CN208278342U - A kind of multi-rotor unmanned aerial vehicle holder damping device - Google Patents
A kind of multi-rotor unmanned aerial vehicle holder damping device Download PDFInfo
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- CN208278342U CN208278342U CN201820924241.9U CN201820924241U CN208278342U CN 208278342 U CN208278342 U CN 208278342U CN 201820924241 U CN201820924241 U CN 201820924241U CN 208278342 U CN208278342 U CN 208278342U
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- holder
- aerial vehicle
- machine host
- fixed block
- damping device
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Abstract
The utility model discloses a kind of multi-rotor unmanned aerial vehicle holder damping device, including unmanned machine host, holder, the bottom of the unmanned machine host is provided with holder；The utility model multi-rotor unmanned aerial vehicle is with holder damping device compared with original structure, it is simpler, it adapts to the structure that fixed block is mutually clamped and replaces original bolt, not only alleviate weight, also facilitate installation, disassembly, it is inserted into inside slot by fixed link, first, second fixed block is mutually clamped, to which holder be connect with unmanned machine host, and it is provided with multiple groups fixed link and slot, it can guarantee connective stability, the second fixed block is pushed by button, it is separated with the first fixed block, to which holder be dismantled, reach requirement easy to disassemble, and the effect for passing through spring, so that push-button reset, facilitate next use, guard ring is provided on the outside of button, effectively it can prevent button from accidentally touching, it ensure that the safe handling of unmanned plane.
Description
Technical field
The utility model belongs to unmanned plane engineering device technique field, and in particular to a kind of multi-rotor unmanned aerial vehicle holder damping dress
It sets.
Background technique
Without cockpit on unmanned plane, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
It is standby that machine tool remote control station personnel by radar etc. set UAV, is tracked, is positioned to it, is remotely controlled, telemetering and number pass
It is defeated.
Currently, by the mechanisms such as carry holder and camera on unmanned plane, so that unmanned plane can be widely applied to landform survey
It draws, engineering geological investigation, take photo by plane, the fields such as remote sensing.However unmanned plane is in flight course, often due to propeller rotational, cloud
Platform shake or the influence of extraneous high wind cause the unstable shaking of camera, cause picture captured by camera unintelligible, shoot
Effect is poor, needs the later period to carry out a large amount of processing work to data, makes up the influence as caused by camera shake, and often pass through
The data for crossing post-processing are still barely satisfactory.
The multi-rotor unmanned aerial vehicle of the prior art is had the following problems with holder damping device: existing most of damping holders
It is fixedly connected by bolt and unmanned plane main body, in connection due to needing many bolts pacifying using tool etc.
There is inconvenience in dress, disassembly process, and needs to consume the regular hour.
Utility model content
To solve the problems mentioned above in the background art.The utility model provides a kind of multi-rotor unmanned aerial vehicle holder
Damping device, have the characteristics that structure it is simple, it is easy for installation etc.,.
To achieve the above object, the utility model provides the following technical solutions: a kind of multi-rotor unmanned aerial vehicle holder damping
The bottom of device, including unmanned machine host, holder, the unmanned machine host is provided with holder；
One side surface of the unmanned machine host is provided with guard ring, and the inside of the guard ring is located at unmanned machine host
Be internally provided with button, one end of the button is provided with push rod, and the circumference of the push rod, which is inserted in, is provided with spring, it is described nobody
The lower inner of machine host is provided with slot, and a side surface of the slot is provided with the first fixed block；
The holder includes the first holder and the second holder, is provided with shock-absorbing ball above second holder, described to subtract
It is provided with the first holder above shake ball, fixed link, the upper side of the fixed link are provided with above first holder
It is provided with the second fixed block.
Preferably, the fixed link is provided with four groups, is evenly arranged in four side of top of the first holder, and each fixed link
Upper side be provided with the second fixed block.
Preferably, the slot is provided with four groups, and position is corresponding with fixed link.
Preferably, second fixed block can be mutually clamped with the first fixed block, and be completely embedded.
Preferably, there are four shock-absorbing balls for setting between first holder and the second holder, and are fixed by screw rod.
Preferably, it there are four the button settings, is arranged separately on inside four sides of unmanned machine host, outside is provided with
Guard ring, inside are provided with push rod, spring.
Compared with prior art, the utility model has the beneficial effects that
1, the utility model multi-rotor unmanned aerial vehicle with holder damping device compared with original structure, it is simpler, adapt to
The structure that fixed block is mutually clamped replaces original bolt, not only alleviates weight, also facilitates installation, disassembly, passes through fixed link
It is inserted into inside slot, the first, second fixed block is mutually clamped, so that holder be connect with unmanned machine host, and is provided with multiple groups
Fixed link and slot can guarantee connective stability.
2, the utility model multi-rotor unmanned aerial vehicle pushes the second fixed block by button with holder damping device, solid with first
Determine block separation, so that holder be dismantled, reaches requirement easy to disassemble, and by the effect of spring, so that push-button reset, convenient
Next time uses, and is provided with guard ring on the outside of button, effectively can prevent button from accidentally touching, ensure that the safety of unmanned plane makes
With.
Detailed description of the invention
Fig. 1 is the structural schematic diagram of the utility model.
Fig. 2 is the tripod head connection structure schematic diagram of the utility model.
Fig. 3 is the structural schematic diagram in the utility model Fig. 2 at A.
In figure: 1, unmanned machine host；101, slot；102, the first fixed block；11, guard ring；12, button；13, push rod；
14, spring；2, holder；21, the first holder；211, fixed link；212, the second fixed block；22, the second holder；23, shock-absorbing ball.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-3 is please referred to, the utility model is the following technical schemes are provided: a kind of multi-rotor unmanned aerial vehicle is filled with holder damping
It sets, including unmanned machine host 1, holder 2, the bottom of unmanned machine host 1 is provided with holder 2；
One side surface of unmanned machine host 1 is provided with guard ring 11, and the inside of guard ring 11 is located at the interior of unmanned machine host 1
Portion is provided with button 12, and one end of button 12 is provided with push rod 13, and the circumference of push rod 13, which is inserted in, is provided with spring 14, unmanned owner
The lower inner of machine 1 is provided with slot 101, and a side surface of slot 101 is provided with the first fixed block 102；
Holder 2 includes the first holder 21 and the second holder 22, and the top of the second holder 22 is provided with shock-absorbing ball 23, shock-absorbing ball
23 top is provided with the first holder 21, and the top of the first holder 21 is provided with fixed link 211, the upper side of fixed link 211
It is provided with the second fixed block 212.
In order to preferably connect holder 2 with unmanned machine host 1, in the present embodiment, it is preferred that fixed link 211 is provided with
Four groups, it is evenly arranged in four side of top of the first holder 21, and the upper side of each fixed link 211 is provided with second and fixes
Block 212.
In order to preferably connect holder 2 with unmanned machine host 1, in the present embodiment, it is preferred that slot 101 is provided with four
Group, position are corresponding with fixed link 211.
In order to which holder 2 and unmanned machine host 1 are completely embedded, in the present embodiment, it is preferred that the second fixed block 212 can be with
First fixed block 102 is mutually clamped, and is completely embedded.
In order to achieve the effect that damping, in the present embodiment, it is preferred that be provided between the first holder 21 and the second holder 22
Four shock-absorbing balls 23, and fixed by screw rod.
In order to which the disassembly of holder 2 is more convenient, in the present embodiment, it is preferred that there are four the settings of button 12, is arranged separately on
Inside four sides of unmanned machine host 1, outside is provided with guard ring 11, and inside is provided with push rod 13, spring 14.
The working principle and process for using of the utility model: pacified between the first holder 21 and the second holder 22 using bolt
Shock-absorbing ball 23 is filled, then holder 2 is connect with unmanned machine host 1, slot is inserted by the fixed link 211 of 21 top of the first holder
In 101, the second fixed block 212 is mutually clamped with the first fixed block 102, thus the connection that is fixed；When needing to dismantle, press by
Button 12, button 12 are generally hidden in inside guard ring 11, not will cause and accidentally touch, the promotion push rod 13 of button 12,14 stress of spring,
Push rod 13 pushes the second fixed block 212, separates it with the first fixed block 102, fixed link 211 skids off slot 101, thus by cloud
Platform 2 is separated with unmanned machine host 1, and 14 promoting button 12 of spring resets, and facilitates next use.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of multi-rotor unmanned aerial vehicle holder damping device, including unmanned machine host (1), holder (2), it is characterised in that: institute
The bottom for stating unmanned machine host (1) is provided with holder (2)；
One side surface of the unmanned machine host (1) is provided with guard ring (11), and the inside of the guard ring (11) is located at nobody
Machine host (1) is internally provided with button (12), and one end of the button (12) is provided with push rod (13), the push rod (13)
Circumference, which is inserted in, to be provided with spring (14), and the lower inner of the unmanned machine host (1) is provided with slot (101), the slot
(101) a side surface is provided with the first fixed block (102)；
The holder (2) includes the first holder (21) and the second holder (22), is provided with and subtracts above second holder (22)
It shakes ball (23), is provided with the first holder (21) above the shock-absorbing ball (23), is provided with above first holder (21)
Fixed link (211) is provided with the second fixed block (212) at the upper side of the fixed link (211).
2. a kind of multi-rotor unmanned aerial vehicle holder damping device according to claim 1, it is characterised in that: the fixed link
(211) four groups are provided with, four side of top of the first holder (21), and the upper side of each fixed link (211) are evenly arranged in
It is provided with the second fixed block (212).
3. a kind of multi-rotor unmanned aerial vehicle holder damping device according to claim 1, it is characterised in that: the slot
(101) four groups are provided with, position is corresponding with fixed link (211).
4. a kind of multi-rotor unmanned aerial vehicle holder damping device according to claim 1, it is characterised in that: described second is solid
Determining block (212) can be mutually clamped with the first fixed block (102), and be completely embedded.
5. a kind of multi-rotor unmanned aerial vehicle holder damping device according to claim 1, it is characterised in that: first cloud
There are four shock-absorbing ball (23) for setting between platform (21) and the second holder (22), and are fixed by screw rod.
6. a kind of multi-rotor unmanned aerial vehicle holder damping device according to claim 1, it is characterised in that: the button
(12) it there are four setting, is arranged separately on inside four sides of unmanned machine host (1), outside is provided with guard ring (11), internal
It is provided with push rod (13), spring (14).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820924241.9U CN208278342U (en) | 2018-06-14 | 2018-06-14 | A kind of multi-rotor unmanned aerial vehicle holder damping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820924241.9U CN208278342U (en) | 2018-06-14 | 2018-06-14 | A kind of multi-rotor unmanned aerial vehicle holder damping device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208278342U true CN208278342U (en) | 2018-12-25 |
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ID=64699084
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820924241.9U Active CN208278342U (en) | 2018-06-14 | 2018-06-14 | A kind of multi-rotor unmanned aerial vehicle holder damping device |
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| CN (1) | CN208278342U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114194406A (en) * | 2021-12-16 | 2022-03-18 | 江苏大学 | Unmanned aerial vehicle carries on platform |
-
2018
- 2018-06-14 CN CN201820924241.9U patent/CN208278342U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114194406A (en) * | 2021-12-16 | 2022-03-18 | 江苏大学 | Unmanned aerial vehicle carries on platform |
| CN114194406B (en) * | 2021-12-16 | 2024-05-14 | 江苏大学 | Unmanned aerial vehicle carries on platform |
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