CN208217003U - A kind of small drone automatic release device - Google Patents
A kind of small drone automatic release device Download PDFInfo
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- CN208217003U CN208217003U CN201820589609.0U CN201820589609U CN208217003U CN 208217003 U CN208217003 U CN 208217003U CN 201820589609 U CN201820589609 U CN 201820589609U CN 208217003 U CN208217003 U CN 208217003U
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- steering engine
- mounting plate
- bottom mounting
- substrate
- release device
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Abstract
A kind of small drone automatic release device, unmanned plane include shell, and controller and power supply are provided in shell, and delivery device includes several dispensing units for being fixed at the bottom mounting plate of housing bottom and being fixed on bottom mounting plate；Launching unit includes the substrate being fixedly connected with bottom mounting plate, U-shaped limiter is fixedly installed on substrate, steering engine installation card slot is offered in the one side that substrate and bottom mounting plate fit, steering engine is provided in steering engine installation card slot, steering engine and controller and power electric connection, steering engine installation card slot is also communicated with through slot, the output shaft of steering engine is pierced by from through slot, the output shaft of steering engine is connected with the flexible suspending bar for hanging missile by gear unit, and flexible suspending bar is adjacent to after a side plate of U-shaped limiter or another side plate far from U-shaped limiter.The utility model is compact-sized, easy to use, and installation process is simple, and carry missile that can be safe and stable simultaneously realizes safe dispensing.
Description
Technical field
The utility model relates to unmanned plane delivery device field, specifically a kind of small drone launches dress automatically
It sets.
Background technique
With the development of science and technology, unmanned plane using more and more extensive, take photo by plane, plant protection, self-timer, express transportation, disaster
There is application in the fields such as rescue, monitoring infectious disease, news report, movies-making, have not only expanded the purposes of unmanned plane itself,
It provides convenience to many industries, many countries are all greatly developing unmanned air vehicle technique.Unmanned plane and dispenser match can
To realize many functions.Wherein, peasant's sowing can be helped in terms of automatic dispensing, launches pesticide, can be used for extra large field
In launch fish food, disaster relief article etc. is launched in disaster relief, it is time saving and energy saving, it is easy to use, greatly improve work efficiency.But
It is current automatic release device, there is that launch type of goods single, replacement missile is inconvenient and the not flexible equal spies of control
Point.
Utility model content
In order to solve deficiency in the prior art, the utility model provides a kind of small drone automatic release device, knot
Structure is compact, easy to use, and carry that can be safe and stable is multiple or a variety of missiles and realizes safe dispensing.
To achieve the goals above, the utility model use the specific scheme is that a kind of small drone launches dress automatically
It sets, the unmanned plane includes shell, and controller and power supply are provided in shell, and the delivery device includes being fixed at institute
Several dispensing units stating the bottom mounting plate of housing bottom and being fixed on bottom mounting plate；The dispensing unit packet
The substrate being fixedly connected with the bottom mounting plate is included, U-shaped limiter is fixedly installed on substrate, U-shaped limiter is by one and half
Arc-shaped plate and two side plate compositions, two side plates are integrally attached to the both ends of semicircular arc plate respectively, and substrate and bottom are installed
Steering engine installation card slot is offered in the one side that plate fits, and is provided with steering engine, steering engine and the controller in steering engine installation card slot
With the power electric connection, steering engine installation card slot is also communicated with through slot, and the output shaft of steering engine is pierced by from through slot, the output of steering engine
Axis is connected with the flexible suspending bar for hanging missile by gear unit, and flexible suspending bar passes through one of U-shaped limiter
Be adjacent to after side plate or far from U-shaped limiter another side plate.
The bottom mounting plate is fixedly connected with side baffle, and side baffle is mutually perpendicular to bottom mounting plate, side baffle it is upper
Edge is fixedly connected with overhead gage, and the length of overhead gage is less than the length of side baffle to respectively form one at the both ends of overhead gage
Bayonet, be fixedly connected on the substrate there are two with the one-to-one fixture block of bayonet.
It is fixedly connected with convex block on the bottom mounting plate, the through-hole to match with convex block is offered on the substrate.
Several the first screw holes are offered on the substrate, offer several and the first screw hole on the bottom mounting plate
One-to-one second screw hole, the first screw hole and the second screw hole are connected by bolts the fixed company for completing bottom mounting plate and substrate
It connects.
First screw hole and second screw hole are disposed as four.
The steering engine drives the flexible suspending bar to do straight reciprocating motion by gear unit.
The gear unit includes the band moving axis being coaxially connected with the output shaft of the steering engine, is rotatably connected on band moving axis
First swing rod, the first swing rod are also fixedly connected with the first articulated shaft, and the second swing rod, the second pendulum are rotatably connected on the first articulated shaft
The second articulated shaft is fixedly connected on bar, the second articulated shaft and the flexible suspending bar are rotatablely connected.
The dispensing unit is set as 12.
12 dispensing units are by the array for being arranged in 2 × 6.
The utility model has the advantages that the utility model is compact-sized, easy to use, installation process is simple, carry that can be safe and stable
Missile simultaneously realizes safe dispensing, and carry and can launch multiple or a variety of missiles simultaneously, more efficient.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of unmanned plane；
Fig. 2 is the structural schematic diagram of the dispensing unit of the utility model；
Fig. 3 is the structural schematic diagram of the bottom mounting plate of the utility model；
Fig. 4 is the set-up mode schematic diagram that the utility model all launches unit.
Appended drawing reference: 1, shell, 2, bottom mounting plate, 3, dispensing unit, 4, fixture block, 5, substrate, the 6, first screw hole, 7, rudder
Machine, 8, band moving axis, the 9, first swing rod, the 10, first articulated shaft, the 11, second swing rod, the 12, second articulated shaft, 13, flexible suspending bar,
14, U-shaped limiter, 15, steering engine installation card slot, 16, through-hole, the 17, second screw hole, 18, side baffle, 19, bayonet, 20, overhead gage,
21, convex block.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
The structural schematic diagram that Fig. 1 to 4, Fig. 1 is unmanned plane is please referred to, Fig. 2 is the structure of the dispensing unit of the utility model
Schematic diagram, Fig. 3 are the structural schematic diagrams of the bottom mounting plate of the utility model, and Fig. 4 is that the utility model all launches unit
Set-up mode schematic diagram.
A kind of small drone automatic release device, unmanned plane include shell 1, are provided with controller and electricity in shell 1
Source, delivery device include ten for being fixed at the bottom mounting plate 2 of 1 bottom of shell and being fixed on bottom mounting plate 2
Two dispensing units 3 can be achieved a fixed connection between bottom mounting plate 2 and shell 1 by welding.
Launching unit 3 includes the substrate 5 being fixedly connected with bottom mounting plate 2, is fixedly installed U-shaped limiter on substrate 5
14, U-shaped limiter 14 is made of a semicircular arc plate and two side plates, and two side plates are integrally attached to semicircular arc plate respectively
Both ends, offer steering engine installation card slot 15 in the one side that substrate 5 and bottom mounting plate 2 fit, steering engine is installed in card slot 15
It is provided with steering engine 7, steering engine 7 and controller and power electric connection, steering engine installation card slot 15 is also communicated with through slot, the output of steering engine 7
Axis is pierced by from through slot, and the output shaft of steering engine 7 is connected with the flexible suspending bar 13 for hanging missile by gear unit, is stretched
Contracting hanger bar 13 is adjacent to after a side plate of U-shaped limiter 14 or another side plate far from U-shaped limiter 14.
In order to guarantee to launch stable connection between unit and bottom mounting plate 2, will not be detached from flight course, in bottom
Side baffle 18 is fixedly connected on mounting plate 2, side baffle 18 is mutually perpendicular to bottom mounting plate 2, and the upper edge of side baffle 18 is fixed
It is connected with overhead gage 20, the length of overhead gage 20 is less than the length of side baffle 18 to respectively form one at the both ends of overhead gage 20
Bayonet 19, be fixedly connected on substrate 5 there are two with the one-to-one fixture block 4 of bayonet 19.Bottom mounting plate 2 also on be fixedly connected with
Convex block 21 offers the through-hole 16 to match with convex block 21 on substrate 5.
When unit is launched in installation, substrate 5 along the width direction of overhead gage 20 be inserted into bottom mounting plate 2 and overhead gage 20 it
Between, substrate 5 is clamped by bottom mounting plate 2 and overhead gage 20, latter two right fixture block 4 is inserted respectively into two bayonets 19, and two
Fixture block 4 is against respectively on the both ends of overhead gage 20, to avoid substrate 5 and bottom mounting plate 2 in the length direction of overhead gage 20
It is upper to be detached from.Convex block 21 is inserted into through-hole 16 simultaneously, and convex block 21 will be successfully inserted in through-hole 16, and the height of convex block 21 is answered
When the thickness for being less than substrate 5, substrate 5 and bottom mounting plate 2 is avoided to be detached from from other directions.The specific side of being fixedly connected
Formula are as follows: opened up on the substrate 5 there are four the first screw hole 6, open up that there are four correspond with the first screw hole 6 on bottom mounting plate 2
The second screw hole 17, the first screw hole 6 and the second screw hole 17, which are connected by bolts, completes bottom mounting plate 2 and the fixed of substrate 5 connects
It connects.
Steering engine 7 drives flexible suspending bar 13 to do straight reciprocating motion by gear unit.Gear unit includes and steering engine 7
The coaxial connected band moving axis 8 of output shaft, is rotatably connected to the first swing rod 9 on band moving axis 8, and the first swing rod 9 is also fixedly connected with the
One articulated shaft 10 is rotatably connected to the second swing rod 11 on first articulated shaft 10, and it is hinged that second is fixedly connected on the second swing rod 11
Axis 12, the second articulated shaft 12 are rotatablely connected with flexible suspending bar 13.When the output shaft rotation of steering engine 7, pass through band 8 band of moving axis
Dynamic first swing rod 9 is swung to the left or to the right, then drives the second pendulum by the first articulated shaft 10 by the swinging end of the first swing rod 9
Bar 11 is swung, and then drives flexible suspending bar 13 to realize straight line fortune by the second articulated shaft 12 by the swinging end of the second swing rod 11
It is dynamic.Flexible suspending bar 13 is worked by the way of straight reciprocating motion, and stroke is most short, efficiency highest.
It launches unit 3 and is set as 12.12 dispensing units 3 are by the array for being arranged in 2 × 6.Wherein every two is thrown
Putting unit 3 is one group, and 12 are launched the array that unit is formed 2 × 3 by group arrangement, and every group of two dispensing units 3 are back-to-back
Setting, i.e., the opening direction of U-shaped limiter 14 are opposite.Because steering engine 7 needs certain space when driving gear unit movement, will be every
Two dispensing units 3 of group can keep structure more compact backwards to setting while that the remote space for reserving transmission, most
The saving space of limits, so that the volume with small drone matches, and then controller can control steering engine 7 to realize that grouping is thrown
It puts, successively the functions such as dispensing.
In use, missile is suspended on flexible suspending pipe 13 by rope, then starts steering engine 7, passed through by steering engine 7
Gear unit drives flexible suspending bar 13 to be against on another side plate of U-shaped limiter 14, so that missile is suspended on nothing
On man-machine.Unmanned plane flies after taking off along projected route, reaches after launching above place, starts steering engine 7, is passed through by steering engine 7
It is mobile that gear unit drives flexible suspending bar 13, and then withdraws from U-shaped limiter 14, because of U-shaped limit during exiting
The side plate of device 14 blocks, so missile will not follow flexible suspending bar 13 mobile, so as to divide with flexible suspending bar 13
From falling on release position finally down.
The utility model is compact-sized, easy to use, and installation process is simple, and carry missile that can be safe and stable is simultaneously
It realizes that safety is launched, and carry and multiple or a variety of missiles can be launched simultaneously, it is more efficient.
It should also be noted that, herein, relational terms such as first and second and the like are used merely to one
Entity or operation are distinguished with another entity or operation, without necessarily requiring or implying between these entities or operation
There are any actual relationship or orders.Moreover, the terms "include", "comprise" or its any other variant are intended to contain
Lid non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.In the absence of more restrictions, the element limited by sentence "including a ...", it is not excluded that
There is also other identical elements in process, method, article or equipment including the element.
The foregoing description of the disclosed embodiments can be realized professional and technical personnel in the field or using originally practical new
Type.Various modifications to these embodiments will be readily apparent to those skilled in the art, and determine herein
The General Principle of justice can be realized in other embodiments without departing from the spirit or scope of the present utility model.Cause
This, the present invention will not be limited to the embodiments shown herein, and is to fit to and principles disclosed herein
The widest scope consistent with features of novelty.
Claims (9)
1. a kind of small drone automatic release device, the unmanned plane includes shell (1), is provided with control in shell (1)
Device and power supply, it is characterised in that: the delivery device includes the bottom mounting plate (2) for being fixed at the shell (1) bottom
Unit (3) are launched with several being fixed on bottom mounting plate (2)；
Dispensing unit (3) includes the substrate (5) being fixedly connected with the bottom mounting plate (2), and substrate is fixedly installed on (5)
Have U-shaped limiter (14), U-shaped limiter (14) is made of a semicircular arc plate and two side plates, two side plates difference one
The both ends of semicircular arc plate are connected to, steering engine installation card slot is offered in the one side that substrate (5) and bottom mounting plate (2) fit
(15), it is provided with steering engine (7) in steering engine installation card slot (15), steering engine (7) and the controller and the power electric connection, steering engine
Installation card slot (15) is also communicated with through slot, and the output shaft of steering engine (7) is pierced by from through slot, and the output shaft of steering engine (7) passes through transmission
Unit is connected with the flexible suspending bar (13) for hanging missile, and flexible suspending bar (13) passes through the one of U-shaped limiter (14)
Be adjacent to after a side plate or far from U-shaped limiter (14) another side plate.
2. a kind of small drone automatic release device as described in claim 1, it is characterised in that: the bottom mounting plate
(2) it is fixedly connected with side baffle (18), side baffle (18) is mutually perpendicular to bottom mounting plate (2), the upper edge of side baffle (18)
It is fixedly connected with overhead gage (20), the length of overhead gage (20) is less than the length of side baffle (18) to the two of overhead gage (20)
Hold one bayonet (19) of each formation, be fixedly connected on the substrate (5) there are two with the one-to-one fixture block (4) of bayonet (19).
3. a kind of small drone automatic release device as described in claim 1, it is characterised in that: the bottom mounting plate
(2) it is fixedly connected on convex block (21), the through-hole (16) to match with convex block (21) is offered on the substrate (5).
4. a kind of small drone automatic release device as described in claim 1, it is characterised in that: opened on the substrate (5)
Equipped with several the first screw holes (6), it is one-to-one with the first screw hole (6) that several are offered on the bottom mounting plate (2)
Second screw hole (17), the first screw hole (6) and the second screw hole (17), which are connected by bolts, completes bottom mounting plate (2) and substrate (5)
Be fixedly connected.
5. a kind of small drone automatic release device as claimed in claim 4, it is characterised in that: first screw hole (6)
Four are disposed as with second screw hole (17).
6. a kind of small drone automatic release device as described in claim 1, it is characterised in that: the steering engine (7) passes through
Gear unit drives the flexible suspending bar (13) to do straight reciprocating motion.
7. a kind of small drone automatic release device as claimed in claim 6, it is characterised in that: the gear unit includes
With coaxial connected band moving axis (8) of the output shaft of the steering engine (7), it is rotatably connected to the first swing rod (9) on band moving axis (8), the
One swing rod (9) is also fixedly connected with the first articulated shaft (10), is rotatably connected on the first articulated shaft (10) the second swing rod (11), the
It is fixedly connected on two swing rods (11) the second articulated shaft (12), the second articulated shaft (12) and the flexible suspending bar (13) rotation connect
It connects.
8. a kind of small drone automatic release device as described in claim 1, it is characterised in that: the dispensing unit (3)
It is set as 12.
9. a kind of small drone automatic release device as claimed in claim 8, it is characterised in that: 12 dispensings are single
First (3) are by the array for being arranged in 2 × 6.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820589609.0U CN208217003U (en) | 2018-04-24 | 2018-04-24 | A kind of small drone automatic release device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820589609.0U CN208217003U (en) | 2018-04-24 | 2018-04-24 | A kind of small drone automatic release device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208217003U true CN208217003U (en) | 2018-12-11 |
Family
ID=64512395
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820589609.0U Active CN208217003U (en) | 2018-04-24 | 2018-04-24 | A kind of small drone automatic release device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208217003U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109795693A (en) * | 2019-01-03 | 2019-05-24 | 西京学院 | A kind of small power-free unmanned plane carry device |
| CN110654543A (en) * | 2019-10-29 | 2020-01-07 | 安徽方圆机电股份有限公司 | Unmanned aerial vehicle device of throwing ammunition |
| WO2021189165A1 (en) * | 2020-03-22 | 2021-09-30 | 南京唐壹信息科技有限公司 | Unmanned aerial vehicle provided with thrower |
| CN114229001A (en) * | 2022-01-25 | 2022-03-25 | 四块科技(深圳)有限公司 | Release device and unmanned aerial vehicle with release device |
-
2018
- 2018-04-24 CN CN201820589609.0U patent/CN208217003U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109795693A (en) * | 2019-01-03 | 2019-05-24 | 西京学院 | A kind of small power-free unmanned plane carry device |
| CN110654543A (en) * | 2019-10-29 | 2020-01-07 | 安徽方圆机电股份有限公司 | Unmanned aerial vehicle device of throwing ammunition |
| WO2021189165A1 (en) * | 2020-03-22 | 2021-09-30 | 南京唐壹信息科技有限公司 | Unmanned aerial vehicle provided with thrower |
| CN114229001A (en) * | 2022-01-25 | 2022-03-25 | 四块科技(深圳)有限公司 | Release device and unmanned aerial vehicle with release device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230309 Address after: Shop 6-S1-8, Building 6, Wanhong Jiayuan, Intersection of Lianmeng Road and Wanhong Road, Panlong District, Kunming City, Yunnan Province Patentee after: Kunming Duke science and Technology Co.,Ltd. Address before: 471000 in Zhuoyang science and Technology Park, Qinling Road, Jianxi District, Luoyang area, China (Henan) pilot Free Trade Zone, Luoyang City, Henan Province Patentee before: HENAN ZEDA INTELLIGENT TECHNOLOGY CO.,LTD. |
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| TR01 | Transfer of patent right |