CN207089641U - A kind of unmanned plane shock mount - Google Patents
A kind of unmanned plane shock mount Download PDFInfo
- Publication number
- CN207089641U CN207089641U CN201720993893.3U CN201720993893U CN207089641U CN 207089641 U CN207089641 U CN 207089641U CN 201720993893 U CN201720993893 U CN 201720993893U CN 207089641 U CN207089641 U CN 207089641U
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- Prior art keywords
- support bar
- unmanned plane
- shock
- spring
- main body
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- 230000035939 shock Effects 0.000 title claims abstract description 18
- 238000003466 welding Methods 0.000 claims description 3
- 238000010586 diagram Methods 0.000 description 4
- 238000013016 damping Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 238000007689 inspection Methods 0.000 description 2
- 230000000116 mitigating effect Effects 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 208000035473 Communicable disease Diseases 0.000 description 1
- 208000015181 infectious disease Diseases 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
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- Vibration Dampers (AREA)
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Abstract
The utility model discloses a kind of unmanned plane shock mount, including unmanned plane main body, first support bar, 3rd support bar, rubber layer, second spring hole and shock-absorbing ball, the both sides of the unmanned plane main body are connected with wing, and it is provided with second support bar below unmanned plane main body, the first support bar is arranged on the lower section of second support bar, and the first spring is provided between first support bar and second support bar, 3rd support bar is arranged on the lower end of first support bar, and the 3rd support bar be provided at both ends with collision avoidance angle, the rubber layer is pasted onto the outside of collision avoidance angle, the second spring hole is arranged on the inside of the 3rd support bar, the shock-absorbing ball is arranged on the lower end of second spring.This carries the unmanned plane shock mount of shock-absorbing function, and the first spring is provided between first support bar and second support bar, the dynamics for the impact for slowing down unmanned plane main body and ground is played, is advantageous to the protection to unmanned plane main body.
Description
Technical field
Unmanned air vehicle technique field is the utility model is related to, specially a kind of unmanned plane shock mount.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft, or fully or intermittently independently operated by car-mounted computer.
Compared with manned aircraft, unmanned plane is often more suitable for the task of those too " slow-witted, dirty or dangerous ".Nobody
Machine presses application field, can be divided into it is military with it is civilian.Military aspect, unmanned plane are divided into reconnaissance plane and target drone.Civilian aspect, unmanned plane
It is that unmanned plane has really just needed in every profession and trade extensive use；At present take photo by plane, agricultural, plant protection, miniature self-timer, express transportation, calamity
Hardly possible rescue, observation wild animal, monitoring infectious disease, mapping, news report, electric inspection process, the disaster relief, movies-making and manufacture are romantic
Etc. field application, greatly expanded the purposes of unmanned plane in itself, developed country is also in actively extension sector application and hair
Open up unmanned air vehicle technique.
But the support base of existing unmanned plane does not have damping device, unmanned plane is easy to ground and hit, make in landing
Into the damage of unmanned plane.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane shock mount, to solve what is proposed in above-mentioned background technology
The support base of existing unmanned plane does not have damping device, and unmanned plane is easy to ground and hit, cause unmanned plane in landing
The problem of damage.
To achieve the above object, the utility model provides following technical scheme：A kind of unmanned plane shock mount, including nobody
Owner's body, first support bar, the 3rd support bar, rubber layer, second spring hole and shock-absorbing ball, the both sides of the unmanned plane main body with
Wing is connected, and second support bar is provided with below unmanned plane main body, and the first support bar is arranged on second support bar
Lower section, and the first spring is provided between first support bar and second support bar, the 3rd support bar is arranged on first
The lower end of strut, and the 3rd support bar is provided at both ends with collision avoidance angle, the rubber layer are pasted onto the outside of collision avoidance angle, and described
Two spring eyes are arranged on the inside of the 3rd support bar, and the 3rd support bar is internally provided with second spring, and the shock-absorbing ball is set
Put in the lower end of second spring.
Preferably, the diameter of bore of the first support bar is more than the diameter of second support bar, and in first support bar
Heart line and the center line of second support bar overlap.
Preferably, the collision avoidance angle is connected by the way of welding with the 3rd support bar, and the mounting structure of collision avoidance angle
Installed to tilt.
Preferably, the second spring hole includes fixing hole, and fixing hole is evenly distributed on the inside of the 3rd support bar.
Preferably, the length in the second spring hole is less than the thickness of the 3rd support bar, and the aperture in second spring hole is big
In the diameter of shock-absorbing ball.
Preferably, the diameter of the fixing hole is less than the diameter of shock-absorbing ball, and the number of fixing hole and the number of shock-absorbing ball
It is identical.
Compared with prior art, the beneficial effects of the utility model are：This carries the unmanned plane shock mount of shock-absorbing function,
The first spring is provided between first support bar and second support bar, plays the power for the impact for slowing down unmanned plane main body and ground
Degree, prevents unmanned plane main body to be damaged, is advantageous to the protection to unmanned plane main body, be provided with the both sides of the 3rd support bar anti-
Breakhead, play a part of mitigating unmanned plane main body and external object and hit dynamics, be advantageous to the protection to unmanned plane main body, the
Three support bars are internally provided with second spring hole, play a part of installing second spring and shock-absorbing ball, are advantageous to second spring
With the fixation of shock-absorbing ball, second spring and shock-absorbing ball are internally provided with second spring hole, plays and further slows down unmanned plane
The dynamics of the impact on main body and ground, be advantageous to the protection further to unmanned plane main body, and the fixing hole on second spring hole
It can prevent shock-absorbing ball from skidding off, be advantageous to the stable installation of shock-absorbing ball.
Brief description of the drawings
Fig. 1 is the utility model structure diagram；
Fig. 2 is the utility model the first spring structure schematic diagram；
Fig. 3 is the utility model A node mplifying structure schematic diagrams；
Fig. 4 is the utility model fixation hole configurations schematic diagram.
In figure：1st, unmanned plane main body, 2, wing, 3, first support bar, 4, second support bar, 5, collision avoidance angle, 6, the 3rd
Strut, the 7, first spring, 8, rubber layer, 9, second spring hole, 901, fixing hole, 10, second spring, 11, shock-absorbing ball.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describing, it is clear that described embodiment is only the utility model part of the embodiment, 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, belong to the scope of the utility model protection.
Fig. 1-4 are referred to, the utility model provides a kind of technical scheme：A kind of unmanned plane shock mount, including unmanned plane
Main body 1, first support bar 3, the 3rd support bar 6, rubber layer 8, second spring hole 9 and shock-absorbing ball 11, the both sides of unmanned plane main body 1
It is connected with wing 2, and the lower section of unmanned plane main body 1 is provided with second support bar 4, first support bar 3 is arranged on the second support
The lower section of bar 4, and the first spring 7, the diameter of bore of first support bar 3 are provided between first support bar 3 and second support bar 4
More than the diameter of second support bar 4, and the center line of first support bar 3 and the center line of second support bar 4 overlap, and set first
Support bar 3 and second support bar 4 play a part of supporting unmanned plane main body 1, and the 3rd support bar 6 is arranged on first support bar 3
Lower end, and the 3rd support bar 6 is provided at both ends with collision avoidance angle 5, collision avoidance angle 5 is connected by the way of welding with the 3rd support bar 6
Connect, and the mounting structure of collision avoidance angle 5 is installed to tilt, and sets collision avoidance angle 5 to play mitigation unmanned plane main body 1 and is hit with external object
The effect of dynamics, be advantageous to the protection to unmanned plane main body 1, rubber layer 8 is pasted onto the outside of collision avoidance angle 5, and second spring hole 9 is set
Put in the inside of the 3rd support bar 6, and the 3rd support bar 6 is internally provided with second spring 10, second spring hole 9 includes fixing
Hole 901, and fixing hole 901 is evenly distributed on the inside of the 3rd support bar 6, sets second spring hole 9 to play installation second spring
10 and the effect of shock-absorbing ball 11, be advantageous to the fixation of second spring 10 and shock-absorbing ball 11, the length in second spring hole 9 is less than the 3rd
The thickness of support bar 6, and the aperture in second spring hole 9 is more than the diameter of shock-absorbing ball 11, is so provided with and exists beneficial to shock-absorbing ball 11
Moved in second spring hole 9, the diameter of fixing hole 901 is less than the diameter of shock-absorbing ball 11, and the number and shock-absorbing ball of fixing hole 901
11 number is identical, sets fixing hole 901 to prevent shock-absorbing ball 11 from skidding off, and is advantageous to the stable installation of shock-absorbing ball 11, shock-absorbing ball
11 are arranged on the lower end of second spring 10.
Operation principle：When carrying the unmanned plane shock mount of shock-absorbing function using this, each of unmanned plane main body 1 is first checked
Whether structure is intact, after inspection, starts unmanned plane main body 1, by the high-speed rotation of wing 2, and then drives unmanned owner
Body 1 rises, and when unmanned plane main body 1 declines, the shock-absorbing ball 11 inside the 3rd support bar 6 contacts with ground, in second spring hole 9
The shock-absorbing ball 11 in portion can slow down the impulsive force of unmanned plane main body 1 and ground by second spring 10, and fixing hole 901 can prevent damping
Ball 11 is skidded off out of second spring hole 9, and second support bar 4 can be slowed down again by the first spring 7 inside first support bar 3
The impulsive force on unmanned plane main body 1 and ground, the rubber layer 8 on collision avoidance angle 5 can mitigate the shock journey of unmanned plane main body 1 and object
Degree, the above are just completed the sequence of operations of the unmanned plane shock mount with shock-absorbing function, not retouched in detail in this specification
The content stated belongs to prior art known to professional and technical personnel in the field.
Although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, it can still be modified to the technical scheme described in foregoing embodiments, or which part technical characteristic is entered
Row equivalent substitution, all within the spirit and principles of the utility model, any modification, equivalent substitution and improvements made etc., all should
Within the scope of protection of the utility model.
Claims (6)
1. a kind of unmanned plane shock mount, including unmanned plane main body（1）, first support bar（3）, the 3rd support bar（6）, rubber layer
（8）, second spring hole（9）And shock-absorbing ball（11）, it is characterised in that：The unmanned plane main body（1）Both sides and wing（2）It is connected
Connect, and unmanned plane main body（1）Lower section be provided with second support bar（4）, the first support bar（3）It is arranged on second support bar
（4）Lower section, and first support bar（3）And second support bar（4）Between be provided with the first spring（7）, the 3rd support bar
（6）It is arranged on first support bar（3）Lower end, and the 3rd support bar（6）Be provided at both ends with collision avoidance angle（5）, the rubber layer
（8）It is pasted onto collision avoidance angle（5）Outside, the second spring hole（9）It is arranged on the 3rd support bar（6）Inside, and the 3rd
Strut（6）Be internally provided with second spring（10）, the shock-absorbing ball（11）It is arranged on second spring（10）Lower end.
A kind of 2. unmanned plane shock mount according to claim 1, it is characterised in that：The first support bar（3）It is interior
Bore dia is more than second support bar（4）Diameter, and first support bar（3）Center line and second support bar（4）Center line
Overlap.
A kind of 3. unmanned plane shock mount according to claim 1, it is characterised in that：The collision avoidance angle（5）Using welding
Mode and the 3rd support bar（6）It is connected, and collision avoidance angle（5）Mounting structure for tilt install.
A kind of 4. unmanned plane shock mount according to claim 1, it is characterised in that：The second spring hole（9）Including
Fixing hole（901）, and fixing hole（901）It is evenly distributed on the 3rd support bar（6）Inside.
A kind of 5. unmanned plane shock mount according to claim 1, it is characterised in that：The second spring hole（9）Length
Degree is less than the 3rd support bar（6）Thickness, and second spring hole（9）Aperture be more than shock-absorbing ball（11）Diameter.
A kind of 6. unmanned plane shock mount according to claim 4, it is characterised in that：The fixing hole（901）Diameter
Less than shock-absorbing ball（11）Diameter, and fixing hole（901）Number and shock-absorbing ball（11）Number it is identical.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720993893.3U CN207089641U (en) | 2017-08-10 | 2017-08-10 | A kind of unmanned plane shock mount |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720993893.3U CN207089641U (en) | 2017-08-10 | 2017-08-10 | A kind of unmanned plane shock mount |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207089641U true CN207089641U (en) | 2018-03-13 |
Family
ID=61542763
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720993893.3U Expired - Fee Related CN207089641U (en) | 2017-08-10 | 2017-08-10 | A kind of unmanned plane shock mount |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207089641U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609163A (en) * | 2018-04-10 | 2018-10-02 | 清远市巨劲科技有限公司 | A kind of mapping unmanned plane lifting shock bracket |
| CN108945444A (en) * | 2018-08-30 | 2018-12-07 | 无锡莱特杰米科技发展有限公司 | A kind of unmanned aerial photography machine of the wedding celebration with landing protection structure |
-
2017
- 2017-08-10 CN CN201720993893.3U patent/CN207089641U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609163A (en) * | 2018-04-10 | 2018-10-02 | 清远市巨劲科技有限公司 | A kind of mapping unmanned plane lifting shock bracket |
| CN108945444A (en) * | 2018-08-30 | 2018-12-07 | 无锡莱特杰米科技发展有限公司 | A kind of unmanned aerial photography machine of the wedding celebration with landing protection structure |
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| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180313 |