CN206202681U - Wing installation connecting hardware for unmanned aerial vehicle - Google Patents
Wing installation connecting hardware for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN206202681U CN206202681U CN201621234054.5U CN201621234054U CN206202681U CN 206202681 U CN206202681 U CN 206202681U CN 201621234054 U CN201621234054 U CN 201621234054U CN 206202681 U CN206202681 U CN 206202681U
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- CN
- China
- Prior art keywords
- wing
- groove
- wing arm
- mounting groove
- screw
- Prior art date
- 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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Links
- 238000009434 installation Methods 0.000 title claims abstract description 15
- 230000035939 shock Effects 0.000 claims abstract description 16
- 238000013016 damping Methods 0.000 claims abstract description 11
- 210000005056 cell body Anatomy 0.000 claims description 13
- 229920000742 Cotton Polymers 0.000 claims description 6
- 239000002390 adhesive tape Substances 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 abstract 3
- 239000004576 sand Substances 0.000 abstract 1
- 230000000694 effects Effects 0.000 description 5
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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- Vibration Dampers (AREA)
Abstract
The utility model relates to a wing installation and connection hardware for an unmanned aerial vehicle, which comprises a wing arm and an installation platform; the side surface of the mounting table is welded with a connecting piece, and the connecting piece comprises a mounting groove body for accommodating the wing arm and a rotating cover plate which is rotatably connected with the upper surface of the mounting groove body; a plurality of clamping grooves are formed in the inner wall of the mounting groove body; the side surface of the wing arm is provided with a convex strip matched with the clamping groove; the rotating cover plate is provided with locking screws, buffering shock absorbing pieces and grooves for mounting the buffering shock absorbing pieces, and a plurality of grooves are distributed on the rotating cover plate in the transverse direction and the longitudinal direction; the height of the buffering and damping piece is greater than the depth of the groove; the mounting groove body is provided with a screw hole matched with the locking screw; during the installation, correspond the card with wing arm tip downwards sand grip and draw-in groove and go into the mounting groove internal, rotate and rotate the apron, lock through locking screw and screw, cushion the damping member this moment and compressed to the recess in, simple to operate, prevent horizontal and vertically not hard up effectual, can effectively reduce the wing arm vibration in addition and influence the fuselage.
Description
Technical field
The utility model is related to hardware-joint technical field, is installed with wing more specifically to a kind of unmanned plane
Connection handware.
Background technology
With the development of unmanned plane, the various connection handwares on unmanned plane have also obtained development faster；Mesh
The preceding unmanned plane wing for using, mostly using being directly connected to or being fixedly connected by screw, is dismounted more inconvenience or connected with mounting disc
Easily occur loosening after connecing, cause flight failure.
Utility model content
The technical problems to be solved in the utility model is, for the drawbacks described above of prior art, there is provided it is a kind of it is anti-loosening,
The unmanned plane of shock-absorbing and good damping effect wing installs connection handware.
The utility model solves the technical scheme that its technical problem used：
Construct a kind of unmanned plane wing and connection handware, including wing arm and erecting bed are installed；Wherein, the erecting bed
Side surface is welded with connector, and the connector includes accommodating the installation cell body of the wing arm and installs cell body upper table with described
Face rotates the rotating plate of connection；Wall is provided with multiple draw-in grooves in the mounting groove body；The wing arm side surface be provided with
The raised line of the pocket matches；Tight lock screw, bumper and absorbing shock part are provided with the rotating plate and the bumper and absorbing shock is installed
The groove of part, the groove on the rotating plate it is horizontal and vertical be distributed with it is a plurality of；The bumper and absorbing shock part is highly more than
The depth of groove；The screw coordinated with the tight lock screw is provided with the installation cell body.
Unmanned plane described in the utility model wing installs connection handware, wherein, the bumper and absorbing shock part includes position
In the shock-absorbing cotton of the inside grooves and the damping adhesive tape being connected with the shock-absorbing cotton.
Unmanned plane described in the utility model wing installs connection handware, wherein, the rotating plate surface is set
There is damping pad.
Unmanned plane described in the utility model wing installs connection handware, wherein, the mounting groove external surface sets
It is equipped with the location hole connected with the screw；Also include the alignment pin coordinated with the location hole；Set on the tight lock screw
There is the annular groove with the detent fit.
The beneficial effects of the utility model are：During installation, peace is snapped in by the downward raised line in wing arm end is corresponding with draw-in groove
In tankage body, rotating plate is rotated, locked with screw by tight lock screw, now bumper and absorbing shock part is compressed into groove
It is interior, it is easy for installation, prevent laterally and longitudinal direction loosen effect it is good, can effectively reduce in addition wing arm vibration on fuselage influence；
Overall structure is simple, low cost.
Brief description of the drawings
In order to illustrate more clearly about the embodiment of the present invention or technical scheme of the prior art, below in conjunction with accompanying drawing and reality
The utility model is described in further detail to apply example, and drawings in the following description are only section Example of the invention, for this
For the those of ordinary skill of field, on the premise of not paying creative work, other can also be obtained according to these accompanying drawings attached
Figure：
Fig. 1 is that the unmanned plane of the utility model preferred embodiment installs connection handware structural representation with wing；
Fig. 2 is that the unmanned plane of the utility model preferred embodiment installs connection handware wing arm, installs cell body with wing
Sectional top view；
Fig. 3 is that the unmanned plane of the utility model preferred embodiment installs connection handware rotating plate structural representation with wing
Figure.
Specific embodiment
In order that the purpose, technical scheme and advantage of the utility model embodiment are clearer, below in conjunction with this practicality
Technical scheme in new embodiment carries out clear, complete description, it is clear that described embodiment is portion of the present utility model
Divide embodiment, rather than whole embodiments.Based on embodiments of the invention, those of ordinary skill in the art are not paying creation
Property work on the premise of the every other embodiment that is obtained, belong to protection domain of the present utility model.
The unmanned plane of the utility model preferred embodiment installs connection handware as shown in figure 1, referring to Fig. 2 simultaneously with wing
And Fig. 3, including wing arm 1 and erecting bed 2, the side surface of erecting bed 2 is welded with connector 3, and connector 3 includes accommodating wing arm 1
Installation cell body 30 and rotate the rotating plate 31 that is connected with cell body 30 upper surface is installed；The inwall of cell body 30 is installed and is provided with multiple
Draw-in groove 300；The side surface of wing arm 1 is provided with the raised line 10 matched with draw-in groove 300；Tight lock screw is provided with rotating plate 31
310th, the groove 312 of bumper and absorbing shock part 311 and installation bumper and absorbing shock part 311, groove 312 is horizontal and vertical on rotating plate 32
It is distributed with a plurality of；The height of bumper and absorbing shock part 311 is more than the depth of groove 312；Install to be provided with cell body 30 and match somebody with somebody with tightly lock screw 310
The screw 301 of conjunction；During installation, snap in corresponding with draw-in groove 300 of the downward raised line 10 in the end of wing arm 1 is installed in cell body 30, rotated
Rotating plate 31, is locked by tight lock screw 310 with screw 301, and now bumper and absorbing shock part 311 is compressed into groove 312
It is interior, it is easy for installation, prevent laterally and longitudinal direction loosen effect it is good, can effectively reduce in addition wing arm 1 vibrate on fuselage influence；
Overall structure is simple, low cost.
As shown in figures 1 and 3, bumper and absorbing shock part 311 include shock-absorbing cotton 313 inside the groove 312 and with shock-absorbing cotton
The damping adhesive tape 314 of 313 connections；Damping and shock-absorbing effect are good.
As shown in figures 1 and 3, the surface of rotating plate 31 is provided with damping pad 315, is deformed upon during installation, damping with
And the rotation of anti-wing arm 1 to loosen effect good.
As depicted in figs. 1 and 2, the outer surface of cell body 30 is installed and is provided with the location hole 302 connected with screw 310；Also include
The alignment pin (not shown) coordinated with location hole 302；It is provided with tight lock screw 310 and is matched somebody with somebody with alignment pin (not shown)
The annular groove (not shown) of conjunction；Further prevent screw from loosening situation occur.
It should be appreciated that for those of ordinary skills, can according to the above description be improved or converted,
And all these modifications and variations should all belong to the protection domain of the utility model appended claims.
Claims (4)
1. a kind of unmanned plane wing installs connection handware, including wing arm and erecting bed；Characterized in that, the erecting bed
Side surface is welded with connector, and the connector includes accommodating the installation cell body of the wing arm and installs cell body upper table with described
Face rotates the rotating plate of connection；Wall is provided with multiple draw-in grooves in the mounting groove body；The wing arm side surface be provided with
The raised line of the pocket matches；Tight lock screw, bumper and absorbing shock part are provided with the rotating plate and the bumper and absorbing shock is installed
The groove of part, the groove on the rotating plate it is horizontal and vertical be distributed with it is a plurality of；The bumper and absorbing shock part is highly more than
The depth of groove；The screw coordinated with the tight lock screw is provided with the installation cell body.
2. unmanned plane according to claim 1 wing installs connection handware, it is characterised in that the bumper and absorbing shock part
The damping adhesive tape being connected including the shock-absorbing cotton positioned at the inside grooves and with the shock-absorbing cotton.
3. unmanned plane according to claim 2 wing installs connection handware, it is characterised in that the rotating plate table
Face is provided with damping pad.
4. unmanned plane according to claim 3 wing installs connection handware, it is characterised in that the mounting groove is external
Surface is provided with the location hole connected with the screw；Also include the alignment pin coordinated with the location hole；The tight lock screw
On be provided with annular groove with the detent fit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621234054.5U CN206202681U (en) | 2016-11-17 | 2016-11-17 | Wing installation connecting hardware for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621234054.5U CN206202681U (en) | 2016-11-17 | 2016-11-17 | Wing installation connecting hardware for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206202681U true CN206202681U (en) | 2017-05-31 |
Family
ID=58750280
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621234054.5U Active CN206202681U (en) | 2016-11-17 | 2016-11-17 | Wing installation connecting hardware for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206202681U (en) |
-
2016
- 2016-11-17 CN CN201621234054.5U patent/CN206202681U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 518000 on the first floor of building B, No.5 Yonghe Road, Longteng community, Shiyan street, Bao'an District, Shenzhen, Guangdong Patentee after: Shenzhen jinchangxing Precision Machinery Co., Ltd Address before: 518000, Guangdong, Shenzhen province Baoan District Shiyan street, dragon community, Yonghe Road, No. 5, the upper Industrial Zone workshop A, B building (B building, 1 floor) Patentee before: SHENZHEN KIM CHANGXING PRECISION HARDWARE Co.,Ltd. |
|
| CP03 | Change of name, title or address |