CN205524975U - Unmanned aerial vehicle wing safety cover - Google Patents
Unmanned aerial vehicle wing safety cover Download PDFInfo
- Publication number
- CN205524975U CN205524975U CN201620173163.4U CN201620173163U CN205524975U CN 205524975 U CN205524975 U CN 205524975U CN 201620173163 U CN201620173163 U CN 201620173163U CN 205524975 U CN205524975 U CN 205524975U
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- CN
- China
- Prior art keywords
- cover
- mouth
- cover body
- hole
- embedding
- 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.)
- Expired - Fee Related
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Abstract
The utility model relates to an unmanned aerial vehicle field, specific unmanned aerial vehicle wing safety cover that says so, personally experience sth. Part of the body and fastening screw including mount, support frame, bracing piece, adapter sleeve, a cover body, no. Two covers. The mount is including the annular ring of circle cover and the dead lever of setting around the ring cover, the dead lever is even to be set up to the side of encircling the cover, has set gradually an embedding mouth and no. Two embedding mouths on the side of dead lever upper portion, and the axle center department of dead lever still is provided with the screw hole, a cover body is the annular, and the position that cover body lower half is corresponding with embedding mouth is provided with the one number service hole, no. Two cover bodies are the annular, and the position that no. Two cover body lower halves are corresponding with no. Two embedding mouths is provided with the through -hole no. Two, fastening screw sets up at threaded hole. The utility model discloses can prevent that the rotor from being disturbed by branch or fallen leaves, also can prevent to hurt sb. 's feelings because of the rotor that unmanned aerial vehicle trouble or misoperation lead to.
Description
Technical field
This utility model relates to unmanned plane field, a kind of unmanned plane wing protective cover.
Background technology
Rotor wing unmanned aerial vehicle, its frame is provided with multiple rotor being driven high speed rotating by motor, by the height of driven by motor rotor
Speed rotates, and the counteracting force by high velocity air drives unmanned plane during flying.In order to alleviate load, rotor wing unmanned aerial vehicle needs as far as possible
Gently, the rotor of traditional unmanned plane is all not provided with any preventer, therefore when indoor and outdoor flight, especially at environment relatively
For, time in complicated forest or city, unmanned plane being made to collide with the object in environment with misoperation inside, with
Time in forest various branches or fallen leaves rotor may be interfered, so can the frame for movement of unmanned plane be caused bigger
Damage, may cause situation that is out of control or that fall.Additionally for the rotor wing unmanned aerial vehicle of toys, owing to being difficult to manipulation, unmanned
Machine is easy to the crowd of flying to, and causes rotor to be cut to the arm of operator or audience, damages.
Summary of the invention
For the problems of the prior art, this utility model provides a kind of unmanned plane wing protective cover, is possible to prevent rotor to be set
Branch or fallen leaves interference, it is also possible to prevent the rotor caused because of unmanned plane fault or operational error from hurting sb.'s feelings.
This utility model solves its technical problem and be the technical scheme is that a kind of unmanned plane wing protective cover, including fixed mount,
Bracing frame, support bar, adapter sleeve, a cover body, No. two cover bodies and trip bolt.
Ring set that described fixed mount includes annular and the fixing bar being arranged on around ring set；Described fixing bar is cylinder,
Fixing bar quantity is three, and three fixing bars are uniformly arranged on ring set side, and fixing bar upper side is disposed with an embedding
Mouth and No. two embedding mouths, be additionally provided with screwed hole at the axle center of fixing bar；A described embedding mouth and No. two embedding mouths are the most solid
At the axle center of fixed pole.
Described bracing frame includes montant and cross bar；Described montant is arranged on below fixed mount；Described cross bar is fixed on montant
Bottom.
Described support bar one end is fixing with cross bar to be connected, and the support bar other end is connected with adapter sleeve；Under described adapter sleeve includes
Lobe and epivalve, this hypovalve and epivalve are all in semi-circular.
Ringwise, a cover body lower half is provided with one number service hole in the position embedding mouth corresponding with No. to a described cover body,
The diameter in this one number service hole is identical with the diameter of screwed hole.
Ringwise, No. two cover body lower half are provided with No. two through holes in the position embedding mouth corresponding with No. two to No. two described cover bodies,
The diameter of these No. two through holes is identical with the diameter of screwed hole.
Described trip bolt is arranged in screwed hole；Described trip bolt passes an one number service hole embedded in mouth, or
This trip bolt is through No. two No. two through holes embedded in mouth.
Preferably, described hypovalve and epivalve both sides correspondence position are provided with threaded connection hole.
The beneficial effects of the utility model are: a kind of unmanned plane wing protective cover of the present utility model, are possible to prevent rotor by branch
Or fallen leaves interference, it is also possible to prevent the rotor caused because of unmanned plane fault or operational error from hurting sb.'s feelings, and this utility model uses
Multiple protective enclosure of different-diameter, can select according to rotor flexible in size.
Accompanying drawing explanation
With embodiment, this utility model is further illustrated below in conjunction with the accompanying drawings.
Fig. 1 is explosive view of the present utility model；
Fig. 2 is perspective view during this utility model number cover body of installation；
Fig. 3 is perspective view during this utility model No. two cover bodies of installation；
Fig. 4 is the perspective view of fixed mount；
In figure: fixed mount (1), bracing frame (2), support bar (3), adapter sleeve (4), cover body (5), No. two cover bodies
(6), trip bolt (7), ring set (11), fixing bar (12), montant (21), cross bar (22), hypovalve (41), epivalve
(42), one number service hole (51), No. two through holes (61), embedding mouth (121), No. two embeddings mouth (122), screwed holes (123).
Detailed description of the invention
For the technological means making this utility model realize, creation characteristic, reach purpose and be easy to understand with effect, below knot
Conjunction is specifically illustrating, and this utility model is expanded on further.
Embodiment 1
As shown in Figure 1, Figure 2, Fig. 4, a kind of unmanned plane wing protective cover of the present embodiment, including fixed mount 1, bracing frame 2,
Strut 3,4, cover body 5 of adapter sleeve and trip bolt 7.
Ring set 11 that described fixed mount 1 includes annular and the fixing bar 12 being arranged on around ring set 11；Described fixing bar
12 in cylinder, and fixing bar 12 quantity is three, and three fixing bars 12 are uniformly arranged on ring set 11 side, fixing bar 12 top
It is disposed with No. one on side and embeds mouth 121 and No. two embedding mouths 122, at the axle center of fixing bar 12, be additionally provided with screwed hole
123；A described embedding mouth 121 and No. two embedding mouths 122 are all crossed at the axle center of fixing bar 12.
Described bracing frame 2 includes montant 21 and cross bar 22；Described montant 21 is arranged on below fixed mount 1；Described horizontal stroke
Bar 22 is fixed on bottom montant 21.
Described support bar 3 one end is fixing with cross bar 22 to be connected, and support bar 3 other end is connected with adapter sleeve 4；Described fastening
Set 4 includes hypovalve 41 and epivalve 42, and this hypovalve 41 and epivalve 42 are all in semi-circular；Described hypovalve 41 and epivalve 42 liang
Side correspondence position is provided with threaded connection hole.
Ringwise, cover body 5 lower half is provided with one in the position embedding mouth 121 corresponding with No. to a described cover body 5
Number through hole 51, the diameter in this one number service hole 51 is identical with the diameter of screwed hole 123.
Described trip bolt 7 is arranged in screwed hole 123, and this trip bolt 7 is through an one number service embedded in mouth 121
Hole 51.
Embodiment 2:
Such as Fig. 1, Fig. 3, Fig. 4, a kind of unmanned plane wing protective cover of the present embodiment, including fixed mount 1, bracing frame 2, prop up
Strut 3,4, No. two cover bodies 6 of adapter sleeve and trip bolt 7, its basic structure is with embodiment 1, and difference is: described
No. two cover bodies 6 ringwise, No. two cover body 6 lower half are provided with No. two through holes 61 in the position embedding mouth 122 corresponding with No. two,
The diameter of these No. two through holes 61 is identical with the diameter of screwed hole 123；Described trip bolt 7 embeds mouth 122 through No. two
No. two interior through holes 61.
A kind of unmanned plane wing protective cover of embodiment 12 in use, is possible to prevent rotor by branch or fallen leaves interference, it is possible to
To prevent the rotor caused because of unmanned plane fault or operational error from hurting sb.'s feelings, and this utility model uses multiple guarantors of different-diameter
Shroud body, can select according to rotor flexible in size.
Of the present utility model ultimate principle, principal character and advantage have more than been shown and described.The technical staff of the industry should
Solve, this utility model is not restricted to the described embodiments, the description in above-mentioned embodiment and description this practicality is simply described
Novel principle, on the premise of without departing from this utility model spirit and scope, this utility model also has various changes and modifications,
These changes and improvements both fall within the scope that this utility model is claimed.This utility model claims scope by appended power
Profit claim and equivalent thereof define.
Claims (2)
1. a unmanned plane wing protective cover, it is characterised in that: include fixed mount (1), bracing frame (2), support bar (3),
Adapter sleeve (4), a cover body (5), No. two cover bodies (6) and trip bolt (7)；
Described fixed mount (1) includes the ring set (11) of annular and is arranged on ring set (11) fixing bar (12) around；
Described fixing bar (12) is in cylinder, and fixing bar (12) quantity is three, and three fixing bars (12) are uniformly arranged on ring set
(11) side, fixing bar (12) upper side is disposed with No. one and embeds mouth (121) and No. two embeddings mouth (122),
It is additionally provided with screwed hole (123) at the axle center of fixing bar (12)；Described embedding mouth (121) and No. two embeddings mouth (122)
All cross at the axle center of fixing bar (12)；
Described bracing frame (2) includes montant (21) and cross bar (22)；Described montant (21) is arranged on fixed mount (1)
Lower section；Described cross bar (22) is fixed on montant (21) bottom；
Described support bar (3) one end is fixing with cross bar (22) to be connected, and support bar (3) other end is connected with adapter sleeve (4)；
Described adapter sleeve (4) includes that hypovalve (41) and epivalve (42), this hypovalve (41) and epivalve (42) are all in semi-circular；
Ringwise, cover body (5) lower half is embedding, with No. one, the position that mouth (121) is corresponding to a described cover body (5)
Being provided with one number service hole (51), the diameter in this one number service hole (51) is identical with the diameter of screwed hole (123)；
Ringwise, No. two cover body (6) lower half are embedding, with No. two, the position that mouth (122) is corresponding to No. two described cover bodies (6)
Being provided with No. two through holes (61), the diameter of these No. two through holes (61) is identical with the diameter of screwed hole (123)；
Described trip bolt (7) is arranged in screwed hole (123)；Described trip bolt (7) embeds mouth (121) through No. one
Interior one number service hole (51), or this trip bolt (7) is through No. two No. two through holes (61) embedded in mouth (122).
A kind of unmanned plane wing protective cover the most according to claim 1, it is characterised in that: described hypovalve (41) and upper
Lobe (42) both sides correspondence position is provided with threaded connection hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620173163.4U CN205524975U (en) | 2016-03-07 | 2016-03-07 | Unmanned aerial vehicle wing safety cover |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620173163.4U CN205524975U (en) | 2016-03-07 | 2016-03-07 | Unmanned aerial vehicle wing safety cover |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205524975U true CN205524975U (en) | 2016-08-31 |
Family
ID=56779917
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620173163.4U Expired - Fee Related CN205524975U (en) | 2016-03-07 | 2016-03-07 | Unmanned aerial vehicle wing safety cover |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205524975U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107458592A (en) * | 2017-07-25 | 2017-12-12 | 芜湖超源力工业设计有限公司 | A kind of new unmanned plane with fan blade protective cover |
-
2016
- 2016-03-07 CN CN201620173163.4U patent/CN205524975U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107458592A (en) * | 2017-07-25 | 2017-12-12 | 芜湖超源力工业设计有限公司 | A kind of new unmanned plane with fan blade protective cover |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Chen Haifeng Inventor before: Li Xialin |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20170713 Address after: 450000 Longhu Road, Taishan Road, Henan electrical machinery, Career Academy, Zhengzhou, Xinzheng, Henan Patentee after: Zhengzhou Yabai Intelligent Technology Co., Ltd. Address before: Wu Tan 246200 Anhui city of Anqing province Wangjiang County Liang Quan Xiang Han Village No. 1275 Patentee before: Li Xialin |
|
| 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: 20160831 Termination date: 20190307 |