CN221542015U - Unmanned aerial vehicle shock attenuation support - Google Patents
Unmanned aerial vehicle shock attenuation support Download PDFInfo
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- CN221542015U CN221542015U CN202323581808.7U CN202323581808U CN221542015U CN 221542015 U CN221542015 U CN 221542015U CN 202323581808 U CN202323581808 U CN 202323581808U CN 221542015 U CN221542015 U CN 221542015U
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- shock
- plate
- aerial vehicle
- unmanned aerial
- shockproof
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- 230000035939 shock Effects 0.000 title claims description 39
- 239000006096 absorbing agent Substances 0.000 claims description 10
- 238000013016 damping Methods 0.000 abstract description 16
- 230000005484 gravity Effects 0.000 abstract description 9
- 230000000694 effects Effects 0.000 abstract description 5
- 238000010521 absorption reaction Methods 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
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- Vibration Dampers (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle damping support, which relates to the technical field of damping support equipment and comprises a bottom plate, a supporting connecting plate, a damping structure and a damping structure; when the unmanned aerial vehicle falls down, the gravity of the unmanned aerial vehicle is pressed on the shockproof slide plate, and the shockproof slide plate is in sliding connection with the slide plate through the sliding frame, so that when the gravity is pressed on the shockproof slide plate, the shockproof slide plate can slide downwards, the downward sliding of the shockproof slide plate can apply pressure to the upper circular plate, and further apply pressure to the shockproof spring, otherwise, the shockproof spring can apply elasticity to the upper circular plate, and further apply elasticity to the shockproof slide plate, and then the pressure of the unmanned aerial vehicle falling down on the shockproof slide plate is reduced under the mutual matching of the shockproof spring and the shockproof telescopic rod, so that the shockproof effect on the falling of the unmanned aerial vehicle is achieved; when the pressure from the shockproof slide plate is sensed, the support plate can be downwards pressed due to the gravity of the support plate, and the downwards pressing of the support plate drives the downwards pressing of the support connecting plate, so that the telescopic rod is driven to downwards stretch.
Description
Technical Field
The utility model relates to the technical field of shock-absorbing support equipment, in particular to an unmanned aerial vehicle shock-absorbing support.
Background
Unmanned aerial vehicle is abbreviated as "unmanned aerial vehicle", is unmanned aerial vehicle that utilizes radio remote control equipment and self-contained program control device to operate, and unmanned aerial vehicle then often need use the support when descending, now, unmanned aerial vehicle on the market is with the support, because of not taking precautions against earthquakes, shock-absorbing effect when it descends, has caused unmanned aerial vehicle to descend the damage, so, the skilled person provides an unmanned aerial vehicle shock attenuation support to solve the problem that proposes among the above-mentioned background art.
Disclosure of Invention
The utility model aims to provide an unmanned aerial vehicle damping bracket to solve the problems in the background art.
In order to achieve the above purpose, the present utility model provides the following technical solutions:
an unmanned aerial vehicle shock absorber bracket comprises a bottom plate, a supporting connecting plate, a shock-proof structure and a shock-proof structure; the four corners of the upper end of the bottom plate are provided with shockproof structures, the lower end of the support connecting plate is provided with a U-shaped plate, and the U-shaped plate is connected with the support connecting plate through the shockproof structures; the anti-vibration structure comprises an anti-vibration telescopic rod, a lower circular plate, an upper circular plate and an anti-vibration spring, wherein the anti-vibration telescopic rod is arranged on the anti-vibration structure, the anti-vibration spring is arranged on a lever arm of the anti-vibration telescopic rod, the upper circular plate is arranged at the upper end of the anti-vibration telescopic rod, and the lower circular plate is arranged at the lower end of the anti-vibration telescopic rod; the shock-absorbing structure comprises a shock-absorbing telescopic rod, an upper connecting plate, a telescopic rod, a shock-absorbing spring and a lower connecting plate, wherein the shock-absorbing telescopic rod is arranged on the shock-absorbing structure, the shock-absorbing spring is arranged on a lever arm of the shock-absorbing telescopic rod, the upper end of the shock-absorbing telescopic rod is provided with the upper connecting plate, the lower end of the shock-absorbing telescopic rod is provided with the lower connecting plate, and the protruding positions of the two sides of the lower end of the upper connecting plate are connected with the protruding positions of the two sides of the upper end of the lower connecting plate through the telescopic rod.
Preferably, the left and right ends of the bottom plate are respectively provided with a sliding plate, both sides on the surface of one end of the inner side of each sliding plate are respectively provided with a sliding groove, the upper end between the two sliding plates and the upper end of the shockproof structure are respectively provided with a shockproof sliding plate, the front and rear sides of the left and right ends of the shockproof sliding plates are respectively provided with a sliding frame which is correspondingly arranged with the sliding grooves, and the sliding grooves are in sliding connection with the sliding frames; the upper end of an upper circular plate on the shock-proof structure is fixedly connected with the lower end of the shock-proof sliding plate, the lower end of a lower circular plate on the shock-proof structure is fixedly connected with the upper end of the bottom plate, the upper end of an upper connecting plate on the shock-proof structure is fixedly connected with the lower end of a supporting connecting plate, and the lower end of a lower connecting plate on the shock-proof structure is fixedly connected with the upper end of the U-shaped plate; the lower extreme of the slide of the left and right both ends of bottom plate all fixedly connected with connects the round bar, connects the equal fixedly connected with backup pad of lower extreme of round bar, the equal fixedly connected with of lower extreme of backup pad supports the connecting plate, and shock-absorbing structure's lower extreme of the U-shaped board all is provided with the slipmat.
Compared with the prior art, the utility model has the beneficial effects that: when the unmanned aerial vehicle falls down, the gravity of the unmanned aerial vehicle is pressed on the shockproof slide plate, and the shockproof slide plate is in sliding connection with the slide plate through the sliding frame, so that when the gravity is pressed on the shockproof slide plate, the shockproof slide plate can slide downwards, the downward sliding of the shockproof slide plate can apply pressure to the upper circular plate, and further apply pressure to the shockproof spring, otherwise, the shockproof spring can apply elasticity to the upper circular plate, and further apply elasticity to the shockproof slide plate, and then the pressure of the unmanned aerial vehicle falling down on the shockproof slide plate is reduced under the mutual matching of the shockproof spring and the shockproof telescopic rod, so that the shockproof effect on the falling of the unmanned aerial vehicle is achieved; when the pressure from the shockproof slide plate is sensed, the support plate can be downwards pressed due to the gravity of the support plate, the support plate downwards presses the support connection plate downwards, the upper connection plate downwards presses the support connection plate, the telescopic rod downwards stretches and contracts, when the upper connection plate downwards presses the upper connection plate, the upper connection plate gives the damping spring a pressure, and otherwise the damping spring gives the upper connection plate an elastic force, and then gives the support plate an elastic force, so that the slide plate and the bottom plate are elastically stressed, and the unmanned aerial vehicle falls down.
Drawings
Fig. 1 is a schematic structural view of a shock mount for an unmanned aerial vehicle.
Fig. 2 is a schematic diagram showing the structural separation of a shock mount for an unmanned aerial vehicle.
Fig. 3 is a schematic view of a shock-proof structure of a shock-absorbing bracket of an unmanned aerial vehicle.
Fig. 4 is a schematic view of a shock absorption structure of a shock absorption bracket of an unmanned aerial vehicle.
In the figure: 1-bottom plate, 2-slide, 3-spout, 4-connect round bar, 5-shock-proof structure, 51-shock-proof telescopic link, 52-lower round plate, 53-upper round plate, 54-shock-proof spring, 6-shock-proof structure, 61-shock-proof telescopic link, 62-upper connecting plate, 63-telescopic link, 64-shock-proof spring, 65-lower connecting plate, 7-shock-proof slide, 8-carriage, 9-backup pad, 10-support connecting plate, 11-U-shaped plate, 12-slipmat.
Detailed Description
The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand. In the description of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance. In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.
Referring to fig. 1 to 4, in an embodiment of the present utility model, an unmanned aerial vehicle shock-absorbing bracket includes a base plate 1, a supporting connection plate 10, a shock-absorbing structure 5 and a shock-absorbing structure 6; the four corners of the upper end of the bottom plate 1 are provided with shockproof structures 5, the lower end of the support connecting plate 10 is provided with a U-shaped plate 11, and the U-shaped plate 11 is connected with the support connecting plate 10 through a shock absorption structure 6; the anti-vibration structure 5 comprises an anti-vibration telescopic rod 51, a lower circular plate 52, an upper circular plate 53 and an anti-vibration spring 54, wherein the anti-vibration telescopic rod 51 is arranged on the anti-vibration structure 5, the anti-vibration spring 54 is arranged on a lever arm of the anti-vibration telescopic rod 51, the upper circular plate 53 is arranged at the upper end of the anti-vibration telescopic rod 51, and the lower circular plate 52 is arranged at the lower end of the anti-vibration telescopic rod 51; the damping structure 6 comprises a damping telescopic rod 61, an upper connecting plate 62, a telescopic rod 63, damping springs 64 and a lower connecting plate 65, wherein the damping telescopic rod 61 is arranged on the damping structure 6, the damping springs 64 are arranged on the lever arms of the damping telescopic rod 61, the upper connecting plate 62 is arranged at the upper end of the damping telescopic rod 61, the lower connecting plate 65 is arranged at the lower end of the damping telescopic rod 61, and the protruding positions at the two sides of the lower end of the upper connecting plate 62 are connected with the protruding positions at the two sides of the upper end of the lower connecting plate 65 through the telescopic rod 63; slide plates 2 are arranged at the left end and the right end of the bottom plate 1, sliding grooves 3 are formed in two sides on the surface of one inner measuring end of each slide plate 2, a shockproof slide plate 7 is arranged at the upper end between the two slide plates 2 and the upper end of a shockproof structure 5, sliding carriages 8 which are arranged corresponding to the sliding grooves 3 are arranged at the front side and the rear side of the left end and the right end of the shockproof slide plate 7, and the sliding grooves 3 are in sliding connection with the sliding carriages 8; the upper end of an upper circular plate 53 on the shock-proof structure 5 is fixedly connected with the lower end of the shock-proof sliding plate 7, the lower end of a lower circular plate 52 on the shock-proof structure 5 is fixedly connected with the upper end of the bottom plate 1, the upper end of an upper connecting plate 62 on the shock-proof structure 6 is fixedly connected with the lower end of the supporting connecting plate 10, and the lower end of a lower connecting plate 65 on the shock-proof structure 6 is fixedly connected with the upper end of the U-shaped plate 11; the lower extreme of slide 2 at the left and right both ends of bottom plate 1 all fixedly connected with connects round bar 4, and the equal fixedly connected with backup pad 9 of lower extreme of connecting round bar 4, the equal fixedly connected with of lower extreme of backup pad 9 supports connecting plate 10, and the lower extreme of the U-shaped plate 11 of the lower extreme of shock-absorbing structure 6 all is provided with slipmat 12.
The working principle of the utility model is as follows: when the unmanned aerial vehicle falls down, the gravity of the unmanned aerial vehicle is pressed on the shockproof slide plate 7, and the shockproof slide plate 7 is in sliding connection with the slide plate 2 through the sliding frame 8, so that when the gravity is pressed on the shockproof slide plate 7, the shockproof slide plate 7 can slide downwards, the downward sliding of the shockproof slide plate 7 can exert pressure on the upper circular plate 53, and further exert pressure on the shockproof spring 54, otherwise, the shockproof spring 54 can exert elastic force on the upper circular plate 53, and further exert elastic force on the shockproof slide plate 7, and then the pressure of the unmanned aerial vehicle falling down on the shockproof slide plate 7 is reduced under the mutual cooperation of the shockproof spring 54 and the shockproof telescopic rod 51, so that the shockproof effect on the falling of the unmanned aerial vehicle is achieved; the supporting plate 9 can also downwards press due to gravity when the pressure from the shockproof slide plate 7 is sensed, the downward pressing of the supporting plate 9 drives the downward pressing of the supporting connecting plate 10, and then the downward pressing of the upper connecting plate 62 is driven, so that the telescopic rod 63 is driven to downwards stretch, when the upper connecting plate 62 downwards presses, the upper connecting plate 62 also gives the shock-absorbing spring 64 a pressure, otherwise, the shock-absorbing spring 64 gives the upper connecting plate 62 a spring force, and then gives the supporting connecting plate 10 a spring force, and then gives the supporting plate 9 a spring force, and thus the slide plate 2 and the bottom plate 1 are provided with a spring force, and the operation is favorable for playing a shock-absorbing role on the landing of the unmanned aerial vehicle.
It will be evident to those skilled in the art that the utility model is not limited to the details of the foregoing illustrative embodiments, and that the present utility model may be embodied in other specific forms without departing from the spirit or essential characteristics thereof. The present embodiments are, therefore, to be considered in all respects as illustrative and not restrictive, the scope of the utility model being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present disclosure describes embodiments, not every embodiment is provided with a separate embodiment, and that this description is provided for clarity only, and that the disclosure is not limited to the embodiments described in detail below, and that the embodiments described in the examples may be combined as appropriate to form other embodiments that will be apparent to those skilled in the art.
Claims (10)
1. An unmanned aerial vehicle shock absorber bracket comprises a bottom plate (1), a supporting connecting plate (10), a shock-proof structure (5) and a shock-proof structure (6); the anti-vibration device is characterized in that four corners of the upper end of the bottom plate (1) are provided with anti-vibration structures (5), the lower end of the support connecting plate (10) is provided with a U-shaped plate (11), and the U-shaped plate (11) is connected with the support connecting plate (10) through the shock-absorbing structures (6).
2. The unmanned aerial vehicle shock absorbing bracket according to claim 1, wherein the shock absorbing structure (5) comprises a shock absorbing telescopic rod (51), a lower circular plate (52), an upper circular plate (53) and a shock absorbing spring (54), and the shock absorbing structure (5) is provided with the shock absorbing telescopic rod (51).
3. The unmanned aerial vehicle shock absorber support according to claim 1, wherein the shock absorber structure (6) comprises a shock absorber telescopic rod (61), an upper connecting plate (62), a telescopic rod (63), a shock absorber spring (64) and a lower connecting plate (65), and the shock absorber structure (6) is provided with the shock absorber telescopic rod (61).
4. The unmanned aerial vehicle shock-absorbing support according to claim 1, wherein the left and right ends of the base plate (1) are provided with sliding plates (2), sliding grooves (3) are formed in two sides on the surface of the inner side end of each sliding plate (2), shock-absorbing sliding plates (7) are arranged at the upper ends of the two sliding plates (2) and the upper ends of the shock-absorbing structures (5), sliding frames (8) corresponding to the sliding grooves (3) are arranged at the front and rear sides of the left and right ends of the shock-absorbing sliding plates (7), and the sliding grooves (3) are in sliding connection with the sliding frames (8).
5. The unmanned aerial vehicle shock absorber support according to claim 1, wherein the upper end of an upper circular plate (53) on the shock-proof structure (5) is fixedly connected with the lower end of the shock-proof sliding plate (7), and the lower end of a lower circular plate (52) on the shock-proof structure (5) is fixedly connected with the upper end of the bottom plate (1).
6. The unmanned aerial vehicle shock absorbing bracket according to claim 1, wherein the upper end of the upper connecting plate (62) on the shock absorbing structure (6) is fixedly connected with the lower end of the supporting connecting plate (10), and the lower end of the lower connecting plate (65) on the shock absorbing structure (6) is fixedly connected with the upper end of the U-shaped plate (11).
7. The unmanned aerial vehicle shock absorber support according to claim 1, wherein the lower ends of the sliding plates (2) at the left end and the right end of the bottom plate (1) are fixedly connected with connecting round rods (4), the lower ends of the connecting round rods (4) are fixedly connected with supporting plates (9), the lower ends of the supporting plates (9) are fixedly connected with supporting connecting plates (10), and anti-slip pads (12) are arranged at the lower ends of the U-shaped plates (11) at the lower ends of the shock absorbing structures (6).
8. The unmanned aerial vehicle shock absorbing bracket according to claim 2, wherein a shock absorbing spring (54) is arranged on a lever arm of the shock absorbing telescopic rod (51), an upper circular plate (53) is arranged at the upper end of the shock absorbing telescopic rod (51), and a lower circular plate (52) is arranged at the lower end of the shock absorbing telescopic rod (51).
9. A shock mount for an unmanned aerial vehicle according to claim 3, wherein the lever arm of the shock mount telescopic lever (61) is provided with a shock mount spring (64), and the upper end of the shock mount telescopic lever (61) is provided with an upper connection plate (62).
10. A shock mount for an unmanned aerial vehicle according to claim 3, wherein the lower end of the shock mount telescopic rod (61) is provided with a lower connecting plate (65), and the protruding positions on both sides of the lower end of the upper connecting plate (62) are connected with the protruding positions on both sides of the upper end of the lower connecting plate (65) by the telescopic rod (63).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323581808.7U CN221542015U (en) | 2023-12-27 | 2023-12-27 | Unmanned aerial vehicle shock attenuation support |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202323581808.7U CN221542015U (en) | 2023-12-27 | 2023-12-27 | Unmanned aerial vehicle shock attenuation support |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN221542015U true CN221542015U (en) | 2024-08-16 |
Family
ID=92260219
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202323581808.7U Active CN221542015U (en) | 2023-12-27 | 2023-12-27 | Unmanned aerial vehicle shock attenuation support |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN221542015U (en) |
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2023
- 2023-12-27 CN CN202323581808.7U patent/CN221542015U/en active Active
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