CN214986035U - Damping mechanism of aerial remote sensing surveying and mapping unmanned aerial vehicle - Google Patents
Damping mechanism of aerial remote sensing surveying and mapping unmanned aerial vehicle Download PDFInfo
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- CN214986035U CN214986035U CN202121180741.4U CN202121180741U CN214986035U CN 214986035 U CN214986035 U CN 214986035U CN 202121180741 U CN202121180741 U CN 202121180741U CN 214986035 U CN214986035 U CN 214986035U
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- damping
- sleeve
- plate
- remote sensing
- aerial vehicle
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- 238000013016 damping Methods 0.000 title claims abstract description 43
- 238000013507 mapping Methods 0.000 title claims abstract description 9
- 230000035939 shock Effects 0.000 claims abstract description 11
- 238000010521 absorption reaction Methods 0.000 claims abstract description 3
- 230000003014 reinforcing effect Effects 0.000 claims description 3
- 230000003139 buffering effect Effects 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 8
- 238000000034 method Methods 0.000 description 3
- 238000012986 modification Methods 0.000 description 3
- 230000004048 modification Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000001771 impaired effect Effects 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle damping mechanism for aerial remote sensing surveying and mapping, which comprises a connecting plate and a damping plate, wherein a damping base is arranged below the damping plate, and a damping piece is arranged between the connecting plate and the damping plate; the buffer piece comprises a sleeve A fixed on the upper surface of the shock absorption base, the bottom surface of the connecting plate is fixedly connected with a guide pillar, the bottom end of the guide pillar is wedge-shaped, two side walls inside the sleeve A are symmetrically provided with buffer sleeves, each buffer sleeve is internally provided with a wedge-shaped block matched with the guide pillar, and a spring A is connected between each wedge-shaped block and the buffer sleeve; the utility model discloses simple structure, buffering effect is good, is suitable for as current aviation remote sensing survey and drawing unmanned aerial vehicle damper's substitute product.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field especially relates to an aviation remote sensing survey and drawing unmanned aerial vehicle damper.
Background
Remote sensing refers to non-contact, remote sensing techniques. Generally refers to a theory, method and applied scientific technology which uses a sensor/remote sensor to detect the radiation and reflection characteristics of electromagnetic waves of an object and analyzes the property, characteristic and state of the object according to the characteristics.
Aviation remote sensing survey and drawing unmanned aerial vehicle makes unmanned aerial vehicle take place the slope because the weight of self is great impact force occasionally at the landing, and then makes wing or organism impaired, is unfavorable for landing of unmanned aerial vehicle safety.
Therefore, a new technical solution is needed to solve the above-mentioned shortcomings.
SUMMERY OF THE UTILITY MODEL
The utility model aims to solve the problem that, overcome not enough among the prior art, provide an aviation remote sensing survey and drawing unmanned aerial vehicle damper.
The utility model discloses a realize through following technical scheme:
a damping mechanism of an aerial remote sensing surveying and mapping unmanned aerial vehicle comprises a connecting plate and a damping plate, wherein a damping base is arranged below the damping plate, and a damping piece is arranged between the connecting plate and the damping plate;
the buffer piece comprises a sleeve A fixed on the upper surface of the shock absorption base, the bottom surface of the connecting plate is fixedly connected with a guide pillar, the bottom end of the guide pillar is wedge-shaped, two side walls inside the sleeve A are symmetrically provided with buffer sleeves, each buffer sleeve is internally provided with a wedge-shaped block matched with the guide pillar, and a spring A is connected between each wedge-shaped block and the buffer sleeve;
damping base includes the connecting rod, the top of connecting rod with the bottom surface fixed connection of shock attenuation board, the bottom fixed connection limiting plate of connecting rod, the limiting plate slip cap is established in sleeve B's inside, sleeve B with be provided with spring B between the shock attenuation board, bottom plate is connected to sleeve B's bottom surface.
Preferably, the number of the damping bases is more than two, and the damping bases are distributed in a central symmetry mode.
Preferably, the bottom surface of the bottom plate is provided with a buffer pad.
Preferably, the bottom surface of the bottom plate is provided with anti-skid grains.
Preferably, reinforcing plates are connected to two sides of the bottom plate and the top of the sleeve B.
Advantageous effects
Compared with the prior art, the utility model has the advantages and positive effects that the damping mechanism of the aerial remote sensing surveying and mapping unmanned aerial vehicle realizes the damping effect through the arrangement of the damping base and the buffer piece, avoids the problem of body damage caused by overlarge landing impact force of the unmanned aerial vehicle, and ensures that the unmanned aerial vehicle plays a supporting role during landing through the bottom plate provided with the buffer piece, thereby ensuring stable landing; the utility model discloses simple structure, buffering effect is good, is suitable for as current aviation remote sensing survey and drawing unmanned aerial vehicle damper's substitute product.
Drawings
Fig. 1 is the utility model discloses aerial remote sensing survey and drawing unmanned aerial vehicle damper's schematic structure diagram.
Fig. 2 is an enlarged schematic view at a of fig. 1.
Detailed Description
To further illustrate the technical means and effects of the present invention adopted to achieve the predetermined objects, the following detailed description of the damping mechanism of the unmanned aerial vehicle for aerial remote sensing surveying and mapping according to the present invention with reference to the accompanying drawings and preferred embodiments shows the following detailed description.
As shown in fig. 1 to 2, the damping mechanism for the aerial remote sensing surveying and mapping unmanned aerial vehicle comprises a connecting plate 1 and a damping plate 2, wherein a damping base 3 is arranged below the damping plate 2, and a damping member 4 is arranged between the connecting plate 1 and the damping plate 2;
the buffer part 4 comprises a sleeve A401 fixed on the upper surface of the damping base 3, the bottom surface of the connecting plate 1 is fixedly connected with a guide pillar 402, the bottom end of the guide pillar 402 is wedge-shaped, two side walls inside the sleeve A401 are symmetrically provided with buffer sleeves 403, each buffer sleeve 403 is internally provided with a wedge-shaped block 404 matched with the guide pillar 402, and a spring A405 is connected between each wedge-shaped block 404 and the buffer sleeve 403;
Further, the number of the damping bases 3 is more than two, and the damping bases are distributed in central symmetry.
Further, a cushion pad is disposed on the bottom surface of the bottom plate 305.
Further, the bottom surface of the bottom plate 305 is provided with anti-slip lines.
Further, reinforcing plates 306 are connected to both sides of the bottom plate 305 and the top of the sleeve B303.
The working principle is as follows:
as shown in fig. 1-2, aerial remote sensing survey and drawing unmanned aerial vehicle is connected to connecting plate 1, when unmanned aerial vehicle descends, connecting plate 1 receives decurrent effort, connecting plate 1 drives guide pillar 402 and moves down, the bottom of guide pillar 402 receives the elasticity of wedge 404 to block, play the shock attenuation effect, guide pillar 402 continues to descend to contact shock attenuation board 2, shock attenuation board 2 drives connecting rod 301 and moves down, receive the elastic force effect of spring B302, play cushioning effect once more, ensure the shock attenuation effect.
In the working principle, the damping base 3 and the buffer piece 4 are arranged to realize the damping effect together, so that the problem of body damage caused by overlarge landing impact force of the unmanned aerial vehicle is avoided, and the base plate 305 provided with the buffer pad is used for ensuring that the unmanned aerial vehicle plays a supporting role during landing and ensures stable landing; the utility model discloses simple structure, buffering effect is good, is suitable for as current aviation remote sensing survey and drawing unmanned aerial vehicle damper's substitute product.
It will be understood by those skilled in the art that in the present disclosure, the terms "longitudinal," "lateral," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like are used in a generic and descriptive sense only and not for purposes of limitation, as the terms are used in the description to indicate that the referenced device or element must have the specified orientation, be constructed and operated in the specified orientation, and not for the purpose of limitation.
It is understood that the terms "a" and "an" should be interpreted as meaning that a number of one element or element is one in one embodiment, while a number of other elements is one in another embodiment, and the terms "a" and "an" should not be interpreted as limiting the number.
References to "one embodiment," "an embodiment," "example embodiment," "various embodiments," "some embodiments," etc., indicate that the embodiment of the invention described herein may include a particular feature, structure, or characteristic, but every embodiment may not necessarily include the feature, structure, or characteristic. In addition, some embodiments may have some, all, or none of the features described for other embodiments.
The above description is only a preferred embodiment of the present invention, and the present invention is not limited to the above embodiments, and although the present invention has been disclosed with the preferred embodiments, it is not limited to the present invention, and any person skilled in the art can make some changes or modifications to equivalent embodiments without departing from the scope of the present invention, but all those skilled in the art can make any simple modifications, equivalent changes and modifications to the above embodiments without departing from the technical scope of the present invention.
Claims (5)
1. The damping mechanism of the aerial remote sensing surveying and mapping unmanned aerial vehicle is characterized by comprising a connecting plate (1) and a damping plate (2), wherein a damping base (3) is arranged below the damping plate (2), and a damping piece (4) is arranged between the connecting plate (1) and the damping plate (2);
the buffer piece (4) comprises a sleeve A (401) fixed on the upper surface of the shock absorption base (3), the bottom surface of the connecting plate (1) is fixedly connected with a guide pillar (402), the bottom end of the guide pillar (402) is wedge-shaped, two side walls inside the sleeve A (401) are symmetrically provided with buffer sleeves (403), each buffer sleeve (403) is internally provided with a wedge-shaped block (404) matched with the guide pillar (402), and a spring A (405) is connected between each wedge-shaped block (404) and the buffer sleeve (403);
damping base (3) include connecting rod (301), the top of connecting rod (301) with the bottom surface fixed connection of shock attenuation board (2), the bottom fixed connection limiting plate (304) of connecting rod (301), limiting plate (304) slip cover is established in the inside of sleeve B (303), sleeve B (303) with be provided with spring B (302) between shock attenuation board (2), bottom plate (305) is connected to the bottom surface of sleeve B (303).
2. The aerial remote sensing surveying and mapping unmanned aerial vehicle damper of claim 1, characterized in that, the quantity of vibration damping mount (3) is more than two, is central symmetry distribution.
3. The aerial remote sensing surveying unmanned aerial vehicle damper of claim 1, characterized in that a bottom surface of the base plate (305) is provided with a cushion pad.
4. The aerial remote sensing surveying unmanned aerial vehicle damper of claim 1, wherein a bottom surface of the base plate (305) is provided with anti-slip lines.
5. The aerial remote sensing surveying unmanned aerial vehicle damper of claim 1, characterized in that reinforcing plates (306) are connected to both sides of the bottom plate (305) and the top of the sleeve B (303).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121180741.4U CN214986035U (en) | 2021-05-28 | 2021-05-28 | Damping mechanism of aerial remote sensing surveying and mapping unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121180741.4U CN214986035U (en) | 2021-05-28 | 2021-05-28 | Damping mechanism of aerial remote sensing surveying and mapping unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN214986035U true CN214986035U (en) | 2021-12-03 |
Family
ID=79087162
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121180741.4U Expired - Fee Related CN214986035U (en) | 2021-05-28 | 2021-05-28 | Damping mechanism of aerial remote sensing surveying and mapping unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN214986035U (en) |
-
2021
- 2021-05-28 CN CN202121180741.4U patent/CN214986035U/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 |
Granted publication date: 20211203 |