CN211663474U - Unmanned aerial vehicle and cloud platform damper thereof - Google Patents
Unmanned aerial vehicle and cloud platform damper thereof Download PDFInfo
- Publication number
- CN211663474U CN211663474U CN202020246331.4U CN202020246331U CN211663474U CN 211663474 U CN211663474 U CN 211663474U CN 202020246331 U CN202020246331 U CN 202020246331U CN 211663474 U CN211663474 U CN 211663474U
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- cloud platform
- fixedly connected
- shock attenuation
- aerial vehicle
- unmanned aerial
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Abstract
The utility model relates to an unmanned aerial vehicle field just discloses an unmanned aerial vehicle and cloud platform damper thereof, including the cloud platform epitheca, the top of cloud platform epitheca is provided with the cloud platform inferior valve, the equal fixedly connected with inserted bar in the left and right sides of cloud platform inferior valve bottom, the equal fixedly connected with sleeve in the left and right sides of diapire in the cloud platform epitheca, two the bottom of inserted bar runs through cloud platform epitheca and sleeve in proper order and extends to telescopic inside. The utility model discloses a, stretch or compress through the inserted bar and carry out the shock attenuation to first spring, the sliding sleeve makes the second spring compress or stretch and carry out the shock attenuation, the shock attenuation board can extrude the shock attenuation ball and carry out the shock attenuation once more, multiple shock attenuation can be at utmost eliminate vibrations and impact force, it makes the cloud platform take place to rock to have solved the flight in-process because the vibration of unmanned aerial vehicle itself perhaps meets the circumstances such as strong wind impact, cause the unstability of camera to rock, lead to the shooting picture unclear, it is poor to shoot the effect, the problem of quality is shot in the influence.
Description
Technical Field
The utility model relates to an unmanned aerial vehicle field specifically is an unmanned aerial vehicle and cloud platform damper thereof.
Background
An unmanned aerial vehicle (unmanned aerial vehicle) is an unmanned aerial vehicle operated by utilizing a radio remote control device and a self-contained program control device, or is completely or intermittently and autonomously operated by an on-board computer, an unmanned aerial vehicle holder is supporting equipment for installing and fixing task loads such as a camera device and the like, and an unmanned aerial vehicle aerial photography holder belongs to one type of holders and is mainly applied to the practical aerial photography aspects such as construction planning, engineering investigation, disaster investigation, emergency rescue and relief work and the like.
At present, unmanned aerial vehicle is at the flight in-process, often can make the cloud platform take place to rock because the vibration of unmanned aerial vehicle itself perhaps meets the circumstances such as strong wind impact, causes the unstability of camera to rock, leads to the shooting picture unclear, and the shooting effect is poor to the influence is shot the quality, provides an unmanned aerial vehicle and cloud platform damper for this reason and solves above-mentioned problem.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides an unmanned aerial vehicle and cloud platform damper thereof has the shock attenuation effectual, improves the stable advantage of shooting the quality of cloud platform, has solved the flight in-process because the vibration of unmanned aerial vehicle itself perhaps meets the circumstances such as strong wind impact and make the cloud platform take place to rock, causes the unstability of camera to rock, leads to the shooting picture unclear, and the shooting effect is poor, influences the problem of shooting the quality.
(II) technical scheme
For realizing above-mentioned shock attenuation effectual, improve the purpose that cloud platform stability shot the quality, the utility model provides a following technical scheme:
an unmanned aerial vehicle and a tripod head damping mechanism thereof comprise a tripod head upper shell, wherein a tripod head lower shell is arranged at the top of the tripod head upper shell, inserting rods are fixedly connected to the left side and the right side of the bottom wall of the tripod head lower shell, sleeves are fixedly connected to the left side and the right side of the inner bottom wall of the tripod head upper shell, the bottom ends of the two inserting rods sequentially penetrate through the tripod head upper shell and the sleeves and extend into the sleeves, sliding plates are fixedly connected to the bottom ends of the two inserting rods, the two sliding plates are respectively in sliding connection with the two sleeves, first springs are fixedly connected to the bottoms of the two sliding plates, the bottom ends of the two first springs are respectively fixedly connected with the inner bottom wall of the sleeve, a connecting rod is fixedly connected between the two inserting rods, two sliding sleeves are slidably connected onto the connecting rod, two second springs are sleeved on the connecting rod, and the opposite ends of, two the one end that the second spring carried on the back mutually respectively with two inserted bar fixed connection, the inside of cloud platform epitheca is provided with the damper plate, the articulated seat of top fixedly connected with of damper plate, the inboard of articulated seat articulates there are two hinge bars, two the one end that hinge bar kept away from articulated seat is articulated with the bottom of two sliding sleeves respectively, the bottom fixedly connected with evenly distributed's of damper plate shock attenuation ball, the bottom of shock attenuation ball all with the interior diapire fixed connection of cloud platform epitheca.
Preferably, the inner side of the upper shell of the holder is fixedly connected with a damping base plate, and the damping base plate is a member formed by overlapping multiple layers of elastic silica gel plates.
Preferably, the top and the bottom of the damping ball are fixedly connected with a fixing plate, the top of the fixing plate at the top is fixedly connected with the bottom of the damping plate, and the bottom of the fixing plate at the bottom is fixedly connected with the inner side of the damping base plate.
Preferably, the left side and the right side of the top of the upper shell of the holder are respectively embedded with an elastic sleeve ring, and the two insertion rods are respectively connected with the inner rings of the two elastic sleeve rings in a sliding manner.
Preferably, the top fixedly connected with shock attenuation protection pad of cloud platform epitheca, shock attenuation protection pad is located between two inserted bars.
Preferably, the tops of the two sliding sleeves are fixedly connected with damping protection blocks.
(III) advantageous effects
Compared with the prior art, the utility model provides an unmanned aerial vehicle and cloud platform damper thereof possesses following beneficial effect:
1. the unmanned aerial vehicle and the tripod head damping mechanism thereof drive the sliding plate to slide in the sleeve through the inserted link, stretch or compress the first spring through the sliding plate, and are damped by the elasticity of the first spring, and simultaneously the inserted link can drive the connecting rod to move, the connecting rod drives the sliding sleeve to push the hinged rod to rotate around the hinged seat, the hinged rod enables the sliding sleeve to slide on the connecting rod, the sliding sleeve compresses or stretches the second spring, and is damped again by the elasticity of the second spring, the connecting rod can also drive the damping plate to move through the damping protection block, the hinged rod and the hinged seat, the damping ball can be extruded by the movement of the damping plate, and is damped again through the damping ball, the vibration and the impact force can be eliminated to the maximum extent by multiple damping, the amplitude and the energy of the vibration are reduced, the stability of the lower shell of the tripod head is ensured, and the stability, improve the shooting effect and shoot the quality, solved the flight in-process because the vibration of unmanned aerial vehicle itself perhaps meets the circumstances such as strong wind impact and makes the cloud platform take place to rock, causes the unstability of camera to rock, leads to shooting the picture not clear, and the shooting effect is poor, influences the problem of shooting the quality.
2. This unmanned aerial vehicle and cloud platform damper thereof through the shock attenuation backing plate that multilayer elasticity silica gel plate stack formed, can play the effect that increases support intensity, still has good cushioning effect simultaneously.
3. This unmanned aerial vehicle and cloud platform damper thereof through the setting of fixed plate, can carry out good support and fixed to the shock attenuation ball to make the shock attenuation ball can be stable play the support cushioning effect to the shock attenuation board.
4. This unmanned aerial vehicle and cloud platform damper thereof, through the setting of the elastic sleeve ring, when receiving the horizontal direction vibration, the inserted bar rocks the extrusion elastic sleeve ring, and the elastic sleeve ring produces elastic deformation and reduces the impact force to carry out the shock attenuation to the level.
5. This unmanned aerial vehicle and cloud platform damper thereof, through the setting of shock attenuation protection pad, can protect between cloud platform epitheca and the cloud platform inferior valve, prevent the collision to there is certain shock attenuation effect.
6. This unmanned aerial vehicle and cloud platform damper thereof, through the setting of shock attenuation protection piece, can drive the interior roof contact of sliding sleeve and cloud platform epitheca when the connecting rod reciprocates at the inserted bar to can prevent that the collision from leading to the damage, and play supplementary absorbing effect.
Drawings
FIG. 1 is a schematic structural view of the present invention;
fig. 2 is a schematic sectional view of the sleeve according to the present invention.
In the figure: 1. a cradle head upper shell; 2. a lower holder shell; 3. inserting a rod; 4. a sleeve; 5. a sliding plate; 6. a first spring; 7. a connecting rod; 8. a sliding sleeve; 9. a second spring; 10. a damper plate; 11. a hinged seat; 12. a hinged lever; 13. a shock absorbing ball; 14. a shock-absorbing base plate; 15. a fixing plate; 16. an elastic collar; 17. a shock absorbing protective pad; 18. shock attenuation protection piece.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-2, an unmanned aerial vehicle and a cradle head damping mechanism thereof comprise a cradle head upper shell 1, wherein the cradle head upper shell 1 is fixed with the bottom of the unmanned aerial vehicle, a cradle head lower shell 2 is arranged at the top of the cradle head upper shell 1, a camera is fixed with the bottom of the cradle head lower shell 2, a certain distance is arranged between the cradle head upper shell 1 and the cradle head lower shell 2 for buffering, insertion rods 3 are fixedly connected with the left side and the right side of the bottom of the cradle head lower shell 2, sleeves 4 are fixedly connected with the left side and the right side of the inner bottom wall of the cradle head upper shell 1, the bottom ends of the two insertion rods 3 sequentially penetrate through the cradle head upper shell 1 and the sleeves 4 and extend into the sleeves 4, sliding plates 5 are fixedly connected with the bottom ends of the two insertion rods 3, the two sliding plates 5 are respectively slidably connected with the two sleeves 4, the sliding plates 5 can limit the insertion rods 3 to prevent the insertion rods 3, the bottom ends of the two first springs 6 are fixedly connected with the inner bottom wall of the sleeve 4, the inserted rods 3 drive the sliding plate 5 to slide in the sleeve 4, the first springs 6 are stretched or compressed through the sliding plate 5, the shock absorption is carried out through the elasticity of the first springs 6, the connecting rod 7 is fixedly connected between the two inserted rods 3, the inserted rods 3 can drive the connecting rod 7 to move, the connecting rod 7 is slidably connected with two sliding sleeves 8, the connecting rod 7 is sleeved with two second springs 9, the second springs 9 are compressed or stretched through the sliding sleeves 8, the shock absorption is carried out again through the elasticity of the second springs 9, the opposite ends of the two second springs 9 are respectively and fixedly connected with the two sliding sleeves 8, the opposite ends of the two second springs 9 are respectively and fixedly connected with the two inserted rods 3, the shock absorption plate 10 is arranged in the cradle head upper shell 1, and the hinging seat 11 is fixedly connected with the top of the shock, the inner side of the hinged seat 11 is hinged with two hinged rods 12, one end of each hinged rod 12, which is far away from the hinged seat 11, is hinged with the bottom of each sliding sleeve 8, the connecting rod 7 drives the sliding sleeves 8 to push the hinged rods 12 to rotate around the hinged seat 11, the hinged rods 12 enable the sliding sleeves 8 to slide on the connecting rod 7, the bottom of each damping plate 10 is fixedly connected with damping balls 13 which are uniformly distributed, the connecting rod 7 can move to drive the damping plates 10 to move through the damping protection blocks 18, the hinged rods 12 and the hinged seats 11, and the damping balls 13 can be extruded by the movement of the damping plates 10, all with the interior diapire fixed connection of cloud platform epitheca 1, multiple shock attenuation can the at utmost eliminate vibrations and impact force, reduce the range and the energy of vibrations, guarantee stability through shock attenuation ball 13 the bottom that carries out shock attenuation ball 13 once more to can guarantee the stability that the camera was shot, improve shooting effect and shooting quality.
Further, the inner side of the holder upper shell 1 is fixedly connected with a damping pad 14, the damping pad 14 is a member formed by overlapping multiple layers of elastic silica gel plates, the damping pad 14 formed by overlapping multiple layers of elastic silica gel plates can play a role in increasing supporting strength, and meanwhile, the damping pad has a good damping effect.
Further, the top and the equal fixedly connected with fixed plate 15 in bottom of shock attenuation ball 13, the top of the fixed plate 15 at top and the bottom fixed connection who subtracts vibrating plate 10, the bottom of the fixed plate 15 of bottom and the inboard fixed connection who subtracts vibrating plate 14, through the setting of fixed plate 15, can carry out good support and fixed to subtract vibrating ball 13 to make that subtract vibrating ball 13 can be stable play the support cushioning effect to subtract vibrating plate 10.
Further, the left and right sides at 1 top of cloud platform epitheca all inlays and is equipped with the elastic sleeve ring 16, and two inserted bars 3 respectively with the inner circle sliding connection of two elastic sleeve rings 16, through the setting of elastic sleeve ring 16, when receiving the horizontal direction vibration, inserted bar 3 rocks extrusion elastic sleeve ring 16, and elastic sleeve ring 16 produces elastic deformation and reduces the impact force to carry out the shock attenuation to the level.
Further, the top fixedly connected with shock attenuation protection pad 17 of cloud platform epitheca 1, shock attenuation protection pad 17 are located between two inserted bars 3, through the setting of shock attenuation protection pad 17, can protect between cloud platform epitheca 1 and the cloud platform inferior valve 2, prevent collision to there is certain shock attenuation effect.
Further, the equal fixedly connected with shock attenuation protection piece 18 in top of two sliding sleeves 8, through the setting of shock attenuation protection piece 18, can avoid the contact of sliding sleeve 8 and the interior roof of cloud platform epitheca 1 when inserted bar 3 drives connecting rod 7 and reciprocates to can prevent collision and lead to the damage, and play supplementary absorbing effect.
The working principle is as follows: when the unmanned aerial vehicle and the tripod head damping mechanism thereof are used, the tripod head upper shell 1 and the bottom of the unmanned aerial vehicle are fixed, the camera and the bottom of the tripod head lower shell 2 are fixed, a certain distance is reserved between the tripod head upper shell 1 and the tripod head lower shell 2 for buffering, in the flight process, when the unmanned aerial vehicle vibrates or is shocked by strong wind and the like, the inserted link 3 drives the sliding plate 5 to slide in the sleeve 4, the sliding plate 5 stretches or compresses the first spring 6, the elastic force of the first spring 6 is used for damping, meanwhile, the inserted link 3 can drive the connecting rod 7 to move, the connecting rod 7 drives the sliding sleeve 8 to push the hinged link 12 to rotate around the hinged seat 11, the hinged link 12 enables the sliding sleeve 8 to slide on the connecting rod 7, the sliding sleeve 8 compresses or stretches the second spring 9, and the damping is carried out again through the elastic force of the second spring 9, connecting rod 7's removal can also be through shock attenuation protection piece 18, articulated rod 12 and articulated seat 11 drive shock attenuation board 10 and remove, shock attenuation ball 13 can be extruded in shock attenuation board 10's removal, carry out the shock attenuation once more through shock attenuation ball 13, multiple shock attenuation can the at utmost eliminate vibrations and impact force, reduce the range and the energy of vibrations, guarantee the stability of cloud platform inferior valve 2, thereby can guarantee the stability that the camera was shot, improve shooting effect and shooting quality, solved the flight in-process because unmanned aerial vehicle itself's vibration or meet the strong wind and strike the circumstances such as make the cloud platform take place to rock, cause the unstability of camera to rock, lead to shooting the picture unclear, shooting effect is poor, the problem of quality is shot in the influence.
It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.
Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.
Claims (6)
1. The utility model provides an unmanned aerial vehicle and cloud platform damper thereof, includes cloud platform epitheca (1), its characterized in that: a lower holder shell (2) is arranged at the top of the upper holder shell (1), inserting rods (3) are fixedly connected to the left side and the right side of the bottom of the lower holder shell (2), sleeves (4) are fixedly connected to the left side and the right side of the inner bottom wall of the upper holder shell (1), the bottoms of the two inserting rods (3) sequentially penetrate through the upper holder shell (1) and the sleeves (4) and extend into the sleeves (4), sliding plates (5) are fixedly connected to the bottoms of the two inserting rods (3), the two sliding plates (5) are respectively in sliding connection with the two sleeves (4), first springs (6) are fixedly connected to the bottoms of the two sliding plates (5), the bottoms of the two first springs (6) are fixedly connected to the inner bottom wall of the sleeves (4), a connecting rod (7) is fixedly connected between the two inserting rods (3), and two sliding sleeves (8) are slidably connected to the connecting rod (7), the cover is equipped with two second springs (9) on connecting rod (7), two the one end that second spring (9) is relative respectively with two sliding sleeve (8) fixed connection, two the one end that second spring (9) carried on the back mutually respectively with two inserted bar (3) fixed connection, the inside of cloud platform epitheca (1) is provided with damper plate (10), the articulated seat of top fixedly connected with (11) of damper plate (10), the inboard of articulated seat (11) articulates there are two articulated rod (12), two the one end that articulated seat (11) were kept away from in articulated rod (12) is articulated with the bottom of two sliding sleeve (8) respectively, the bottom fixedly connected with evenly distributed's of damper plate (10) damping ball (13), the bottom of damping ball (13) all with the inner diapire fixed connection of cloud platform epitheca (1).
2. The unmanned aerial vehicle and cloud platform damper thereof of claim 1, characterized in that: the inboard fixedly connected with shock attenuation backing plate (14) of cloud platform epitheca (1), shock attenuation backing plate (14) are the component that multilayer elasticity silica gel plate stack formed.
3. The unmanned aerial vehicle and cloud platform damper thereof of claim 2, characterized in that: the top and the bottom of shock attenuation ball (13) are equal fixedly connected with fixed plate (15), the top of fixed plate (15) and the bottom fixed connection of shock attenuation board (10), the bottom of fixed plate (15) and the inboard fixed connection of shock attenuation backing plate (14).
4. The unmanned aerial vehicle and cloud platform damper thereof of claim 1, characterized in that: the left side and the right side of the top of the holder upper shell (1) are respectively embedded with an elastic sleeve ring (16), and the two insertion rods (3) are respectively connected with the inner rings of the two elastic sleeve rings (16) in a sliding manner.
5. The unmanned aerial vehicle and cloud platform damper thereof of claim 1, characterized in that: the top fixedly connected with shock attenuation protection pad (17) of cloud platform epitheca (1), shock attenuation protection pad (17) are located between two inserted bars (3).
6. The unmanned aerial vehicle and cloud platform damper thereof of claim 1, characterized in that: the tops of the two sliding sleeves (8) are fixedly connected with damping and protecting blocks (18).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020246331.4U CN211663474U (en) | 2020-03-04 | 2020-03-04 | Unmanned aerial vehicle and cloud platform damper thereof |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202020246331.4U CN211663474U (en) | 2020-03-04 | 2020-03-04 | Unmanned aerial vehicle and cloud platform damper thereof |
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| Publication Number | Publication Date |
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| CN211663474U true CN211663474U (en) | 2020-10-13 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202020246331.4U Expired - Fee Related CN211663474U (en) | 2020-03-04 | 2020-03-04 | Unmanned aerial vehicle and cloud platform damper thereof |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112224428A (en) * | 2020-10-26 | 2021-01-15 | 湖南库里斯智能科技有限公司 | Aerial photography is camera cloud platform seismic isolation device for unmanned aerial vehicle platform |
| CN114261513A (en) * | 2022-01-14 | 2022-04-01 | 周国峰 | Take absorbing transport unmanned aerial vehicle of braking |
| CN115783331A (en) * | 2022-12-02 | 2023-03-14 | 北京工业职业技术学院 | Intelligent building engineering surveying and mapping device based on unmanned aerial vehicle |
-
2020
- 2020-03-04 CN CN202020246331.4U patent/CN211663474U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112224428A (en) * | 2020-10-26 | 2021-01-15 | 湖南库里斯智能科技有限公司 | Aerial photography is camera cloud platform seismic isolation device for unmanned aerial vehicle platform |
| CN114261513A (en) * | 2022-01-14 | 2022-04-01 | 周国峰 | Take absorbing transport unmanned aerial vehicle of braking |
| CN115783331A (en) * | 2022-12-02 | 2023-03-14 | 北京工业职业技术学院 | Intelligent building engineering surveying and mapping device based on unmanned aerial vehicle |
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20201013 |
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| CF01 | Termination of patent right due to non-payment of annual fee |