CN213899723U - Unmanned aerial vehicle support damping device for aerial survey remote sensing - Google Patents
Unmanned aerial vehicle support damping device for aerial survey remote sensing Download PDFInfo
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- CN213899723U CN213899723U CN202022729627.4U CN202022729627U CN213899723U CN 213899723 U CN213899723 U CN 213899723U CN 202022729627 U CN202022729627 U CN 202022729627U CN 213899723 U CN213899723 U CN 213899723U
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- fixedly connected
- damping device
- aerial vehicle
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- remote sensing
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- 238000013016 damping Methods 0.000 title claims abstract description 40
- 230000035939 shock Effects 0.000 claims abstract description 10
- 239000007787 solid Substances 0.000 claims description 8
- 238000010521 absorption reaction Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 4
- 230000002349 favourable effect Effects 0.000 abstract description 4
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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Abstract
The utility model discloses an unmanned aerial vehicle support damping device for aerial survey remote sensing, the camera includes a supporting plate, the equal fixedly connected with carriage in four corners department of backup pad lower surface, the inside wall of carriage has the slide through spout swing joint. This unmanned aerial vehicle support damping device for aerial survey remote sensing, pass through the backup pad, the carriage, the slide, a supporting plate, the setting of slider and shock attenuation pole isotructure, when unmanned aerial vehicle descending takes place vibrations, the carriage slides in the casing and makes the second spring produce deformation, thereby can once slow down vibrations, and use through damping device's cooperation, holistic stability when having improved the device again and using, and simultaneously, the connecting plate drives the shock attenuation pole and removes, make the slider slide and drive reset spring and produce deformation on the bracing piece, and then can carry out the secondary to vibrations and slow down, then the effectual shock attenuation effect that improves the device, be favorable to the protection of unmanned aerial vehicle electrical components, the practicality of the device has been strengthened.
Description
Technical Field
The utility model relates to an unmanned air vehicle technique field specifically is an unmanned aerial vehicle support damping device for aerial survey remote sensing.
Background
Unmanned aircraft, abbreviated as "drone" in short, and abbreviated as "UAV" in english, is an unmanned aircraft operated by means of a radio remote control device and a self-contained program control device, or autonomously operated by an on-board computer, completely or intermittently.
Often involve unmanned aerial vehicle in aerial survey remote sensing field, unmanned aerial vehicle commonly used produces great vibrations around rising and falling easily, causes the damage of the inside components and parts of unmanned aerial vehicle easily, provides an unmanned aerial vehicle support damping device for aerial survey remote sensing for this.
SUMMERY OF THE UTILITY MODEL
Technical problem to be solved
Not enough to prior art, the utility model provides an unmanned aerial vehicle support damping device for aerial survey remote sensing has solved the problem that proposes in the above-mentioned background art.
(II) technical scheme
In order to achieve the above purpose, the utility model discloses a following technical scheme realizes: the utility model provides an unmanned aerial vehicle support damping device for aerial survey remote sensing, includes the backup pad, the equal fixedly connected with carriage in four corners department of backup pad lower surface, the inside wall of carriage has the slide through spout swing joint, the lower surface of slide has the bracing piece through recess fixedly connected with, the surface swing joint of bracing piece has the slider, the lower surface of slider has the shock attenuation pole through pivot swing joint, the one end of shock attenuation pole has the connecting plate through pivot swing joint, the lower fixed surface of connecting plate is connected with the support frame, the both sides of support frame all have damping device through pivot swing joint, the surface of support frame has the casing through spout swing joint, the lower fixed surface of casing is connected with the bottom plate.
Optionally, the equal fixedly connected with supporting leg in both sides of bottom plate lower surface, the equal fixedly connected with in four corners department of backup pad upper surface is solid fixed ring, gu fixed ring's surperficial threaded connection has the bolt.
Optionally, the upper surface of the sliding plate is fixedly connected with a first spring, and one end of the first spring is fixedly connected to the inner top wall of the supporting frame.
Optionally, a reset spring is sleeved on the surface of the supporting rod, and two ends of the reset spring are fixedly connected to one side of the sliding block.
Optionally, the lower surface of the support frame is fixedly connected with a second spring, and one end of the second spring is fixedly connected to the inner bottom wall of the casing.
Optionally, the damping device comprises a movable plate, sleeves are movably connected to two sides of the movable plate through sliding grooves, damping springs are fixedly connected to the inner portions of the sleeves, and one ends of the damping springs are fixedly connected to the surface of the movable plate.
(III) advantageous effects
The utility model provides an unmanned aerial vehicle support damping device for aerial survey remote sensing possesses following beneficial effect:
1. this unmanned aerial vehicle support damping device for aerial survey remote sensing, pass through the backup pad, the carriage, the slide, a supporting plate, the setting of slider and shock attenuation pole isotructure, when unmanned aerial vehicle descending takes place vibrations, the carriage slides in the casing and makes the second spring produce deformation, thereby can once slow down vibrations, and use through damping device's cooperation, holistic stability when having improved the device again and using, and simultaneously, the connecting plate drives the shock attenuation pole and removes, make the slider slide and drive reset spring and produce deformation on the bracing piece, and then can carry out the secondary to vibrations and slow down, then the effectual shock attenuation effect that improves the device, be favorable to the protection of unmanned aerial vehicle electrical components, the practicality of the device has been strengthened.
2. This unmanned aerial vehicle support damping device for aerial survey remote sensing through the setting of backup pad, solid fixed ring, first spring and slide isotructure, has both been favorable to the device shock attenuation back slide in time to reset, simultaneously, has made things convenient for the device's installation fixed again, the staff's of being convenient for use.
Drawings
FIG. 1 is a schematic structural view of the present invention;
FIG. 2 is a schematic sectional view of the present invention;
FIG. 3 is an enlarged schematic view of the structure at A in FIG. 2 according to the present invention;
fig. 4 is an enlarged schematic structural diagram of the point B in fig. 2 according to the present invention.
In the figure: 1. a support plate; 2. a support frame; 3. a slide plate; 4. a support bar; 5. a slider; 6. a shock-absorbing lever; 7. a connecting plate; 8. a support frame; 9. a damping device; 901. a movable plate; 902. a sleeve; 903. a damping spring; 10. a housing; 11. a base plate; 12. a fixing ring; 13. a first spring; 14. a return spring; 15. a second spring.
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.
Referring to fig. 1 to 4, the present invention provides a technical solution: an unmanned aerial vehicle support damping device for aerial survey remote sensing comprises a supporting plate 1, wherein supporting frames 2 are fixedly connected at four corners of the lower surface of the supporting plate 1, the inner side wall of each supporting frame 2 is movably connected with a sliding plate 3 through a sliding chute, the upper surface of each sliding plate 3 is fixedly connected with a first spring 13, one end of each first spring 13 is fixedly connected to the inner top wall of each supporting frame 2, when an unmanned aerial vehicle contacts the ground to generate a rotating ring 3 which slides in each supporting frame 2, each first spring 13 can slow down vibration and is beneficial to resetting of each sliding plate 3, the lower surface of each sliding plate 3 is fixedly connected with a supporting rod 4 through a groove, a reset spring 14 is sleeved on the surface of each supporting rod 4, two ends of each reset spring 14 are fixedly connected to one side of a sliding block 5, the surface of each supporting rod 4 is movably connected with a sliding block 5, the lower surface of each sliding block 5 is movably connected with a damping rod 6 through a rotating shaft, one end of each damping rod 6 is movably connected with a connecting plate 7 through a rotating shaft, the lower surface of the connecting plate 7 is fixedly connected with a supporting frame 8, the lower surface of the supporting frame 8 is fixedly connected with a second spring 15, one end of the second spring 15 is fixedly connected to the inner bottom wall of the shell 10, both sides of the supporting frame 8 are movably connected with a damping device 9 through a rotating shaft, the damping device 9 comprises a movable plate 901, both sides of the movable plate 901 are movably connected with sleeves 902 through sliding grooves, damping springs 903 are fixedly connected inside the two sleeves 902, one end of each damping spring 903 is fixedly connected to the surface of the movable plate 901, one side of one sleeve 902 is movably connected to the upper surface of the bottom plate 11 through the rotating shaft, the other sleeve 902 is movably connected to the surface of the supporting frame 8 through the rotating shaft, the surface of the supporting frame 8 is movably connected with the shell 10 through the sliding grooves, when the unmanned aerial vehicle falls to contact the ground and vibrates the supporting frame 8 and slides in the shell 10, the movable plate 901 and the sleeves 902 slide oppositely or deform the damping springs 903, the existing slowing down that does benefit to vibrations, the stability when being favorable to improving the device simultaneously again when using, the lower fixed surface of casing 10 is connected with bottom plate 11, the equal fixedly connected with supporting leg in both sides of bottom plate 11 lower surface, the solid fixed ring 12 of the equal fixedly connected with in four corners department of the 1 upper surface in backup pad, the surperficial threaded connection of solid fixed ring 12 has the bolt, with solid fixed ring 12 joint on unmanned aerial vehicle, thereby the rotation bolt can be connected the device with unmanned aerial vehicle fixedly.
The detailed description of the known functions and the known components is omitted in the embodiment of the disclosure, and in order to ensure the compatibility of the equipment, the adopted operation means are consistent with the parameters of the instruments on the market.
In conclusion, the operation steps of the unmanned aerial vehicle support damping device for aerial survey remote sensing are as follows;
1. during the use, the user rotates the below that the bolt will fix solid fixed ring 12 in unmanned aerial vehicle, when the descending of unmanned aerial vehicle takes place vibrations, support frame 8 slides in casing 10 and makes second spring 15 produce deformation, thereby can once slow down vibrations, and at the in-process that support frame 8 removed, use through damping device 9's cooperation, holistic stability when having improved the device again and using, and simultaneously, when descending contact ground, connecting plate 7 drives shock-absorbing rod 6 and removes, make slider 5 slide and drive reset spring 14 and produce deformation on bracing piece 4, and then can carry out the secondary to vibrations and slow down.
The above description is only a preferred embodiment of the present invention, but the scope of protection of the present invention is not limited thereto, and any person skilled in the art should be covered by the scope of protection of the present invention, and equivalent alternatives or modifications according to the technical solution of the present invention and the concept thereof, wherein the standard parts used can be purchased from the market, and can be customized according to the description of the specification and the drawings, the specific connection manner of each part adopts the conventional means of bolt, rivet, welding, etc. developed in the prior art, the machinery, parts and equipment all adopt the conventional models in the prior art, and the parts known to those skilled in the art, the structure and principle thereof can be known to the person skilled in the art through technical manuals or through conventional experimental methods in the description of the present invention, the terms "connect", "mount", "fix", "set" and the like are used in a broad sense, for example, the term "connect" may be a fixed connection or an indirect connection through intermediate components without affecting the relationship and technical effects of the components, or may be an integral connection or a partial connection, and as in this case, for a person skilled in the art, the specific meaning of the above terms in the present invention or the present invention can be understood according to specific situations.
Claims (6)
1. The utility model provides an unmanned aerial vehicle support damping device for aerial survey remote sensing, includes backup pad (1), its characterized in that: the four corners of the lower surface of the supporting plate (1) are fixedly connected with supporting frames (2), the inner side wall of the supporting frame (2) is movably connected with a sliding plate (3) through a sliding chute, the lower surface of the sliding plate (3) is fixedly connected with a supporting rod (4) through a groove, the surface of the supporting rod (4) is movably connected with a sliding block (5), the lower surface of the sliding block (5) is movably connected with a damping rod (6) through a rotating shaft, one end of the shock absorption rod (6) is movably connected with a connecting plate (7) through a rotating shaft, the lower surface of the connecting plate (7) is fixedly connected with a supporting frame (8), both sides of the supporting frame (8) are movably connected with a damping device (9) through a rotating shaft, the surface of the support frame (8) is movably connected with a shell (10) through a sliding groove, and the lower surface of the shell (10) is fixedly connected with a bottom plate (11).
2. The unmanned aerial vehicle support damping device for aerial survey remote sensing of claim 1, characterized in that: the equal fixedly connected with supporting legs in both sides of bottom plate (11) lower surface, the solid fixed ring of the equal fixedly connected with in four corners department of backup pad (1) upper surface (12), the surperficial threaded connection of solid fixed ring (12) has the bolt.
3. The unmanned aerial vehicle support damping device for aerial survey remote sensing of claim 1, characterized in that: the upper surface of slide (3) is fixedly connected with first spring (13), the one end fixed connection of first spring (13) is in the interior roof of carriage (2).
4. The unmanned aerial vehicle support damping device for aerial survey remote sensing of claim 1, characterized in that: the surface of the supporting rod (4) is sleeved with a return spring (14), and two ends of the return spring (14) are fixedly connected to one side of the sliding block (5).
5. The unmanned aerial vehicle support damping device for aerial survey remote sensing of claim 1, characterized in that: the lower surface of support frame (8) is fixedly connected with second spring (15), the one end fixed connection of second spring (15) is in the interior diapire of casing (10).
6. The unmanned aerial vehicle support damping device for aerial survey remote sensing of claim 1, characterized in that: the damping device (9) comprises a movable plate (901), sleeves (902) are movably connected to two sides of the movable plate (901) through sliding grooves, damping springs (903) are fixedly connected to the inner portions of the sleeves (902), and one ends of the damping springs (903) are fixedly connected to the surface of the movable plate (901).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022729627.4U CN213899723U (en) | 2020-11-23 | 2020-11-23 | Unmanned aerial vehicle support damping device for aerial survey remote sensing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202022729627.4U CN213899723U (en) | 2020-11-23 | 2020-11-23 | Unmanned aerial vehicle support damping device for aerial survey remote sensing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN213899723U true CN213899723U (en) | 2021-08-06 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202022729627.4U Expired - Fee Related CN213899723U (en) | 2020-11-23 | 2020-11-23 | Unmanned aerial vehicle support damping device for aerial survey remote sensing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN213899723U (en) |
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2020
- 2020-11-23 CN CN202022729627.4U patent/CN213899723U/en not_active Expired - Fee Related
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20210806 |