CN206336441U - A kind of unmanned plane drop buffer - Google Patents
A kind of unmanned plane drop buffer Download PDFInfo
- Publication number
- CN206336441U CN206336441U CN201621340423.9U CN201621340423U CN206336441U CN 206336441 U CN206336441 U CN 206336441U CN 201621340423 U CN201621340423 U CN 201621340423U CN 206336441 U CN206336441 U CN 206336441U
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- main
- auxiliary
- transverse slat
- shifting chute
- folding
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- 239000003795 chemical substances by application Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
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Abstract
A kind of unmanned plane drop buffer of the utility model discloses a kind of device of stability when can improve the landing of unmanned baby plane.It is characterized in that fixed plate is placed on transverse slat, the elongated central line of the fixed plate and the elongated central line of transverse slat are on a horizontal line, two magnet are respectively placed in the two ends of fixed plate, mounting hole is provided with the middle part of transverse slat, and through fixed plate, one end of transverse slat is provided with main folding and unfolding groove, the other end of transverse slat is provided with auxiliary folding and unfolding groove, one end of main diagonal is placed in main folding and unfolding groove, and be placed in by rotary shaft on transverse slat, the other end of main diagonal is provided with main shifting chute, one end of master link is placed in main shifting chute, main feet is placed on the other end of master link, main compression spring is placed on master link, one end of main compression spring is connected with the other end of main diagonal, the other end is connected with main feet, one end of main extension spring be connected in the middle part of main diagonal, the other end is connected through main shifting chute with transverse slat.
Description
Technical field
A kind of unmanned plane drop buffer of the utility model, being related to one kind can play when unmanned baby plane lands
The device of cushioning effect, belongs to unmanned plane field.It is more particularly to a kind of to improve stability when unmanned baby plane lands
Device.
Background technology
At present, because unmanned plane has the advantages of can adapt to complicated adverse circumstances, flexible design, small volume, nobody flies
Machine is widely used in every field, still, and because the flying speed of unmanned aerial vehicle is very fast, running into emergency case needs promptly
During landing, unmanned aerial vehicle can produce strong vibrations, and stability during landing is excessively poor, existing that damping is set in unmanned plane
The method of air bag, although cushioning effect can be played in unmanned plane descent, but is due to that air bag does not have in descent
There is defined shape, in descent, easily fuselage is tumbled by air drag, not only reduce the effect of damping, land
When stability it is still very poor, it is serious in the case of, also unmanned plane itself can be caused to damage.
The content of the invention
In order to improve above-mentioned situation, a kind of unmanned plane drop buffer of the utility model can improve nothing there is provided one kind
The device of stability when people's baby plane lands.It is simple in construction, it is convenient and practical.
A kind of unmanned plane drop buffer of the utility model is realized in：A kind of unmanned plane landing of the utility model
Buffer unit is made up of agent set and buffer unit, agent set by transverse slat, mounting hole, fixed plate, magnet, main folding and unfolding groove and
Auxiliary folding and unfolding groove composition, fixed plate is placed on transverse slat, and the elongated central line of the fixed plate and the elongated central line of transverse slat are at one
On horizontal line, two magnet, which are respectively placed in the middle part of the two ends of fixed plate, transverse slat, is provided with mounting hole, and through fixed plate, transverse slat
One end be provided with main folding and unfolding groove, the other end of transverse slat is provided with auxiliary folding and unfolding groove, and buffer unit is by rotary shaft, main extension spring, main shifting
Dynamic groove, master link, main compression spring, main feet, main bundle bar, main diagonal, auxiliary bundle bar, auxiliary feet, auxiliary compression spring, auxiliary connection
Bar, auxiliary shifting chute, auxiliary brace and auxiliary extension spring composition, one end of main diagonal is placed in main folding and unfolding groove, and is put by rotary shaft
In on transverse slat, the other end of main diagonal is provided with main shifting chute, and one end of master link is placed in main shifting chute, and main feet is placed in master
On the other end of connecting rod, main compression spring is placed on master link, one end of main compression spring and the other end of main diagonal
Be connected, the other end is connected with main feet, one end of main extension spring be connected in the middle part of main diagonal, the other end through master
Shifting chute is connected with transverse slat, and one end of auxiliary brace is placed in auxiliary folding and unfolding groove, and is placed in by rotary shaft on transverse slat, described auxiliary oblique
Bar is symmetrical with main diagonal with the elongated central line of transverse slat, and the other end of auxiliary brace is provided with auxiliary shifting chute, and one end of auxiliary connecting rod is put
In in auxiliary shifting chute, auxiliary feet is placed on the other end of auxiliary connecting rod, and auxiliary compression spring is placed in auxiliary connecting rod, auxiliary compression bullet
One end of spring is connected with the other end of auxiliary brace, and the other end is connected with auxiliary feet, one end of auxiliary extension spring and auxiliary brace
Middle part be connected, the other end is connected through auxiliary shifting chute with transverse slat, it is main prick bar one end be placed in transverse slat through main folding and unfolding groove
On, and positioned between main diagonal and auxiliary brace, the main bundle bar is bow, and one end of auxiliary bundle bar is placed in horizontal stroke through auxiliary folding and unfolding groove
On plate, and positioned between main diagonal and auxiliary brace, the auxiliary bundle bar is bow.
In use, fixed plate is inhaled in the bottom of unmanned baby plane, Ran Houtong by the magnet at fixed plate two ends first
Mounting hole is crossed, fixed plate and transverse slat are fixed on unmanned baby plane, the mistake earthward landed in unmanned baby plane
Cheng Zhong, main bundle bar and auxiliary bundle bar can touch ground in advance, and then inject in ground, when main feet and auxiliary feet are fallen to the ground
Afterwards, main feet drives master link to be moved into main shifting chute, and main compression spring is compressed, and auxiliary feet drives auxiliary connecting rod to auxiliary
Moved in shifting chute, auxiliary compression spring is compressed, when master link is moved to main shifting chute end points, master link drives main oblique
Bar is moved along rotary shaft, now, and main extension spring is compressed, when auxiliary connecting rod is moved to auxiliary shifting chute end points, auxiliary connection
Bar drives auxiliary brace to be moved along rotary shaft, and now, auxiliary extension spring is compressed, and main bundle bar and auxiliary bundle bar continue earthward deep
Place's insertion, when unmanned aerial vehicle is dropped on ground completely, main diagonal is moved in the main folding and unfolding groove on transverse slat, auxiliary brace movement
In auxiliary folding and unfolding groove on to transverse slat, the purpose of stability when improving unmanned baby plane landing is reached.
Beneficial effect.
First, it is simple in construction, it is convenient and practical.
2nd, it is with low cost, it is easy to promote.
3rd, stability during unmanned baby plane landing can be improved.
Brief description of the drawings
Accompanying drawing 1 is a kind of structural representation of unmanned plane drop buffer of the utility model.
In accompanying drawing
Wherein part is：Transverse slat（1）, mounting hole（2）, fixed plate（3）, magnet（4）, rotary shaft（5）, main folding and unfolding groove（6）,
Main extension spring（7）, main shifting chute（8）, master link（9）, main compression spring（10）, main feet（11）, main bundle bar（12）, it is main
Brace（13）, auxiliary bundle bar（14）, auxiliary feet（15）, auxiliary compression spring（16）, auxiliary connecting rod（17）, auxiliary shifting chute（18）, it is auxiliary oblique
Bar（19）, auxiliary extension spring（20）, auxiliary folding and unfolding groove（21）.
Embodiment：
A kind of unmanned plane drop buffer of the utility model is realized in：In use, passing through fixed plate first（3）
The magnet at two ends（4）By fixed plate（3）Inhale in the bottom of unmanned baby plane, then pass through mounting hole（2）, by fixed plate（3）
And transverse slat（1）It is fixed on unmanned baby plane, during unmanned baby plane earthward lands, main bundle bar（12）
With auxiliary bundle bar（14）Ground can be touched in advance, and then is injected in ground, when main feet（11）With auxiliary feet（15）Fall earthward
After upper, main feet（11）Drive master link（9）To main shifting chute（8）Interior movement, main compression spring（10）Compressed, auxiliary feet
（15）Drive auxiliary connecting rod（17）To auxiliary shifting chute（18）Interior movement, auxiliary compression spring（16）Compressed, work as master link（9）Move
Move main shifting chute（8）During end points, master link（9）Drive main diagonal（13）Along rotary shaft（5）It is mobile, now, main stretching
Spring（7）Compressed, when auxiliary connecting rod（17）It is moved to auxiliary shifting chute（18）During end points, auxiliary connecting rod（17）Drive auxiliary brace
（19）Along rotary shaft（5）It is mobile, now, auxiliary extension spring（20）Compressed, and main bundle bar（12）With auxiliary bundle bar（14）Continue
Earthward depths is inserted, when unmanned aerial vehicle is dropped on ground completely, main diagonal（13）It is moved to transverse slat（1）On main folding and unfolding
Groove（6）It is interior, auxiliary brace（19）It is moved to transverse slat（1）On auxiliary folding and unfolding groove（21）It is interior, when reaching that the unmanned baby plane of raising lands
Stability purpose.
Claims (3)
1. a kind of unmanned plane drop buffer, it is characterized in that：Fixed plate is placed on transverse slat, and two magnet are respectively placed in fixed plate
Two ends, mounting hole is provided with the middle part of transverse slat, and through fixed plate, one end of transverse slat is provided with main folding and unfolding groove, the other end of transverse slat
Auxiliary folding and unfolding groove is provided with, one end of main diagonal is placed in main folding and unfolding groove, and is placed in by rotary shaft on transverse slat, the other end of main diagonal
Main shifting chute is provided with, one end of master link is placed in main shifting chute, and main feet is placed on the other end of master link, main compression
Spring is placed on master link, and one end of main compression spring is connected with the other end of main diagonal, the other end and main feet phase
Connection, one end of main extension spring be connected in the middle part of main diagonal, the other end is connected through main shifting chute with transverse slat, auxiliary oblique
One end of bar is placed in auxiliary folding and unfolding groove, and is placed in by rotary shaft on transverse slat, and the other end of auxiliary brace is provided with auxiliary shifting chute, auxiliary company
One end of extension bar is placed in auxiliary shifting chute, and auxiliary feet is placed on the other end of auxiliary connecting rod, and auxiliary compression spring is placed on auxiliary connection
On bar, one end of auxiliary compression spring is connected with the other end of auxiliary brace, and the other end is connected with auxiliary feet, auxiliary extension spring
One end be connected in the middle part of auxiliary brace, the other end is connected through auxiliary shifting chute with transverse slat, it is main prick bar one end through it is main receive
Groove is put to be placed on transverse slat, and positioned between main diagonal and auxiliary brace, main bundle bar is bow, one end of auxiliary bundle bar passes through auxiliary folding and unfolding
Groove is placed on transverse slat, and positioned between main diagonal and auxiliary brace, auxiliary bundle bar is bow.
2. a kind of unmanned plane drop buffer according to claim 1, it is characterised in that prolong at the center of the fixed plate
The elongated central line of long line and transverse slat is on a horizontal line.
3. a kind of unmanned plane drop buffer according to claim 1, it is characterised in that the auxiliary brace is with transverse slat
Elongated central line is symmetrical with main diagonal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621340423.9U CN206336441U (en) | 2016-12-08 | 2016-12-08 | A kind of unmanned plane drop buffer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621340423.9U CN206336441U (en) | 2016-12-08 | 2016-12-08 | A kind of unmanned plane drop buffer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206336441U true CN206336441U (en) | 2017-07-18 |
Family
ID=59308421
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621340423.9U Expired - Fee Related CN206336441U (en) | 2016-12-08 | 2016-12-08 | A kind of unmanned plane drop buffer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206336441U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110550220A (en) * | 2019-09-05 | 2019-12-10 | 新昌县诺趣智能科技有限公司 | Aerial photography unmanned aerial vehicle with falling protection function |
| CN110606216A (en) * | 2019-09-16 | 2019-12-24 | 安徽天德无人机科技有限公司 | Intelligent sensing anti-collision device and plant protection unmanned aerial vehicle with same |
| CN113200150A (en) * | 2021-06-18 | 2021-08-03 | 徐州质普智能设备有限公司 | High-ejection-take-off intelligent unmanned aerial vehicle |
-
2016
- 2016-12-08 CN CN201621340423.9U patent/CN206336441U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110550220A (en) * | 2019-09-05 | 2019-12-10 | 新昌县诺趣智能科技有限公司 | Aerial photography unmanned aerial vehicle with falling protection function |
| CN110606216A (en) * | 2019-09-16 | 2019-12-24 | 安徽天德无人机科技有限公司 | Intelligent sensing anti-collision device and plant protection unmanned aerial vehicle with same |
| CN113200150A (en) * | 2021-06-18 | 2021-08-03 | 徐州质普智能设备有限公司 | High-ejection-take-off intelligent unmanned aerial vehicle |
| CN113200150B (en) * | 2021-06-18 | 2022-01-25 | 徐州质普智能设备有限公司 | High-ejection-take-off intelligent unmanned aerial vehicle |
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| Date | Code | Title | Description |
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| 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: 20170718 |