CN206374964U - A kind of push type unmanned plane horn fold mechanism - Google Patents
A kind of push type unmanned plane horn fold mechanism Download PDFInfo
- Publication number
- CN206374964U CN206374964U CN201621155932.4U CN201621155932U CN206374964U CN 206374964 U CN206374964 U CN 206374964U CN 201621155932 U CN201621155932 U CN 201621155932U CN 206374964 U CN206374964 U CN 206374964U
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- CN
- China
- Prior art keywords
- rotating shaft
- unmanned plane
- contiguous block
- fold mechanism
- push type
- 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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Abstract
The utility model discloses a kind of push type unmanned plane horn fold mechanism, including rotating pipe clip, rotating shaft contiguous block, pushing block, optical axis, spring, Duct fixing clamp and inside and outside horn.Rotating pipe clip one end is connected with outer boom, the other end is played bolt by plug and is connected with rotating shaft contiguous block, rotating shaft contiguous block top surface is provided with barb via, inside is provided with respective track groove and screwed hole, and guide rail groove location is provided with a pushing block by boss, and pushing block one end is connected with optical axis, the other end is used as press surface, a helical spring is installed on the inside of pushing block press surface and between boss, Duct fixing clamp one end is connected by bolt with rotating shaft contiguous block, horn in the connection of one end.The utility model unmanned plane horn fold mechanism can realize that horn turns folding and deploys to fix, reasonable in design is solid and reliable, unmanned plane structure high intensity, the design requirement of downsizing are met, the use demand of the convenient carrying of unmanned plane, Fast Installation and storage is realized.
Description
Technical field
The utility model is related to a kind of UAV Components, specifically a kind of push type unmanned plane horn fold mechanism.
Background technology
At present, unmanned plane（UAV）Correlation technique is developed rapidly, be widely used in taking photo by plane, rescue, gloomy another fire prevention, security protection
It is that the live and work of people brings many facilities etc. various fields.Classify by flying platform configuration, unmanned plane can be divided into solid
Determine wing unmanned plane, rotor wing unmanned aerial vehicle, unmanned airship, umbrella wing unmanned plane, flapping wing unmanned plane etc., wherein multi-rotor unmanned aerial vehicle is in each row
The application in industry field is increasingly extensive.
Usual unmanned plane needs, according to different use fields, to carry corresponding functional devices, cause part type knot
Structure volume becomes big, especially multi-rotor unmanned aerial vehicle, and horn accordingly can increase and lengthen so that the storage and transport of body are carried
Become difficult, now in industry multi-rotor unmanned aerial vehicle is generally folded using latch plug-in type attachment structure, but its process is numerous
It is trivial complicated and to carry instrument at any time, it is related to that parts are more, installs and folding process is cumbersome, it is necessary to which certain technology is known
Know.This not only results in poor usage experience, and causes operating efficiency low, and structural reliability declines.
Utility model content
The purpose of this utility model is to provide a kind of push type unmanned plane horn fold mechanism, to solve above-mentioned background skill
The problem of being proposed in art.
To achieve the above object, the utility model provides following technical scheme：A kind of push type unmanned plane horn folding machine
Structure, including rotating pipe clip, rotating shaft contiguous block, pushing block, optical axis, spring, Duct fixing clamp and inside and outside horn.Characterized in that, described
Rotating pipe clip is connected with outer boom, and pipe clamp bottom side is provided with two vertical barbs, passes through rotary shaft and rotating shaft contiguous block phase
Even, the rotating shaft contiguous block top surface is provided with two slots wide with barb width, and inside is provided with pushing block and optical axis, institute
State pushing block one end using through hole with optical axis to be connected, the other end is used as press surface, and guide rail is installed on by the boss of rotating shaft contiguous block one
In groove, one section of the spring is fixed on one section of pushing block inside and is fixed on rotating shaft contiguous block lug boss position, described Duct fixing clamp one end
It is connected by bolt with rotating shaft contiguous block, horn in the connection of one end.
It is used as further program of the utility model：The rotating pipe clip surface is provided with two barbs.
It is used as further program of the utility model：Led in the rotating shaft contiguous block provided with corresponding optical axis guide rail groove and pushing block
Track slot.
It is used as further program of the utility model：When the folding or expansion, spring is produced by pressing pushing block
Elastic force promotes optical axis movement.
It is used as further program of the utility model：The anglec of rotation between the rotating pipe clip and rotating shaft contiguous block is maximum
For 135 °.
It is used as further program of the utility model：Provided with three fixing screwed holes, fixing pipe in the rotating shaft contiguous block
Folder opposite position has three installation through-holes, and its radius is identical.
It is used as further program of the utility model：The rotating shaft contiguous block, rotation pipe clamp, fixing pipe sandwiched are equipped with line
Road passes through hole.
Compared with prior art, the beneficial effects of the utility model are：Structure is novel, highly reliable, not only strengthens machine
Arm and can guarantee that fold after light-weight design, fold and expansion easy switching, meanwhile, described horn fold mechanism is pressed
Pressure pushing block moves inward optical axis, is rotated further by the first pipe clamp, can realize the folding and expansion of horn, and operating method is simple, real
Strong with property, the technical requirements to user are low.
Brief description of the drawings
Fig. 1 is structural representation when utility model is in deployed condition.
In figure：1- outer booms, 2- rotating pipe clips, 3- bolts, 4- barbs, 5- contiguous blocks, 6- plugs are played bolt, 7- circuits and passed through
Hole, 8- optical axises, 9 Duct fixing clamps, 10- springs, 11- pushing blocks, horn in 12-.
Embodiment
Below in conjunction with the accompanying drawing in this implementation new embodiment, the technical scheme in the utility model embodiment is carried out
It is clear, it is fully described by, it is clear that described embodiment is only a part of embodiment of the utility model, rather than whole
Embodiment.Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belongs to the scope of the utility model protection.
Referring to Fig. 1, in the utility model embodiment, a kind of push type unmanned plane horn fold mechanism, including outer boom
1, it is connected by bolt 3 with rotating pipe clip 2, the end face side of rotating pipe clip 2 is provided with barb 4, and makes a call to 6 by plug in spindle portion
It is connected with rotating shaft contiguous block 5, the top of rotating shaft contiguous block 5 is provided with the barb wide with barb by hole, and pushing block 10 is installed in its inside,
Pushing block 10 is spacing by guide groove, and square slot part installs spring 10 and throughhole portions install optical axis 8 to press and fix,
Contiguous block 5 is internally threaded hole, is connected by bolt with Duct fixing clamp 9, and interior horn 12 is equally bolted to fixing pipe
One end of folder, rotating pipe clip 2, contiguous block 5, Duct fixing clamp 9 are equipped with circuit and pass through hole 7.
The utility model structure is novel, by rational foldover design, accomplishes fast folding, and rapid deployment reduces space
Waste, transport portable, substantially increase operating efficiency and reduce cost of transportation.
It is obvious to a person skilled in the art that the utility model is not limited to the details of above-mentioned example embodiment, and
In the case of without departing substantially from spirit or essential attributes of the present utility model, it can realize that this practicality is new in other specific forms
Type.Therefore, no matter from the point of view of which point, embodiment all should be regarded as exemplary, and is nonrestrictive, this practicality is new
The scope of type limits by appended claims rather than described above, it is intended that the equivalency fallen in claim is contained
All changes in justice and scope are included in the utility model.Any reference in claim should not be considered as limitation
Involved claim.
Moreover, it will be appreciated that although the present specification is described in terms of embodiments, not each embodiment is only wrapped
Containing an independent technical scheme, this narrating mode of specification is only that for clarity, those skilled in the art should
Using specification as an entirety, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
It may be appreciated other embodiment.
Claims (7)
1. a kind of push type unmanned plane horn fold mechanism, including it is rotating pipe clip, rotating shaft contiguous block, pushing block, optical axis, spring, solid
Fixed tube is pressed from both sides and inside and outside horn, it is characterised in that the rotating pipe clip is connected with outer boom, and pipe clamp bottom side is provided with two and hung down
Straight barb, is connected by rotary shaft with rotating shaft contiguous block, and the rotating shaft contiguous block top surface is provided with two wide with barb width
Slot, inside is provided with pushing block and optical axis, and described pushing block one end is connected using through hole with optical axis, and the other end is used as pressing
Face, is installed in guide groove by the boss of rotating shaft contiguous block one, and the spring one end, which is fixed on one end inside pushing block and is fixed on, to be turned
Axle contiguous block lug boss position, described Duct fixing clamp one end is connected by bolt with rotating shaft contiguous block, horn in the connection of one end.
2. a kind of push type unmanned plane horn fold mechanism according to claim 1, it is characterised in that：The rotating pipe clip
Surface is provided with two barbs.
3. a kind of push type unmanned plane horn fold mechanism according to claim 1, it is characterised in that：The rotating shaft connection
Corresponding optical axis guide rail groove and pushing block guide groove are provided with block.
4. a kind of push type unmanned plane horn fold mechanism according to claim 1, it is characterised in that：It is described folding or
During expansion, spring is set to produce elastic force promotion optical axis movement by pressing pushing block.
5. a kind of push type unmanned plane horn fold mechanism according to claim 1, it is characterised in that：The rotating pipe clip
The anglec of rotation between rotating shaft contiguous block is 135 ° to the maximum.
6. a kind of push type unmanned plane horn fold mechanism according to claim 1, it is characterised in that：The rotating shaft connects
Connect provided with three fixing screwed holes in block, Duct fixing clamp opposite position there are three installation through-holes, and its radius is identical.
7. a kind of push type unmanned plane horn fold mechanism according to claim 1, it is characterised in that：The rotating shaft connects
Block, rotation pipe clamp, fixing pipe sandwiched is connect to be equipped with circuit and pass through hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621155932.4U CN206374964U (en) | 2016-10-31 | 2016-10-31 | A kind of push type unmanned plane horn fold mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621155932.4U CN206374964U (en) | 2016-10-31 | 2016-10-31 | A kind of push type unmanned plane horn fold mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206374964U true CN206374964U (en) | 2017-08-04 |
Family
ID=59402522
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621155932.4U Expired - Fee Related CN206374964U (en) | 2016-10-31 | 2016-10-31 | A kind of push type unmanned plane horn fold mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206374964U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110466736A (en) * | 2019-09-26 | 2019-11-19 | 吉林大学 | A kind of unmanned plane horn folding device and unmanned plane |
| CN113734416A (en) * | 2021-09-01 | 2021-12-03 | 深圳供电局有限公司 | Double-rod folding type unmanned aerial vehicle arm |
-
2016
- 2016-10-31 CN CN201621155932.4U patent/CN206374964U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110466736A (en) * | 2019-09-26 | 2019-11-19 | 吉林大学 | A kind of unmanned plane horn folding device and unmanned plane |
| CN113734416A (en) * | 2021-09-01 | 2021-12-03 | 深圳供电局有限公司 | Double-rod folding type unmanned aerial vehicle arm |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| 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: 20170804 Termination date: 20201031 |