CN207773481U - A kind of unmanned plane - Google Patents
A kind of unmanned plane Download PDFInfo
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- CN207773481U CN207773481U CN201721659791.4U CN201721659791U CN207773481U CN 207773481 U CN207773481 U CN 207773481U CN 201721659791 U CN201721659791 U CN 201721659791U CN 207773481 U CN207773481 U CN 207773481U
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- pressure block
- top pressure
- unmanned plane
- bottom end
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Abstract
The utility model discloses a kind of unmanned plane, body, propeller component and pickup folder, propeller component is rotatably installed on body and for driving body to fly;Pickup folder is installed on the bottom end of body;Pickup folder includes top pressure block, at least two clamping jaws and at least two connecting rods, and top pressure block is installed on the bottom end of body and can be moved along the short transverse of body, and at least two clamping jaws are arranged around the top pressure block circle spacing;One end of at least two connecting rods corresponds and is articulated at least two clamping jaws;The other end of at least two connecting rods is articulated on top pressure block;The top of clamping jaw is articulated with the bottom end of body;The bottom end of clamping jaw, which is equipped with to hook, takes portion.The unmanned plane of the utility model, it is when gripping article, top pressure block can move downward, and drive the side for hooking the inside close abutting article in the portion of taking of at least two clamping jaws, on top pressure block can be also connected at the top of article while capturing article, so that grasping structures is stablized, effectively avoids excessively rocking in article flight course.
Description
Technical field
The utility model is related to a kind of unmanned planes.
Background technology
Currently, unmanned plane is the not manned aircraft manipulated using radio robot and the presetting apparatus provided for oneself.
And with the development of science and technology, unmanned plane is applied to take photo by plane, launch article more and more industries.It is applied to boat in unmanned plane
When clapping or launching article, it is both needed to have pickup folder, to prevent camera or other articles from falling.But existing unmanned plane
The crawl of article is carried out generally by manipulator is arranged, crawl structure is not sufficiently stable.
Utility model content
For overcome the deficiencies in the prior art, the purpose of this utility model is that a kind of unmanned plane, can capture article, and
Capture stable structure.
The purpose of this utility model adopts the following technical scheme that realization:
A kind of unmanned plane, body, propeller component and pickup folder, propeller component are rotatably installed on body simultaneously
For driving body to fly;Pickup folder is installed on the bottom end of body;The pickup folder include top pressure block, at least two clamping jaws and
At least two connecting rods, the top pressure block are installed on the bottom end of body and can be moved along the short transverse of body, at least two clamping jaws
It arranges around the top pressure block circle spacing;One end of at least two connecting rods corresponds and is articulated at least two clamping jaws;At least
The other end of two connecting rods is articulated on top pressure block;The top of clamping jaw is articulated with the bottom end of body;The bottom end of clamping jaw is equipped with
Hook takes portion.
Further, one of portion of taking that hooks is used to form closing structure with another opposite hook portion of taking.
Further, pickup folder includes driving device, and driving device is used to drive top pressure block to be transported along the short transverse of body
It is dynamic.
Further, driving device includes driving motor and screw rod, and the driving motor is installed on body, the spiral shell
Bar extends along the short transverse of body and connection synchronous with the shaft of driving motor;The top pressure block is set on screw rod and and spiral shell
Bar screw-thread fit.
Further, the bottom end of the top pressure block is equipped with rubber pad.
Further, propeller component is equipped with multiple, and multiple propeller components are between the central axis circumference of the body
Every arrangement.
Further, propeller component includes link, helical blade and rotary electric machine, and link is fixed in body
On, it is set on link there are two spaced linking arm;It is articulated with the helical blade on two linking arms;The rotation
Motor is for driving helical blade to rotate.
Further, body is equipped with fender bracket, and the fender bracket is enclosed set on the periphery of multiple propeller components.
Further, the top of body is equipped with battery cavities and battery, and the battery is removably installed on electricity
In cell cavity and for powering to body.
Further, the side wall of battery cavities is equipped with bayonet, and the side of battery is equipped with hook, and hook is connected in bayonet.
Compared with prior art, the beneficial effects of the utility model are:Its unmanned plane can drive pickup folder to fly, and grip
Article.And when gripping article, top pressure block can move downward, and drive the hook portion of taking of at least two clamping jaws inwardly close to abutting object
The side of product, top pressure block can be also connected on article top while capturing article, so that grasping structures is stablized, effectively avoided article
It is excessively rocked in flight course.
Description of the drawings
Fig. 1 is the structural schematic diagram of the utility model;
Fig. 2 is the structural schematic diagram of the pickup folder of the utility model.
In figure:10, body;11, fender bracket;20, propeller component;21, link;22, helical blade;30, pickup folder;
31, top pressure block;311, rubber pad;32, clamping jaw;321, it hooks and takes portion;33, connecting rod;34, driving motor;35, screw rod;40, article;
50, battery.
Specific implementation mode
In the following, in conjunction with attached drawing and specific implementation mode, the utility model is described further, it should be noted that
Under the premise of not colliding, it can be formed in any combination between various embodiments described below or between each technical characteristic new
Embodiment.
A kind of unmanned plane as shown in Figure 1 and Figure 2, body 10, propeller component 20 and pickup folder 30, propeller group
Part 20 is rotatably installed on body 10, and body 10 can be driven to fly when propeller component 20 rotates.In addition, above-mentioned folder
Pickup 30 is installed on the bottom end of body 10, and specific pickup folder 30 includes top pressure block 31, at least two clamping jaws 32 and at least two
Connecting rod 33, top pressure block 31 is mounted on the bottom end of body 10, and top pressure block 31 can be moved along the short transverse of body 10.At least two
Clamping jaw 32 can arrange around 31 circle spacing of top pressure block, and one end of at least two connecting rods 33, which corresponds, is articulated at least two clamping jaws
On 32, and the other end of at least two connecting rods 33 is articulated on top pressure block 31.The top of above-mentioned clamping jaw 32 is articulated with body
10 bottom end is equipped with hook in the bottom end of clamping jaw 32 and takes portion 321.
When on the basis of the said structure, using the unmanned plane of the utility model, band motivation is rotated by propeller component 20
Body 10 fly, flight to 40 placement location of article when, can by making top pressure block 31 be moved downward along the short transverse of body 10,
During top pressure block 31 moves downward, top pressure block 31 can be driven by connecting rod 33, drive each clamping jaw 32 towards close to top
Briquetting 31 moves, i.e., each clamping jaw 32 mutually collapses close, and the hook of such clamping jaw 32 takes portion 321 that can be connected to the side of article 40
Portion.Referring to Fig. 1, at the same time, when top pressure block 31 moves to bottom, top pressure block 31 can be connected on article 40 or article
On 40 hanging ring, while clamping jaw 32 can be also near the state held together, and the hook of clamping jaw 32 takes portion 321 that can firmly be connected to article
40 side, makes grasping structures stablize, and effectively avoids excessively rocking in 40 flight course of article.
Specifically in the present embodiment, above-mentioned one of hook takes portion 321 to can be used for taking portion 321 to be formed with another opposite hook
Closing structure, that is, when top pressure block 31 moves downward, drive two opposite clamping jaws 32 to collapse by connecting rod 33 close, pressing from both sides
When taking the article 40 of hanging ring, during clamping jaw 32 is close to each other, hook takes portion 321 that can stretch into the hanging ring of article 40 or hang
In hook, opposite two hooks take portion 321 to form closing structure, and the hanging ring of article 40 can be made to stablize in closing structure, while on
The top pressure block 31 stated can be connected on hanging ring, in this way, grasping structures are more stablized.
Further, pickup folder 30 may also include driving device, and the driving device is for driving top pressure block 31 along body 10
Short transverse movement, and and Electronic control.It certainly, can be manually or by other works in the case of no driving device
Tool drives top pressure block 31 to move up and down.
Particularly, above-mentioned driving device includes driving motor 34 and screw rod 35, and driving motor 34 is installed on machine
On body 10, screw rod 35 extends along the short transverse of body 10, and the connection synchronous with the shaft of driving motor 34 of screw rod 35.Above-mentioned
Top pressure block 31 be set on screw rod 35 and with 35 screw-thread fit of screw rod.In this way, when driving top pressure block 31 to move up and down, can pass through
The shaft of driving motor 34 rotates, and screw rod 35 is driven to rotate, and the rotary motion of screw rod 35 is limited by connecting rod 33 and clamping jaw 32,
Thus top pressure block 31 can move up and down along the extending direction of screw rod 35, and driving structure is stablized.Certainly, driving device also can be selected and drive
The mechanism of other linear movement outputs such as cylinder or linear motor of taking offence replaces.
Further, also it can be equipped with rubber pad 311 in the bottom end of top pressure block 31, in this way, top pressure block 31 and article 40 can be made
Between contact be flexibility, prevent top pressure block 31 caused during top pressure article 40 damage.
Further, in this embodiment propeller component 20 can be equipped with multiple, and multiple propeller components 20 are around body
10 central axis circle spacing arrangement makes machine in this way, body 10 can be driven to fly by the rotation of multiple propeller components 20
The flight structure of body 10 is stablized.
More particularly, propeller component 20 includes link 21, helical blade 22 and rotary electric machine, and link 21 is solid
It is connected on body 10, is set on link 21 there are two linking arm, two linking arm intervals are arranged.It is corresponding in two linking arms
On be articulated with helical blade 22, rotary electric machine is for driving helical blade 22 to rotate.In this way, each propeller component 20 has
There are two spaced helical blades 22, keep the distribution bigger of helical blade 22 wider, flight structure is more stable.Certainly, on
State rotary electric machine can be equipped with it is multiple, for driving each helical blade 22 respectively, rotary electric machine also can only be arranged one, for uniting
The one multiple helical blades 22 of driving rotate.
Further, it can also be equipped with fender bracket 11 on body 10, fender bracket 11 is made to enclose set on multiple propeller components 20
Periphery prevent the flight of propeller component 20 impacted in this way, fender bracket 11 can block external wind-force or sundries, fly
Row structure is more stablized.
Further, also it can be equipped with battery cavities and battery 50 on the top of body 10, makes battery 50 with dismountable side
Formula is installed in battery cavities, and battery 50 is used to power to body 10, is specifically used for powering to the flight of propeller component 20.And it is electric
Pond 50 is removable convenient for replacement battery 50 at any time.
Particularly, bayonet is equipped on the side wall of 50 chamber of battery, it is corresponding to be equipped with hook in the side of battery 50, make card
Hook is connected in bayonet, can realize the detachable affixed of battery 50 and battery cavities.
The above embodiment is only preferred embodiments of the present invention, cannot be protected with this to limit the utility model
Range, the variation of any unsubstantiality that those skilled in the art is done on the basis of the utility model and replacing belongs to
In the utility model range claimed.
Claims (10)
1. a kind of unmanned plane, body, propeller component and pickup folder, propeller component are rotatably installed on body and are used in combination
It flies in driving body;It is characterized in that:Pickup folder is installed on the bottom end of body;The pickup folder includes top pressure block, at least two
A clamping jaw and at least two connecting rods, the top pressure block are installed on the bottom end of body and can be moved along the short transverse of body, until
Few two clamping jaws are arranged around the top pressure block circle spacing;One end of at least two connecting rods corresponds and is articulated at least two folders
On pawl;The other end of at least two connecting rods is articulated on top pressure block;The top of clamping jaw is articulated with the bottom end of body;Clamping jaw
Bottom end, which is equipped with to hook, takes portion.
2. unmanned plane as described in claim 1, it is characterised in that:One of portion of taking that hooks is used to take portion with another opposite hook
Form closing structure.
3. unmanned plane as described in claim 1, it is characterised in that:Pickup folder includes driving device, and driving device is for driving
Top pressure block is moved along the short transverse of body.
4. unmanned plane as claimed in claim 3, it is characterised in that:Driving device includes driving motor and screw rod, the drive
Dynamic motor is installed on body, and the screw rod extends along the short transverse of body and connection synchronous with the shaft of driving motor;Institute
Top pressure block is stated to be set on screw rod and with screw flight coordinate.
5. unmanned plane as described in claim 1, it is characterised in that:The bottom end of the top pressure block is equipped with rubber pad.
6. unmanned plane as described in any one in claim 1-5, it is characterised in that:Propeller component is equipped with multiple, multiple spirals
Paddle component is arranged around the central axis circle spacing of the body.
7. unmanned plane as claimed in claim 6, it is characterised in that:Propeller component includes link, helical blade and turns
Dynamic motor, link are fixed on body, set that there are two spaced linking arms on link;It is pivotally connected on two linking arms
There is the helical blade;The rotary electric machine is for driving helical blade to rotate.
8. unmanned plane as claimed in claim 6, it is characterised in that:Body is equipped with fender bracket, and the fender bracket is enclosed set on more
The periphery of a propeller component.
9. unmanned plane as described in any one in claim 1-5, it is characterised in that:The top of body is equipped with battery cavities and electricity
Pond, the battery are removably installed in battery cavities and for powering to body.
10. unmanned plane as claimed in claim 9, it is characterised in that:The side wall of battery cavities is equipped with bayonet, and the side of battery is set
There are hook, hook to be connected in bayonet.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201721659791.4U CN207773481U (en) | 2017-12-01 | 2017-12-01 | A kind of unmanned plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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CN201721659791.4U CN207773481U (en) | 2017-12-01 | 2017-12-01 | A kind of unmanned plane |
Publications (1)
Publication Number | Publication Date |
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CN207773481U true CN207773481U (en) | 2018-08-28 |
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CN201721659791.4U Active CN207773481U (en) | 2017-12-01 | 2017-12-01 | A kind of unmanned plane |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110606216A (en) * | 2019-09-16 | 2019-12-24 | 安徽天德无人机科技有限公司 | Intelligent sensing anti-collision device and plant protection unmanned aerial vehicle with same |
-
2017
- 2017-12-01 CN CN201721659791.4U patent/CN207773481U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN110606216A (en) * | 2019-09-16 | 2019-12-24 | 安徽天德无人机科技有限公司 | Intelligent sensing anti-collision device and plant protection unmanned aerial vehicle with same |
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