CN208412103U - A kind of doublet cord stringing unmanned plane - Google Patents
A kind of doublet cord stringing unmanned plane Download PDFInfo
- Publication number
- CN208412103U CN208412103U CN201820915440.3U CN201820915440U CN208412103U CN 208412103 U CN208412103 U CN 208412103U CN 201820915440 U CN201820915440 U CN 201820915440U CN 208412103 U CN208412103 U CN 208412103U
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- CN
- China
- Prior art keywords
- unmanned plane
- fence
- unwrapping wire
- fixed link
- doublet cord
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- 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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- 230000000903 blocking effect Effects 0.000 claims abstract description 21
- 230000000694 effects Effects 0.000 abstract description 6
- 238000000034 method Methods 0.000 abstract description 5
- 230000005484 gravity Effects 0.000 abstract description 4
- 230000007812 deficiency Effects 0.000 description 1
- 230000003447 ipsilateral effect Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
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Abstract
The utility model belongs to air vehicle technique field, and in particular to a kind of doublet cord stringing unmanned plane.The doublet cord stringing unmanned plane includes: drone body, and the bottom of drone body has four undercarriages, is provided with the first blocking fence between two adjacent undercarriages of side, is provided with the second blocking fence between two adjacent undercarriages of the other side；Fixed link, fixed link stop fence and second to stop fence through first；And it is separately positioned on two unwrapping wire components at fixed link both ends.Unwrapping wire or air line working can be implemented by the unwrapping wire component of setting.The unwrapping wire component of the doublet cord stringing unmanned plane is set in the occupied height space of undercarriage, it can the center of gravity for reducing unmanned plane, which plays, to be stablized or avoid unstable effect, and can save space.Also, two unwrapping wire components are relatively independent, will not have an impact mutually.
Description
Technical field
The utility model belongs to air vehicle technique field, and in particular to a kind of doublet cord stringing unmanned plane.
Background technique
Referred to as " unmanned plane ", english abbreviation is " UAV " to UAV, is using radio robot and to provide for oneself
The not manned aircraft of presetting apparatus manipulation.From technical standpoint definition can be divided into: unmanned helicopter, unmanned fixed-wing aircraft,
Unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc..By the remote control to unmanned plane, it can be made to be answered extensively
For the every field such as taking photo by plane, rescuing.In unmanned air vehicle technique application field, various tasks are carried out with unmanned plane and need that task is installed
Task carry part is usually fixed on the fuselage of unmanned plane by executive device, can carry out various tasks as required.By right
The improvement of carry part can give the more functions of unmanned plane.
Because of requirement of engineering, generally require to set up cable for communicating or powering, in more complex landform, artificial stringing or
It is routed time-consuming and laborious, unmanned plane can be improved, increase corresponding function.
Utility model content
To solve the deficiencies in the prior art, the utility model provides a kind of doublet cord stringing unmanned plane.The bifilar coil holder
Line unmanned plane can carry out the stringing of doublet cord by the flight performance of unmanned plane, be suitble to different terrain.
Technical solution provided by the utility model is as follows:
A kind of doublet cord stringing unmanned plane, comprising:
The bottom of drone body, the drone body has four undercarriages, in two adjacent undercarriages of side
Between be provided with the first blocking fence, be provided with the second blocking fence between two adjacent undercarriages of the other side；
Fixed link, the fixed link through it is described first stop fence and it is described second stop fence, and respectively with it is described
First blocking fence is fixedly connected with the second blocking fence；
And two unwrapping wire components at the fixed link both ends are separately positioned on, each unwrapping wire component is located at institute
Side and the first blocking fence of the second blocking fence far from the first blocking fence is stated to stop to enclose far from described second
The side on column.
As, the first blocking fence through the first blocking fence and is stretched to far from institute in one end of the fixed link
The side of the second blocking fence is stated, the other end of the fixed link through the second blocking fence and stretches to second blocking
The side that fence stops fence far from described first.
Doublet cord stringing unmanned plane provided by above-mentioned technical proposal, by the unwrapping wire component of setting can be implemented unwrapping wire or
Air line working.Unwrapping wire component is set in the occupied height space of undercarriage, it can the center of gravity for reducing unmanned plane plays surely
Determine or avoid unstable effect, and space can be saved.Also, two unwrapping wire components are relatively independent, will not generate shadow mutually
It rings.
Specifically, each unwrapping wire component includes the line sleeve being socketed in the fixed link and is wrapped in the line sleeve
On cable volume, each line sleeve respectively with the fixed link be rotatablely connected.
Based on the above-mentioned technical proposal, the rotation of line sleeve may be implemented, thus realize cable volume around from.
Further, it is fixedly installed a ring baffle respectively in the two sides of each line sleeve.
Based on the above-mentioned technical proposal, it is wound into together during unwrapping wire being rolled up to avoid the cable of two sides.
Further, the outer diameter of the ring baffle is greater than the outer diameter of cable volume.
Based on the above-mentioned technical proposal, it is wound into fixed link during unwrapping wire being rolled up to avoid the cable of two sides.
Further, the height of the unwrapping wire component is less than the height of the undercarriage, the lower end surface of the unwrapping wire component
Level height be higher than each undercarriage lower end surface level height.
Based on the above-mentioned technical proposal, cable volume will not influence the start and stop of unmanned plane.
Further, the fixed link is horizontally disposed.
Based on the above-mentioned technical proposal, line sleeve horizontally rotates, be conducive to unmanned plane during flying during cable volume smoothly around from
With the stabilization of unmanned plane during flying.
Generally, doublet cord stringing unmanned plane provided by the utility model can be carried out by the flight performance of unmanned plane
The stringing of doublet cord is suitble to different terrain.Unwrapping wire or air line working can be implemented by the unwrapping wire component being arranged in it.Unwrapping wire component
It is then set between undercarriage, it can the center of gravity for reducing unmanned plane, which plays, to be stablized or avoid unstable effect, and can be saved
Save space, also, two unwrapping wire components are relatively independent, will not have an impact mutually.
Detailed description of the invention
Fig. 1 is the main view of doublet cord stringing unmanned plane provided by the utility model.
Fig. 2 is the side view of doublet cord stringing unmanned plane provided by the utility model.
In attached drawing 1,2, structure list representated by each label is as follows:
1, drone body, 2, undercarriage, 3, first stops fence, and 4, second stops fence, 5, fixed link, 6, line set
Cylinder, 7, cable volume, 8, ring baffle.
Specific embodiment
The principles of the present invention and feature are described below, illustrated embodiment is served only for explaining the utility model,
It is not intended to limit the scope of the utility model.
In a specific embodiment, as shown in Figure 1, 2, doublet cord stringing unmanned plane includes: drone body 1, consolidates
Fixed pole 5 and two unwrapping wire components for being separately positioned on 5 both ends of fixed link.
The bottom of drone body 1 has four undercarriages 2, and the is provided between two adjacent undercarriages 2 of side
One stops fence 3, is provided with the second blocking fence 4 between two adjacent undercarriages 2 of the other side.Fixed link 5 runs through first
Stop fence 3 and second to stop fence 4, and is fixedly connected respectively with the first blocking fence 3 and the second blocking fence 4.Each unwrapping wire
Component is located at side and first blocking fence 3 of the second blocking fence 4 far from the first blocking fence 3 to be stopped to enclose far from second
The side on column 4.
Each unwrapping wire component includes that the line sleeve 6 being socketed in fixed link 5 and the cable wound on online sleeve 6 roll up 7, each line
Sleeve 6 is rotatablely connected with fixed link 5 respectively.It is fixedly installed a ring baffle 8 respectively in the two sides of each line sleeve 6.Annular
The outer diameter of baffle 8 is greater than the outer diameter of cable volume 7.The height of unwrapping wire component is less than the height of undercarriage 2.Fixed link 5 is horizontally disposed.
The distance of two ipsilateral ring baffles 8 is more than or equal to the length of cable volume 7.
It for line sleeve 6 is in the set-up mode in fixed link 5, can be rotatablely connected, can also be fixedly connected.This is practical
Novel embodiment is using rotation connection.The line sleeve 6 at 5 both ends of fixed link is rotatablely connected respectively at both ends, and on the one hand nobody flies
Resistance during row by unwrapping wire component is small, and the interference being subject to is also corresponding small, does not influence the smooth flight of unmanned plane；It is another
Aspect, when two cable volumes 7 are because when setting needs or external cause cause payingoff speed inconsistent, two line sleeves 6 be may be implemented
Different payingoff speeds leads to unmanned plane during flying to avoid the inhomogenous of effect of two line sleeves 6 to the power of fixed link 5
Two sides is unbalance in the process, even deflects.
And be respectively fixedly connected with according to the line sleeve 6 at 5 both ends of fixed link at both ends, when two cable volumes 7 are because of setting
It needs or when external cause causes payingoff speed inconsistent, two line sleeves 6 can generate different payingoff speeds, so as to cause two lines
Sleeve 6 is inhomogenous to the effect of the power of fixed link 5, leads to the unbalance or even body inclined of two sides during unmanned plane during flying
Turn.
Doublet cord stringing unmanned plane provided by the utility model can carry out doublet cord by the flight performance of unmanned plane
Stringing, be suitble to different terrain.Unwrapping wire or air line working can be implemented by the unwrapping wire component being arranged in it.Unwrapping wire component is then arranged
Between undercarriage, it can the center of gravity for reducing unmanned plane, which plays, to be stablized or avoids unstable effect, and can save space,
Also, two unwrapping wire components are relatively independent, will not have an impact mutually.
The above is only the preferred embodiment of the present invention, is not intended to limit the utility model, all practical at this
Within novel spirit and principle, any modification, equivalent replacement, improvement and so on should be included in the guarantor of the utility model
Within the scope of shield.
Claims (6)
1. a kind of doublet cord stringing unmanned plane characterized by comprising
Drone body (1), the bottom of the drone body (1) have four undercarriages (2), and in side, adjacent two are risen
It falls between frame (2) and is provided with the first blocking fence (3), be provided with the second resistance between two adjacent undercarriages (2) of the other side
Confining column (4)；
Fixed link (5), fixed link (5) both ends extend through described first and fence (3) and described second are stopped to stop fence
(4), it and is fixedly connected；
And two unwrapping wire components at the fixed link (5) both ends are separately positioned on, each unwrapping wire component is located at described
Second side for stopping fence (4) to stop fence (3) far from described first and described first stops fence (3) far from described second
Stop the side of fence (4).
2. doublet cord stringing unmanned plane according to claim 1, it is characterised in that: each unwrapping wire component includes being socketed in
Line sleeve (6) on the fixed link (5) and the cable being wrapped on the line sleeve (6) volume (7), each line sleeve (6)
It is rotatablely connected respectively with the fixed link (5).
3. doublet cord stringing unmanned plane according to claim 2, it is characterised in that: in the two sides of each line sleeve (6)
It is fixedly installed a ring baffle (8) respectively.
4. doublet cord stringing unmanned plane according to claim 3, it is characterised in that: the outer diameter of the ring baffle (8) is big
In the outer diameter of cable volume (7).
5. doublet cord stringing unmanned plane according to claim 1, it is characterised in that: the height of the unwrapping wire component is less than institute
State the height of undercarriage (2).
6. doublet cord stringing unmanned plane according to any one of claims 1 to 5, it is characterised in that: the fixed link (5) is horizontal
Setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820915440.3U CN208412103U (en) | 2018-06-13 | 2018-06-13 | A kind of doublet cord stringing unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820915440.3U CN208412103U (en) | 2018-06-13 | 2018-06-13 | A kind of doublet cord stringing unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208412103U true CN208412103U (en) | 2019-01-22 |
Family
ID=65109981
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820915440.3U Expired - Fee Related CN208412103U (en) | 2018-06-13 | 2018-06-13 | A kind of doublet cord stringing unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208412103U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112882538A (en) * | 2021-02-01 | 2021-06-01 | 深圳市旭联信息技术有限公司 | Docking station |
-
2018
- 2018-06-13 CN CN201820915440.3U patent/CN208412103U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112882538A (en) * | 2021-02-01 | 2021-06-01 | 深圳市旭联信息技术有限公司 | Docking station |
| CN112882538B (en) * | 2021-02-01 | 2024-03-29 | 深圳市旭联信息技术有限公司 | Docking station |
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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: 20190122 |