CN114368423B

CN114368423B - Military foldable bats group suicide type unmanned aerial vehicle placing device

Info

Publication number: CN114368423B
Application number: CN202210135101.4A
Authority: CN
Inventors: 柳占; 李涛; 胡中强; 孙建峰
Original assignee: Hangzhou Fuling Technology Co ltd
Current assignee: Hangzhou Fuling Technology Co ltd
Priority date: 2022-02-14
Filing date: 2022-02-14
Publication date: 2023-01-20
Anticipated expiration: 2042-02-14
Also published as: CN114368423A

Abstract

The invention relates to an unmanned aerial vehicle placing device, in particular to a military foldable batwing group suicide type unmanned aerial vehicle placing device. The invention aims to provide a military foldable batwing group suicide unmanned aerial vehicle placing device capable of limiting an unmanned aerial vehicle. The invention provides a military foldable bats suicide unmanned aerial vehicle placing device which comprises a base, storage boxes, a discharging hopper, a storage mechanism, a feeding mechanism and the like, wherein the storage boxes are arranged on the front side and the rear side of the top of the base, the discharging hopper is arranged on the lower portion of the left side of each storage box, the storage mechanism is arranged on the top of the base, and the feeding mechanism used for pushing the unmanned aerial vehicle to the left is arranged on the upper portion of the base. The storage barrel can store the unmanned aerial vehicle, and then the soft plate can be driven to move outwards to be tightened by rotating the large gear, so that wings of the unmanned aerial vehicle can be folded, the unmanned aerial vehicle is limited, and the wings of the unmanned aerial vehicle are prevented from shaking and being damaged.

Description

Military foldable bats group suicide type unmanned aerial vehicle placing device

Technical Field

The invention relates to an unmanned aerial vehicle placing device, in particular to a military foldable batwing group suicide type unmanned aerial vehicle placing device.

Background

Suicide unmanned aerial vehicle is used for doing suicide type attack just like a remote control grenade, can give the effectual strike of enemy in the medium and long distance, and suicide unmanned aerial vehicle need be deposited when not using, avoids taking place the explosion.

Patent application CN208603004U, the publication date is 20190315, discloses an unmanned aerial vehicle rack, includes base, support frame, places board and remote controller box, the support frame is all installed in the base four corners, the roof is installed at the support frame top, the board is installed and places to the base upper end, place the board lower extreme and install the slider, the spout has been seted up in the base, the slider is arranged in the spout, base both sides upper end is located and installs the dust screen between the support frame, the remote controller box is installed to the support frame rear side, the lid is installed to remote controller box upper end, the hinge is installed to remote controller box left end. The placing plate is pulled out through the handle, the placing plate is located in the sliding groove through the sliding block to slide when pulled out, the unmanned aerial vehicle is placed and placed on the placing plate, then the placing plate is pushed back, effects such as pressure prevention and rain prevention can be effectively achieved on the unmanned aerial vehicle, damage to the unmanned aerial vehicle caused by external force is avoided, meanwhile, people who are convenient to use can conveniently store the unmanned aerial vehicle, and the placing plate is practical and suitable for wide popularization and use. Although above-mentioned patent can avoid external force to lead to unmanned aerial vehicle's damage, can't carry on spacingly to unmanned aerial vehicle, at the in-process of transportation, unmanned aerial vehicle takes place to rock very easily, leads to the wing to take place to damage.

To sum up, so now urgent need one kind can carry out spacing for military use collapsible bat crowd suicide type unmanned aerial vehicle placer to unmanned aerial vehicle for solve above-mentioned problem.

Disclosure of Invention

In order to overcome the defects that the existing unmanned aerial vehicle placing rack is generally simpler in function and cannot limit an unmanned aerial vehicle, the invention aims to provide a military foldable batwing group suicide type unmanned aerial vehicle placing device capable of limiting the unmanned aerial vehicle.

The invention is realized by the following technical approaches:

the utility model provides a for military use collapsible bat crowd suicide type unmanned aerial vehicle placer, the on-line screen storage device comprises a base, deposit the case, the blowing fill, deposit mechanism, feeding mechanism and wing packing up mechanism, both sides all are equipped with deposits the case around the base top, the left side lower part of depositing the case all is equipped with the blowing fill, the top of base is equipped with storage mechanism, the upper portion of base is equipped with the feeding mechanism who is used for pushing unmanned aerial vehicle to left, it is used for carrying out spacing wing packing up mechanism to unmanned aerial vehicle to be equipped with on the storage mechanism, storage mechanism is including the guide rail, damping spring, the guide block, the pivot, storage cylinder and baffle, the equal slidingtype in both sides is equipped with the guide rail around the base top, equal bilateral symmetry is equipped with damping spring between guide rail and the base, the equal slidingtype in upper portion left side of guide rail is equipped with the guide block, the equal rotary type in centre of guide block is equipped with the pivot, the equal rotary type in pivot upper portion is equipped with the baffle, the baffle all is connected with adjacent guide block, the baffle top all is equipped with the storage cylinder that is used for placing unmanned aerial vehicle.

Further, feeding mechanism is including belt pulley, drive belt, hand wheel and shifting block, and the equal bilateral symmetry rotary type in both sides upper portion is equipped with the bull stick around the base, all is equipped with the belt pulley on the bull stick, all around having the drive belt between two belt pulleys of horizontal homonymy, and two left bull stick outsides all are equipped with the hand wheel, all are equipped with the shifting block on the drive belt, and the shifting block all is connected with adjacent case slidingtype of depositing, and the guide block is turned right the motion and can be contacted with the shifting block.

Further, the mechanism is packed up including soft board to the wing, protruding tooth block, major axis tooth post, the backplate, the pinion, the gear wheel, the ratchet, the deflector, the leading truck, ratchet and first spring, both sides all are equipped with soft board around the storage cylinder, the soft board outside all is equipped with protruding tooth block, equal rotary type is equipped with two major axis tooth posts on the baffle, major axis tooth post all meshes with adjacent protruding tooth block, both sides all are equipped with the backplate about the storage cylinder, the other end of soft board all is located adjacent backplate inboard, the lower part of major axis tooth post all is equipped with the pinion, the upper portion of pivot all is equipped with the gear wheel, the pinion all meshes with adjacent gear wheel, the middle part of pivot all is equipped with the ratchet, the top inboard of deflector all is equipped with the deflector, the equal slidingtype in deflector upper portion is equipped with the leading truck, the leading truck outside all is equipped with the ratchet, the ratchet blocks the ratchet, all be equipped with two first springs between ratchet inboard and the adjacent deflector.

Further, still including being used for driving gear wheel pivoted drive mechanism, drive mechanism is including the guide post, the Z template, the stopper, the second spring, drive gear, clockwork spring, contact bar and fixed rack, the inboard left part of guide rail all is equipped with the guide post, the inboard equal slidingtype of guide post is equipped with the Z template, the middle part of guide post all is equipped with the stopper, the stopper all contacts with adjacent Z template, all be equipped with the second spring between Z template rear side and the adjacent guide post, the lower part of pivot all is connected with drive gear through one way clutch, all be equipped with clockwork spring between the lower part of pivot and the adjacent guide block, the bottom inboard of leading truck all is equipped with the contact bar, contact bar rightward movement can contact with the Z template, the inboard left part of guide rail all is equipped with fixed rack, drive gear rightward movement can mesh with fixed rack.

Further, still including the moving mechanism who makes things convenient for the foldable bat crowd suicide type unmanned aerial vehicle placer of removal, moving mechanism is equipped with the pull rod including pull rod and universal wheel, the left side lower part of base, both sides around the base right side and the equal rotary type in right side upper portion of depositing the case are equipped with the universal wheel.

The storage cylinder is characterized by further comprising a protection mechanism used for preventing the storage cylinder from sliding leftwards, the protection mechanism comprises three triangular blocks, a protection cover and a magnetic force plate, the lower portion of the left side of the discharging hopper is provided with the three triangular blocks, the protection cover is arranged on the lower portion of the left side of the discharging hopper in an equal rotating mode, the protection cover is in contact with the adjacent three triangular blocks, and the magnetic force plate is arranged on the left side of the upper portion of the protection cover.

Further, still including being used for carrying out the sealing mechanism who protects unmanned aerial vehicle, sealing mechanism is including the slide bar, the closing plate, the connecting plate, the third spring, the connecting axle, a cam, handle and protecting crust, the equal interval slidingtype in top of depositing the case is equipped with the slide bar, the slide bar bottom all is equipped with the closing plate, all be equipped with the connecting plate between the slide bar top of horizontal homonymy, all around having the third spring on the slide bar of the left and right sides, the quantity of third spring is four, the both ends of third spring respectively with deposit case and connecting plate and be connected, it is equipped with the protecting crust to deposit between the top of case, the slide bar all is located the protecting crust inboardly, the rotary type is equipped with the connecting axle in the middle of the lower part of protecting crust, both sides all are equipped with the cam around the connecting axle, the cam all withstands adjacent connecting plate, the rear end of connecting axle is equipped with the handle.

Furthermore, the left side and the right side of the bottom of the base are both provided with non-slip mats.

Compared with the prior art, the invention has the following advantages:

1. the storage barrel can store the unmanned aerial vehicle, and then the soft plate can be driven to move outwards to be tightened by rotating the large gear, so that wings of the unmanned aerial vehicle can be folded, the unmanned aerial vehicle is limited, and the wings of the unmanned aerial vehicle are prevented from shaking and being damaged.

2. According to the ratchet wheel, the driving gear and the fixed rack are matched, so that manual rotation of the large gear can be replaced, and then manual pulling of the guide frame towards the inner side can be replaced through matching of the Z-shaped plate and the contact rod, so that the ratchet wheel is driven to move towards the inner side, the ratchet wheel is loosened by the ratchet wheel, and time and labor are saved.

3. The invention can drive the cam to rotate forwards and backwards through the forward and reverse rotating handle, can drive the sealing plate to move up and down under the action of the third spring, and can cover the top of the storage cylinder when the sealing plate moves downwards to play the roles of dust prevention and moisture prevention.

Drawings

Fig. 1 is a schematic perspective view of the present invention.

Fig. 2 is a cross-sectional view of the present invention.

Fig. 3 is a partial perspective view of the storage mechanism of the present invention.

Fig. 4 is a schematic partial perspective view of a first wing retraction mechanism according to the present invention.

Fig. 5 is a schematic partial perspective view of a second wing retraction mechanism according to the present invention.

FIG. 6 is an enlarged view of the present invention at A.

Fig. 7 is a partial perspective view of the wing retraction mechanism and the transmission mechanism of the present invention.

Fig. 8 is a partial perspective view of the sealing mechanism of the present invention.

In the drawings above: 1-base, 2-storage box, 3-discharge hopper, 4-storage mechanism, 41-guide rail, 42-damping spring, 43-guide block, 44-rotation shaft, 45-storage barrel, 46-baffle, 5-feeding mechanism, 51-belt pulley, 52-transmission belt, 53-hand wheel, 54-shifting block, 6-wing retraction mechanism, 61-flexible plate, 62-cam block, 63-long shaft toothed column, 64-guard plate, 65-pinion, 66-bull gear, 67-ratchet wheel, 68-guide plate, 69-guide frame, 610-ratchet bar, 611-first spring, 7-transmission mechanism, 71-guide column, 72-Z plate, 73-stop block, 74-second spring, 75-drive gear, 76-clockwork spring, 77-contact bar, 78-fixed bar, 8-moving mechanism, 81-pull bar, 82-universal wheel, 9-protection mechanism, 91-triangle block, 92-protection cover, 93-magnetic plate, 10-sealing mechanism, 101-sealing plate, 101-103-sealing plate, 102-sliding bar, 103-sealing plate, 103-sliding bar, 106-connecting plate, and 106-connecting shaft.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Example 1

The utility model provides a for military use collapsible bat crowd suicide type unmanned aerial vehicle placer, refer to fig. 1-7, including base 1, storage box 2, blowing fill 3, storage mechanism 4, feeding mechanism 5 and wing packing up mechanism 6, both sides all are equipped with storage box 2 around the base 1 top, the left and right sides of base 1 bottom all is equipped with the slipmat, play the antiskid, storage box 2's left side lower part all welds blowing fill 3, base 1's top is equipped with storage mechanism 4, base 1's upper portion is equipped with feeding mechanism 5, be equipped with wing packing up mechanism 6 on storage mechanism 4, storage mechanism 4 is including guide rail 41, damping spring 42, guide block 43, pivot 44, storage cylinder 45 and baffle 46, the equal slidingtype in both sides is equipped with guide rail 41 around the base 1 top, all bilateral symmetry is equipped with damping spring 42 between guide rail 41 and the base 1, the upper portion left side of guide rail 41 all slidingtype is equipped with guide block 43, the middle equal rotary type of guide block 43 is equipped with pivot 44, pivot 44 rotary type upper portion all is equipped with baffle 46, baffle 46 all is equipped with baffle 46, the top all is equipped with storage cylinder 45, the unmanned aerial vehicle can put into a proper amount people's storage cylinder 45.

Referring to fig. 1-2, feeding mechanism 5 is including belt pulley 51, drive belt 52, hand wheel 53 and shifting block 54, the equal bilateral symmetry rotary type in both sides upper portion is equipped with the bull stick around base 1, all be equipped with belt pulley 51 on the bull stick, all around having drive belt 52 between two belt pulleys 51 of horizontal homonymy, two left bull stick outsides all are equipped with hand wheel 53, all be equipped with shifting block 54 on the drive belt 52, shifting block 54 all with adjacent case 2 sliding type connection of depositing, guide block 43 moves to the right and can contact with shifting block 54, shifting block 54 moves to the left and can drive all storage barrel 45 and move to the left, make things convenient for the manual work to take out unmanned aerial vehicle.

Referring to fig. 1, 2, 4, 5, 6 and 7, the wing retraction mechanism 6 includes a flexible plate 61, a protruding tooth block 62, a long axis tooth post 63, a guard plate 64, a pinion 65, a large gear 66, a ratchet 67, a guide plate 68, a guide frame 69, a ratchet 610 and a first spring 611, the flexible plate 61 is disposed on each of the front and rear sides of the storage cylinder 45, when the flexible plate 61 moves toward the outside, the wing of the unmanned aerial vehicle can be retracted and limited, the protruding tooth block 62 is disposed on the outer side of the flexible plate 61, two long axis tooth posts 63 are rotatably disposed on the baffle 46, the long axis tooth posts 63 are respectively engaged with the adjacent protruding tooth blocks 62, the guard plates 64 are welded on each of the left and right sides of the storage cylinder 45, the other end of the flexible plate 61 is disposed on the inner side of the adjacent guard plate 64, the pinion 65 is connected with the lower portion of the long axis tooth post 63 through a key, the pinion 66 is connected with the upper pinion of the upper portion of the rotating shaft 44 through a key, the pinion is respectively engaged with the adjacent ratchet 66, the middle portion of the rotating shaft 44 is connected with the ratchet 67 through the inner side of the guide block 43, the guide plate 68 is disposed on the upper portion of the guide frame 610, and the guide frame 610 is disposed on the outer side of the guide plate 610, the ratchet 610 and the ratchet 68, the ratchet 610 are respectively disposed on the inner side of the guide frame 610.

When people need to use the device, firstly, a proper amount of unmanned aerial vehicle is placed in the storage barrel 45 in sequence, then the large gear 66 is rotated to drive the rotating shaft 44 and the ratchet 67 to rotate, the ratchet 67 can extrude the ratchet strip 610 and the guide frame 69 to move inwards, the first spring 611 is compressed, meanwhile, the large gear 66 drives the small gear 65 to rotate, the small gear 65 drives the long shaft tooth post 63 to rotate, the long shaft tooth post 63 drives the convex tooth block 62 to move outwards, so as to drive the soft plate 61 to move outwards, the guard plate 64 can limit the soft plate 61, at the moment, the soft plate 61 is tightened, the soft plate 61 can fold the wing of the unmanned aerial vehicle, so as to limit the unmanned aerial vehicle, then the large gear 66 stops rotating, the first spring 611 restores the original state, the ratchet strip 610 and the guide frame 69 are driven to move outwards to reset, so that the ratchet 67 is clamped by the ratchet strip 610 again, and then the storage barrel 45 is pushed rightwards, can drive the rotating shaft 44 and the guide block 43 to move rightwards, the storage cylinder 45 drives the unmanned aerial vehicle to move rightwards, thereby transmitting the unmanned aerial vehicle to the inside of the storage box 2, then two new storage cylinders 45 are respectively placed at the left sides of the tops of the two guide rails 41, the operation is repeated, the unmanned aerial vehicle can be stored again, the reciprocating is carried out, when the guide block 43 at the rightmost side is contacted with the shifting block 54, the shifting block 54 can be extruded to move rightwards, thereby driving the transmission belt 52, the belt pulley 51 and the hand wheel 53 rotate clockwise, after all the unmanned aerial vehicles are stored, people can transport the device away, thereby completing the transportation work of the unmanned aerial vehicle, in the transportation process, the whole device can generate slight vibration, at the moment, the damping spring 42 can be deformed adaptively, thereby playing a damping effect, playing a protection effect on the unmanned aerial vehicle, when people need to take out the unmanned aerial vehicle, the hand wheel 53 is rotated counterclockwise to drive the belt pulley 51 and the transmission belt 52 to rotate counterclockwise, so as to drive the shifting block 54 to move leftwards and reset, the shifting block 54 extrudes the rightmost guide block 43 to move leftwards, so as to push all the storage cylinders 45 to move leftwards, then the storage cylinders 45 are manually taken out, then the guide frame 69 is pulled inwards, the ratchet bar 610 is driven to move inwards, the first spring 611 is compressed, the ratchet bar 610 loosens the ratchet wheel 67, then the large gear 66 is reversed, so as to drive the rotating shaft 44 and the ratchet wheel 67 to reverse, the large gear 66 drives the small gear 65 to reverse, the small gear 65 drives the long shaft toothed column 63 to reverse, the long shaft toothed column 63 drives the convex toothed block 62 to move inwards and reset, so as to drive the soft board 61 to move inwards and reset, so as to loosen the soft board 61, the soft board 61 can be loosened, then the unmanned aerial vehicle stops rotating the large gear 66, then the guide frame 69 is loosened, the first spring 611 restores to the original state, the ratchet bar 610 and the guide frame 69 are driven to move outwards and reset, so that the ratchet bar 67 is manually clamped again, and finally the unmanned vehicle can be taken out in turn.

Example 2

On the basis of embodiment 1, referring to fig. 2, 4, 5, 6 and 7, the device further comprises a transmission mechanism 7, wherein the transmission mechanism 7 comprises guide posts 71, Z-shaped plates 72, limit blocks 73, second springs 74, a driving gear 75, a clockwork spring 76, contact rods 77 and fixed racks 78, the guide posts 71 are welded to the left portion of the inner side of the guide rail 41, the Z-shaped plates 72 are arranged on the inner sides of the guide posts 71 in a sliding manner, the limit blocks 73 are arranged in the middle of the guide posts 71, the limit blocks 73 are in contact with the adjacent Z-shaped plates 72, the second springs 74 are arranged between the rear sides of the Z-shaped plates 72 and the adjacent guide posts 71, the driving gear 75 is connected to the lower portion of the rotating shaft 44 through a one-way clutch, the clockwork springs 76 are arranged between the lower portion of the rotating shaft 44 and the adjacent guide blocks 43, the contact rods 77 are welded to the inner sides of the bottoms of the guide frames 69, the contact rods 77 can be in contact with the Z-shaped plates 72 when moving rightwards, the left portion of the inner side of the guide rail 41 is provided with the fixed racks 78, and the driving gear 75 can be engaged with the fixed racks 78 when moving rightwards.

When people push the storage cylinder 45 to the right, the driving gear 75 and the contact rod 77 are driven to move to the right, when the contact rod 77 contacts the Z-shaped plate 72, the pressing Z-shaped plate 72 moves inward, the second spring 74 is compressed, so that the Z-shaped plate 72 is separated from the stopper 73, when the driving gear 75 is engaged with the fixed rack 78, the fixed rack 78 drives the driving gear 75 to rotate, the driving gear 75 drives the rotating shaft 44 to rotate, the spiral spring 76 is deformed, thereby tightening the flexible board 61, folding the wings of the unmanned aerial vehicle by the flexible board 61, when the contact rod 77 is separated from the Z-shaped plate 72, the second spring 74 is restored to drive the Z-shaped plate 72 to move and reset to the outside, so that the Z-shaped plate 72 is contacted with the limit block 73 again, when the driving gear 75 is separated from the fixed rack 78, the driving gear 75 stops rotating, and when the storage cylinder 45 moves to the left, the driving gear 75 and the contact rod 77 are driven to move to the left, when the driving gear 75 is engaged with the fixed rack gear 78, the fixed rack gear 78 rotates the driving gear 75 in the reverse direction, and at this time the driving gear 75 does not rotate the rotation shaft 44 in the reverse direction, when the contact rod 77 contacts the Z-shaped plate 72, since the stopper 73 blocks the Z-shaped plate 72, the Z-shaped plate 72 presses the contact rod 77 to move inward, thereby moving the ratchet 610 and the guide bracket 69 inward, the first spring 611 is compressed, so that the ratchet bar 610 releases the ratchet 67, and the spring 76 is restored to the original state, driving the rotating shaft 44 to rotate reversely and reset, so that the soft board 61 can loosen the unmanned aerial vehicle, when the driving gear 75 is separated from the fixed rack 78, the driving gear 75 stops reversing, when the contact rod 77 is separated from the Z-shaped plate 72, the first spring 611 is restored to its original shape, and drives the ratchet bar 610, the guide bracket 69 and the contact rod 77 to move and return to the outside.

Referring to fig. 1 and 2, the mobile device 8 further comprises a moving mechanism 8, the moving mechanism 8 comprises a pull rod 81 and universal wheels 82, the pull rod 81 is welded to the lower portion of the left side of the base 1, the universal wheels 82 are rotatably arranged on the front side, the rear side and the upper portion of the right side of the base 1 and the upper portion of the right side of the storage box 2, and when the universal wheels 82 are in contact with the ground, the universal wheels can roll on the ground, so that the device can be assisted to move.

Referring to fig. 1 and 2, still including protection machanism 9, protection machanism 9 is including three hornblocks 91, protection casing 92 and magnetic force board 93, three hornblocks 91 have all been welded to the left side lower part of blowing fill 3, the equal rotary type in left side lower part of blowing fill 3 is equipped with protection casing 92, protection casing 92 all contacts with adjacent three hornblocks 91, the upper portion left side of protection casing 92 all is equipped with magnetic force board 93, when protection casing 92 up rotated, can drive magnetic force board 93 up and rotate and hold storage box 2, thereby block storage box 2 left side, avoid storage cylinder 45 to the roll-off of turning left.

After all unmanned aerial vehicles all save, the manual work is with protection casing 92 up rotate 90 degrees, drive magnetic plate 93 up rotate 90 degrees, make magnetic plate 93 hold deposit case 2, thereby can fix the position of protection casing 92, protection casing 92 can block and deposit 2 left sides of case, avoid having storage cylinder 45 to turn left roll-off, then people can up stimulate pull rod 81, make the device take place to rotate, universal wheel 82 and ground contact, then stimulate pull rod 81, can remove the device, universal wheel 82 can subaerial roll, after the device removes suitable position, put down pull rod 81, make the device take place the reversal, universal wheel 82 and ground separation, when people need take out unmanned aerial vehicle, with protection casing 92 down rotate 90 degrees earlier and reset, drive magnetic plate 93 down and rotate 90 degrees and reset, make magnetic plate 93 loosen and deposit case 2, triangular block 91 can carry out spacingly to protection casing 92, then people can take out storage cylinder 45, take out unmanned aerial vehicle at last.

Referring to fig. 1, 2 and 8, the unmanned aerial vehicle further comprises a sealing mechanism 10, the sealing mechanism 10 comprises sliding rods 101, sealing plates 102, connecting plates 103, third springs 104, connecting shafts 105, cams 106, handles 107 and protective shells 108, the sliding rods 101 are arranged at the tops of the storage boxes 2 at intervals in a sliding mode, the sealing plates 102 are arranged at the bottoms of the sliding rods 101, the sealing plates 102 can cover the tops of the storage cylinders 45 when moving downwards, the storage boxes are dustproof and moistureproof, the connecting plates 103 are welded between the tops of the sliding rods 101 on the same transverse side, the third springs 104 are wound on the sliding rods 101 on the left side and the right side, the number of the third springs 104 is four, two ends of each third spring 104 are respectively connected with the storage boxes 2 and the connecting plates 103, the protective shells 108 are welded between the tops of the storage boxes 2, the sliding rods 101 are located on the inner sides of the protective shells 108, the connecting shafts 105 are rotatably arranged in the middles of the lower portions of the protective shells 108, the cams 106 are arranged on the front and the rear sides and the front sides and the rear ends of the adjacent connecting plates 103, and the connecting shafts 107 are arranged at the rear ends of the cams 106.

Initially, the third spring 104 is in a stretching state, after all the unmanned aerial vehicles are stored, people can rotate the handle 107 by 90 degrees, drive the connecting shaft 105 and the cam 106 to rotate by 90 degrees, so that the cam 106 loosens the connecting plate 103, the third spring 104 is restored to the original state, and drive the connecting plate 103 to move down, so as to drive the sliding rod 101 and the sealing plate 102 to move down, so that the sealing plate 102 covers the top of the storage cylinder 45 respectively, so that the storage cylinder 45 is in a sealing state, and the dustproof and moistureproof effects are achieved.

The above description is only for the specific embodiments of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art can easily conceive of the changes or substitutions within the technical scope of the present invention, and all the changes or substitutions should be covered within the scope of the present invention. Therefore, the protection scope of the present invention shall be subject to the protection scope of the appended claims.

Claims

1. A military foldable bats suicide unmanned aerial vehicle placement device is characterized by comprising a base (1), storage boxes (2), a discharge hopper (3), a storage mechanism (4), a feeding mechanism (5) and a wing retraction mechanism (6), wherein the storage boxes (2) are arranged on the front side and the rear side of the top of the base (1), the discharge hopper (3) is arranged on the lower portion of the left side of the storage box (2), the storage mechanism (4) is arranged on the top of the base (1), the feeding mechanism (5) used for pushing the unmanned aerial vehicle to the left is arranged on the upper portion of the base (1), the wing retraction mechanism (6) used for limiting the unmanned aerial vehicle is arranged on the storage mechanism (4), the storage mechanism (4) comprises guide rails (41), damping springs (42), guide blocks (43), a rotating shaft (44), storage cylinders (45) and baffle plates (46), guide rails (41) are arranged on the front side and the rear side of the top of the base (1) in a sliding mode, damping springs (42) are arranged between the guide rails (41) and the base (1) and are symmetrically left and right, sliding guide blocks (43) are arranged on the left side of the upper portion of the guide rails (41), the middle of the guide blocks (43), and the guide blocks (44) and the baffle plates (46) are connected with the rotating mode, the tops of the baffles (46) are provided with storage barrels (45) for placing the unmanned aerial vehicles; the feeding mechanism (5) comprises belt pulleys (51), a transmission belt (52), a hand wheel (53) and a shifting block (54), wherein rotating rods are symmetrically arranged on the upper portions of the front side and the rear side of the base (1) in a left-right rotating mode, the belt pulleys (51) are arranged on the rotating rods, the transmission belt (52) is wound between the two belt pulleys (51) on the same transverse side, the hand wheel (53) is arranged on the outer side of each of the two rotating rods on the left side, the shifting block (54) is arranged on the transmission belt (52), the shifting block (54) is connected with the adjacent storage boxes (2) in a sliding mode, and the guide block (43) can be contacted with the shifting block (54) when moving rightwards; the wing retracting mechanism (6) comprises flexible plates (61), convex tooth blocks (62), long-axis toothed columns (63), guard plates (64), pinions (65), large gears (66), ratchets (67), guide plates (68), guide frames (69), ratchets (610) and first springs (611), the flexible plates (61) are arranged on the front side and the rear side of the storage barrel (45), the convex tooth blocks (62) are arranged on the outer sides of the flexible plates (61), two long-axis toothed columns (63) are rotatably arranged on the baffle plate (46), the long-axis toothed columns (63) are respectively meshed with the adjacent convex tooth blocks (62), the guard plates (64) are arranged on the left side and the right side of the storage barrel (45), the other ends of the flexible plates (61) are respectively positioned on the inner sides of the adjacent guard plates (64), the pinions (65) are arranged on the lower portions of the long-axis toothed columns (63), the large gears (66) are arranged on the upper portions of the rotating shafts (44), the pinions (65) are respectively meshed with the adjacent ratchets (66), the ratchets (65) are respectively arranged on the middle portions of the rotating shafts (44), the ratchets (67) are respectively arranged on the inner sides of the guide plates (43), the guide frames (69), the guide frames (610) are respectively arranged on the top portions of the guide plates (69), the guide frames (610), two first springs (611) are arranged between the inner side of each ratchet bar (610) and the adjacent guide plate (68).

2. A military foldable batswarm suicide drone placer according to claim 1, the mechanism is characterized by further comprising a transmission mechanism (7) used for driving the large gear (66) to rotate, the transmission mechanism (7) comprises guide posts (71), Z-shaped plates (72), limiting blocks (73), second springs (74), driving gears (75), clockwork springs (76), contact rods (77) and fixed racks (78), the left parts of the inner sides of the guide rails (41) are provided with the guide posts (71), the Z-shaped plates (72) are arranged on the inner sides of the guide posts (71) in a sliding mode, the limiting blocks (73) are arranged in the middle of the guide posts (71), the limiting blocks (73) are in contact with the adjacent Z-shaped plates (72), the second springs (74) are arranged between the rear sides of the Z-shaped plates (72) and the adjacent guide posts (71), the lower portions of the rotating shafts (44) are connected with the driving gears (75) through one-way clutches, the clockwork springs (76) are arranged between the lower portions of the rotating shafts (44) and the adjacent guide blocks (43), the inner sides of the bottoms of the guide frames (69) are provided with the contact rods (77), the contact rods (77) can move to the right and the guide rails (78) can move to be engaged with the inner sides of the fixed racks (41).

3. The military foldable batwing group suicide unmanned aerial vehicle placing device as claimed in claim 2, further comprising a moving mechanism (8) for conveniently moving the military foldable batwing group suicide unmanned aerial vehicle placing device, wherein the moving mechanism (8) comprises a pull rod (81) and universal wheels (82), the lower portion of the left side of the base (1) is provided with the pull rod (81), and the front side and the rear side of the right side of the base (1) and the upper portion of the right side of the storage box (2) are rotatably provided with the universal wheels (82).

4. The military foldable batwing group suicide type unmanned aerial vehicle placing device as claimed in claim 3, further comprising a protection mechanism (9) for preventing the storage barrel (45) from sliding out leftward, wherein the protection mechanism (9) comprises triangular blocks (91), a protection cover (92) and magnetic plates (93), the triangular blocks (91) are arranged on the lower portion of the left side of the discharging hopper (3), the protection cover (92) is rotatably arranged on the lower portion of the left side of the discharging hopper (3), the protection cover (92) is in contact with the adjacent triangular blocks (91), and the magnetic plates (93) are arranged on the left side of the upper portion of the protection cover (92).

5. The military foldable baton group suicide unmanned aerial vehicle placing device as claimed in claim 4, further comprising a sealing mechanism (10) for protecting the unmanned aerial vehicle, wherein the sealing mechanism (10) comprises sliding rods (101), sealing plates (102), connecting plates (103), third springs (104), connecting shafts (105), cams (106), handles (107) and protective shells (108), the sliding rods (101) are arranged at the tops of the storage boxes (2) at intervals in a sliding manner, the sealing plates (102) are arranged at the bottoms of the sliding rods (101), the connecting plates (103) are arranged between the tops of the sliding rods (101) on the same transverse side, the third springs (104) are wound around the sliding rods (101) on the left side and the right side, the third springs (104) are four in number, the two ends of the third springs (104) are respectively connected with the storage boxes (2) and the connecting plates (103), the protective shells (108) are arranged between the tops of the storage boxes (2), the sliding rods (101) are all located on the inner sides of the protective shells (108), the connecting shafts (105) are arranged in the middle of the lower portion of the connecting shafts, the connecting shafts (105) are respectively arranged on the front side and the back side of the cams (106) which abut against the connecting plates (106), and the connecting plates (107) are arranged on the connecting shafts.

6. The military foldable batwing group suicide unmanned aerial vehicle placing device as claimed in claim 1, wherein non-slip mats are arranged on the left side and the right side of the bottom of the base (1).