CN214649097U - Unmanned aerial vehicle base that rises and falls - Google Patents
Unmanned aerial vehicle base that rises and falls Download PDFInfo
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- CN214649097U CN214649097U CN202120859525.6U CN202120859525U CN214649097U CN 214649097 U CN214649097 U CN 214649097U CN 202120859525 U CN202120859525 U CN 202120859525U CN 214649097 U CN214649097 U CN 214649097U
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Abstract
The utility model discloses an unmanned aerial vehicle base that rises and falls, press from both sides tight fixing device including vertical direction damping device, horizontal direction damping device and unmanned aerial vehicle bottom. The utility model belongs to the technical field of unmanned aerial vehicle base equipment that rises and falls, specifically indicate an unmanned aerial vehicle base that rises and falls, damping device through the vertical direction of increase when unmanned aerial vehicle whereabouts, reduce the impact force that unmanned aerial vehicle bottom support received, avoid the bottom support to fall a lot of and roll over the damage at a high speed, the horizontal direction reduces the shake, can avoid because unmanned aerial vehicle can't descend and put at lift base central point and make the base take place to incline, so that the base is emptyd, the clamping device and the cooperation of vertical direction damping device of unmanned aerial vehicle bottom, can be with unmanned aerial vehicle's bottom mounting, collision bounce once more when avoiding unmanned aerial vehicle to fall, effectively solved current unmanned aerial vehicle landing device on the existing market low unmanned aerial vehicle protection efficiency, and self structure is complicated, maintain comparatively inconvenient problem.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle base equipment that rises and falls, specifically indicate an unmanned aerial vehicle base that rises and falls.
Background
An unmanned aircraft, abbreviated as "drone", and abbreviated in english as "UAV", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. People's unmanned aerial vehicle that often uses is when descending, because the operation is not skilled or because the damage of internal control ware, leads to unmanned aerial vehicle to descend not steadily, loses the unmanned aerial vehicle of power directly to weigh down in the twinkling of an eye, and the unbalanced acting force of production makes unmanned aerial vehicle slope fall over, can damage unmanned aerial vehicle's flight control ware when serious.
SUMMERY OF THE UTILITY MODEL
To the above circumstances, for overcoming prior art's defect, the utility model provides an unmanned aerial vehicle base that rises and falls, damping device through increasing vertical direction when unmanned aerial vehicle whereabouts, reduce the impact force that unmanned aerial vehicle bottom support received, avoid the bottom support to fall to reduce the loss at a high speed many times, the horizontal direction reduces the shake, can avoid because unmanned aerial vehicle can't descend and put at lift base central point and make the base take place to incline, so that the base is emptyd, the clamping device and the cooperation of vertical direction damping device of unmanned aerial vehicle bottom, can be with unmanned aerial vehicle's bottom mounting, collision bounces once more when avoiding unmanned aerial vehicle to fall, effectively solved current unmanned aerial vehicle landing device on the existing market and to unmanned aerial vehicle protection inefficiency, and self structure is complicated, maintain comparatively inconvenient problem.
The utility model adopts the following technical scheme: the utility model relates to an unmanned aerial vehicle rises and falls base, including vertical direction damping device, horizontal direction damping device and unmanned aerial vehicle bottom clamping fixing device, horizontal direction damping device locates on the vertical direction damping device, unmanned aerial vehicle bottom clamping fixing device locates on the vertical direction damping device; the vertical direction damping device comprises a placing bottom plate, an upper end bearing plate, a balance rotating sleeve, a balance rotating bracket, a balance rotating groove, a vertical damping sleeve, a vertical damping limiting block, a vertical damping spring, a limiting block pressing bracket and a pressing bracket connecting column, wherein the placing bottom plate is connected with the horizontal direction damping device, the upper end bearing plate is connected with an unmanned aerial vehicle bottom clamping and fixing device, the balance rotating sleeve is arranged on the upper end bearing plate, the balance rotating groove is arranged on the balance rotating sleeve, the balance rotating bracket is clamped and rotatably arranged on the balance rotating groove, the vertical damping sleeve is arranged on the balance rotating bracket, the vertical damping limiting block is arranged on the vertical damping sleeve, the vertical damping spring is arranged on the vertical damping sleeve, the pressing bracket connecting column is arranged on the horizontal direction damping device, and the limiting block pressing bracket is arranged on the pressing bracket connecting column, the limiting block presses the support block to slide on the vertical shock absorption sleeve.
Further, horizontal direction damping device includes that bottom horizontal fixation plate, level rock the connecting plate, the shock absorber spring is rocked to level upper end shake linking bridge, upper end horizontal stand swinging groove and level, bottom horizontal fixation plate locates on placing the bottom plate, the level is rocked the connecting plate block and is rotated and locate on the bottom horizontal fixation plate, the connecting plate is rocked with the level to level upper end shake linking bridge and is linked to each other, the upper end horizontal stand swinging groove is located the level and is rocked on the connecting plate, level upper end shake linking bridge block rotate locate on the upper end horizontal stand swinging groove, level upper end shake linking bridge block rotate locate press down on the support spliced pole, the level is rocked the shock absorber spring and is located the level and rock on the connecting plate.
Further, tight fixing device of unmanned aerial vehicle bottom clamp includes that gear block groove, gear press connecting plate and unmanned aerial vehicle are pressed to power motor, rotating gear, rack block groove, slip rack, rack connection shock attenuation extrusion spring, rack, gear block groove is located on the upper end loading board, the gear is located on the upper end loading board for power motor, rotating gear block rotates and locates on the gear block groove, rack block groove links to each other with gear block groove, slip rack block slides and locates on the rack block groove, rack connection shock attenuation extrusion spring locates on the slip rack, the rack is pressed the connecting plate and is located on the rack connection shock attenuation extrusion spring, unmanned aerial vehicle links to each other with the contact of upper end loading board.
Further, the diameter of the pressing bracket connecting column is smaller than that of the vertical shock-absorbing sleeve.
Further, the vertical damping limiting block is electrically connected with a gear power supply motor.
Further, the rack engaging groove is formed in an arc shape, and the slide rack is formed in an arc shape.
Adopt above-mentioned structure the utility model discloses the beneficial effect who gains as follows: this scheme an unmanned aerial vehicle base that rises and falls, damping device through increasing vertical direction when unmanned aerial vehicle whereabouts, reduce the impact force that unmanned aerial vehicle bottom support received, avoid the bottom support to fall at a high speed many times and roll over the damage, the horizontal direction reduces the shake, can avoid because unmanned aerial vehicle can't descend and put the base and take place the slope at lift base central point, so that the base is emptyd, the clamping device and the cooperation of vertical direction damping device of unmanned aerial vehicle bottom, can be with unmanned aerial vehicle's bottom mounting, collision bounces once more when avoiding unmanned aerial vehicle to fall, effectively solved present unmanned aerial vehicle landing device on the existing market low unmanned aerial vehicle protection efficiency, and self structure is complicated, maintain comparatively inconvenient problem.
Drawings
Fig. 1 is a front sectional view of an unmanned aerial vehicle landing base of the present invention;
fig. 2 is a front view of an unmanned aerial vehicle landing base of the present invention;
FIG. 3 is an enlarged view of a portion A of FIG. 1;
FIG. 4 is a partial enlarged view of portion B of FIG. 1;
FIG. 5 is an enlarged view of a portion C of FIG. 1;
fig. 6 is a partially enlarged view of a portion D in fig. 1.
Wherein, 1, vertical direction damping device, 2, horizontal direction damping device, 3, unmanned aerial vehicle bottom presss from both sides tight fixing device, 4, place the bottom plate, 5, the upper end loading board, 6, balanced rotating sleeve, 7, balanced rotating bracket, 8, balanced rotating groove, 9, vertical damping sleeve, 10, vertical shock attenuation stopper, 11, vertical damping spring, 12, stopper pressing bracket, 13, pressing bracket connecting post, 14, bottom horizontal fixing plate, 15, the connecting plate is rocked to the level, 16, horizontal upper end shake linking bridge, 17, upper end horizontal stand wobbling groove, 18, damping spring is rocked to the level, 19, gear block groove, 20, gear gives driving motor, 21, rotating gear, 22, rack block groove, 23, the slip rack, 24, rack connection shock attenuation extrusion spring, 25, pressing connecting plate, 26, small-size unmanned aerial vehicle rack.
The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the 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.
As shown in fig. 1-6, the utility model relates to an unmanned aerial vehicle lifting base, which comprises a vertical direction damping device 1, a horizontal direction damping device 2 and an unmanned aerial vehicle bottom clamping and fixing device 3, wherein the horizontal direction damping device 2 is arranged on the vertical direction damping device 1, and the unmanned aerial vehicle bottom clamping and fixing device 3 is arranged on the vertical direction damping device 1; the vertical direction damping device 1 comprises a placing bottom plate 4, an upper end bearing plate 5, a balance rotating sleeve 6, a balance rotating bracket 7, a balance rotating groove 8, a vertical damping sleeve 9, a vertical damping stopper 10, a vertical damping spring 11, a stopper pressing bracket 12 and a pressing bracket connecting column 13, wherein the placing bottom plate 4 is connected with a horizontal direction damping device 2, the upper end bearing plate 5 is connected with an unmanned aerial vehicle bottom clamping and fixing device 3, the balance rotating sleeve 6 is arranged on the upper end bearing plate 5, the balance rotating groove 8 is arranged on the balance rotating sleeve 6, the balance rotating bracket 7 is clamped and rotatably arranged on the balance rotating groove 8, the vertical damping sleeve 9 is arranged on the balance rotating bracket 7, the vertical damping stopper 10 is arranged on the vertical damping sleeve 9, the vertical damping spring 11 is arranged on the vertical damping sleeve 9, the pressing support connecting column 13 is arranged on the horizontal damping device 2, the limiting block pressing support 12 is arranged on the pressing support connecting column 13, and the limiting block pressing support 12 is clamped and slidably arranged on the vertical damping sleeve 9.
Horizontal direction damping device 2 includes that bottom horizontal fixation board 14, level rock connecting plate 15, level upper end shake connecting bracket 16, upper end horizontal bracket swinging groove 17 and level rock damping spring 18, bottom horizontal fixation board 14 is located and is placed on bottom plate 4, the level is rocked connecting plate 15 block and is rotated and locate bottom horizontal fixation board 14 on, level upper end shake connecting bracket 16 and level rock connecting plate 15 and link to each other, upper end horizontal bracket swinging groove 17 is located the level and is rocked on connecting plate 15, level upper end shake connecting bracket 16 block and rotate and locate on upper end horizontal bracket swinging groove 17, level upper end shake connecting bracket 16 block and rotate and locate on pressing down support connecting post 13, level rock damping spring 18 and locate the level and rock on connecting plate 15.
Unmanned aerial vehicle bottom presss from both sides tight fixing device 3 and includes that gear block groove 19, gear press connecting plate 25 and small-size unmanned aerial vehicle 26 for driving motor 20, rotating gear 21, rack block groove 22, slip rack 23, rack junction shock attenuation extrusion spring 24, rack, gear block groove 19 is located on upper end loading board 5, the gear is located on upper end loading board 5 for driving motor 20, rotating gear 21 block is rotated and is located on gear block groove 19, rack block groove 22 links to each other with gear block groove 19, slip rack 23 block slides and locates on rack block groove 22, rack junction shock attenuation extrusion spring 24 is located on slip rack 23, rack press connecting plate 25 to locate on rack junction shock attenuation extrusion spring 24, small-size unmanned aerial vehicle 26 links to each other with the contact of upper end loading board 5.
The diameter of the pressing bracket connecting column 13 is smaller than that of the vertical damper sleeve 9.
The vertical damping limiting block 10 is electrically connected with a gear power supply motor 20.
The rack engaging groove 22 is formed in an arc shape, and the slide rack 23 is formed in an arc shape.
When the small unmanned aerial vehicle 26 is landed on the upper end bearing plate 5 by a user, the bottom of the small unmanned aerial vehicle 26 collides with the upper end bearing plate 5, the upper end bearing plate 5 descends, the vertical damping spring 11 deforms, the stopper pressing bracket 12 collides with the vertical damping stopper 10, the vertical damping stopper 10 sends an electric signal to the power motor 20 through the gear, the rotating gear 21 rotates to drive the sliding rack 23 to slide along the rack clamping groove 22, the rack pressing connecting plate 25 collides with the bottom bracket of the small unmanned aerial vehicle 26, the rack connecting damping extrusion spring 24 deforms, the rack pressing connecting plate 25 fixes the small unmanned aerial vehicle 26, when the landing point of the small unmanned aerial vehicle 26 is not at the center of the upper end bearing plate 5, the upper end bearing plate 5 inclines and shakes, the horizontal upper end shaking connecting bracket 16 rotates along the clamping point with the pressing bracket connecting column 13, and the horizontal shaking connecting plate 15 rotates along the clamping point with the bottom horizontal fixing plate 14, damping spring 18 deformation is rocked to the level, and the level rocks connecting plate 15 and rocks the inclination that slows down upper end loading board 5 gradually, makes upper end loading board 5 tend to balanced, and it is above that the utility model discloses holistic work flow, repeated this step can when using next time.
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.
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.
The present invention and the embodiments thereof have been described above, but the description is not limited thereto, and the embodiment shown in the drawings is only one of the embodiments of the present invention, and the actual structure is not limited thereto. In summary, those skilled in the art should understand that they should not be limited to the embodiments described above, and that they can design the similar structure and embodiments without departing from the spirit of the invention.
Claims (6)
1. The utility model provides an unmanned aerial vehicle base that rises and falls which characterized in that: the damping device is arranged on the damping device in the vertical direction, and the clamping and fixing device for the bottom end of the unmanned aerial vehicle is arranged on the damping device in the vertical direction; the vertical direction damping device comprises a placing bottom plate, an upper end bearing plate, a balance rotating sleeve, a balance rotating bracket, a balance rotating groove, a vertical damping sleeve, a vertical damping limiting block, a vertical damping spring, a limiting block pressing bracket and a pressing bracket connecting column, wherein the placing bottom plate is connected with the horizontal direction damping device, the upper end bearing plate is connected with an unmanned aerial vehicle bottom clamping and fixing device, the balance rotating sleeve is arranged on the upper end bearing plate, the balance rotating groove is arranged on the balance rotating sleeve, the balance rotating bracket is clamped and rotatably arranged on the balance rotating groove, the vertical damping sleeve is arranged on the balance rotating bracket, the vertical damping limiting block is arranged on the vertical damping sleeve, the vertical damping spring is arranged on the vertical damping sleeve, the pressing bracket connecting column is arranged on the horizontal direction damping device, and the limiting block pressing bracket is arranged on the pressing bracket connecting column, the limiting block presses the support block to slide on the vertical shock absorption sleeve.
2. An unmanned aerial vehicle landing base as claimed in claim 1, wherein: horizontal direction damping device includes that bottom horizontal fixation plate, level rock the connecting plate, horizontal upper end shake linking bridge, upper end horizontal stand swinging groove and level rock damping spring, bottom horizontal fixation plate is located and is placed on the bottom plate, the level rocks the connecting plate block and rotates and locate on the horizontal fixation plate of bottom, the connecting plate links to each other is rocked with the level to horizontal upper end shake linking bridge, upper end horizontal stand swinging groove is located the level and is rocked on the connecting plate, horizontal upper end shake linking bridge block rotate locate on the upper end horizontal stand swinging groove, horizontal upper end shake linking bridge block rotate locate press down on the support spliced pole, damping spring is rocked to the level and is located on the connecting plate.
3. An unmanned aerial vehicle landing base as claimed in claim 2, wherein: unmanned aerial vehicle bottom presss from both sides tight fixing device includes that gear block groove, gear give motor power, rotating gear, rack block groove, slip rack, rack connection shock attenuation extrusion spring, rack press connecting plate and unmanned aerial vehicle, gear block groove is located on the upper end loading board, the gear is located on the upper end loading board for motor power, rotating gear block rotates and locates on the gear block groove, rack block groove links to each other with gear block groove, slip rack block slides and locates on the rack block groove, rack connection shock attenuation extrusion spring locates on the slip rack, the rack presses the connecting plate and locates on the rack connection shock attenuation extrusion spring, unmanned aerial vehicle links to each other with the contact of upper end loading board.
4. An unmanned aerial vehicle landing base as claimed in claim 3, wherein: the diameter of the pressing support connecting column is smaller than that of the vertical shock absorption sleeve.
5. An unmanned aerial vehicle landing base as claimed in claim 4, wherein: and the vertical damping limiting block is electrically connected with a power motor through a gear.
6. An unmanned aerial vehicle landing base as claimed in claim 5, wherein: the rack engaging groove is formed in an arc shape, and the sliding rack is formed in an arc shape.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120859525.6U CN214649097U (en) | 2021-04-25 | 2021-04-25 | Unmanned aerial vehicle base that rises and falls |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202120859525.6U CN214649097U (en) | 2021-04-25 | 2021-04-25 | Unmanned aerial vehicle base that rises and falls |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214649097U true CN214649097U (en) | 2021-11-09 |
Family
ID=78471529
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202120859525.6U Expired - Fee Related CN214649097U (en) | 2021-04-25 | 2021-04-25 | Unmanned aerial vehicle base that rises and falls |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214649097U (en) |
-
2021
- 2021-04-25 CN CN202120859525.6U patent/CN214649097U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20211109 |