CN211442790U - Vibration damping base for unmanned aerial vehicle - Google Patents
Vibration damping base for unmanned aerial vehicle Download PDFInfo
- Publication number
- CN211442790U CN211442790U CN201922017168.4U CN201922017168U CN211442790U CN 211442790 U CN211442790 U CN 211442790U CN 201922017168 U CN201922017168 U CN 201922017168U CN 211442790 U CN211442790 U CN 211442790U
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- fixedly connected
- base main
- unmanned aerial
- connecting rod
- aerial vehicle
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Abstract
The utility model relates to the technical field of unmanned aerial vehicles, specifically disclose a vibration damping mount for unmanned aerial vehicles, including the base main body, the second spout has been seted up in the center of base main body bottom, the inside sliding connection of second spout has the balancing weight, the central fixedly connected with first spring at balancing weight top, the top of balancing weight uses balancing weight top center as centre of a circle annular equidistance fixedly connected with four head rods, the top of head rod rotates and is connected with the second connecting rod, the one end that the second connecting rod kept away from the base main body center rotates and is connected with the support that falls to the ground, the top of the support that falls to the ground fixedly connected with second spring, the left and right sides of base main body fixedly connected with guard frame, the top fixedly connected with connecting block of base main body, the bottom of base has seted up first spout; the utility model discloses bottom surface fish tail chassis when preventing that unmanned aerial vehicle from descending has avoided the descending impact force to damage unmanned aerial vehicle's structure.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field, concretely relates to vibration damping mount for unmanned aerial vehicle.
Background
Along with the continuous development of communication technology and control chip technique, unmanned aerial vehicle no longer leaves our inaccessible thing, has become the fresh toy that people accessible at will slowly, and small-size unmanned aerial vehicle has also played its advantage in each field simultaneously and has given play and give out light to generate heat, but unmanned aerial vehicle cost is higher, if do not have the good operation during the landing, then probably the bottom on fish tail chassis, the produced impact force of falling from the sky in addition can damage unmanned aerial vehicle's inner structure.
SUMMERY OF THE UTILITY MODEL
Not enough to prior art, the utility model provides a vibration damping mount for unmanned aerial vehicle possesses can not the fish tail chassis, can cushion advantages such as impact force during the descending, has solved easy fish tail chassis, and the descending impact force can damage the problem of unmanned aerial vehicle structure.
The utility model discloses a vibration damping mount for unmanned aerial vehicle, comprising a base main body, the second spout has been seted up to the central authorities of base main part bottom, the inside sliding connection of second spout has the balancing weight, the first spring of central fixedly connected with at balancing weight top, four head rods of fixedly connected with of balancing weight top central authorities for centre of a circle annular equidistance, the top of head rod is rotated and is connected with the second connecting rod, the one end that base main part central authorities were kept away from to the second connecting rod is rotated and is connected with the support that falls to the ground, the top fixedly connected with second spring of support that falls to the ground, the left and right sides fixedly connected with bearer bar of base main part, the top fixedly connected with connecting block of base main part.
The utility model discloses a vibration damping mount for unmanned aerial vehicle, wherein four first spouts have been seted up as centre of a circle annular equidistance to base main body's bottom with base main body central authorities, fall to the ground support sliding connection in the inside of first spout, this structure sets up for fall to the ground the inside that the support can stretch out and retract base main body, logical groove has been seted up to the inside left and right sides of base main body, the left and right sides of second connecting rod all runs through the left and right sides that leads to the groove, and this structure sets up for the second connecting rod can reciprocate in base main body is inside.
The utility model discloses a vibration damping mount for unmanned aerial vehicle, wherein the inner wall of second spout uses second spout central authorities to offer four third spouts for circular equidistance, the front of balancing weight, the back, the equal fixedly connected with stopper in left side and right side, stopper sliding connection is in the inside of third spout, and this structure setting has injectd the removal orbit of balancing weight, avoids the balancing weight to deviate from second spout is inside.
The utility model discloses a vibration damping mount for unmanned aerial vehicle, wherein the equal fixedly connected with in the left and right sides of second connecting rod changes the piece, the central fixedly connected with pivot of piece changes, the connecting rod groove has been seted up at the positive top of head rod, the support groove has been seted up at the positive top of the support that falls to the ground, the head rod all is connected with the second connecting rod through the pivot with the support that falls to the ground, and this structure sets up for the rise of the support that falls to the ground with put down the control that can receive head rod and second connecting rod.
The utility model discloses a vibration damping mount for unmanned aerial vehicle, wherein the top and the base main part looks fixed connection of first spring, the top of second spring and the inner wall looks fixed connection of bearer bar, this result sets up, has played the cushioning effect to the impact force when unmanned aerial vehicle falls to the ground, the elasticity of first spring is greater than two second spring elasticity sums, and this structure setting avoids falling to the ground the support can't stretch out and retract from the base main part is inside.
The utility model discloses a vibration damping mount for unmanned aerial vehicle, wherein lead to the position department fixedly connected with fulcrum piece that groove inner wall bottom is close to base main part central authorities, the top of fulcrum piece is laminated with the bottom of second connecting rod mutually, and this structure sets up, makes to form a lever between second connecting rod and the fulcrum piece, makes things convenient for the balancing weight to the control of falling to the ground support.
Compared with the prior art, the beneficial effects of the utility model are as follows:
1. the utility model discloses a head rod and the second connecting rod that set up, the cooperation falls to the ground the support, make when the head rod moves down, can drive and fall to the ground the support rebound, when the head rod upward movement, can drive and fall to the ground the support downward movement simultaneously, cooperate the fulcrum piece simultaneously, make to form the lever between fulcrum piece and the head rod, make things convenient for the head rod and the removal of falling to the ground the support, through the first spring that sets up, the cooperation second spring has played the effect of buffering impact force to unmanned aerial vehicle's descending.
2. The utility model discloses a balancing weight that sets up, the cooperation falls to the ground the support for when unmanned aerial vehicle descends, the balancing weight with fall to the ground the support and can play the effect of support and protection to unmanned aerial vehicle, prevent unsmooth bottom surface fish tail unmanned aerial vehicle base, through the third spout that sets up, the cooperation stopper has restricted the balancing weight at the inside slip orbit of second spout, avoid the balancing weight to deviate from the second spout is inside.
Drawings
The accompanying drawings, which are included to provide a further understanding of the application and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the application and together with the description serve to explain the application and not to limit the application. In the drawings:
FIG. 1 is a schematic front sectional view of the present invention;
FIG. 2 is a schematic view of the bottom of the present invention;
FIG. 3 is a schematic top view of the counterweight of the present invention;
fig. 4 is a schematic view of a second connecting rod of the present invention.
In the figure: 1. a base body; 11. a first chute; 12. a through groove; 13. a fulcrum block; 14. a second chute; 15. a third chute; 2. a balancing weight; 21. a limiting block; 3. a first spring; 4. a first connecting rod; 41. a connecting rod slot; 5. a second connecting rod; 51. rotating the block; 52. a rotating shaft; 6. a floor stand; 61. a bracket groove; 7. a second spring; 8. a protective frame; 9. and (4) connecting the blocks.
Detailed Description
In the following description, numerous implementation details are set forth in order to provide a more thorough understanding of the present invention. It should be understood, however, that these implementation details should not be used to limit the invention. That is, in some embodiments of the invention, details of these implementations are not necessary. In addition, some conventional structures and components are shown in simplified schematic form in the drawings.
In addition, the descriptions related to "first", "second", etc. in the present invention are only for description purposes, not specifically referring to the order or sequence, and are not intended to limit the present invention, but only to distinguish the components or operations described in the same technical terms, and are not to be construed as indicating or implying any relative importance or implicit indication of the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include at least one such feature. In addition, the technical solutions in the embodiments may be combined with each other, but it must be based on the realization of those skilled in the art, and when the technical solutions are contradictory or cannot be realized, the combination of the technical solutions should not be considered to exist, and is not within the protection scope of the present invention.
Please refer to fig. 1-4, the utility model discloses a vibration damping mount for unmanned aerial vehicle, including base main body 1, second spout 14 has been seted up to the central authorities of base main body 1 bottom, the inside sliding connection of second spout 14 has balancing weight 2, the first spring of central fixedly connected with 3 at 2 tops of balancing weight, four head rod 4 of fixedly connected with of annular equidistance are regarded as centre of a circle to 2 top central authorities of balancing weight at balancing weight 2's top, head rod 4's top is rotated and is connected with second connecting rod 5, the one end that base main body 1 central authorities were kept away from to second connecting rod 5 is rotated and is connected with and falls to the ground support 6, the top fixedly connected with second spring 7 of the support 6 that falls to the ground, the left and right sides fixedly connected with fender frame 8 of base main body 1.
Four first spouts 11 have been seted up as centre of a circle annular equidistance to base body 1's bottom and use base body 1 central authorities, 6 sliding connection of falling to the ground in the inside of first spout 11, this structure sets up, make falling to the ground support 6 can stretch out and retract base body 1's inside, logical groove 12 has been seted up to the inside left and right sides of base body 1, the left and right sides of logical groove 12 all runs through to the left and right sides of second connecting rod 5, this structure sets up, make second connecting rod 5 can reciprocate in base body 1 is inside.
The inner wall of second spout 14 uses second spout 14 central authorities to offer four third spouts 15 for circular equidistance, the equal fixedly connected with stopper 21 in front, the back, the left side and the right side of balancing weight 2, stopper 21 sliding connection in the inside of third spout 15, and this structure setting has injectd the removal orbit of balancing weight 2, avoids balancing weight 2 to deviate from second spout 14 is inside.
The equal fixedly connected with in the left and right sides of second connecting rod 5 changes piece 51, changes piece 51's central fixedly connected with pivot 52, and connecting rod groove 41 has been seted up at the positive top of head rod 4, and support groove 61 has been seted up at the positive top of support 6 that falls to the ground, and head rod 4 all is connected with second connecting rod 5 through pivot 52 with support 6 that falls to the ground, and this structure sets up for the rise of support 6 that falls to the ground with put down the control that can receive head rod 4 and second connecting rod 5.
The top and the base main part 1 looks fixed connection of first spring 3, the top of second spring 7 and the inner wall looks fixed connection of bearer bar 8, this result sets up, and the impact force when falling to the ground to unmanned aerial vehicle has played the cushioning effect, and the elasticity of first spring 3 is greater than the sum of two second spring 7 elasticity, and this structure setting is avoided falling to the ground support 6 and can't stretch out and retract from base main part 1 is inside.
Through 12 inner walls of the groove bottom of the base near the center of the base body 1 fixed connection with the fulcrum block 13, the top of the fulcrum block 13 is attached to the bottom of the second connecting rod 5, the structure is arranged, so that a lever is formed between the second connecting rod 5 and the fulcrum block 13, and the counterweight block 2 is convenient to control the floor stand 6.
When the utility model is used, a worker firstly connects the base main body 1 with the unmanned aerial vehicle through the connecting block 9, then operates the unmanned aerial vehicle to lift off, at the moment, the first spring 3 is in a stretching state under the action of the balancing weight 2, meanwhile, the balancing weight 2 and the first connecting rod 4 pull the second connecting rod 5, the landing bracket 6 is retracted into the first chute 11 arranged on the base main body 1 under the action of the first connecting rod 4 and the second connecting rod 5, at the moment, the second spring 7 is in an extruding state, when the unmanned aerial vehicle lands, the balancing weight 2 is firstly contacted with the ground, along with the landing of the unmanned aerial vehicle, the balancing weight 2 moves to the top of the second chute 14 and drives the first connecting rod 4 and the second connecting rod 5 to move, at the moment, the landing bracket 6 extends out of the base main body 1 under the action of the second connecting rod 5 and protects the unmanned aerial vehicle from landing, at last, when the bottom of the balancing weight 2 and the bottom, unmanned aerial vehicle descends and finishes, and then the staff retrieve unmanned aerial vehicle can.
The above description is only an embodiment of the present invention, and is not intended to limit the present invention. Various modifications and changes may occur to those skilled in the art. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.
Claims (6)
1. The utility model provides a vibration damping mount for unmanned aerial vehicle, includes base main part (1), its characterized in that: a second sliding chute (14) is arranged at the center of the bottom of the base main body (1), a balancing weight (2) is connected inside the second sliding chute (14) in a sliding manner, the center of the top of the balancing weight (2) is fixedly connected with a first spring (3), the top of the balancing weight (2) is annularly and fixedly connected with four first connecting rods (4) at equal intervals by taking the center of the top of the balancing weight (2) as a circle center, the top of the first connecting rod (4) is rotationally connected with a second connecting rod (5), one end of the second connecting rod (5) far away from the center of the base main body (1) is rotatably connected with a floor stand (6), the top of the floor stand (6) is fixedly connected with a second spring (7), the left side and the right side of the base main body (1) are fixedly connected with a protective frame (8), the top of the base body (1) is fixedly connected with a connecting block (9).
2. The vibration damping mount for the unmanned aerial vehicle according to claim 1, wherein: the bottom of base main part (1) uses base main part (1) central authorities to offer four first spouts (11) as centre of a circle annular equidistance, fall to ground support (6) sliding connection in the inside of first spout (11), logical groove (12) have been seted up to the inside left and right sides of base main part (1), the left and right sides that lead to groove (12) all runs through to the left and right sides of second connecting rod (5).
3. The vibration damping mount for the unmanned aerial vehicle according to claim 1, wherein: the inner wall of second spout (14) uses second spout (14) central authorities to offer four third spouts (15) for circular equidistance, the equal fixedly connected with stopper (21) in front, the back, the left side and the right side of balancing weight (2), stopper (21) sliding connection is in the inside of third spout (15).
4. The vibration damping mount for the unmanned aerial vehicle according to claim 1, wherein: the equal fixedly connected with in the left and right sides of second connecting rod (5) changes piece (51), the central fixedly connected with pivot (52) of changing piece (51), connecting rod groove (41) have been seted up at the positive top of head rod (4), support slot (61) have been seted up at the positive top of support (6) that falls to the ground, head rod (4) and support (6) that fall to the ground all are connected with second connecting rod (5) through pivot (52).
5. The vibration damping mount for the unmanned aerial vehicle according to claim 1, wherein: the top of the first spring (3) is fixedly connected with the base main body (1), the top of the second spring (7) is fixedly connected with the inner wall of the protective frame (8), and the elastic force of the first spring (3) is greater than the sum of the elastic forces of the two second springs (7).
6. The vibration damping mount for the unmanned aerial vehicle according to claim 2, wherein: the bottom of the inner wall of the through groove (12) is fixedly connected with a fulcrum block (13) at a position close to the center of the base main body (1), and the top of the fulcrum block (13) is attached to the bottom of the second connecting rod (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922017168.4U CN211442790U (en) | 2019-11-21 | 2019-11-21 | Vibration damping base for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922017168.4U CN211442790U (en) | 2019-11-21 | 2019-11-21 | Vibration damping base for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211442790U true CN211442790U (en) | 2020-09-08 |
Family
ID=72317971
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922017168.4U Expired - Fee Related CN211442790U (en) | 2019-11-21 | 2019-11-21 | Vibration damping base for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211442790U (en) |
-
2019
- 2019-11-21 CN CN201922017168.4U patent/CN211442790U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210106 Address after: 510000 B1B2, one, two, three and four floors of the podium building 231 and 233, science Avenue, Guangzhou, Guangdong. Patentee after: BOAO ZONGHENG NETWORK TECHNOLOGY Co.,Ltd. Address before: 239300 No.16 Wanyuan team, Hushan village, Ping'an Town, Tianchang City, Chuzhou City, Anhui Province Patentee before: Xu Jiabing Effective date of registration: 20210106 Address after: Room 405, building A2, 555 Chuangye Road, Dayun Town, Jiashan County, Jiaxing City, Zhejiang Province Patentee after: Jiaxing Ness Technology Co.,Ltd. Address before: 510000 B1B2, one, two, three and four floors of the podium building 231 and 233, science Avenue, Guangzhou, Guangdong. Patentee before: BOAO ZONGHENG NETWORK TECHNOLOGY Co.,Ltd. |
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| TR01 | Transfer of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20200908 Termination date: 20211121 |
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| CF01 | Termination of patent right due to non-payment of annual fee |