CN206590119U - Uas - Google Patents
Uas Download PDFInfo
- Publication number
- CN206590119U CN206590119U CN201720259009.3U CN201720259009U CN206590119U CN 206590119 U CN206590119 U CN 206590119U CN 201720259009 U CN201720259009 U CN 201720259009U CN 206590119 U CN206590119 U CN 206590119U
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- CN
- China
- Prior art keywords
- grab
- uas
- housing
- remote control
- unmanned plane
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Abstract
The utility model discloses a kind of UAS, including unmanned plane and remote control, the shell of the remote control is provided with the first grab, the unmanned plane is provided with the second grab, and first grab and/or second grab are flexible, first grab and second grab are by mutually supporting to fix the unmanned plane and the remote control.Technical solutions of the utility model are mutually supported to fix unmanned plane and remote control by using the first grab and the second grab is set on unmanned plane and remote control by the first grab and the second grab, reach that unmanned plane and remote control pick and place convenient effect.
Description
Technical field
The utility model is related to unmanned plane field, more particularly to a kind of UAS.
Background technology
With the development of science and technology, unmanned plane technology is increasingly favored by people, but nobody is used in people
After machine, existing unmanned plane and its remote control are all separately taken, and user needs to take unmanned plane on the other hand, and another hand is taken distant
Control device carries out picking and placeing for equipment, causes unmanned plane and its problem of picking and placeing inconvenience of remote control.
Utility model content
Main purpose of the present utility model is to propose a kind of UAS, it is intended to solve unmanned plane and its remote control is picked and placeed
Inconvenient the problem of.
To achieve the above object, the utility model proposes UAS, including unmanned plane and remote control, the remote control
The shell of device is provided with the first grab, and the unmanned plane is provided with the second grab, and first grab and/or second card
Hitcher is flexible, and first grab and second grab are by mutually supporting to fix the unmanned plane and the remote control
Device.
Preferably, the remote control includes the first housing, the second housing and is connected to first housing and second shell
Telescoping mechanism between body；The UAS includes the first grab and the second grab described in two groups, two first cards
Hook is separately positioned in the relative position of first housing and the second housing, and the line side between two first grabs
To consistent with the telescopic direction of the telescoping mechanism.
Preferably, the telescoping mechanism includes the elastic component and slide bar being arranged in the first shell body, the slide bar one
End is connected with the elastic component, and the other end is fixed on second housing.
Preferably, the remote control also includes the first bottom being detachably fixed with first housing and is arranged on described
Retaining mechanism on first bottom, the retaining mechanism includes being arranged on neck on second housing and with described first
The Fastener that bottom is oppositely arranged, the Fastener includes fixed part and the pothook with the neck shape adaptation, the card
The thickness of hook portion is more than the thickness of the fixed part；The pothook is moveable sliding to setting one away from the side of the neck
Block, the sliding block is provided with a shifting block away from the side of the pothook；First bottom is opened with the shifting block corresponding position
There is a strip groove, the shifting block stretches out from the strip groove, and can be moved along the strip groove.
Preferably, the pothook is provided with guiding surface with the position that the sliding block offsets.
Preferably, the catch surface of first grab and second grab is plane.
Preferably, the end of first grab is provided with the first spigot surface, and the end of second grab is led provided with second
To face.
Preferably, first spigot surface and second spigot surface are inclined-plane or arc surface.
Preferably, second grab is arranged on the unmanned motor spindle.
Technical solutions of the utility model are led to by using the first grab and the second grab is set on unmanned plane and remote control
Cross the first grab and the second grab mutually supports to fix unmanned plane and remote control, reach that unmanned plane and remote control are picked and placeed easily
Effect.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
Or the accompanying drawing used required in description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to the structure shown in these accompanying drawings.
Fig. 1 is the structural representation of the utility model UAS first embodiment；
Fig. 2 is the partial enlarged drawing at A in Fig. 1；
Fig. 3 is the structural representation of the utility model UAS second embodiment；
Fig. 4 is the structural representation of the utility model UAS 3rd embodiment；
Fig. 5 is the partial enlarged drawing at B in Fig. 4；
Fig. 6 is the structural representation of the utility model UAS fourth embodiment；
Drawing reference numeral explanation：
Realization, functional characteristics and the advantage of the utility model purpose will be described further referring to the drawings in conjunction with the embodiments.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the utility model embodiment is carried out
Clearly and completely describe, it is clear that described embodiment is only a part of embodiment of the present utility model, rather than all
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not making creative work premise
Lower obtained every other embodiment, belongs to the scope of the utility model protection.
If it is to be appreciated that related in the utility model embodiment directionality indicate (such as upper and lower, left and right, it is preceding,
Afterwards ...), then directionality indicates to be only used for explaining relative between each part under a certain particular pose (as shown in drawings)
Position relationship, motion conditions etc., if the particular pose changes, directionality indicates also correspondingly therewith to change.
If, should " first ", " the in addition, relate to the description of " first ", " second " etc. in the utility model embodiment
Two " etc. description is only used for describing purpose, and it is not intended that indicating or implying its relative importance or implicit indicate meaning
The quantity of the technical characteristic shown.Thus, " first " is defined, the feature of " second " can express or implicitly include at least one
Individual this feature.In addition, the technical scheme between each embodiment can be combined with each other, but must be with ordinary skill
Personnel can be implemented as basis, when the combination appearance of technical scheme is conflicting or can not realize it will be understood that this technical side
The combination of case is not present, also not within the protection domain of the utility model requirement.
The utility model proposes a kind of UAS.
In the utility model embodiment, as shown in Fig. 1, Fig. 4 and Fig. 6, the UAS includes unmanned plane 100 and distant
Device 200 is controlled, the shell of the remote control 200 is provided with the first grab 300, and the unmanned plane 100 is provided with the second grab 400,
First grab 300 and/or second grab 400 are flexible, first grab 300 and second grab 400
Mutually support.Unmanned plane 100 and remote control 200 by the first grab 300 and the second grab 400 be fastened on together with to realize nobody
Machine 100 is fixedly connected with remote control 200, so that user is when without using unmanned plane 100, convenient unmanned plane 100 of taking simultaneously
With remote control 200.At least needed in first grab 300 and the second grab 400 one it is flexible, could realize and block
Function.In the present embodiment, the shape and position of the first grab 300 and the second grab 400 are preferably corresponding, and actually should
During, only there need to be certain overlapping area, area is bigger when the first grab 300 and the second grab 400 are being hooked, block
Effect firmly is more stablized, and to determine the size of grab according to the size of actual remote control 200 and unmanned plane 100 certainly.
In the present embodiment, the clamping length of first grab 300 and second grab 400 is preferably set to 34mm, also can be according to reality
Border situation is set to other length.The remote control 200 and unmanned plane 100 can be by way of sideslips by the He of the first grab 300
Second grab 400, which is blocked, to offset, and also can directly be interlocked by conventional click on fashion.
Technical solutions of the utility model on unmanned plane 100 and remote control 200 by using setting the first grab 300 and
Two grabs 400, are mutually supported to fix unmanned plane 100 and remote control 200 by the first grab 300 and the second grab 400, reached
Unmanned plane 100 and remote control 200 pick and place convenient effect.
Further, reference picture 3, the remote control 200 includes the first housing 210, the second housing 220 and is connected to institute
State the telescoping mechanism 230 between the first housing 210 and the second housing 220；The UAS includes two group of first grab 300
With the second grab 400, two first grabs 300 are separately positioned on the relative of the housing 220 of the first housing 210 and second
On position, and the line direction between two first grabs 300 is consistent with the telescopic direction of the telescoping mechanism 230.Institute
State telescoping mechanism 230 to be connected between the first housing 210 and the second housing 220, when the first housing 210 and the quilt of the second housing 220
When pulling open, telescoping mechanism 230 can give screen resilience mutual between the first housing 210 and the second housing 220, and two first are blocked
Hook 300 is separately positioned on the first housing 210 and the second housing 220, and the line direction between two first grabs 300
It is consistent with the telescopic direction of the telescoping mechanism 230, then certain screen resilience can be also produced between two the first grabs 300, when
When first grab 300 and the second grab 400 interlock, the first grab 300 can give the second grab 400 certain fastening force, so that
So that the effect that the first grab 300 and the second grab 400 are blocked is more preferably, the fixed effect between unmanned plane 100 and remote control 200
It is more stable.
Specifically, with continued reference to Fig. 3, the telescoping mechanism 230 includes the elastic component being arranged in first housing 210
231 and slide bar 232, described one end of slide bar 232 is connected with the elastic component 231, and the other end is fixed on second housing 220
On.The elastic component 231 is returned to original position, i.e., the cunning that 231 pairs of elastic component is pulled out after being pulled out by slide bar 232
Bar 232 has a screen resilience.Elastic component 231 can use spring base part, in the present embodiment, preferably use wind spring.Slide bar 232
It is fixedly connected with the second housing 220 so that the second housing 220 is more stablized during slip.Meanwhile, can be according to unmanned plane
100 size determines the stretching distance between the first housing 210 and the second housing 220, that is, two the first grabs 300 it
Between distance.
Further, reference picture 3, the remote control 200 also includes first be detachably fixed with first housing 210
Bottom 250 and the retaining mechanism 240 being arranged on first bottom 250, the retaining mechanism 240 include being arranged on described the
Neck 241 on two housings 220 and the Fastener 242 being oppositely arranged with first bottom 250, the Fastener 242 are wrapped
Fixed part 243 and the pothook 244 with the shape adaptation of neck 241 are included, the thickness of the pothook 244 is more than the fixation
The thickness in portion 243；The pothook 244 supports away from the side of the neck 241 and sets a movable sliding block 246, the sliding block
246 are provided with a shifting block 247 away from the side of the pothook 244；First bottom 250 and the relevant position of shifting block 247
Place is provided with a strip groove 251, and the shifting block 247 stretches out from the strip groove 251, and can be along the strip groove 251
It is mobile.When the second housing 220 and the first housing 210 are pulled open, by (direction in figure) to the right mobile shifting block 247 with band movable slider
246 slide to the right so that sliding block 246 is given the pothook 244 and upwarded pressure, so top pressure pothook 244 be caught in it is described
In neck 241, to realize the continuation campaign of the second housing 220 of limitation, so as to limit the continuation campaign of the first grab 300.
The Fastener 242 is oppositely arranged with the first bottom 250, and fixed part 243 is used to fix Fastener 242, the card
The thickness of hook portion 244 is more than the thickness of the fixed part 243 so that can be upward by pothook 244 when sliding block 246 is slided to the right
Top.In actual applications, depending on the thickness of pothook 244 can be according to actual conditions, as long as can guarantee that pothook 244 can be caught in card
In groove 241.Pothook 244 is set as guiding surface 245 with the position that sliding block 246 offsets, and is risen in the sliding process of sliding block 246
Guide effect.The shape of the pothook 244 is adapted with the shape of the neck 241, so that the can completely card of pothook 244
Enter in the neck 241.The shape of the neck 241 can be circular or zigzag, in the present embodiment, in order to which card sets effect more
Good, preferably neck 241 is serrated.In actual application, also pothook 241 can need to only be blocked by the way of button
Enter in neck 241.In the present embodiment, in order to save space, the sliding block 246 with shifting block 247 is preferably provided with, by the right
(direction in such as figure) stirs shifting block 247, then pothook 241 described in the top pressure of sliding block 246, and then be caught in the neck 241.
Further, reference picture 4 and Fig. 5, the first catch surface 310 of first grab 300 and second grab 400
For plane, the second catch surface 410 of second grab 400 and first grab 300 is plane.When the first grab 300 with
When second grab 400 interlocks, its face abutted against is set to platen surface, when the first housing 210 and second shell of stretching remote control 200
During body 220, first grab 300 on the second housing 220 directly can depart from second grab 400, so as to realize
Tripping between unmanned plane 100 and the remote control 200.
Further, referring to Figures 1 and 2, the end of first grab 300 is provided with the first spigot surface 320, described second
The end of grab 400 is provided with the second spigot surface 420.When unmanned plane 100 needs to be connected with remote control 200, by unmanned plane 100 to
Remote control 200 is pressed, so that the first spigot surface 320 and the second spigot surface 420 are contacted and compressed, is preferably provided to arc surface or oblique
Face causes the pressure energy of second 400 pair of first grab 300 of grab to resolve into downward pressure and outside pressure (side in such as figure
To), so that the first grab 300 top be opened, continue to press unmanned plane 100 so that the second kink 410 enters first groove 320
In, while remote control 200 is by screen resilience so that the first grab 300 is caught in second groove 420, realize the first grab 300
With the fastening function of the second grab 400.
Further, first grab 300 is symmetrical set with second grab 400 so that unmanned plane 100 with it is distant
The effect that control device 200 is fixedly connected more preferably, while the second grab 400 is arranged on into unmanned motor spindle, more adapts to taking for user
Take custom.
Preferred embodiment of the present utility model is the foregoing is only, the scope of the claims of the present utility model is not thereby limited,
It is every under inventive concept of the present utility model, the equivalent structure made using the utility model specification and accompanying drawing content is become
Change, or directly/be used in other related technical fields indirectly and be included in scope of patent protection of the present utility model.
Claims (9)
1. a kind of UAS, it is characterised in that including unmanned plane and remote control, the shell of the remote control is provided with first
Grab, the unmanned plane is provided with the second grab, and first grab and/or second grab are flexible, and described the
One grab and the second grab are by mutually supporting the fixed unmanned plane and remote control.
2. UAS as claimed in claim 1, it is characterised in that the remote control includes the first housing, the second housing
And it is connected to the telescoping mechanism between first housing and the second housing；The UAS is included first described in two groups
Grab and the second grab, two first grabs are separately positioned in the relative position of first housing and the second housing,
And the line direction between two first grabs is consistent with the telescopic direction of the telescoping mechanism.
3. UAS as claimed in claim 2, it is characterised in that the telescoping mechanism includes being arranged on the first shell
Internal elastic component and slide bar, described slide bar one end is connected with the elastic component, and the other end is fixed on second housing.
4. UAS as claimed in claim 2 or claim 3, it is characterised in that the remote control also includes and the first shell
The first bottom that body is detachably fixed and the retaining mechanism being arranged on first bottom, the retaining mechanism include being arranged on
Neck on second housing and the Fastener being oppositely arranged with first bottom, the Fastener include fixed part and
With the pothook of the neck shape adaptation, the thickness of the pothook is more than the thickness of the fixed part；The pothook back of the body
From the side of the neck to a movable sliding block is set, the sliding block is away from the side of the pothook provided with a shifting block；Institute
State the first bottom and be provided with a strip groove with the shifting block corresponding position, the shifting block stretches out from the strip groove, and
It can be moved along the strip groove.
5. UAS as claimed in claim 4, it is characterised in that the position that the pothook offsets with the sliding block is set
There is guiding surface.
6. the UAS as described in claims 1 to 3 any one, it is characterised in that first grab and described the
The catch surface of two grabs is plane.
7. UAS as claimed in claim 6, it is characterised in that the end of first grab is oriented to provided with first
Face, the end of second grab is provided with the second spigot surface.
8. UAS as claimed in claim 7, it is characterised in that first spigot surface and second spigot surface are
Inclined-plane or arc surface.
9. UAS as claimed in claim 1, it is characterised in that second grab is arranged on the unmanned plane bottom
Portion.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720259009.3U CN206590119U (en) | 2017-03-16 | 2017-03-16 | Uas |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720259009.3U CN206590119U (en) | 2017-03-16 | 2017-03-16 | Uas |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206590119U true CN206590119U (en) | 2017-10-27 |
Family
ID=60124412
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720259009.3U Active CN206590119U (en) | 2017-03-16 | 2017-03-16 | Uas |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206590119U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110155331A (en) * | 2019-01-03 | 2019-08-23 | 国网山东省电力公司济宁供电公司 | A kind of attachment device and its application method of connection unmanned plane and throwing hang device |
| CN110155331B (en) * | 2019-01-03 | 2024-05-17 | 国网山东省电力公司济宁供电公司 | Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof |
-
2017
- 2017-03-16 CN CN201720259009.3U patent/CN206590119U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110155331A (en) * | 2019-01-03 | 2019-08-23 | 国网山东省电力公司济宁供电公司 | A kind of attachment device and its application method of connection unmanned plane and throwing hang device |
| CN110155331B (en) * | 2019-01-03 | 2024-05-17 | 国网山东省电力公司济宁供电公司 | Connecting device for connecting unmanned aerial vehicle and throwing and hanging device and using method thereof |
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