CN112407313B - Unmanned aerial vehicle automatic rising storage facilities - Google Patents
Unmanned aerial vehicle automatic rising storage facilities Download PDFInfo
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- CN112407313B CN112407313B CN202011336587.5A CN202011336587A CN112407313B CN 112407313 B CN112407313 B CN 112407313B CN 202011336587 A CN202011336587 A CN 202011336587A CN 112407313 B CN112407313 B CN 112407313B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U80/00—Transport or storage specially adapted for UAVs
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Abstract
The invention relates to storage equipment, in particular to automatic lifting storage equipment for an unmanned aerial vehicle, which comprises a cooling mechanism, a lifting platform mechanism and a machine body mechanism, wherein the equipment can start to cool the equipment after the unmanned aerial vehicle falls, the equipment can protect the unmanned aerial vehicle in the equipment, the equipment can discharge air in the equipment, the equipment can stop cooling, the cooling mechanism is connected with the machine body mechanism, and the machine body mechanism is connected with the lifting platform mechanism.
Description
Technical Field
The invention relates to storage equipment, in particular to unmanned aerial vehicle automatic lifting storage equipment.
Background
At unmanned aerial vehicle's lift and descending in-process, to the unmanned aerial vehicle in fixed lift place, do not have good protection device to save unmanned aerial vehicle and can make unmanned aerial vehicle accelerate ageing at the in-process of parking, so designed this kind of unmanned aerial vehicle automatic rising storage facilities.
Disclosure of Invention
The invention mainly solves the technical problem of providing the automatic lifting storage equipment for the unmanned aerial vehicle, the equipment can start to cool the equipment after the unmanned aerial vehicle falls, the equipment can protect the unmanned aerial vehicle in the equipment, the equipment can discharge air in the equipment, and the equipment can stop cooling.
In order to solve the technical problem, the invention relates to storage equipment, in particular to automatic lifting storage equipment for an unmanned aerial vehicle.
The cooling mechanism is connected with the machine body mechanism, and the machine body mechanism is connected with the lifting platform mechanism.
As a further optimization of the technical scheme, the cooling mechanism of the automatic lifting storage equipment of the unmanned aerial vehicle comprises a motor, a coupler, a cam with a shaft, a matching seat, a sliding rod, a spring, a seat with double holes, a connecting seat, a connecting pipe, a buffer box, a U-shaped pipe, a buffer box I, a connecting pipe I, a water tank, a connecting seat I, a sliding rod I, a spring I, a matching seat A, a flanged inlet pipe, a valve with a rod, an accelerating wheel, a valve with a rod I, a water outlet pipe, a sliding cavity and a sliding cavity I, wherein the motor is connected with the coupler, the cam with the shaft is hinged with the matching seat, the matching seat is connected with the sliding rod, the spring is sleeved on the sliding rod, two ends of the spring are connected with the matching seat and the seat with the double holes, the sliding rod is connected with the seat with the double holes in a sliding manner, the seat with the double holes is symmetrically connected, take pole valve and sliding chamber sliding connection, the sliding chamber sets up on the water tank, the connecting pipe is with the water tank, the baffle-box is linked together, the baffle-box links to each other and communicates with the U type pipe, the U type pipe links to each other and communicates with baffle-box I, baffle-box I links to each other and communicates with connecting pipe I, connecting seat I links to each other and communicates with slide bar I, slide bar I links to each other with taking double-hole seat sliding connection, spring I overlaps on slide bar I, spring I supports taking double-hole seat, cooperation seat A is on, cooperation seat A links to each other with slide bar I, cooperation seat A contacts with the tape spool cam, flanged admission pipe sets up on the water tank, the accelerating pulley links to each other with the tape spool cam, tape spool cam and water tank rotate to be connected, tape pole valve I links to each other with connecting seat I, tape pole valve I and sliding chamber I sliding connection, sliding chamber I sets up on the water tank.
As a further optimization of the technical scheme, the lifting platform mechanism of the automatic lifting storage equipment of the unmanned aerial vehicle comprises a servo motor, a motor belt pulley, a belt pulley I, a lead screw, a lifting platform, a connecting seat A, a sliding column, a reset spring, a supporting platform, a magnet, a plug, a rack, a step rod, a spring, a magnet seat, a mutual exclusion magnet, a socket, a magnet I, a magnet seat I, a hydraulic cylinder and a hole seat, wherein the servo motor is connected with the motor belt pulley, the motor belt pulley is in friction connection with the belt, the belt is in friction connection with the belt pulley I, both the motor belt pulley and the belt pulley I are connected with the lead screw, the lead screw is in threaded connection with the lifting platform, the connecting seat A is connected with the sliding column which is in sliding connection with the lifting platform, the sliding column is connected with the supporting platform, the reset spring is sleeved on the sliding column, two ends of the, the rack sets up in the elevating platform both sides, ladder bar and foraminiferous seat sliding connection, foraminiferous seat links to each other with the elevating platform, the spring housing is on ladder bar and both ends are connected in foraminiferous seat, on ladder bar, ladder bar links to each other with the magnetite seat, the mutual exclusion magnetite links to each other with the magnetite seat, the socket is located under the plug and connects on the elevating platform, magnetite I symmetry sets up on magnetite seat I, magnetite seat I links to each other with the elevating platform, the pneumatic cylinder links to each other with the magnetite seat, the pneumatic cylinder links to each other with the elevating platform.
As a further optimization of the technical scheme, the machine body mechanism of the automatic lifting storage equipment of the unmanned aerial vehicle comprises a base, a box body, a motor base, a servo motor I, a belt pulley A, a belt A, a through hole, a belt pulley B, a movable door, a bidirectional screw rod, a track with a sliding groove, a motor base A, a wind wheel, a gear with a shaft, a wind wheel groove, a vertical groove and a vertical moving groove, wherein the base is connected with the box body, the box body is connected with the motor base, the motor base is connected with the servo motor I, the servo motor I is connected with the belt pulley A, the belt pulley A is in friction connection with the belt A, the belt A is in friction connection with the belt pulley B, the through hole is formed in the box body, the belt pulley A and the belt pulley B are both connected with the bidirectional screw rod, the bidirectional screw rod is in rotation connection with the track with the sliding groove, dodge gate and two-way lead screw threaded connection, motor cabinet A links to each other with the base, the wind wheel links to each other with the tape spool gear, the tape spool gear rotates with the box body to be connected, the wind wheel groove sets up on the box body, the wind wheel sets up in the wind wheel inslot, the tape spool gear sets up in vertical inslot, vertical groove symmetry sets up on the box body, vertical shifting chute symmetry sets up on the box body, base and servo motor, servo motor all links to each other, the lead screw rotates with the box body to be connected, elevating platform and vertical shifting chute sliding connection, rack and vertical groove sliding connection, the rack meshes with the tape spool gear mutually, U type pipe inserts in the through-hole and links to each other with the box body, the water tank links to each other with the box.
As a further optimization of the technical scheme, the magnets and the magnets I attract each other, and the mutually exclusive magnets, the magnets and the magnets I repel each other.
As further optimization of the technical scheme, after the plug and the socket of the automatic lifting storage equipment of the unmanned aerial vehicle are connected, the power supply of the motor is connected.
As further optimization of the technical scheme, the invention provides the automatic lifting storage equipment for the unmanned aerial vehicle.
The unmanned aerial vehicle automatic lifting storage equipment has the beneficial effects that:
according to the automatic lifting storage device for the unmanned aerial vehicle, the device can be cooled after the unmanned aerial vehicle falls down, the unmanned aerial vehicle can be protected in the device, air in the device can be discharged by the device, and the device can stop cooling.
Drawings
The invention is described in further detail below with reference to the accompanying drawings and specific embodiments.
Fig. 1 is a schematic structural diagram of an automatic unmanned aerial vehicle lifting storage device according to the present invention.
Fig. 2 is a schematic structural diagram of an automatic unmanned aerial vehicle lifting storage device according to the present invention.
Fig. 3 is a schematic structural diagram of an automatic unmanned aerial vehicle lifting storage device according to the present invention.
Fig. 4 is a schematic structural diagram of an automatic unmanned aerial vehicle lifting storage device according to the present invention.
Fig. 5 is a first structural schematic diagram of the cooling mechanism 1 of the automatic lifting storage device of the unmanned aerial vehicle of the present invention.
Fig. 6 is a schematic structural diagram of a cooling mechanism 1 of an automatic unmanned aerial vehicle lifting storage device according to the present invention.
Fig. 7 is a third schematic structural diagram of the cooling mechanism 1 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 8 is a first structural schematic diagram of the lifting table mechanism 2 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 9 is a second schematic structural diagram of the lifting platform mechanism 2 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 10 is a third schematic structural diagram of the lifting table mechanism 2 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 11 is a first structural schematic diagram of the body mechanism 3 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 12 is a second schematic structural diagram of the body mechanism 3 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 13 is a third schematic structural diagram of the body mechanism 3 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 14 is a fourth schematic structural diagram of the body mechanism 3 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
Fig. 15 is a fifth schematic structural view of the body mechanism 3 of the automatic unmanned aerial vehicle lifting storage device of the present invention.
In the figure: a cooling mechanism 1; a motor 1-1; 1-2 of a coupler; 1-3 of cam with shaft; 1-4 of a matching seat; 1-5 slide bars; 1-6 of a spring; 1-7 with a double-hole seat; connecting seats 1-8; connecting pipes 1-9; 1-10 parts of a buffer tank; 1-11 parts of a U-shaped pipe; buffer box I1-12; connecting pipe I1-13; 1-14 parts of a water tank; connecting seat I1-15; slide bar I1-16; a spring I1-17; the matching seat A1-18; 1-19 of flanged inlet pipe; 1-20 parts of a valve with a rod; 1-21 of an accelerator wheel; a valve I1-22 with a rod; water outlet pipes 1 to 23; sliding cavities 1-24; a sliding cavity I1-25; a lifting table mechanism 2; a servo motor 2-1; a motor belt pulley 2-2; 2-3 of a belt; pulley I2-4; 2-5 parts of a screw rod; 2-6 of a lifting platform; connecting seat A2-7; 2-8 parts of a sliding column; 2-9 parts of a return spring; 2-10 of a support platform; 2-11 parts of magnets; 2-12 parts of a plug; 2-13 of racks; step bars 2-14; 2-15 parts of a spring; 2-16 parts of magnet seat; 2-17 parts of mutual exclusion magnet; 2-18 of the socket; a magnet I2-19; a magnet seat I2-20; 2-21 parts of a hydraulic cylinder; 2-22 parts of a perforated base; a body mechanism 3; a base 3-1; a box body 3-2; 3-3 of a motor base; a servo motor I3-4; pulley A3-5; belt A3-6; 3-7 of a through hole; pulley B3-8; 3-9 parts of a movable door; 3-10 parts of a bidirectional screw; 3-11 parts of tracks with sliding chutes; motor base A3-12; 3-13 parts of wind wheel; gears 3-14 with shafts; 3-15 parts of wind wheel grooves; 3-16 parts of vertical grooves; vertically moving the slots 3-17.
Detailed Description
The first embodiment is as follows:
the present embodiment is described below with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, and fig. 15, and the present invention relates to a storage device, and more specifically, to an automatic unmanned aerial vehicle lifting storage device, which includes a cooling mechanism 1, a lifting platform mechanism 2, and a fuselage mechanism 3, and is capable of starting to cool down the device after the unmanned aerial vehicle falls down, protecting the unmanned aerial vehicle in the device, discharging air in the device, and stopping cooling.
The cooling mechanism 1 is connected with the machine body mechanism 3, and the machine body mechanism 3 is connected with the lifting platform mechanism 2.
The second embodiment is as follows:
the following describes the present embodiment with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, and the present embodiment further describes the present embodiment, where the cooling mechanism 1 includes a motor 1-1, a coupling 1-2, a cam with a shaft 1-3, a mating seat 1-4, a sliding rod 1-5, a spring 1-6, a seat with a double hole 1-7, a connecting seat 1-8, a connecting pipe 1-9, a buffer tank 1-10, a U-shaped pipe 1-11, a buffer tank I1-12, a connecting pipe I1-13, a water tank 1-14, a connecting seat I1-15, a sliding rod I1-16, a spring I1-17, a mating seat a1-18, a flanged inlet pipe 1-19, a valve with a rod 1-20, a cam with, 1-21 parts of accelerating pulley, 1-22 parts of valve with rod I1, 1-23 parts of water outlet pipe, 1-24 parts of sliding cavity and I1-25 parts of sliding cavity, 1-1 parts of motor is connected with 1-2 parts of coupler, 1-2 parts of coupler are connected with 1-3 parts of cam with shaft, 1-3 parts of cam with shaft are hinged with 1-4 parts of matching seat, 1-4 parts of matching seat are connected with 1-5 parts of sliding rod, 1-6 parts of spring are sleeved on 1-5 parts of sliding rod, two ends of spring are connected with 1-4 parts of matching seat and 1-7 parts of seat with double holes, 1-5 parts of sliding rod are connected with 1-7 parts of seat with double holes, 1-7 parts of seat with double holes are symmetrically connected with 1-14 parts of water tank, 1-5 parts of sliding rod are connected with 1-8 parts of connecting seat, 1-8 parts of connecting seat are connected with 1-20 parts of valve with, the sliding cavity 1-24 is arranged on the water tank 1-14, the connecting pipe 1-9 connects the water tank 1-14 and the buffer tank 1-10, the buffer tank 1-10 is connected and communicated with the U-shaped pipe 1-11, the U-shaped pipe 1-11 is connected and communicated with the buffer tank I1-12, the buffer tank I1-12 is connected and communicated with the connecting pipe I1-13, the connecting pipe I1-13 is connected and communicated with the water tank 1-14, the connecting seat I1-15 is connected with the sliding rod I1-16, the sliding rod I1-16 is connected with the double-hole seat 1-7 in a sliding way, the spring I1-17 is sleeved on the sliding rod I1-16, the spring I1-17 is abutted against the double-hole seat 1-7 in a belt and the matching seat A1-18, the matching seat A1-18 is connected with the sliding rod I1-16, the matching seat A1-18 is contacted with the cam 1-, an inlet pipe 1-19 with a flange is arranged on a water tank 1-14, an accelerating wheel 1-21 is connected with a cam 1-3 with a shaft, the cam 1-3 with a shaft is rotatably connected with the water tank 1-14, a valve I1-22 with a rod is connected with a connecting seat I1-15, a valve I1-22 with a rod is slidably connected with a sliding cavity I1-25, the sliding cavity I1-25 is arranged on the water tank 1-14, a water outlet pipe 1-23 is arranged on the water tank 1-14, before the device is used, a water pipe which can continuously feed water is required to be externally connected with the inlet pipe 1-19 with a flange, the U-shaped pipe 1-11 and the water tank 1-14 are filled with water, then when an unmanned aerial vehicle lands on the supporting platform 2-10, the supporting platform 2-10 is driven to descend due to the gravity, when the supporting platform 2-10 descends, because the magnets 2-11 and the magnets I2-19 attract each other, the supporting platform 2-10 can be continuously descended until the plug 2-12 is communicated with the socket 2-18, at the moment, the motor 1-1 operates, the motor 1-1 can drive the cam with the shaft 1-3 to rotate through the coupler 1-2, the cam with the shaft 1-3 can drive the accelerating pulley 1-21 to rotate, the rotation of the accelerating pulley 1-21 is placed clockwise when viewed from the motor 1-1 to the accelerating pulley 1-21, so that the rotation of the accelerating pulley 1-21 can accelerate the water tank 1-14, water enters the buffer tank 1-10 from the connecting pipe 1-9 from the water tank 1-14, then circulates into the buffer tank I1-12 from the U-shaped pipe 1-11 for one circle, and then flows back into the water tank 1-14 through the connecting pipe I1-13, in the process, the cam 1-3 with the shaft rotates to continuously push the matching seats 1-4 and the matching seats A1-18 at two sides, the matching seats 1-4 are pushed to drive the valve with the rod 1-20 to move through the sliding rods 1-5 and the connecting seats 1-8, so that water of an external water pipe can enter the water tanks 1-14 and then reset under the elastic force of the springs 1-6, so that new cold water can be intermittently supplemented into the water tanks 1-14, the matching seats A1-18 are pushed to drive the valve with the rod I1-22 to move through the sliding rods I1-16 and the connecting seats I1-15, so that the water in the water tanks 1-14 can leak out of the water outlet pipes 1-23 and then reset under the elastic force of the springs I1-17, because the supplemented cold water is accelerated to circulate, the water flowing out is the water which circulates back, so the temperature of the water can be kept all the time, and the effect of cooling is achieved.
The third concrete implementation mode:
the following describes the present embodiment with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, and the present embodiment further describes the present embodiment, where the lifting platform mechanism 2 includes a servo motor 2-1, a motor pulley 2-2, a belt 2-3, a pulley I2-4, a lead screw 2-5, a lifting platform 2-6, a connection seat a2-7, a slide column 2-8, a return spring 2-9, a support platform 2-10, a magnet 2-11, a plug 2-12, a rack 2-13, a step rod 2-14, a spring 2-15, a magnet seat 2-16, a repelling magnet 2-17, a socket 2-18, a magnet I2-19, a magnet seat I2-20, a magnet seat I2-13, The hydraulic cylinder 2-21, the perforated seat 2-22, the servo motor 2-1 is connected with the motor belt pulley 2-2, the motor belt pulley 2-2 is connected with the belt 2-3 in a friction mode, the belt 2-3 is connected with the belt pulley I2-4 in a friction mode, the motor belt pulley 2-2 and the belt pulley I2-4 are connected with the screw rod 2-5, the screw rod 2-5 is connected with the lifting platform 2-6 in a threaded mode, the connecting seat A2-7 is connected with the sliding column 2-8, the sliding column 2-8 is connected with the lifting platform 2-6 in a sliding mode, the sliding column 2-8 is connected with the supporting platform 2-10, the reset spring 2-9 is sleeved on the sliding column 2-8, two ends of the reset spring 2-9 are connected to the supporting platform 2-10 and the lifting platform 2-6, the magnets 2-11 are symmetrically arranged, the rack 2-13 is arranged at two sides of the lifting platform 2-6, the ladder bar 2-14 is connected with the perforated seat 2-22 in a sliding way, the perforated seat 2-22 is connected with the lifting platform 2-6, the spring 2-15 is sleeved on the ladder bar 2-14, two ends of the spring are connected with the perforated seat 2-22 and the ladder bar 2-14, the ladder bar 2-14 is connected with the magnet seat 2-16, the mutual exclusion magnet 2-17 is connected with the magnet seat 2-16, the socket 2-18 is arranged right below the plug 2-12 and is connected with the lifting platform 2-6, the magnets I2-19 are symmetrically arranged on the magnet seat I2-20, the magnet seat I2-20 is connected with the lifting platform 2-6, the hydraulic cylinder 2-21 is connected with the magnet seat 2-16, the hydraulic cylinder 2-21 is connected with the lifting platform 2-6, the servo motor 2-1 is operated to drive the motor belt pulley 2-2 to rotate, the motor belt pulley 2-2 drives the belt pulley I2-4 to synchronously rotate through the belt 2-3, the motor belt pulley 2-2 and the belt pulley I2-4 drive the screw rod 2-5 to rotate, the screw rod 2-5 drives the lifting platform 2-6 to descend so as to drive the unmanned aerial vehicle to descend, then the servo motor I3-4 is operated to drive the belt pulley A3-5 to rotate, the belt pulley A3-5 drives the belt pulley B3-8 to synchronously rotate through the belt A3-6 so as to synchronously rotate the bidirectional screw rods 3-10 on two sides, the bidirectional screw rods 3-10 drive the two movable doors 3-9 to approach each other so as to complete the protection of the unmanned aerial vehicle, when the cooling needs to be stopped, the magnet seats 2-16 can be pushed through the hydraulic cylinders 2-21, the magnet seat 2-16 will drive the mutual exclusion magnet 2-17 to move between the magnet 2-11 and the magnet I2-19, so the mutual exclusion force will drive the magnet 2-11 to move upwards to match with the elastic force of the return spring 2-9 to disconnect the plug 2-12 and the socket 2-18, thereby stopping the motor 1-1.
The fourth concrete implementation mode:
referring to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, fig. 15, the present embodiment further illustrates the present embodiment, in which the fuselage mechanism 3 includes a base 3-1, a box body 3-2, a motor base 3-3, a servo motor I3-4, a pulley A3-5, a belt A3-6, a through hole 3-7, a pulley B3-8, a movable door 3-9, a bidirectional screw 3-10, a sliding groove track 3-11, a motor base A3-12, a wind wheel 3-13, a shaft gear 3-14, a wind wheel groove 3-15, a vertical groove 3-16, a vertical moving groove 3-17, the base 3-1 is connected to the box body 3-2, the box body 3-2 is connected with the motor base 3-3, the motor base 3-3 is connected with the servo motor I3-4, the servo motor I3-4 is connected with the belt pulley A3-5, the belt pulley A3-5 is connected with the belt A3-6 in a friction mode, the belt A3-6 is connected with the belt pulley B3-8 in a friction mode, the through hole 3-7 is formed in the box body 3-2, the belt pulley A3-5 and the belt pulley B3-8 are both connected with the bidirectional screw rod 3-10, the bidirectional screw rod 3-10 is rotatably connected with the track with the sliding groove 3-11, the track with the sliding groove 3-2 is connected with the box body 3-2, the bidirectional screw rod 3-10 is connected with the movable door 3-9 in a sliding mode, the movable door 3-9 is connected with the bidirectional screw rod 3-10 in a threaded mode, the motor base A3-, the wind wheel 3-13 is connected with the gear 3-14 with the shaft, the gear 3-14 with the shaft is rotationally connected with the box body 3-2, the wind wheel groove 3-15 is arranged on the box body 3-2, the wind wheel 3-13 is arranged in the wind wheel groove 3-15, the gear 3-14 with the shaft is arranged in the vertical groove 3-16, the vertical groove 3-16 is symmetrically arranged on the box body 3-2, the vertical moving groove 3-17 is symmetrically arranged on the box body 3-2, the base 3-1 is connected with the servo motor 2-1 and the servo motor 2-1, the screw rod 2-5 is rotationally connected with the box body 3-2, the lifting platform 2-6 is slidably connected with the vertical moving groove 3-17, the rack 2-13 is slidably connected with the vertical groove 3-16, the rack 2-13 is engaged with the gear 3-14 with the shaft, the U-shaped pipe 1-11 is inserted into the through hole 3-7 and connected with the box body 3-2, the water tank 1-14 is connected with the box body 3-2, in the descending process of the lifting platform 2-6, the lifting platform 2-6 can extrude air below the lifting platform 2-6, so that the air is upwards discharged from the vertical groove 3-16, meanwhile, the descending of the lifting platform 2-6 can drive the rack 2-13 to descend, the rack 2-13 can drive the gear with the shaft 3-14 to rotate, the gear with the shaft 3-14 can drive the wind wheel 3-13 to rotate, and the wind wheel 3-13 can accelerate the airflow flowing outwards, so that the air is discharged.
The fifth concrete implementation mode:
the present embodiment will be described with reference to fig. 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, and 15, and the present embodiment further describes the first embodiment in which the magnets 2-11 and the magnets I2-19 attract each other, and the repulsive magnets 2-17 and the magnets 2-11 and the magnets I2-19 repel each other.
The sixth specific implementation mode:
the present embodiment will be described below with reference to fig. 1, fig. 2, fig. 3, fig. 4, fig. 5, fig. 6, fig. 7, fig. 8, fig. 9, fig. 10, fig. 11, fig. 12, fig. 13, fig. 14, and fig. 15, and the present embodiment further describes the present embodiment, in which after the plugs 2 to 12 are connected to the sockets 2 to 18, the power supply of the motor 1-1 is connected.
The working principle of the device is as follows: the equipment can start to cool the equipment after the unmanned aerial vehicle falls, the equipment can be used by needing a water pipe which is externally connected with a flange inlet pipe 1-19 and can continuously feed water, water is filled in a U-shaped pipe 1-11 and a water tank 1-14, then when the unmanned aerial vehicle falls on a supporting platform 2-10, the supporting platform 2-10 is driven to fall due to gravity, when the supporting platform 2-10 falls to one end, the supporting platform 2-10 can continue to fall until a plug 2-12 is communicated with a socket 2-18 due to mutual attraction of a magnet 2-11 and a magnet I2-19, at the moment, a motor 1-1 operates, the motor 1-1 can drive a shaft cam 1-3 to rotate through a coupler 1-2, the shaft cam 1-3 can drive an accelerating pulley 1-21 to rotate, the rotation of the accelerating wheels 1-21 is placed clockwise when seen from the motor 1-1 to the accelerating wheels 1-21, so that the water tanks 1-14 are accelerated by the rotation of the accelerating wheels 1-21, water enters the buffer tanks 1-10 from the water tanks 1-14, circulates a circle from the U-shaped pipes 1-11 to the buffer tanks I1-12 and then flows back to the water tanks 1-14 through the connecting pipes I1-13, in the process, the cam 1-3 with the shaft continuously pushes the matching seats 1-4 and the matching seats A1-18 at two sides, the matching seats 1-4 are pushed to drive the valves with the rods 1-20 to move through the sliding rods 1-5 and the connecting seats 1-8, and water of external water pipes can enter the water tanks 1-14, then the water tank is reset under the action of the elastic force of the springs 1 to 6, so that new cold water can be intermittently supplemented to enter the water tanks 1 to 14, the matching seat A1 to 18 can drive the valve I1 to 22 with the rod to move through the sliding rod I1 to 16 and the connecting seat I1 to 15 when being pushed, so that the water in the water tanks 1 to 14 can leak out from the water outlet pipes 1 to 23, and then the water tank is reset under the action of the elastic force of the springs I1 to 17, because the supplemented cold water is accelerated to circulate, and the outflowing water is circulated water, the temperature of the water can be kept all the time, and the effect of cooling is achieved; the device can protect the unmanned aerial vehicle in the device, the servo motor 2-1 operates to drive the motor belt pulley 2-2 to rotate, the motor belt pulley 2-2 drives the belt pulley I2-4 to synchronously rotate through the belt 2-3, the motor belt pulley 2-2 and the belt pulley I2-4 drive the screw rod 2-5 to rotate, the screw rod 2-5 drives the lifting platform 2-6 to descend so as to drive the unmanned aerial vehicle to descend, then the servo motor I3-4 is operated to drive the belt pulley A3-5 to rotate, the belt pulley A3-5 drives the belt pulley B3-8 to synchronously rotate through the belt A3-6, therefore, the bidirectional screw rods 3-10 on the two sides rotate synchronously, and the bidirectional screw rods 3-10 drive the two movable doors 3-9 to approach each other, so that the unmanned aerial vehicle is protected; the equipment can discharge air in the equipment, in the process that the lifting platform 2-6 descends, the lifting platform 2-6 can extrude the air below the lifting platform 2-6 to enable the air to be upwards discharged from the vertical grooves 3-16, meanwhile, the descending of the lifting platform 2-6 can drive the racks 2-13 to descend, the racks 2-13 can drive the gear with shafts 3-14 to rotate, the gear with shafts 3-14 can drive the wind wheels 3-13 to rotate, and the wind wheels 3-13 can accelerate the air flow flowing outwards to discharge the air; the equipment can stop cooling, when the equipment needs to stop cooling, the magnet seats 2-16 can be pushed through the hydraulic cylinders 2-21, the magnet seats 2-16 can drive the mutually exclusive magnets 2-17 to move between the magnets 2-11 and the magnets I2-19, so that the mutually exclusive force can drive the magnets 2-11 to move upwards to match with the elastic force of the return springs 2-9, the plugs 2-12 can be disconnected with the sockets 2-18, and the motor 1-1 can stop rotating.
It is to be understood that the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and that various changes, modifications, additions and substitutions which are within the spirit and scope of the present invention and which may be made by those skilled in the art are also within the scope of the present invention.
Claims (3)
1. The utility model provides an unmanned aerial vehicle automatic rising storage facilities, includes cooling body (1), elevating platform mechanism (2), fuselage mechanism (3), its characterized in that: the cooling mechanism (1) is connected with the machine body mechanism (3), and the machine body mechanism (3) is connected with the lifting platform mechanism (2);
the cooling mechanism (1) comprises a motor (1-1), a coupler (1-2), a cam with a shaft (1-3), a matching seat (1-4), a sliding rod (1-5), a spring (1-6), a seat with double holes (1-7), a connecting seat (1-8), a connecting pipe (1-9), a buffer box (1-10), a U-shaped pipe (1-11), a buffer box I (1-12), a connecting pipe I (1-13), a water tank (1-14), a connecting seat I (1-15), a sliding rod I (1-16), a spring I (1-17), a matching seat A (1-18), an inlet pipe with a flange (1-19), a valve with a rod (1-20), an accelerating wheel (1-21), a valve with a rod I (1-22), A water outlet pipe (1-23), a sliding cavity (1-24) and a sliding cavity I (1-25), wherein a motor (1-1) is connected with a coupler (1-2), the coupler (1-2) is connected with a cam with a shaft (1-3), the cam with a shaft (1-3) is hinged with a matching seat (1-4), the matching seat (1-4) is connected with a sliding rod (1-5), a spring (1-6) is sleeved on the sliding rod (1-5), two ends of the spring are connected with the matching seat (1-4) and a seat with double holes (1-7), the sliding rod (1-5) is connected with the seat with double holes (1-7) in a sliding way, the seat with double holes (1-7) is symmetrically connected with a water tank (1-14), the sliding rod (1-5) is connected with a connecting seat (1-8), the connecting seat (1-8) is connected with the valve (1-20) with the rod, the valve (1-20) with the rod is connected with the sliding cavity (1-24) in a sliding way, the sliding cavity (1-24) is arranged on the water tank (1-14), the water tank (1-14) and the buffer tank (1-10) are communicated through the connecting pipe (1-9), the buffer tank (1-10) is connected and communicated with the U-shaped pipe (1-11), the U-shaped pipe (1-11) is connected and communicated with the buffer tank I (1-12), the buffer tank I (1-12) is connected and communicated with the connecting pipe I (1-13), the connecting pipe I (1-13) is connected and communicated with the water tank (1-14), the connecting seat I (1-15) is connected with the sliding rod I (1-16), the sliding rod I (1-16) is connected with the seat (1-7) with the double holes in a sliding way, the spring I (1-17) is sleeved on the sliding rod I (1-16), the spring I (1-17) is abutted against the double-hole seat (1-7) and the matching seat A (1-18), the matching seat A (1-18) is connected with the sliding rod I (1-16), the matching seat A (1-18) is contacted with the cam (1-3) with a shaft, the inlet pipe (1-19) with a flange is arranged on the water tank (1-14), the accelerating wheel (1-21) is connected with the cam (1-3) with the shaft, the cam (1-3) with the shaft is rotatably connected with the water tank (1-14), the valve I (1-22) with a rod is connected with the connecting seat I (1-15), the valve I (1-22) with the rod is slidably connected with the sliding cavity I (1-25), the sliding cavity I (1-25) is arranged on the water tank (1-14), the water outlet pipes (1-23) are arranged on the water tanks (1-14);
the lifting platform mechanism (2) comprises a servo motor (2-1), a motor belt pulley (2-2), a belt (2-3), a belt pulley I (2-4), a lead screw (2-5), a lifting platform (2-6), a connecting seat A (2-7), a sliding column (2-8), a reset spring (2-9), a supporting platform (2-10), a magnet (2-11), a plug (2-12), a rack (2-13), a stepped rod (2-14), a spring (2-15), a magnet seat (2-16), a mutual exclusion magnet (2-17), a socket (2-18), a magnet I (2-19), a magnet seat I (2-20), a hydraulic cylinder (2-21) and a hole seat (2-22), wherein the servo motor (2-1) is connected with the motor belt pulley (2-2), the motor belt pulley (2-2) is in friction connection with the belt (2-3), the belt (2-3) is in friction connection with the belt pulley I (2-4), the motor belt pulley (2-2) and the belt pulley I (2-4) are both in friction connection with the lead screw (2-5), the lead screw (2-5) is in threaded connection with the lifting platform (2-6), the connecting seat A (2-7) is connected with the sliding column (2-8), the sliding column (2-8) is in sliding connection with the lifting platform (2-6), the sliding column (2-8) is connected with the supporting platform (2-10), the reset spring (2-9) is sleeved on the sliding column (2-8), two ends of the reset spring (2-9) are connected onto the supporting platform (2-10) and the lifting platform (2-6), the magnets (2-11) are symmetrically arranged on the supporting platform (2-10), the gear racks (2-13) are arranged on two sides of the lifting platform (2-6), the ladder rods (2-14) are connected with the hole seats (2-22) in a sliding mode, the hole seats (2-22) are connected with the lifting platform (2-6), the springs (2-15) are sleeved on the ladder rods (2-14) and are connected with the hole seats (2-22) and the ladder rods (2-14), the ladder rods (2-14) are connected with the magnet seats (2-16), the mutual exclusion magnets (2-17) are connected with the magnet seats (2-16), the sockets (2-18) are located right below the plugs (2-12) and are connected onto the lifting platform (2-6), the magnets I (2-19) are symmetrically arranged on the magnet seats I (2-20), the magnet seats I (2-20) are connected with the lifting platform (2-6), the hydraulic cylinder (2-21) is connected with the magnet seat (2-16), and the hydraulic cylinder (2-21) is connected with the lifting platform (2-6);
the machine body mechanism (3) comprises a base (3-1), a box body (3-2), a motor base (3-3), a servo motor I (3-4), a belt pulley A (3-5), a belt A (3-6), through holes (3-7), a belt pulley B (3-8), a movable door (3-9), a bidirectional screw rod (3-10), a track with a sliding groove (3-11), a motor base A (3-12), a wind wheel (3-13), a gear with a shaft (3-14), a wind wheel groove (3-15), a vertical groove (3-16) and a vertical moving groove (3-17), wherein the base (3-1) is connected with the box body (3-2), the box body (3-2) is connected with the motor base (3-3), the motor base (3-3) is connected with a servo motor I (3-4), the servo motor I (3-4) is connected with a belt pulley A (3-5), the belt pulley A (3-5) is in friction connection with a belt A (3-6), the belt A (3-6) is in friction connection with a belt pulley B (3-8), a through hole (3-7) is formed in the box body (3-2), the belt pulley A (3-5) and the belt pulley B (3-8) are both connected with a bidirectional screw rod (3-10), the bidirectional screw rod (3-10) is rotatably connected with a track (3-11) with a chute, the track (3-11) with the chute is connected with the box body (3-2), the bidirectional screw rod (3-10) is in sliding connection with the movable door (3-9), the movable door (3-9) is in threaded connection with the bidirectional screw rod (3-10), the motor base A (3-12) is connected with the base (3-1), the wind wheel (3-13) is connected with the gear with a shaft (3-14), the gear with a shaft (3-14) is rotationally connected with the box body (3-2), the wind wheel grooves (3-15) are arranged on the box body (3-2), the wind wheel (3-13) is arranged in the wind wheel grooves (3-15), the gear with a shaft (3-14) is arranged in the vertical grooves (3-16), the vertical grooves (3-16) are symmetrically arranged on the box body (3-2), the vertical moving grooves (3-17) are symmetrically arranged on the box body (3-2), the base (3-1) is connected with the servo motor (2-1) and the servo motor (2-1), and the screw rod (2-5) is rotationally connected with the box body (3-2), the lifting platform (2-6) is connected with the vertical moving groove (3-17) in a sliding mode, the rack (2-13) is connected with the vertical groove (3-16) in a sliding mode, the rack (2-13) is meshed with the gear (3-14) with the shaft, the U-shaped pipe (1-11) is inserted into the through hole (3-7) and connected with the box body (3-2), and the water tank (1-14) is connected with the box body (3-2).
2. The unmanned aerial vehicle automatic rising storage facilities of claim 1, characterized in that: the magnets (2-11) and the magnets I (2-19) attract each other, and the mutually exclusive magnets (2-17) and the magnets (2-11) and the magnets I (2-19) repel each other.
3. The unmanned aerial vehicle automatic rising storage facilities of claim 1, characterized in that: after the plug (2-12) is connected with the socket (2-18), the power supply of the motor (1-1) is connected.
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| CN111776442A (en) * | 2020-06-04 | 2020-10-16 | 兰钰识 | Unmanned aerial vehicle deposits case |
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| CN107985624A (en) * | 2017-12-25 | 2018-05-04 | 成都壹橙科技有限公司 | A kind of unmanned plane supporting rack |
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