CN214524431U - Effectual unmanned aerial vehicle cloud platform of shock attenuation - Google Patents
Effectual unmanned aerial vehicle cloud platform of shock attenuation Download PDFInfo
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- CN214524431U CN214524431U CN202023061631.4U CN202023061631U CN214524431U CN 214524431 U CN214524431 U CN 214524431U CN 202023061631 U CN202023061631 U CN 202023061631U CN 214524431 U CN214524431 U CN 214524431U
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Abstract
Effectual unmanned aerial vehicle cloud platform of shock attenuation, including the mount table that connects gradually can be connected with the unmanned aerial vehicle fuselage, be used for changing camera device angle of making a video recording mechanism, and camera device, be equipped with the shock-absorbing structure who is used for alleviateing unmanned aerial vehicle operation vibrations on the mount table, shock-absorbing structure includes shock attenuation mounting structure and installs in the shock attenuation body of shock attenuation mounting structure, shock attenuation mounting structure is gone up and is formed an at least interval part along vibrations direction of transfer at least part. The utility model discloses when the operation, the interval portion alleviates the vibrations that the source transmission was come in advance, and later vibrations are transmitted to the shock attenuation body again, realize the unmanned aerial vehicle shock attenuation. The utility model discloses have non-closed interval portion, compare in closed mounting structure among the prior art, can be on the basis that does not increase the space and occupy more effectual improvement of carrying out shock-absorbing structure, have more excellent shock attenuation effect.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, more specifically relates to an effectual unmanned aerial vehicle cloud platform of shock attenuation.
Background
The unmanned aerial vehicle cloud platform is that unmanned aerial vehicle is used for the support equipment of task load such as installation, fixed camera. In the unmanned aerial vehicle operation process, there are vibrations inevitable, for example the vibrations that the operation of paddle arouses, and the vibrations that camera device radiator fan operation arouses, these vibrations are unfavorable for the effect of making a video recording, should make technological improvement in order to reduce the influence of vibrations to the effect of making a video recording. The utility model discloses a chinese utility model patent 201820380685.0 triaxial cloud platform passes through last shock attenuation board, lower shock attenuation board and installs go up the shock attenuation board with the technical scheme of the shock attenuation body between the shock attenuation board alleviates vibrations down. Because the connection mode of the shock absorber and the upper and lower shock absorbing plates is compact connection, the effect of reducing the shock still needs to be further improved.
SUMMERY OF THE UTILITY MODEL
The utility model discloses a first aim at is to above-mentioned defect and not enough, solves among the prior art shock attenuation body and the tight real shock attenuation effect of connecting leading to of shock attenuation board and remains the technical problem who optimizes, provides an adoption and sets up the effectual unmanned aerial vehicle cloud platform of shock attenuation of interval portion.
Another object of the utility model is to provide an assemble convenient, safe in utilization's effectual unmanned aerial vehicle cloud platform of shock attenuation.
In order to achieve the above object, the utility model discloses a specific technical scheme be:
effectual unmanned aerial vehicle cloud platform of shock attenuation, including the mount table that can be connected with the unmanned aerial vehicle fuselage that connects gradually, be used for changing camera device angle of making a video recording mechanism, and camera device, be equipped with the shock-absorbing structure who is used for alleviateing unmanned aerial vehicle operation vibrations on the mount table, shock-absorbing structure includes shock attenuation mounting structure and installs in the shock attenuation body of shock attenuation mounting structure, at least part formation an at least interval portion along vibrations direction of transfer on the shock attenuation mounting structure, during operation, the interval portion alleviates the vibrations that the source transmission was come in advance, later vibrations transmit again to the shock attenuation body, realize the unmanned aerial vehicle shock attenuation.
Preferably, the number of the spacers is plural, and the plural spacers are distributed in the circumferential direction.
Preferably, the spacer is notched in the longitudinal direction.
Preferably, the number of the spacers is plural, and the plural spacers form a multilayer structure in the longitudinal direction.
Preferably, the spacer portion forms a non-closed gap in a circumferential direction.
Preferably, an elastic member is arranged in the gap.
Preferably, the shock absorption mounting structure comprises shock absorption mounting plates which are arranged at two ends of the shock absorption body and protrude out of the mounting table, and spacing parts are arranged on the shock absorption mounting plates.
Preferably, the shock attenuation body is spherical main part including the shape and locates the ladder connecting piece of main part tip, the shock attenuation mounting structure forms the ladder groove corresponding to the ladder connecting piece along circumference, ladder connecting piece sets up the interval portion with shock attenuation mounting structure cooperation department.
Preferably, the mount table can be dismantled with the unmanned aerial vehicle fuselage and be connected, just be equipped with the battery on the mount table and with battery electric connection's plug, through detachable mount table and unmanned aerial vehicle fuselage, realize the switch-on and the disconnection of power.
Preferably, the angle adjusting mechanism comprises a yaw rotating mechanism, a roll rotating mechanism and a pitch rotating mechanism which are connected in sequence, the yaw rotating mechanism is connected with the roll rotating mechanism through a first connecting arm, the first connecting arm comprises a first following end connected with the yaw rotating mechanism and a first driving end connected with the roll rotating mechanism, the roll rotating mechanism is connected with the pitch rotating mechanism through a second connecting arm, the second connecting arm comprises a second following end connected with the roll rotating mechanism and a second driving end connected with the pitch rotating mechanism, when the angle is adjusted, the first following end moves along the deviated sailing direction along the yaw rotating mechanism, the first driving end drives the roll rotating mechanism to move, the second following end rotates around the cross shaft along with the roll rotating mechanism, the second driving end drives the pitch rotating mechanism to move, and the pitch rotating mechanism drives the camera device to pitch move, so as to realize the multi-dimensional angle adjustment of the camera device.
Compared with the prior art, the utility model, following beneficial effect has:
the utility model discloses in at least part forms an at least interval portion along vibrations direction of transfer on the shock attenuation mounting structure, and when the operation, the interval portion alleviates the vibrations that the source of vibration transmitted in advance, and later vibrations are retransmitted to the shock attenuation body, realize the unmanned aerial vehicle shock attenuation. The utility model discloses have non-closed interval portion, compare in closed mounting structure among the prior art, can be on the basis that does not increase the space and occupy more effectual improvement of carrying out shock-absorbing structure, have more excellent shock attenuation effect.
On this basis, the utility model discloses a back-off structure realizes being connected of mount table and unmanned aerial vehicle fuselage, has the equipment convenience, uses convenient advantage. Meanwhile, the power supply is switched on and off by detaching the mounting platform from the unmanned aerial vehicle body, and the unmanned aerial vehicle has the technical effects of safety in use and safety in electricity utilization.
The present invention will be further described with reference to the accompanying drawings.
Drawings
Fig. 1 is a schematic diagram of an explosion structure of a cloud platform in a preferred embodiment of the present invention.
Fig. 2 is a schematic structural view of a cloud platform in a preferred embodiment of the present invention.
FIG. 3 is a schematic view of a partial cross-sectional view taken along line A-A in FIG. 2.
Fig. 4 is a schematic view of another shock-absorbing structure according to the preferred embodiment of the present invention.
Description of reference numerals:
10 mounting table, 11 batteries, 12 plugs, 13 connecting pieces,
A 20-degree adjusting mechanism, a 21-yaw rotating mechanism, a 22-roll rotating mechanism, a 23-pitch rotating mechanism, a 24-first connecting arm, a 241-first following end, a 242-first driving end, a 25-second connecting arm, a 251-second following end, a 252-second driving end,
30 an image pickup device,
40 shock-absorbing structures, 41 shock-absorbing mounting structures, 411 spacing parts, 4111 gaps, 4112 multi-layer structures, 4113 gaps, 412 shock-absorbing mounting plates, 42 shock-absorbing bodies, 421 main bodies, 422 step connectors.
Detailed Description
The present invention is further explained and illustrated by the following embodiments, it should be understood that the following embodiments are for the purpose of making the technical solution of the present invention clearer and easier to understand, and do not limit the scope of the claims.
As shown in fig. 1-3, effectual unmanned aerial vehicle cloud platform of shock attenuation, including the mount table 10 that can be connected with the unmanned aerial vehicle fuselage that connects gradually, be used for changing camera device 30 angle of making a video recording 20, and camera device 30, be equipped with the shock-absorbing structure 40 that is used for alleviateing unmanned aerial vehicle operation vibrations on the mount table 10, shock-absorbing structure 40 includes shock attenuation mounting structure 41 and installs in the shock attenuation body 42 of shock attenuation mounting structure 41, at least part forms an at least interval portion 411 along vibrations direction of transfer on the shock attenuation mounting structure 41, during the operation, interval portion 411 alleviates the vibrations that the source transmission was come in advance, later vibrations are retransmitted to shock attenuation body 42, realize the unmanned aerial vehicle shock attenuation.
In a preferred embodiment, the number of the spacers 411 is plural, and the plurality of spacers 411 are distributed in the circumferential direction.
In a preferred embodiment, the spacing portion 411 forms a notch 4111 along the longitudinal direction.
In a preferred embodiment, the number of the spacers 411 is plural, and the plural spacers 411 form a multi-layer structure 4112 in the longitudinal direction.
As shown in fig. 4, in a preferred embodiment, the spacing portion 411 forms a non-closed void 4113 along the circumferential direction.
In a preferred embodiment, an elastic member is disposed in the gap 4113.
In a preferred embodiment, the damper mounting structure 41 includes damper mounting plates 412 provided at both ends of the damper body 42 and protruding from the mounting table 10, and the damper mounting plates 412 are provided with spacers 411.
In a preferred embodiment, the shock absorbing body 42 includes a main body 421 having a spherical shape and a step connection member 422 provided at an end of the main body 421, the shock absorbing mounting structure 41 forms a step groove corresponding to the step connection member 422 along a circumferential direction, and a spacing portion 411 is provided at a position where the step connection member 422 is engaged with the shock absorbing mounting structure 41.
In the preferred embodiment, mount table 10 can be dismantled with the unmanned aerial vehicle fuselage and be connected, just be equipped with battery 11 on the mount table 10 and with battery 11 electric connection's plug 12, through detachable mount table 10 and unmanned aerial vehicle fuselage, realize the switch-on and the disconnection of power.
In a preferred embodiment, the angle adjusting mechanism 20 includes a yaw rotating mechanism 21, a roll rotating mechanism 22, and a pitch rotating mechanism 23, which are connected in sequence, the yaw rotating mechanism 21 and the roll rotating mechanism 22 are connected through a first connecting arm 24, the first connecting arm 24 includes a first following end 241 connected with the yaw rotating mechanism 21 and a first driving end 242 connected with the roll rotating mechanism 22, the roll rotating mechanism 22 and the pitch rotating mechanism 23 are connected through a second connecting arm 25, the second connecting arm 25 includes a second following end 251 connected with the roll rotating mechanism 22 and a second driving end 252 connected with the pitch rotating mechanism 23, when the angle is adjusted, the first following end 241 follows the yaw rotating mechanism 21 to move in the off-course direction, the first driving end 242 drives the roll rotating mechanism 22 to move, the second following end 251 follows the roll rotating mechanism 22 to rotate around the transverse axis, the second driving end 252 drives the pitching rotation mechanism 23 to move, and the pitching rotation mechanism 23 drives the camera device 30 to pitch, so as to realize multi-dimensional angle adjustment of the camera device 30.
The present invention will be further described with reference to the following specific examples.
Example 1
This embodiment 1 provides a three-axis pan-tilt, and this pan-tilt is used for loading camera device, including mount table 10, driftage slewing mechanism 21, roll slewing mechanism 22, pitch slewing mechanism 23, and mount table 10 is connected with the fuselage, and mount table 10, driftage slewing mechanism 21, roll slewing mechanism 22, pitch slewing mechanism 23 connect gradually. The direction of rotation of driftage slewing mechanism 21 is along the unmanned aerial vehicle direction of moving ahead skew, and the direction of rotation of roll slewing mechanism 22 is rotatory around the unmanned aerial vehicle direction of moving ahead, and every single move is rotated along the upper and lower every single move in the direction of rotation of every single move slewing mechanism 23, through the rotation of the not equidimension degree of three slewing mechanism, realizes making a video recording of camera device 30 in three dimension.
The imaging device 30 is connected to the tilting mechanism 23 and can rotate together with the tilting mechanism 23, and the imaging device 30 is used for imaging.
Be equipped with power structure on mount table 10, provide the electric energy for unmanned aerial vehicle. The power structure comprises a battery unit 11 and a power plug 12, wherein the battery unit 11 is electrically connected with the power plug 12, the power plug 12 is arranged at the top of the mounting table 10, and a power socket is arranged on the machine body corresponding to the power plug. The power plug 12 is used for connecting the power consumption device of the machine body and the three-axis pan-tilt, when the three-axis pan-tilt is connected with the machine body, power supply can be achieved, and when the three-axis pan-tilt is separated from the machine body, power failure is achieved.
The connecting piece 13 is a barb structure, and the connecting piece is established at the top of mount table for connect fuselage and triaxial cloud platform.
Shock-absorbing structure 40 establishes the four corners at mount table 10, is spherical shock attenuation body 42 and has the mounting structure 41 of breach 4111 including the shape, alleviates the vibrations that the unmanned aerial vehicle operation brought through setting up breach 41, compares in traditional closed mounting structure, and the shock attenuation effect is more excellent.
The mounting structure 40 includes an upper mounting plate and a lower mounting plate (both the upper mounting plate and the lower mounting plate are damping mounting plates 412), the upper mounting plate and the lower mounting plate protrude out of the main body of the mounting table 10, the upper mounting plate and the lower mounting plate are basically circular in matching with a damping body, a notch is arranged at the top along the protruding direction of the upper mounting plate and the lower mounting plate, and the damping body is mounted in a clamping manner by the upper mounting plate and the lower mounting plate.
The shock absorber 42 includes a main body 421 shaped as a sphere, and stepped connection structures 422 are provided at both ends of the main body, and are respectively connected to the upper and lower mounting structures.
The yaw rotating mechanism comprises a yaw motor, and the output end of the yaw motor is connected with the mounting table in a key mode.
The first connecting arm 24 includes a first following end 241 and a first driving end 242, the first following end 241 is connected to a motor main body of the yaw motor, the first driving end 242 is connected to the second connecting arm 25, the first connecting arm 24 rotates along with the motor main body under the driving of the yaw motor, and drives the second connecting arm 25 to move in a deviation course.
The second connecting arm 25 includes a second following end 251 and a second driving end 252, the second following end 251 is connected to an output shaft of the roll motor, the second driving end 252 is connected to the pitch rotating mechanism 23, and under the driving of the roll motor, the second connecting arm 25 rotates in the roll direction and drives the pitch rotating mechanism 23 to rotate in the roll direction.
The base body part of the roll motor is connected with the first connecting arm 24, so that the roll motor rotates along with the first connecting arm 24 in a yawing mode.
The pitching rotation mechanism 23 comprises a pitching motor, a base body of the pitching motor is fixedly connected with a driving end of the second connecting arm 25, an output end of the pitching motor is connected with the camera device 30, and the pitching motor is used for providing power for pitching motion of the camera device 30.
Example 2
This embodiment 2 provides another structure of the spacer, and the number of the spacers 411 is 3, and the 3 spacers 411 form a multi-layer structure 4112 along the longitudinal direction of the mounting board. Specifically, the spacer 411 forms a non-closed void 4113 in the circumferential direction. An elastic member may be further provided in the space 4113.
The present invention has been described in terms of embodiments, but not limitations, and other variations of the disclosed embodiments, as would be readily apparent to one skilled in the art, are intended to be included within the scope of the present invention as defined in the following claims, in view of the description of the present invention.
Claims (9)
1. The utility model provides an effectual unmanned aerial vehicle cloud platform of shock attenuation, its characterized in that:
comprises a mounting platform (10) which is connected with the body of the unmanned aerial vehicle, an angle adjusting mechanism (20) for changing the camera angle and a camera device (30) which are connected in sequence,
a damping structure (40) for reducing the operation vibration of the unmanned aerial vehicle is arranged on the mounting table (10),
the shock absorption structure (40) comprises a shock absorption mounting structure (41) and a shock absorption body (42) mounted on the shock absorption mounting structure (41),
at least one spacing part (411) is formed on the shock absorption mounting structure (41) along the shock transmission direction at least partially;
the spacing part (411) forms a notch (4111) along the longitudinal direction;
during operation, the interval part (411) relieves the vibration transmitted by the seismic source in advance, and then the vibration is transmitted to the damping body (42) to realize the damping of the unmanned aerial vehicle.
2. The effectual unmanned aerial vehicle cloud platform of shock attenuation of claim 1, characterized in that:
the number of the spacing parts (411) is a plurality,
and a plurality of the spacers (411) are distributed in the circumferential direction.
3. The effectual unmanned aerial vehicle cloud platform of shock attenuation of claim 1, characterized in that:
the number of the spacing parts (411) is a plurality,
and a plurality of the spacers (411) form a multilayer structure (4112) in the longitudinal direction.
4. The effectual unmanned aerial vehicle cloud platform of shock attenuation according to claim 3, characterized in that:
the spacer portion (411) forms a non-closed gap (4113) in the circumferential direction.
5. The effectual unmanned aerial vehicle cloud platform of shock attenuation according to claim 4, characterized in that:
an elastic piece is arranged in the gap (4113).
6. The effectual unmanned aerial vehicle cloud platform of shock attenuation of claim 1, characterized in that:
the shock absorption mounting structure (41) comprises shock absorption mounting plates (412) which are arranged at two ends of a shock absorption body (42) and protrude out of the mounting table (10),
the shock absorption mounting plate (412) is provided with a spacing part (411).
7. The effectual unmanned aerial vehicle cloud platform of shock attenuation of claim 1, characterized in that:
the shock absorption body (42) comprises a main body (421) with a spherical shape and a step connecting piece (422) arranged at the end part of the main body (421),
the shock-absorbing mounting structure (41) forms a stepped groove corresponding to the stepped connecting piece (422) along the circumferential direction,
and a spacing part (411) is arranged at the matching part of the step connecting piece (422) and the shock absorption mounting structure (41).
8. The effectual unmanned aerial vehicle cloud platform of shock attenuation of claim 1, characterized in that:
the mounting table (10) is detachably connected with the unmanned aerial vehicle body,
a battery (11) and a plug (12) electrically connected with the battery (11) are arranged on the mounting table (10),
through detachable mount table (10) and unmanned aerial vehicle fuselage, realize the switch-on and the disconnection of power.
9. The effectual unmanned aerial vehicle cloud platform of shock attenuation of claim 1, characterized in that:
the angle adjusting mechanism (20) comprises a yaw rotating mechanism (21), a roll rotating mechanism (22) and a pitch rotating mechanism (23) which are connected in sequence,
the yaw rotating mechanism (21) is connected with the roll rotating mechanism (22) through a first connecting arm (24),
the first connecting arm (24) comprises a first following end (241) connected with the yawing rotating mechanism (21) and a first driving end (242) connected with the rolling rotating mechanism (22),
the roll rotating mechanism (22) is connected with the pitch rotating mechanism (23) through a second connecting arm (25),
the second connecting arm (25) comprises a second following end (251) connected with the rolling rotating mechanism (22) and a second driving end (252) connected with the pitching rotating mechanism (23),
during angle adjustment, the first following end (241) moves along deviating the navigation direction along with yaw slewing mechanism (21), the first driving end (242) drives roll slewing mechanism (22) to move, the second following end (251) rotates around the horizontal axis along with roll slewing mechanism (22), the second driving end (252) drives pitch slewing mechanism (23) to move, and pitch slewing mechanism (23) drives camera device (30) to move in pitch, so that multi-dimensional angle adjustment of camera device (30) is realized.
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| CN202023061631.4U CN214524431U (en) | 2020-12-16 | 2020-12-16 | Effectual unmanned aerial vehicle cloud platform of shock attenuation |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113859541A (en) * | 2021-11-24 | 2021-12-31 | 徐州独角兽信息科技有限公司 | Unmanned aerial vehicle for environment detection |
| CN115395976A (en) * | 2022-09-19 | 2022-11-25 | 亿航智能设备（广州）有限公司 | Integrated tripod head |
-
2020
- 2020-12-16 CN CN202023061631.4U patent/CN214524431U/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113859541A (en) * | 2021-11-24 | 2021-12-31 | 徐州独角兽信息科技有限公司 | Unmanned aerial vehicle for environment detection |
| CN115395976A (en) * | 2022-09-19 | 2022-11-25 | 亿航智能设备（广州）有限公司 | Integrated tripod head |
| CN115395976B (en) * | 2022-09-19 | 2024-01-26 | 亿航智能设备（广州）有限公司 | Integrated cradle head |
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