is different from the above embodiment in that the main frame 100 of the hangar includes a bottom frame body 101, a front frame body 102, a rear frame body 103, a left frame body 104 and a right frame body 105 disposed on the left and right sides of the bottom frame body 101, which are disposed on the front side frame body 102, the rear frame body 103, the left frame body 104 and the right frame body 105, respectively, the bottoms of which are detachably connected to the bottom frame body 101, and the installation windows 120 are disposed on the front side frame body 102, the rear side frame body 103, the left frame body 104 and the right frame body 105, respectively.

Preferably, four mounting windows 120 are respectively provided on the left side frame 104 and the right side frame 105, three mounting windows 120 are respectively provided on the front side frame 102 and the rear side frame 103, a reinforcing rib 121 is provided in each of the mounting windows 120, the machine base housing 110 is made of iron sheet, and the machine base housing 110 is detachably mounted in each of the mounting windows 120.

Preferably, the installation window 120 is square, a triangular fixing piece 122 is arranged in the installation window 120, and four corners of the machine base shell 110 are detachably connected with the triangular fixing piece 122 through bolts.

Preferably, the bottoms of the front frame 102, the rear frame 103, the left frame 104 and the right frame 105 are detachably connected to the bottom frame 101 by bolts.

When the garage main frame 100 is used, the garage main frame 100 can be assembled quickly, the installation of the garage main frame 100 is facilitated, meanwhile, the garage main frame 100 has stronger stability due to the arrangement of the plurality of reinforcing ribs 121, the possibility of deformation of the garage main frame 100 is further reduced, the bottom frame body 101 can be fixed on a vehicle through ropes, and therefore the garage is installed on the vehicle, and the garage is suitable for large-sized vehicles or medium-sized vehicles, such as trucks, pick-up cards or SUV family household sedans.

As shown in fig. 1 to 5, in order to facilitate the opening or closing of the sliding hatch 140 on the hangar, the unmanned aerial vehicle is released and flies back from the hatch 11, and this embodiment is improved on the basis of the above embodiment, and is different from the above embodiment in that the top of the front side frame 102 and the rear side frame 103 in the hangar main frame 100 are both provided with sliding rails 160, the sliding rails 160 include a sliding rail 161 and two sliding connection blocks 162 that are disposed at two ends of the sliding rail 161 and slidingly connected with the sliding rail 161, two ends of the sliding rail 161 are respectively contacted with the left side frame 104 and the right side frame 105, and the sliding hatch 140 is respectively fixedly connected with the sliding connection blocks 162.

Preferably, the sliding door 140 may slide in the left-right direction of the main frame 100 of the hangar to open or close the hatch 11.

Preferably, the cabin door driving assembly 150 includes a driving motor 151 disposed in the main frame 100 of the cabin and located on the right frame 105, and a transmission assembly 152 connected to the driving motor 151, and an output end of the driving motor 151 is disposed toward the top of the main frame 100 of the cabin.

Preferably, the transmission assembly 152 includes a first bidirectional threaded rod 153 disposed at an upper end of the front side frame 102, a second bidirectional threaded rod 154 disposed at an upper end of the rear side frame 103, a first transmission rod 155 and a second transmission rod 156, one ends of the first transmission rod 155 and the second transmission rod 156 are connected with an output end of the driving motor 151 through a first corner gearbox 157, the other end of the first transmission rod 155 is connected with one end of the first bidirectional threaded rod 153 through a second corner gearbox 158, the other end of the first bidirectional threaded rod 153 is rotatably connected with a first rotation mounting seat 170, the first rotation mounting seat 170 is disposed on the left side frame 104, the other end of the second transmission rod 156 is connected with one end of the second bidirectional threaded rod 154 through a third corner gearbox 159, the other end of the second bidirectional threaded rod 154 is connected with a second rotation mounting seat 171, the second rotation mounting seat 171 is disposed on the left side frame 104, the first bidirectional threaded rod 153 and the second bidirectional threaded rod 154 are respectively arranged in a matching manner with a sliding guide rail 160 disposed on the front side frame 102 and the rear side frame 103, the other end of the first bidirectional threaded rod 153 is provided with a second threaded rod 172, and the second threaded rod 161 is respectively arranged in a sliding manner on the two ends of the connecting block 161 is respectively in a sliding manner.

When the unmanned aerial vehicle cabin opening cabin door is used, the driving motor 151 drives the first transmission rod 155 and the second transmission rod 156 to rotate through the first corner gearbox 157, then the first transmission rod 155 drives the first bidirectional threaded rod 153 to rotate through the second corner gearbox 158, so that the first threaded connection block 172 positioned on the first bidirectional threaded rod 153 rotates, and then the sliding connection block 162 connected with the first threaded connection block 172 is driven to slide, the second transmission rod 156 drives the second bidirectional threaded rod 154 to rotate through the third corner gearbox 159, so that the second threaded connection block 173 positioned on the second bidirectional threaded rod 154 rotates, and then the sliding connection block 162 connected with the second threaded connection block 173 is driven to slide, and then the sliding cabin door 140 arranged on the sliding connection block 162 is driven to be opened or closed, so that the problems that a plurality of motors are required to be arranged for opening the cabin door of the unmanned aerial vehicle cabin at present, and the structure for opening the cabin door is complex and difficult to overhaul are solved.

In order to improve the sliding process of the sliding door 140 with synchronism, this embodiment is different from the foregoing embodiment in that the first bidirectional threaded rod 153 and the second bidirectional threaded rod 154 are provided with a positive thread and a negative thread from the middle to both ends, the positive thread on the first bidirectional threaded rod 153 corresponds to the negative thread on the second bidirectional threaded rod 154, and the negative thread on the first bidirectional threaded rod 153 corresponds to the positive thread on the second bidirectional threaded rod 154, and in use, the rotation directions of the first bidirectional threaded rod 153 and the second bidirectional threaded rod are opposite, so that the threads on the first bidirectional threaded rod 153 and the second bidirectional threaded rod need to be oppositely arranged.

As shown in fig. 1 to 6, in order to achieve stable lifting of the placement platform 200, this embodiment is modified on the basis of the above embodiment, and is different from the above embodiment in that the screw lifting assembly 210 includes four screw rotating rods 230 and a gear reverser 233 disposed at the bottom of the screw rotating rods 230, a fixed screw block 231 and a fixed mounting block 232 are disposed on the screw rotating rods 230 in a matching manner, one end of the fixed screw block 231 is in screw matching with the screw rotating rods 230, the other end of the fixed mounting block 232 is disposed at the bottom of the placement platform 200, one end of the fixed mounting block 232 is disposed at the top of the screw rotating rods 230 and is rotatably connected with the screw rotating rods 230, and the other end of the fixed mounting block 232 is disposed on the main frame 100 of the hangar.

Preferably, the screw driving assembly 220 includes a rotation motor 221 and a first gear reversing box 222, the first gear reversing box 222 is connected with a driving end of the rotation motor 221, a first rotating rod 223 and a second rotating rod 224 are connected to the first gear reversing box 222, a second gear reversing box 225 is disposed at one end, close to the left side frame 104, of the bottom frame 101, a third gear reversing box 226 is disposed at one end, close to the right side frame 105, of the bottom frame 101, the first rotating rod 223 and the second rotating rod 224 are respectively connected with the second gear reversing box 225 and the third gear reversing box 226, two third rotating rods 227 are connected to the second gear reversing box 225, the third rotating rods 227 are respectively connected with the gear reversing box 233, two fourth rotating rods 228 are connected to the third gear reversing box 226, and the fourth rotating rods 228 are respectively connected with the gear reversing box 233.

Preferably, two screw rotating rods 230 are disposed in the main frame 100 of the machine base near the left side frame 104, the other two screw rotating rods 230 are disposed in the main frame 100 of the machine base near the right side frame 105, the third rotating rods 227 are respectively connected with the gear reverser 233 at the bottom of the screw rotating rod 230 near the left side frame 104, and the fourth rotating rods 228 are respectively connected with the gear reverser 233 at the bottom of the screw rotating rod 230 near the right side frame 105.

Preferably, the placement platform 200 is square, the threaded rotating rods 230 are respectively arranged at one ends of the left side frame 104 and the right side frame 105 of the placement platform 200, and the number of the threaded rotating rods 230 positioned on the left side frame 104 and the right side frame 105 is two, when the placement platform is used, the threaded rotating rods 230 symmetrically arranged on two sides can enable the lifting of the placement platform 200 to be more stable, reduce the collision between the unmanned aerial vehicle and the inner wall of a hangar, and cause damage.

Preferably, the screw rotating rods 230 are located at four top corners of the square placement platform 200, the screw threads on the two screw rotating rods 230 located on the diagonal are identical, the screw threads on the two screw rotating rods 230 located on the same side of the square placement platform 200 are opposite, in use, the screw rotating rods 230 located on the same side of the square placement platform 200 are opposite in rotation direction, the screw rotating rods 230 located on the diagonal are identical in rotation direction, in order to achieve simultaneous upward or simultaneous downward movement of the fixed screw blocks 231 connected with the placement platform 200 on the screw rotating rods 230, the screw rotating rods 230 located on the diagonal use screw threaded identical screw threaded rotating rods 230, and the screw threaded rotating rods 230 located on the same side of the square placement platform 200 use screw threaded rotating rods 230 opposite in screw threads.

When the unmanned aerial vehicle is used, the first gear reversing box 222 is driven by the rotating motor 221, the first rotating rod 223 and the second rotating rod 224 are driven to rotate, the first rotating rod 223 drives the two third rotating rods 227 on the second gear reversing box 225 to rotate, the gear reverser 233 connected with the third rotating rods 227 drives the threaded rotating rod 230, meanwhile, the second rotating rod 224 drives the two fourth rotating rods 228 on the third gear reversing box 226 to rotate, the gear reverser 233 connected with the fourth rotating rod 228 drives the threaded rotating rod 230, and the fixed threaded block 231 in threaded connection with the threaded rotating rod 230 moves on the threaded rotating rod 230, so that the lifting of the placing platform 200 is realized, and the problems that a plurality of motors are needed to be used for realizing a lifting function of an unmanned aerial vehicle warehouse at present, the structure of the warehouse is complex and maintenance is inconvenient are solved.

Preferably, the hangar module 10 further includes a controller module for controlling the driving motor 151 and the rotating motor 221, and the controller module is a PLC controller.

The working principle of the utility model is as follows:

when the unmanned aerial vehicle is used, the hangar module 10 and the screw lifting module 20 can be matched and installed on a vehicle, the unmanned aerial vehicle is placed on the placing platform 200, and meanwhile, the foot rest of the unmanned aerial vehicle is positioned in the foot rest fixing groove 201, so that the unmanned aerial vehicle cannot shake easily; the machine base main frame 100 is provided with a plurality of mounting windows 120, and the mounting windows 120 are internally provided with reinforcing ribs 121, so that the machine base main frame 100 has better stability and is not easy to deform, and the front end of the machine base main frame 100 is provided with a flow guide head 130 for guiding air in running, so that air resistance generated by a vehicle in high-speed running is dispersed, and the machine base is not easy to deform; the sliding hatch door 140 is driven to be opened through the hatch door driving assembly 150, the screw lifting assembly 210 is driven through the screw driving assembly 220, and the placing platform 200 is driven, so that the unmanned aerial vehicle hangar can complete the opening of the sliding hatch door 140 and the lifting of the placing platform 200 only by arranging two driving components.

The foregoing examples merely illustrate specific embodiments of the utility model, which are described in greater detail and are not to be construed as limiting the scope of the utility model. It should be noted that it will be apparent to those skilled in the art that several variations and modifications can be made without departing from the spirit of the utility model, which are all within the scope of the utility model.

Claims

1. The utility model provides a vehicle-mounted rotor unmanned aerial vehicle modularization hangar, its characterized in that includes hangar module (10) and screw rod elevating module (20), hangar module (10) are including hangar body frame (100) and hangar casing (110), hangar body frame (100) top is equipped with hatch (11) that are used for unmanned aerial vehicle to come in and go out, it has a plurality of installing window (120) to open on hangar body frame (100), all be equipped with strengthening rib (121) in installing window (120), strengthening rib (121) vertical setting is in installing window (120), hangar casing (110) cooperation is installed in installing window (120), and can dismantle with hangar body frame (100) and be connected, hangar body frame (100) front end is equipped with water conservancy diversion head (130) that are used for water conservancy diversion in going air;

the top of the hangar main frame (100) is provided with two sliding cabin doors (140) for closing or opening a hatch (11) at the top of the hangar main frame (100), the sliding cabin doors (140) are in sliding connection with the hangar main frame (100), and a cabin door driving assembly (150) for driving the sliding cabin doors (140) to open or close is arranged in the hangar main frame (100);

the screw lifting module (20) is arranged in the hangar main frame (100), the screw lifting module (20) comprises a placing platform (200), a screw lifting assembly (210) which is matched with the placing platform (200) and used for driving the placing platform (200) to ascend or descend, and a screw driving assembly (220) which is used for driving the screw lifting assembly (210), and a foot rest fixing groove (201) used for fixing the foot rest of the unmanned aerial vehicle is formed in the placing platform (200).

2. The vehicle-mounted rotary unmanned aerial vehicle modularized hangar according to claim 1, wherein the hangar main frame (100) comprises a bottom frame body (101), a front side frame body (102) arranged on the front side and the rear side of the bottom frame body (101), a rear side frame body (103), a left side frame body (104) arranged on the left side and the right side of the bottom frame body (101) and a right side frame body (105), the bottoms of the front side frame body (102), the rear side frame body (103), the left side frame body (104) and the right side frame body (105) are respectively detachably connected with the bottom frame body (101), and the mounting window (120) is respectively arranged on the front side frame body (102), the rear side frame body (103), the left side frame body (104) and the right side frame body (105).

3. The vehicle-mounted rotor unmanned aerial vehicle modularized hangar according to claim 2, wherein the tops of the front side frame body (102) and the rear side frame body (103) in the hangar main frame (100) are respectively provided with a sliding guide rail (160), the sliding guide rail (160) comprises a sliding rail (161) and two sliding connecting blocks (162) which are arranged at two ends of the sliding rail (161) and are in sliding connection with the sliding rail (161), two ends of the sliding rail (161) are respectively contacted with the left side frame body (104) and the right side frame body (105), and the sliding cabin door (140) is respectively fixedly connected with the sliding connecting blocks (162).

4. A modular hangar for a vehicular rotorcraft according to claim 3, wherein the hatch drive assembly (150) comprises a drive motor (151) disposed in the hangar main frame (100) and on the right frame (105) and a transmission assembly (152) connected to the drive motor (151), the output of the drive motor (151) being disposed towards the top of the hangar main frame (100).

5. The modular hangar of claim 4, wherein the transmission assembly (152) comprises a first bidirectional threaded rod (153) arranged at the upper end of the front side frame body (102), a second bidirectional threaded rod (154) arranged at the upper end of the rear side frame body (103), a first transmission rod (155) and a second transmission rod (156), one end of the first transmission rod (155) and one end of the second transmission rod (156) are connected with the output end of the driving motor (151) through a first corner gearbox (157), the other end of the first transmission rod (155) is connected with one end of the first bidirectional threaded rod (153) through a second corner gearbox (158), the other end of the first bidirectional threaded rod (153) is rotatably connected with a first rotary mounting seat (170), the first rotary mounting seat (170) is arranged on the left side frame body (104), the other end of the second transmission rod (156) is connected with one end of the second bidirectional threaded rod (154) through a third corner gearbox (159), the other end of the second transmission rod (155) is connected with the output end of the driving motor (151), the second transmission rod (155) is rotatably connected with one end of the second bidirectional threaded rod (171) through a second corner gearbox (171) arranged on the rear side frame body (102), the second rotary mounting seat (170) is arranged on the left side frame body (102), and the second side frame body (153) is rotatably arranged on the left side frame body (102) respectively, the two ends on the first bidirectional threaded rod (153) are respectively provided with a first threaded connection block (172), the first threaded connection blocks (172) are respectively connected with two sliding connection blocks (162) arranged on the sliding rail (161) on the front side frame body (102) in a matched mode, the two ends on the second bidirectional threaded rod (154) are respectively provided with a second threaded connection block (173), and the second threaded connection blocks (173) are respectively connected with two sliding connection blocks (162) arranged on the sliding rail (161) on the rear side frame body (103) in a matched mode.

6. The vehicle-mounted unmanned rotorcraft modular hangar of claim 5, wherein the first bidirectional threaded rod (153) and the second bidirectional threaded rod (154) are respectively provided with a positive thread and a negative thread from the middle part to two ends, the positive thread on the first bidirectional threaded rod (153) corresponds to the negative thread on the second bidirectional threaded rod (154), and the negative thread on the first bidirectional threaded rod (153) corresponds to the positive thread on the second bidirectional threaded rod (154).

7. The vehicle-mounted unmanned rotorcraft modular hangar according to claim 2 or 5, wherein the screw lifting assembly (210) comprises four screw rotating rods (230) and a gear reverser (233) arranged at the bottom of the screw rotating rods (230), fixed screw blocks (231) and fixed mounting blocks (232) are matched on the screw rotating rods (230), one ends of the fixed screw blocks (231) are in screw matching with the screw rotating rods (230), the other ends of the fixed mounting blocks (232) are arranged at the bottom of the placement platform (200), one ends of the fixed mounting blocks are arranged at the tops of the screw rotating rods (230) and are in rotary connection with the screw rotating rods (230), and the other ends of the fixed mounting blocks are arranged on the hangar main frame (100).

8. The vehicle-mounted unmanned rotorcraft modular hangar according to claim 7, wherein the screw driving assembly (220) comprises a rotating motor (221) and a first gear reversing box (222), the first gear reversing box (222) is connected with the driving end of the rotating motor (221), a first rotating rod (223) and a second rotating rod (224) are connected to the first gear reversing box (222), a second gear reversing box (225) is arranged on the bottom frame body (101) near one end of the left side frame body (104), a third gear reversing box (226) is arranged near one end of the right side frame body (105), the first rotating rod (223) and the second rotating rod (224) are respectively connected with the second gear reversing box (225) and the third gear reversing box (226), two third rotating rods (227) are respectively connected to the second gear reversing box (225), two fourth rotating rods (227) are respectively connected to the third gear reversing box (226), and the fourth rotating rods (228) are respectively connected to the fourth gear reversing box (228).

9. The modular hangar of a vehicular rotary-wing unmanned aerial vehicle according to claim 8, wherein two screw rotating rods (230) are arranged in the hangar main frame (100) near one end of the left side frame (104), the other two screw rotating rods (230) are arranged in the hangar main frame (100) near one end of the right side frame (105), the third rotating rods (227) are respectively connected with the gear reverser (233) near the bottom of the screw rotating rod (230) near one end of the left side frame (104), and the fourth rotating rods (228) are respectively connected with the gear reverser (233) near the bottom of the screw rotating rod (230) near one end of the right side frame (105).

10. The vehicle-mounted unmanned rotorcraft modular hangar of claim 9, wherein the placement platform (200) is square, the threaded rotating rods (230) are respectively arranged at one ends of the left side frame body (104) and the right side frame body (105) of the placement platform (200), and the number of the threaded rotating rods (230) arranged at the left side frame body (104) and the right side frame body (105) is two.