CN207045776U - A kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear - Google Patents
A kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear Download PDFInfo
- Publication number
- CN207045776U CN207045776U CN201720583352.3U CN201720583352U CN207045776U CN 207045776 U CN207045776 U CN 207045776U CN 201720583352 U CN201720583352 U CN 201720583352U CN 207045776 U CN207045776 U CN 207045776U
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- China
- Prior art keywords
- ejection
- motor
- vehicle
- base
- unmanned aerial
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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- Forklifts And Lifting Vehicles (AREA)
Abstract
The utility model discloses a kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear,Including base,Battery is provided with base,Hydraulic pump and two symmetrical motors I,The main shaft of motor I is provided with contiguous block,Contiguous block is provided with strut,Strut is provided with rain cover,Hydraulic pump is provided with hydraulic cylinder,Base side is provided with charging device and controlling switch,Controlling switch is furnished with Digiplex,Base bottom is provided with lock ring,Ejection platform is hinged with base,The piston rod of hydraulic cylinder is connected with ejection platform bottom,Ejection platform is provided with solar charging panel,Motor II is provided with ejection platform,Ejection groove is provided with the middle part of ejection platform,Gear I is provided with ejection groove,Gear II and the chain for being enclosed on its outer end,Gear II is socketed on the main shaft of motor II,Fixed block is cased with chain,Fixed block is provided with U-bracket,U-bracket is provided with stopper slot and lock,This apparatus structure is simple,Easily operation,Use environment is unfettered,Make full use of solar energy.
Description
Technical field
It the utility model is related to unmanned plane and aid in supporting field, more particularly to a kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear.
Background technology
In recent years, unmanned air vehicle technique is developed rapidly.Need to be fed after unmanned plane power source depletes and (add
Oil, charging etc.), it is by manually completing, for example, being carried out to rechargeable unmanned plane to carry out power supply to unmanned plane at present
During charging, need manual operation to reclaim unmanned plane, then charged manually to unmanned plane, in the prior art, can also without one kind
The platform to be charged to unmanned plane, simultaneously for ejection shape unmanned plane, catapult-launching gear be not easily carried and one ask
Topic.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear, to solve existing skill
Caused above-mentioned multinomial defect in art.
To achieve the above object, the utility model provides following technical scheme：A kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear, bag
Base is included, battery, hydraulic pump and two symmetrical motors I are provided with the base, the main shaft of the motor I is provided with connection
Block, the contiguous block are provided with strut, and the strut is provided with rain cover, and the hydraulic pump is provided with hydraulic cylinder, the base
Side is provided with charging device and controlling switch, and the base bottom is provided with lock ring, ejection platform is hinged with the base, described
The piston rod of hydraulic cylinder is connected with ejection platform bottom, and motor II is provided with the ejection platform, is set in the middle part of the ejection platform
There is ejection groove, be provided with gear I, gear II and the chain for being enclosed on its outer end in the ejection groove, the gear II is socketed in motor
On II main shaft, fixed block is cased with the chain, the fixed block is provided with U-bracket, and the U-bracket is provided with spacing
Groove, the hydraulic pump, motor I, motor II and controlling switch and battery are electrically connected with.
Preferably, the charging device includes unmanned plane charging socket and USB.
Preferably, lock is hinged with the U-bracket.
Preferably, the ejection platform is provided with solar charging panel, and the solar charging panel electrically connects with battery
Connect.
Preferably, the controlling switch is furnished with Digiplex.
Beneficial effect using above technical scheme is：Vehicle-mounted unmanned aerial vehicle catapult-launching gear of the present utility model, utilize this dress
Device is fixed on the goods carrier of automobile by the lock ring put, in the stopper slot that the wing of unmanned plane is placed to U-bracket, Ran Houxuan
Twist lock button fixes unmanned plane, opens motor I, be rotatablely connected block, drive strut to move downward, will prevent to stopper slot opening
Canopy is shut, and makes to avoid unmanned plane from being damaged in transit, in use, opening rain cover, is opened lock, is used Digiplex
Hydraulic pump is opened in control, is risen the piston rod in hydraulic cylinder, is risen ejection platform, be then turned on unmanned plane, when appropriate
When, motor II is opened, moves fixed block brought forward U-bracket, completes ejection work, the solar charging in ejection platform
Electroplax can be that battery is powered for a long time out of doors, while the power supply stored can also be by charging device to unmanned plane or movement
Equipment charge, this apparatus structure is simple, easily operation, and use environment is unfettered, makes full use of solar energy.
Brief description of the drawings
Fig. 1 is front view of the present utility model；
Fig. 2 is side view of the present utility model；
Fig. 3 is top view of the present utility model.
Wherein, 1- bases, 2- charging devices, 3- controlling switches, 4- lock rings, 5- batteries, 6- contiguous blocks, 7- motors I, 8-
Strut, 9- rain covers, 10- hydraulic pumps, 11- hydraulic cylinders, 12- ejection platforms, 13- gears I, 14- chains, 15- motors II, 16-
Gear II, 17- fixed blocks, 18-U shape supports, 19- stopper slots, 20- lock, 21- solar charging panels, 22- ejection groove, 23- without
Line remote control.
Embodiment
Describe preferred embodiment of the present utility model in detail below in conjunction with the accompanying drawings.
Fig. 1, Fig. 2 and Fig. 3 show specific embodiment of the present utility model：A kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear, including
Base 1, the base 1 is interior to be provided with battery 5, hydraulic pump 10 and two symmetrical motors I 7, is set on the main shaft of the motor I 7
There is contiguous block 6, the contiguous block 6 is provided with strut 8, and the strut 8 is provided with rain cover 9, and the hydraulic pump 10 is provided with liquid
Cylinder pressure 11, the side of base 1 are provided with charging device 2 and controlling switch 3, and the bottom of base 1 is provided with lock ring 4, the base
Ejection platform 12 is hinged with 1, the piston rod of the hydraulic cylinder 11 is connected with the bottom of ejection platform 12, in the ejection platform 12
Provided with motor II 15, the middle part of ejection platform 12 is provided with ejection groove 22, and gear I 13, gear II are provided with the ejection groove 22
16 and the chain 14 of its outer end is enclosed on, the gear II 16 is socketed on the main shaft of motor II 15, is cased with the chain 14 solid
Determine block 17, the fixed block 17 is provided with U-bracket 18, and the U-bracket 18 is provided with stopper slot 19, the hydraulic pump 10,
Motor I 7, motor II 15 and controlling switch 3 are electrically connected with battery 5.
In the present embodiment, the charging device 2 includes unmanned plane charging socket and USB, can be set out of doors for movement
Standby charging.
In the present embodiment, lock 20 is hinged with the U-bracket 18, the unmanned plane in stopper slot 19 can be prevented after rotation
Wing rocks.
In the present embodiment, the ejection platform 12 is provided with solar charging panel 21, and the solar charging panel 21 is with storing
Battery 5 is electrically connected with, and provides continuous electric energy out of doors for battery 5.
In the present embodiment, the controlling switch 3 is furnished with Digiplex 23, easy to operation.
Based on above-mentioned, the vehicle-mounted unmanned aerial vehicle catapult-launching gear of the utility model structure, device is consolidated using the lock ring 4 of this device
It is scheduled on the goods carrier of automobile, in the stopper slot 19 that the wing of unmanned plane is placed to U-bracket 18, then rotating latch 20 to limit
The position opening of groove 19, fixes unmanned plane, opens motor I 7, is rotatablely connected block 6, drives strut 8 to move downward, by rain cover 9
Shut, make to avoid unmanned plane from being damaged in transit, in use, opening rain cover 9, open lock 20, use Digiplex
Hydraulic pump 10 is opened in 23 controls, is risen the piston rod in hydraulic cylinder 11, is risen ejection platform 12, be then turned on unmanned plane,
Proper time is waited until, motor II 15 is opened, moves the brought forward U-bracket 18 of fixed block 17, complete ejection work, ejection is flat
Solar charging panel 21 on platform 12 can be that battery 5 is powered for a long time out of doors, while the power supply stored can also be by filling
Electric installation 2 gives unmanned plane or charging of mobile devices, and this apparatus structure is simple, easily operation, and use environment is unfettered, fully profit
Use solar energy.
Above-described is only preferred embodiment of the present utility model, it is noted that for the ordinary skill of this area
For personnel, on the premise of not departing from the utility model and creating design, various modifications and improvements can be made, these all belong to
In the scope of protection of the utility model.
Claims (5)
1. a kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear, including base (1), it is characterised in that：Battery is provided with the base (1)
(5), hydraulic pump (10) and two symmetrical motors I (7), the main shaft of the motor I (7) are provided with contiguous block (6), the connection
Block (6) is provided with strut (8), and the strut (8) is provided with rain cover (9), and the hydraulic pump (10) is provided with hydraulic cylinder (11),
Base (1) side is provided with charging device (2) and controlling switch (3), and base (1) bottom is provided with lock ring (4), the bottom
Ejection platform (12) is hinged with seat (1), the piston rod of the hydraulic cylinder (11) is connected with ejection platform (12) bottom, the bullet
Penetrate in platform (12) and be provided with motor II (15), ejection groove (22), the ejection groove (22) are provided with the middle part of the ejection platform (12)
Interior to be provided with gear I (13), gear II (16) and the chain (14) for being enclosed on its outer end, the gear II (16) is socketed in motor II
(15) on main shaft, fixed block (17) is cased with the chain (14), the fixed block (17) is provided with U-bracket (18), institute
State U-bracket (18) and be provided with stopper slot (19), the hydraulic pump (10), motor I (7), motor II (15) and controlling switch (3)
It is electrically connected with battery (5).
2. vehicle-mounted unmanned aerial vehicle catapult-launching gear according to claim 1, it is characterised in that：The charging device (2) includes nothing
Man-machine charging socket and USB.
3. vehicle-mounted unmanned aerial vehicle catapult-launching gear according to claim 1, it is characterised in that：It is hinged on the U-bracket (18)
There is lock (20).
4. vehicle-mounted unmanned aerial vehicle catapult-launching gear according to claim 1, it is characterised in that：The ejection platform (12) is provided with
Solar charging panel (21), the solar charging panel (21) are electrically connected with battery (5).
5. vehicle-mounted unmanned aerial vehicle catapult-launching gear according to claim 1, it is characterised in that：The controlling switch (3), which is matched somebody with somebody, to be whether there is
Line remote control (23).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720583352.3U CN207045776U (en) | 2017-05-23 | 2017-05-23 | A kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720583352.3U CN207045776U (en) | 2017-05-23 | 2017-05-23 | A kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207045776U true CN207045776U (en) | 2018-02-27 |
Family
ID=61491191
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720583352.3U Expired - Fee Related CN207045776U (en) | 2017-05-23 | 2017-05-23 | A kind of vehicle-mounted unmanned aerial vehicle catapult-launching gear |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207045776U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502043A (en) * | 2018-09-30 | 2019-03-22 | 沈阳戈达德智能装备科技有限公司 | A kind of long-range Quality Initiative driven motor ejector system of small drone |
-
2017
- 2017-05-23 CN CN201720583352.3U patent/CN207045776U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109502043A (en) * | 2018-09-30 | 2019-03-22 | 沈阳戈达德智能装备科技有限公司 | A kind of long-range Quality Initiative driven motor ejector system of small drone |
| CN109502043B (en) * | 2018-09-30 | 2023-08-08 | 沈阳戈达德智能装备科技有限公司 | Small unmanned aerial vehicle remote control chain transmission electric catapult system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180227 Termination date: 20180523 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |