CN206031787U - A kicker for unmanned aerial vehicle - Google Patents
A kicker for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN206031787U CN206031787U CN201620993078.2U CN201620993078U CN206031787U CN 206031787 U CN206031787 U CN 206031787U CN 201620993078 U CN201620993078 U CN 201620993078U CN 206031787 U CN206031787 U CN 206031787U
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- CN
- China
- Prior art keywords
- cylinder
- cover
- unmanned plane
- spinner
- baffle plate
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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.)
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Abstract
The utility model discloses a kicker for unmanned aerial vehicle, a kicker for unmanned aerial vehicle includes that an upper fixed plate, bottom plate and fixed connection are in at least one slinger between an upper fixed plate and the bottom plate, the slinger includes the barrel, sets up in the barrel and can glidingly about in the barrel throw the board, install be used for the drive in the barrel throw first driving piece that the board moved down, articulate being used for of the lower extreme of barrel is opened and is closed cover, the setting of the lower port of barrel are in the lower terminal surface department of cover is used for stoping baffle and drive that the cover was opened the baffle leaves the cover so that the second driving piece that the cover can be opened. Consequently the utility model provides a kicker can load article on unmanned aerial vehicle to it throws in the automation of setting for the position to realize article.
Description
Technical field
This utility model is related to unmanned air vehicle technique field, more particularly to a kind of spinner for unmanned plane.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on unmanned plane, but the equipment such as automatic pilot, presetting apparatus, ground remote control are installed
The personnel that stand by control device, which is tracked, is positioned, remote control, remote measurement and Digital Transmission.The species of unmanned plane is various, main
To include fixed-wing unmanned plane, flapping wing unmanned plane and multi-rotor unmanned aerial vehicle etc..
Unmanned plane have small volume, low lightweight, expense, flexible operation and it is safe the features such as, be widely used in boat
The every field such as bat, monitoring, search and rescue, resource exploration, agricultural.Unmanned plane is when in use, it is sometimes desirable to carry one by unmanned plane
A little articles, then drop these articles to the place specified.But existing unmanned plane has loading and throws in article
Structure.
Utility model content
The purpose of this utility model is to provide a kind of spinner for unmanned plane, article can be loaded in unmanned plane
On, and realize automatic throwing of the article in setting position.
To achieve these goals, this utility model provides a kind of spinner for unmanned plane, described for nobody
The spinner of machine includes upper mounted plate, bottom plate and be fixedly connected between fixed plate and bottom plate at least one
Individual slinger, the slinger include cylinder, are arranged in the cylinder and can slide up and down in the cylinder
Throwing board, be used for driving the first actuator that the throwing board moves down in the cylinder, be hinged on the cylinder
The cover for opening and closing the lower port of the cylinder of the lower end of body, be arranged at the lower surface of the cover be used for hinder
Baffle plate that only cover is opened and the baffle plate is driven to leave the cover so that the second drive that can open of the cover
Moving part, offers the installing hole passed through for the lower end of the cylinder on the bottom plate, the lower end of the cylinder extends downwardly from
The installing hole, the cover, baffle plate are respectively positioned on the lower section of the bottom plate, the throwing board, cylinder and cover formation
Product placement space.
Preferably, first actuator is compression spring, and the upper end of the compression spring is fixed on the top of cylinder, institute
The lower end for stating compression spring is fixed on the throwing board.
Preferably, the upper and lower ends of the compression spring are fixed on the cylinder and the throwing board by fixture
On.
Preferably, the installing hole passed through for the spring silk of the compression spring, the installing hole is offered on the fixture
Horizontally disposed, the spring silk of the top and bottom of the compression spring both passes through corresponding fixture, and the fixture passes through bolt
It is fixed on cylinder or throwing board.
Preferably, second actuator is steering wheel, and the steering wheel is fixedly mounted on the bottom plate, the steering wheel
Output shaft be connected with the one end in the outside positioned at the cover of the baffle plate, the steering wheel can drive the baffle plate turn
It is dynamic, so that the other end of the baffle plate turns to the outside of the cover.
Preferably, the cover is by hinge means fixed cylinder.
Preferably, the hinge means includes the first articulated slab and is hinged by bearing pin and the first articulated slab are hinged second
Plate, first articulated slab are fixed on the lower surface of cover, and second articulated slab is fixed on the barrel outer surface of cylinder.
Preferably, the baffle plate is generally circular in shape, and the quantity of the slinger is 5, and 5 slingers enclose
Axis around the baffle plate is uniform.
Preferably, the hinge means of each slinger is respectively positioned on the radial outside of the baffle plate, each described throwing
Second actuator for throwing device is respectively positioned on the radially inner side of the baffle plate.
This utility model with the difference of prior art is, the spinner for unmanned plane that this utility model is provided
It is fixed on unmanned plane by upper mounted plate, and the article for needing throwing is placed on into what is be made up of throwing board, cylinder and cover
In article placement space, when unmanned plane needs throwing article in flight course, it is only necessary to control the second actuator, make second
Actuator drives flapper, and baffle plate is removed from cover, now, under the driving force effect of the first actuator, the throwing
Plate is moved down, and is promoted positioned at being cast out from cylinder lower port in the article in article placement space, therefore this practicality is newly
The spinner that type is provided can be loaded in article on unmanned plane, and realize automatic throwing of the article in setting position.
Description of the drawings
Fig. 1 is a kind of structural representation of the spinner for unmanned plane of embodiment that this utility model is provided；
Fig. 2 is the structural representation in another direction of the spinner shown in Fig. 1；
Fig. 3 is the front view of the spinner shown in Fig. 1；
Fig. 4 is the structural representation of the slinger of the spinner shown in Fig. 1；
Fig. 5 is the front view of the slinger shown in Fig. 4；
Sectional view during Fig. 6 in Fig. 5 along A-A directions；
Description of reference numerals：
1- slingers；11- cylinders；12- throwing boards；The first actuators of 13-；14- covers；15- baffle plates；16- second drives
Moving part；17- article placement spaces；18- fixtures；19- hinge means；2- upper mounted plates；3- bottom plates.
Specific embodiment
This utility model is further illustrated with embodiment below in conjunction with the accompanying drawings.But the use of these exemplary embodiments
Way and purpose are only used for enumerating this utility model, not real protection scope of the present utility model are constituted any type of any
Limit, it is more non-that protection domain of the present utility model is confined to into this.
Some nouns of locality are defined in this utility model, in the case where not being specified to the contrary, the orientation for being used
Word such as " upper and lower " refers to what the spinner for unmanned plane that this utility model is provided was defined under normal usage, and with
Direction up and down shown in accompanying drawing 3 is consistent." inside and outside " is referred to relative to inside and outside each parts profile itself.These sides
Position word is adopted for the ease of understanding, thus does not constitute the restriction to this utility model protection domain.
Suitably with reference to shown in Fig. 1-3, the spinner for unmanned plane of the basic embodiment that this utility model is provided can
With including upper mounted plate 2, bottom plate 3 and at least one throwing being fixedly connected between fixed plate 2 and bottom plate 3
Throw device 1.Suitably with reference to shown in Fig. 4-6, the slinger 1 includes cylinder 11, is arranged in the cylinder 11 and can be with
The throwing board 12 that slides up and down in the cylinder 11, in the cylinder 11 for driving the throwing board 12 to moving down
Dynamic the first actuator 13, be hinged on the cylinder 11 lower end the cylinder for opening and closing the lower port of the cylinder 11
Lid 14, it is arranged at the lower surface of the cover 14 baffle plate 15 that is used for preventing the cover 14 from opening and drives the baffle plate 15
The cover 14 is left so that the second actuator 16 that can open of the cover 14, offers confession on the bottom plate 3
The installing hole that the lower end of the cylinder 11 passes through, the lower end of the cylinder 11 extend downwardly from the installing hole, the cover 14, gear
Plate 15 is respectively positioned on the lower section of the bottom plate 3, and the throwing board 12, cylinder 11 and cover 14 form article placement space 17.
In above-mentioned basic embodiment, the cylinder 11 can using any appropriate ways and fixed plate 2 and
Bottom plate 3 connects, and for example, the conventional connected mode connection such as can be bolted or weld.
The cylinder 11 can be the open structure in upper end, it would however also be possible to employ the open structure in upper end closed, lower end, and
The shape of cross section of the cylinder 11 can be using various appropriate shapes such as polygon, rectangle, circle, ellipses, in this reality
In new, it is preferred to use cross section is circular cylinder.
The throwing board 12 is the structure for promoting the article for needing throwing, therefore throwing board 12 can be with any shape
Tabular or circulus, as long as article can be pushed down on.In this utility model, it is preferable that the throwing board 12
It is generally circular in shape, and its external diameter be slightly less than between the internal diameter of cylinder 11, i.e. throwing board 12 and cylinder 11 for gap coordinate, from
And enable throwing board 12 to realize self direction.
The spinner for unmanned plane of above-mentioned basic embodiment when in use, is fixed on by upper mounted plate 2 first
On unmanned plane body, fixed form can be fixed for bolt, in order to dismantle.Then the second actuator 16, flap shutter are controlled
15, make baffle plate 15 leave cover 14, cover 14 of checking card, it would be desirable to which the article of throwing is placed on by throwing board 12, cylinder 11 and cylinder
In the article placement space 17 that lid 14 is constituted, then cover 14 is shut, then control the second actuator 16 so that baffle plate 15 is turned to
Block the cover 14 in the lower section of cover 14.When unmanned plane needs throwing article in flight course, it is only necessary to control second
Actuator 16, makes the second actuator 16 drive baffle plate 15 to rotate, and baffle plate 15 is removed from cover 14, now, in the first actuator
Under 13 driving force effect, the throwing board 12 is moved down, and is promoted positioned at the article in the article placement space 17 from cylinder
It is cast out in 11 lower ports.
Wherein the control mode of second actuator 16 can be automatically controlled using the control device on unmanned plane, or
By the way of remotely control.
In this utility model, first actuator 13 can adopt any knot that can provide downward driving force
Structure, such as linear electric motors etc..In order that spinner structure of the present utility model is simpler, and reduces cost, it is preferable that institute
Stating the first actuator 13 adopts elastic component, elastic component provide downward elastic force, is ideal driving element.Further
Preferably, as shown in fig. 6, first actuator 13 is compression spring, the upper end of the compression spring is fixed on cylinder 11
Top, the lower end of the compression spring are fixed on the throwing board 12.
It is fixed on cylinder 11 and throwing board 12 for the ease of compression spring, in the side of being preferable to carry out of the present utility model
In formula, the upper and lower ends of the compression spring are fixed on the cylinder 11 and the throwing board 12 by fixture 18.When
So, in other embodiments, the compression spring can also be directly welded on cylinder 11 and throwing board 12, this utility model
This is not construed as limiting.
Further, in this utility model, the spring silk for the compression spring is offered on the fixture 18 and is passed through
Installing hole, the installing hole be horizontally disposed with, the spring silk of the top and bottom of the compression spring both passes through corresponding fixture
18, the fixture 18 is bolted on cylinder 11 or throwing board 12.Preferably, for fixing the upper end of compression spring
Three are with the fixture of lower end, and it is uniform around the axis of the cylinder 11.
In this utility model, second actuator 16 is used in the knot for driving the baffle plate 15 to remove from cover 14
Structure, therefore, the second actuator 16 can be using any appropriate configuration for being capable of linear movement output or rotary motion.Such as institute
State the second actuator 16 and can adopt linear electric motors, now, the outer end of the output shaft of linear electric motors is fixedly connected with baffle plate 15, is led to
The output shaft for crossing linear electric motors stretches out or retracts, you can realize that baffle plate 15 is blocked or leaves the cover 14.
In a preferred implementation of the present utility model, in order that the volume of spinner is less, with reference to Fig. 4 institutes
Show, second actuator 16 is steering wheel, and the steering wheel is fixedly mounted on the bottom plate 3, the output shaft of the steering wheel
It is connected with the one end in the outside positioned at the cover 14 of the baffle plate 15, the steering wheel can drive the baffle plate 15 to rotate,
So that the other end of the baffle plate 15 turns to the outside of the cover 14 such that it is able to so that cover 14 is opened.
In this utility model, the cover 14 is by 19 fixed cylinder 11 of hinge means.The hinge means 19 can
With using existing various appropriate structures.
In a preferred implementation of the present utility model, as shown in figure 4, the hinge means 19 includes that first is hinged
Plate and the second articulated slab being hinged by bearing pin and the first articulated slab, first articulated slab are fixed on the lower surface of cover 14
On, second articulated slab is fixed on the barrel outer surface of cylinder.
As shown in Fig. 2 in order to when unmanned plane carries out flight task, multiple things for needing throwing can be carried
Product, it is preferable that the baffle plate 15 it is generally circular in shape, the quantity of the slinger 1 is 5, and 5 slingers 1 enclose
Axis around the baffle plate 15 is uniform.Thus, it is possible in the case where the volume of guarantee spinner is as little as possible, with more
Slinger 1.
On the basis of above-mentioned embodiment, the arrangement in order that the second actuator 16 of slinger 1 is more convenient for, preferably
Ground, the hinge means 19 of each slinger 1 are respectively positioned on the radial outside of the baffle plate 15, each described slinger 1
Second actuator 16 be respectively positioned on the radially inner side of the baffle plate 15.
The sequencing of embodiment of above only for ease of description, does not represent the quality of embodiment.
Finally it should be noted that：Embodiment of above is only illustrating the technical solution of the utility model, rather than which is limited
System；Although being described in detail to this utility model with reference to aforementioned embodiments, one of ordinary skill in the art should
Understand：Which still can be modified to the technical scheme described in aforementioned each embodiment, or special to which part technology
Levying carries out equivalent；And these modifications or replacement, do not make the essence of appropriate technical solution depart from each reality of this utility model
Apply the spirit and scope of mode technical scheme.
Claims (9)
1. a kind of spinner for unmanned plane, it is characterised in that the spinner for unmanned plane includes upper mounted plate
(2), bottom plate (3) and at least one slinger being fixedly connected between fixed plate (2) and bottom plate (3)
(1), described slinger (1) includes cylinder (11), is arranged in the cylinder (11) and can be in the cylinder (11)
The throwing board (12) that slides up and down, in the cylinder (11) for drive that the throwing board (12) moves down first
Actuator (13), be hinged on the cylinder (11) lower end the cover for opening and closing the lower port of the cylinder (11)
(14), it is arranged at the lower surface of the cover (14) described in the baffle plate (15) and driving for being used for preventing the cover (14) from opening
Baffle plate (15) leaves the cover (14) so that the second actuator (16) that can open of the cover (14), the lower fixation
Offer the installing hole passed through for the lower end of the cylinder (11) on plate (3), the lower end of cylinder (11) extends downwardly from described
Installing hole, cover (14), baffle plate (15) are respectively positioned on the lower section of the bottom plate (3), throwing board (12), cylinder
(11) and cover (14) formed article placement space (17).
2. the spinner for unmanned plane according to claim 1, it is characterised in that described first actuator (13) are pressure
Contracting spring, the upper end of the compression spring are fixed on the top of cylinder (11), and the lower end of the compression spring is fixed on the throwing
Throw on plate (12).
3. the spinner for unmanned plane according to claim 2, it is characterised in that the upper and lower ends of the compression spring
It is fixed on the cylinder (11) and the throwing board (12) by fixture (18).
4. the spinner for unmanned plane according to claim 3, it is characterised in that offer on fixture (18)
For the installing hole that the spring silk of the compression spring is passed through, the installing hole is horizontally disposed with, the top and bottom of the compression spring
Spring silk both pass through corresponding fixture (18), fixture (18) are bolted on cylinder (11) or throwing board (12)
On.
5. the spinner for unmanned plane according to claim 1, it is characterised in that described second actuator (16) are rudder
Machine, the steering wheel are fixedly mounted on the bottom plate (3), and the output shaft of the steering wheel is with the baffle plate (15) positioned at institute
One end connection in the outside of cover (14) is stated, the steering wheel can drive the baffle plate (15) to rotate, so that the baffle plate
(15) the other end turns to the outside of the cover (14).
6. the spinner for unmanned plane according to claim 1, it is characterised in that cover (14) are filled by hinge
Put on (19) fixed cylinder (11).
7. the spinner for unmanned plane according to claim 6, it is characterised in that described hinge means (19) include the
One articulated slab and the second articulated slab being hinged by bearing pin and the first articulated slab, first articulated slab are fixed on cover (14)
On lower surface, second articulated slab is fixed on the barrel outer surface of cylinder.
8. the spinner for unmanned plane according to claim 6, it is characterised in that baffle plate (15) are shaped as circle
Shape, the quantity of slinger (1) is 5, and 5 described slinger (1) is uniform around the axis of the baffle plate (15).
9. the spinner for unmanned plane according to claim 8, it is characterised in that each slinger (1)
Hinge means (19) is respectively positioned on the radial outside of the baffle plate (15), second actuator of each slinger (1)
(16) it is respectively positioned on the radially inner side of the baffle plate (15).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620993078.2U CN206031787U (en) | 2016-08-30 | 2016-08-30 | A kicker for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620993078.2U CN206031787U (en) | 2016-08-30 | 2016-08-30 | A kicker for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206031787U true CN206031787U (en) | 2017-03-22 |
Family
ID=58302331
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620993078.2U Expired - Fee Related CN206031787U (en) | 2016-08-30 | 2016-08-30 | A kicker for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206031787U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107600413A (en) * | 2017-09-08 | 2018-01-19 | 厦门大学 | The rotor of multi-chamber microminiature container-type four transports unmanned plane |
| CN109229409A (en) * | 2018-10-23 | 2019-01-18 | 西北工业大学 | A kind of aerial rapid fire system of cluster type small drone |
| CN109229410A (en) * | 2018-10-23 | 2019-01-18 | 西北工业大学 | A kind of rotary unmanned plane air-launching method and device |
| CN109573485A (en) * | 2018-12-29 | 2019-04-05 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensor conveying mechanism and application method in high-altitude |
| CN109747830A (en) * | 2018-12-27 | 2019-05-14 | 中国航空工业集团公司西安飞机设计研究所 | A kind of single group wheel link-type unmanned plane delivery device and put-on method |
| CN110239718A (en) * | 2019-07-23 | 2019-09-17 | 安徽天路航空科技股份有限公司 | A kind of aircraft external hanging type article throwing device |
| CN111717393A (en) * | 2020-05-26 | 2020-09-29 | 河北柒壹壹玖工业自动化技术有限公司 | Material is from formula of delivering transport unmanned aerial vehicle |
-
2016
- 2016-08-30 CN CN201620993078.2U patent/CN206031787U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107600413A (en) * | 2017-09-08 | 2018-01-19 | 厦门大学 | The rotor of multi-chamber microminiature container-type four transports unmanned plane |
| CN109229409A (en) * | 2018-10-23 | 2019-01-18 | 西北工业大学 | A kind of aerial rapid fire system of cluster type small drone |
| CN109229410A (en) * | 2018-10-23 | 2019-01-18 | 西北工业大学 | A kind of rotary unmanned plane air-launching method and device |
| CN109747830A (en) * | 2018-12-27 | 2019-05-14 | 中国航空工业集团公司西安飞机设计研究所 | A kind of single group wheel link-type unmanned plane delivery device and put-on method |
| CN109747830B (en) * | 2018-12-27 | 2022-04-19 | 中国航空工业集团公司西安飞机设计研究所 | Single-group wheel connecting rod type unmanned aerial vehicle throwing device and throwing method |
| CN109573485A (en) * | 2018-12-29 | 2019-04-05 | 成都紫瑞青云航空宇航技术有限公司 | Launch sensor conveying mechanism and application method in high-altitude |
| CN109573485B (en) * | 2018-12-29 | 2020-12-29 | 成都紫瑞青云航空宇航技术有限公司 | High-altitude drop sensor conveying mechanism and using method |
| CN110239718A (en) * | 2019-07-23 | 2019-09-17 | 安徽天路航空科技股份有限公司 | A kind of aircraft external hanging type article throwing device |
| CN110239718B (en) * | 2019-07-23 | 2024-03-22 | 安徽天路航空科技股份有限公司 | Aircraft external-hanging type article throwing device |
| CN111717393A (en) * | 2020-05-26 | 2020-09-29 | 河北柒壹壹玖工业自动化技术有限公司 | Material is from formula of delivering transport unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170322 Termination date: 20200830 |