CN210063389U - Unmanned aerial vehicle's fixed strorage device - Google Patents
Unmanned aerial vehicle's fixed strorage device Download PDFInfo
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- CN210063389U CN210063389U CN201822249782.9U CN201822249782U CN210063389U CN 210063389 U CN210063389 U CN 210063389U CN 201822249782 U CN201822249782 U CN 201822249782U CN 210063389 U CN210063389 U CN 210063389U
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Abstract
The utility model discloses an unmanned aerial vehicle's fixed strorage device, including synthesizing unmanned aerial vehicle application platform, synthesize the switch door that is provided with two divisions on the unmanned aerial vehicle application platform, synthesize unmanned aerial vehicle application platform's top movable mounting has the skylight, the skylight sets up for bilateral symmetry, synthesize unmanned aerial vehicle application platform's top for shutting down the platform, it has the remote control unmanned aerial vehicle to park on the platform to shut down. The utility model has the advantages that: not only can let unmanned aerial vehicle be in the state of preparing to take off at any time but also simplify the operation flow, can also reduce the space of synthesizing the unmanned aerial vehicle platform simultaneously.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle's fixed strorage device.
Background
The unmanned aerial vehicle application platform is now synthesized and is developed rapidly. And when synthesizing unmanned aerial vehicle application platform transportation and dormancy state, need protect the unmanned aerial vehicle in the platform, avoid unmanned aerial vehicle to damage. The utility model discloses solve this kind of problem exactly, through install a fixed unmanned aerial vehicle's device additional in synthesizing the platform, reach the effect of protection and location.
SUMMERY OF THE UTILITY MODEL
The utility model provides a technical problem lie in overcoming the defect that prior art exists, provide an unmanned aerial vehicle's fixed strorage device. Unmanned aerial vehicle's fixed strorage device not only can let unmanned aerial vehicle be in the state of preparing to take off at any time but also has simplified the operation flow, can also reduce the space of synthesizing the unmanned aerial vehicle platform simultaneously.
In order to achieve the above object, the utility model provides a following technical scheme:
the utility model provides an unmanned aerial vehicle's fixed strorage device, includes and synthesizes unmanned aerial vehicle application platform, synthesize the switch door that is provided with two divisions on the unmanned aerial vehicle application platform, synthesize unmanned aerial vehicle application platform's top movable mounting has the skylight, the skylight sets up for bilateral symmetry, synthesize unmanned aerial vehicle application platform's top is for shutting down the platform, it has parked remote control unmanned aerial vehicle on the platform to shut down, shut down the platform and include the track groove, and the track groove runs through the last lower of shutting down the platform, it has servo drive arrangement still to fix mounting in the bottom of shutting down the platform, fixed mounting has the stopper on the drive arrangement, stopper activity joint remote control unmanned aerial vehicle, the stopper is located the top of shutting down the platform.
Preferably, drive arrangement includes servo motor, servo motor's power take off end fixed connection rotation axis, the equal vertical transmission in both ends of rotation axis is connected with synchronous belt, fixed mounting has the slider on the synchronous belt, dispose the guiding axle on the slider, the direction of guiding axle is the same with synchronous belt's the direction that sets up and is located synchronous belt under, stopper fixed mounting and slider are last.
Preferably, the track grooves are arranged in a shape like a Chinese character 'jing', the synchronous belts are positioned in the track grooves, and the synchronous belts are designed in a mode of being staggered up and down at the intersection of the track grooves.
Preferably, the inner wall both sides of synthesizing unmanned aerial vehicle application platform all are provided with single-axis manipulator, the inner chamber bottom of synthesizing unmanned aerial vehicle application platform is provided with battery package and battery controller, battery package and battery controller set up side by side and the top is provided with the protection apron, the top fixed mounting of protection apron has the horn locating part.
Preferably, the horn locating part has four montants of fixed mounting at the protection apron and fills electric pile and constitute, wherein the draw-in groove that is used for joint remote control unmanned aerial vehicle is seted up at the top of montant, is provided with the elasticity card in the both sides of draw-in groove.
Preferably, the bottom of remote control unmanned aerial vehicle is provided with the supporting legs, the supporting legs comprises two "T" type poles that the symmetry set up, has all cup jointed the podotheca at the bottom both ends of "T" type pole, and two mutual symmetrical supporting legs are through the carbon pipe interconnect of podotheca fixed connection.
Preferably, the single-shaft manipulator mainly comprises a single-shaft driver and a manipulator, wherein one end of the manipulator, which is far away from the single-shaft driver, is forked into a Y-shaped structure.
Compared with the prior art, the beneficial effects of the utility model are that: not only can let unmanned aerial vehicle be in the state of preparing to take off at any time but also simplify the operation flow, can also reduce the space of synthesizing the unmanned aerial vehicle platform simultaneously.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic structural view of the shutdown platform of the present invention;
FIG. 3 is a schematic structural view of the driving device of the present invention;
FIG. 4 is a schematic view of the internal structure of the present invention;
FIG. 5 is a schematic view of the arm limiting member of the present invention;
FIG. 6 is a schematic view of the structure of the top elastic card of the arm position limiter of the present invention;
fig. 7 is a schematic structural view of the remote control unmanned aerial vehicle of the present invention;
fig. 8 is a schematic view of the fixing mode of the remote control unmanned aerial vehicle of the present invention;
fig. 9 is a schematic diagram of the structure of the limiting block of the present invention.
Reference numbers in the figures: 1 synthesize unmanned aerial vehicle application platform, 2 switch doors, 3 skylights, 4 remote control unmanned aerial vehicle, 401 podotheca, 402 carbon pipe, 5 platforms that stop, 501 track groove, 6 drive arrangement, 601 servo motor, 602 rotation axis, 603 synchronous belt, 604 slider, 605 guiding axle, 7 stopper, 8 unipolar manipulators, 801 unipolar driver, 802 manipulator, 9 battery package, 10 battery controller, 11 horn locating parts, 12 protection cover boards, 13 fill electric pile, 14 elasticity cards.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-8, the present invention provides a technical solution: a fixed storage device of an unmanned aerial vehicle comprises a comprehensive unmanned aerial vehicle application platform 1, wherein a double-opening switch door 2 is arranged on the comprehensive unmanned aerial vehicle application platform 1, a skylight 3 is movably arranged at the top of the comprehensive unmanned aerial vehicle application platform 1, the skylight 3 is arranged in a bilateral symmetry manner, a shutdown platform 5 is arranged at the top end of the comprehensive unmanned aerial vehicle application platform 1, a remote-controlled unmanned aerial vehicle 4 is parked on the shutdown platform 5, support legs are arranged at the bottom of the remote-controlled unmanned aerial vehicle 4 and consist of two symmetrically arranged T-shaped rods, foot sleeves 401 are sleeved at two ends of the bottom of the T-shaped rods, the two mutually symmetrical support legs are mutually connected through carbon tubes 402 fixedly connected on the foot sleeves 401, and the shutdown platform 5 comprises a track groove 501, the track groove 501 penetrates through the upper bottom and the lower bottom of the shutdown platform 5, it has servo drive arrangement 6 to shut down still fixed mounting in the bottom of platform 5, fixed mounting has stopper 7 on drive arrangement 6, stopper 7 activity joint remote control unmanned aerial vehicle 4, stopper 7 is located the top of shutting down platform 5, and it is worth noting, the inner wall both sides of synthesizing unmanned aerial vehicle application platform 1 all are provided with unipolar manipulator 8, wherein, unipolar manipulator 8 mainly comprises unipolar driver 801 and manipulator 802, wherein the one end fork that unipolar driver 801 was kept away from to manipulator 802 is "Y" style of calligraphy structure, the inner chamber bottom of synthesizing unmanned aerial vehicle application platform 1 is provided with battery package 9 and battery controller 10, battery package 9 and battery controller 10 set up side by side and the top is provided with protective cover plate 12, protective cover plate 12's top fixed mounting has horn locating part 11.
It is worth noting that the driving device 6 comprises a servo motor 601, a power output end of the servo motor 601 is fixedly connected with a rotating shaft 602, two ends of the rotating shaft 602 are vertically connected with a synchronous belt 603 in a transmission manner, a sliding block 604 is fixedly installed on the synchronous belt 603, a guide shaft 605 is configured on the sliding block 604, the direction of the guide shaft 605 is the same as the setting direction of the synchronous belt 603 and is located right below the synchronous belt 603, a limiting block 7 is fixedly installed on the sliding block 604, the track grooves 501 are arranged in a shape like a Chinese character 'jing', the synchronous belt 603 is located in the track grooves 501, and the synchronous belt 603 is designed in a vertically staggered manner at the intersection of the track grooves 501.
It is worth noting that the horn locating part 11 is provided with four vertical rods fixedly mounted on the protective cover plate 12 and a charging pile 13, wherein a clamping groove used for clamping the remote control unmanned aerial vehicle 4 is formed in the top of each vertical rod, and elastic clamping pieces 14 are arranged on two sides of the clamping groove.
A platform fixing method for a fixed storage device of an unmanned aerial vehicle comprises the following specific steps:
the first embodiment is as follows:
s1: when the remote control unmanned aerial vehicle 4 lands in the shutdown platform 5, the driving device 6 moving in the front-back direction pushes the unmanned remote control 4 to the middle position, so that the limiting blocks 7 in the front-back direction can realize front-back fixation;
s2: after the previous step is completed, the driving device 6 moving in the left-right direction pushes the remote control unmanned aerial vehicle 4 to the middle position of the shutdown platform 5, so that the limiting blocks 7 on the left side and the right side realize the left-right direction fixation;
s3: when the remote control unmanned aerial vehicle 4 is fixed on the shutdown platform 5, the shutdown platform 5 starts to descend through the single-shaft manipulator 8, and when the platform descends to a preset height, the arm limiting parts 11 extend through the shutdown platform 5 to fix the four arms of the remote control unmanned aerial vehicle 4, so that the whole aircraft is fixed.
Example two:
the first step is as follows: when the remote control unmanned aerial vehicle 4 lands in the shutdown platform 5, the driving device 6 moving in the front-back direction pushes the unmanned remote control 4 to the middle position, so that the limiting blocks 7 in the front-back direction can realize front-back fixation;
the second step is that: after the previous step is completed, the driving device 6 moving in the left-right direction pushes the remote control unmanned aerial vehicle 4 to the middle position of the shutdown platform 5, so that the limiting blocks 7 on the left side and the right side realize the left-right direction fixation;
the third step: when the remote-controlled unmanned aerial vehicle 4 is fixed to the stopping platform 5, the stopping platform 5 starts to descend by the single-axis robot 8, and when the platform descends to a predetermined height, the left and right sides of the remote-controlled unmanned aerial vehicle 4 are respectively extended by one robot 802 through the single-axis driver 801 to grasp the four arms of the aircraft.
Principle of operation
The unmanned aerial vehicle is fixed by the shutdown platform 5 in four different directions through the servo motor 601 and the synchronous belt 603, the unmanned aerial vehicle is pushed to the middle part of the shutdown platform 5 through the servo motor 601, and after the pushing process is finished, the two supporting legs of the unmanned aerial vehicle can be just buckled by the limiting blocks 7 on the synchronous belt 603; after fixed the accomplishing, can also descend whole shut down platform 5 together with unmanned aerial vehicle through single-axis manipulator 8, not only can fix through horn locating part 11 after descending, can also fix through manipulator 802, then can cooperate and fill electric pile 13 and charge to unmanned aerial vehicle.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (7)
1. The utility model provides an unmanned aerial vehicle's fixed strorage device, includes synthesizes unmanned aerial vehicle application platform (1), its characterized in that: the integrated unmanned aerial vehicle application platform (1) is provided with double-open switch doors (2), the top of the integrated unmanned aerial vehicle application platform (1) is movably provided with a skylight (3), the skylight (3) is arranged in a bilateral symmetry manner, the top end of the integrated unmanned aerial vehicle application platform (1) is provided with a shutdown platform (5), and a remote control unmanned aerial vehicle (4) is parked on the shutdown platform (5); shut down platform (5) and include track groove (501), and track groove (501) run through the upper and lower end of shutting down platform (5), shut down the bottom of platform (5) still fixed mounting have servo drive arrangement (6), fixed mounting has stopper (7) on drive arrangement (6), stopper (7) activity joint remote control unmanned aerial vehicle (4), stopper (7) are located the top of shutting down platform (5).
2. The fixed storage device of unmanned aerial vehicle of claim 1, wherein: drive arrangement (6) include servo motor (601), power take off end fixed connection rotation axis (602) of servo motor (601), the equal vertical transmission in both ends of rotation axis (602) is connected with synchronous belt (603), fixed mounting has slider (604) on synchronous belt (603), dispose guiding axle (605) on slider (604), the direction of guiding axle (605) is the same with the direction that sets up of synchronous belt (603) and is located synchronous belt (603) under, stopper (7) fixed mounting and slider (604) are last.
3. The fixed storage device of unmanned aerial vehicle of claim 2, wherein: the track groove (501) is arranged in a shape like a Chinese character 'jing', the synchronous belt (603) is located in the track groove (501), and the synchronous belt (603) is designed in a mode of being staggered up and down at the intersection of the track groove (501).
4. The fixed storage device of unmanned aerial vehicle of claim 1, wherein: synthesize the inner wall both sides of unmanned aerial vehicle application platform (1) and all be provided with unipolar manipulator (8), the inner chamber bottom of synthesizing unmanned aerial vehicle application platform (1) is provided with battery package (9) and battery controller (10), battery package (9) and battery controller (10) set up side by side and the top is provided with protective cover board (12), the top fixed mounting of protective cover board (12) has horn locating part (11).
5. The fixed storage device of unmanned aerial vehicle of claim 4, wherein: the horn locating part (11) have by four fixed mounting at the montant of protection apron (12) with fill electric pile (13) and constitute, wherein the draw-in groove that is used for joint remote control unmanned aerial vehicle (4) is seted up at the top of montant, be provided with elasticity card (14) in the both sides of draw-in groove.
6. The fixed storage device of unmanned aerial vehicle of claim 1, wherein: the bottom of remote control unmanned aerial vehicle (4) is provided with the supporting legs, the supporting legs comprises two "T" type poles that the symmetry set up, has all cup jointed podotheca (401) at the bottom both ends of "T" type pole, and two mutual symmetrical supporting legs pass through carbon pipe (402) interconnect of fixed connection on podotheca (401).
7. The fixed storage device of unmanned aerial vehicle of claim 4, wherein: the single-shaft mechanical arm (8) mainly comprises a single-shaft driver (801) and a mechanical arm (802), wherein one end, far away from the single-shaft driver (801), of the mechanical arm (802) is forked into a Y-shaped structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822249782.9U CN210063389U (en) | 2018-12-29 | 2018-12-29 | Unmanned aerial vehicle's fixed strorage device |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201822249782.9U CN210063389U (en) | 2018-12-29 | 2018-12-29 | Unmanned aerial vehicle's fixed strorage device |
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| CN210063389U true CN210063389U (en) | 2020-02-14 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502040A (en) * | 2018-12-29 | 2019-03-22 | 深圳市多翼创新科技有限公司 | A kind of the fixation storing unit and its platform fixing means of unmanned plane |
| CN112009295A (en) * | 2020-08-14 | 2020-12-01 | 五邑大学 | Unmanned aerial vehicle independently charges and changes battery device |
| WO2022062174A1 (en) * | 2020-09-28 | 2022-03-31 | 深圳市大疆创新科技有限公司 | Location correcting apparatus and storage system for unmanned aerial vehicle |
-
2018
- 2018-12-29 CN CN201822249782.9U patent/CN210063389U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502040A (en) * | 2018-12-29 | 2019-03-22 | 深圳市多翼创新科技有限公司 | A kind of the fixation storing unit and its platform fixing means of unmanned plane |
| CN112009295A (en) * | 2020-08-14 | 2020-12-01 | 五邑大学 | Unmanned aerial vehicle independently charges and changes battery device |
| WO2022062174A1 (en) * | 2020-09-28 | 2022-03-31 | 深圳市大疆创新科技有限公司 | Location correcting apparatus and storage system for unmanned aerial vehicle |
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