CN216360019U - Landing buffering support for unmanned aerial vehicle - Google Patents
Landing buffering support for unmanned aerial vehicle Download PDFInfo
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- CN216360019U CN216360019U CN202122758844.0U CN202122758844U CN216360019U CN 216360019 U CN216360019 U CN 216360019U CN 202122758844 U CN202122758844 U CN 202122758844U CN 216360019 U CN216360019 U CN 216360019U
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- unmanned aerial
- support
- fixedly connected
- main body
- electric
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- 230000003139 buffering effect Effects 0.000 title claims description 9
- 238000013016 damping Methods 0.000 claims description 18
- 230000001681 protective effect Effects 0.000 claims description 12
- 239000000853 adhesive Substances 0.000 claims description 5
- 230000001070 adhesive effect Effects 0.000 claims description 5
- 238000003466 welding Methods 0.000 claims 1
- 230000000694 effects Effects 0.000 abstract description 5
- 230000017525 heat dissipation Effects 0.000 description 9
- 230000035939 shock Effects 0.000 description 3
- 238000010521 absorption reaction Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000033228 biological regulation Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 235000012054 meals Nutrition 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model belongs to the field of unmanned aerial vehicles, and particularly relates to a landing buffer support for an unmanned aerial vehicle, which comprises a main body and a support mechanism, wherein the support mechanism comprises a base, and an electric lifting sleeve rod is fixedly connected to the surface below the base; through the base, the electric lift loop bar, electric rotating shaft, the landing leg, cooperation between protection piece and the rubber pad lets the whole of support adjust and accomodate better, it is too fast to have solved the support that probably appears when using, and accomodate inconveniently, thereby make the support use inconvenient, thereby the availability factor of support has been influenced, the problem of result of use has been reduced, during the use, the electric lift loop bar can be adjusted the lift of landing leg, and protection piece and rubber pad can be when unmanned aerial vehicle falls to the ground, play protection and descending stable effect to the landing leg, electric rotating shaft can be when unmanned aerial vehicle collects up simultaneously, outwards rotate the landing leg, reach the effect of accomodating the volume in the reduction, thereby better guarantee has been improved for this landing leg.
Description
Technical Field
The utility model relates to the field of unmanned aerial vehicles, in particular to a landing buffering support for an unmanned aerial vehicle.
Background
At present, because unmanned aerial vehicle can realize the quick acquisition of geographic information, and efficient, with low costs, data are accurate, and the flexible operation can satisfy the different demands of survey and drawing trade, obtains wide application in the survey and drawing field. When the unmanned aerial vehicle descends, the function of realizing buffering by using descending support is needed.
The descending buffering support for the existing unmanned aerial vehicle can not adjust and store the support better in the using process, the support is too rigid possibly, and the storage is inconvenient, so that the phenomenon of poor using effect is caused, the using efficiency of the support is reduced when the landing buffering support is used, and the damage to the unmanned aerial vehicle is possibly caused.
SUMMERY OF THE UTILITY MODEL
In order to make up the defects of the prior art, the utility model provides a landing buffer bracket for an unmanned aerial vehicle.
The technical scheme adopted by the utility model for solving the technical problems is as follows: the landing buffer support for the unmanned aerial vehicle comprises a main body and a supporting mechanism, wherein the supporting mechanism comprises a base, an electric lifting sleeve rod is fixedly connected to the surface below the base, and an electric rotating shaft is fixedly connected to the side face of one end of the electric lifting sleeve rod;
one side of the electric rotating shaft is movably connected with a supporting leg, a protective sheet is fixedly connected below the supporting leg, and a rubber pad is bonded on the surface below the protective sheet.
Preferably, the landing leg passes through to constitute elevation structure between electric lift loop bar and the base, and electric lift loop bar is parallel distribution in the below of main part, elevation structure can be better ensure the connection regulation nature between landing leg and the base.
Preferably, the landing leg passes through to constitute swing joint between electric rotating shaft and the electric lift loop bar, and the size of electric rotating shaft is less than the size of landing leg, and swing joint can be better the guarantee landing leg and the connection mobility between the electric lift loop bar.
Preferably, an integrated structure is formed between the protection sheet and the supporting legs, the outer side radius of the supporting legs is smaller than that of the protection sheet, and the integrated structure can better guarantee the connection strength between the protection sheet and the supporting legs.
Preferably, an adhesive structure is formed between the rubber pad and the protective sheet, the upper surface of the rubber pad is attached to the lower surface of the protective sheet, and the adhesive structure can better guarantee the convenience of connection between the rubber pad and the protective sheet.
Preferably, the below fixed surface of main part is connected with damper, and damper includes the bottom plate, and the below fixed surface of bottom plate is connected with the connecting block, and the below fixedly connected with damping spring of connecting block, and damping spring passes through to constitute welded connection between connecting block and the bottom plate, and damping spring's size is less than the bottom plate size, and welded connection can be better ensure the joint strength between damping spring and the bottom plate.
Preferably, the below fixedly connected with fixing bolt of main part, and one side swing joint of fixing bolt has the gasket, and fixing bolt passes through to constitute swing joint between gasket and the main part, and fixing bolt is parallel distribution on the below surface of main part, swing joint can be better guarantee the stability of being connected between fixing bolt and the main part.
Preferably, the thermovent has been seted up on the surface of main part, and the inside swing joint of thermovent has the radiator-grid, and the fixed frame of outside fixedly connected with of radiator-grid, and the radiator-grid constitutes swing joint through between fixed frame and the thermovent, and coincides mutually between the axis of radiator-grid and the axis of thermovent, swing joint can be better guarantee the convenience is dismantled in being connected between radiator-grid and the thermovent.
The utility model has the advantages that:
1. the support is integrally adjusted and accommodated through the matching work among the base, the electric lifting sleeve rod, the electric rotating shaft, the support legs, the protective sheets and the rubber pads, the problems that the support is too rigid when in use and inconvenient to accommodate, and the use of the support is inconvenient are solved, so that the use efficiency of the support is influenced, and the use effect is reduced are solved.
Drawings
In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the description of the embodiments or the prior art will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to these drawings without inventive exercise.
FIG. 1 is a schematic front view of the present invention;
FIG. 2 is a schematic structural diagram of the supporting mechanism of the present invention;
FIG. 3 is a schematic view of the shock absorbing mechanism of the present invention;
FIG. 4 is a schematic view of a threaded connection according to the present invention;
fig. 5 is an enlarged view of the structure at a in fig. 1 according to the present invention.
In the figure: 1. a main body; 2. a support mechanism; 201. a base; 202. an electric lifting loop bar; 203. an electric rotating shaft; 204. a support leg; 205. a protective sheet; 206. a rubber pad; 3. a damping mechanism; 301. a base plate; 302. connecting blocks; 303. a damping spring; 4. fixing the bolt; 5. a gasket; 6. a heat dissipation port; 7. a heat-dissipating web; 8. a fixing frame is provided.
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 a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
Referring to fig. 1-5, a landing buffering bracket for an unmanned aerial vehicle includes a main body 1 and a supporting mechanism 2, the supporting mechanism 2 includes a base 201, an electric lifting loop bar 202 is fixedly connected to the lower surface of the base 201, and an electric rotating shaft 203 is fixedly connected to one end side of the electric lifting loop bar 202;
one side of the electric rotating shaft 203 is movably connected with a supporting leg 204, a protecting sheet 205 is fixedly connected below the supporting leg 204, and a rubber pad 206 is bonded on the surface below the protecting sheet 205.
In this embodiment, the supporting legs 204 form a lifting structure through the electric lifting sleeve rod 202 and the base 201, and the electric lifting sleeve rods 202 are distributed in parallel below the main body 1; during operation, the lifting structure between the supporting legs 204 and the base 201 plays a role in lifting adjustment on the whole support.
In this embodiment, the supporting leg 204 is movably connected with the electric lifting sleeve rod 202 through the electric rotating shaft 203, and the size of the electric rotating shaft 203 is smaller than that of the supporting leg 204; when the folding electric lifting support is in work, the support legs 204 are movably connected with the electric lifting sleeve rod 202, and the folding and contracting volume is convenient to store when the support legs 204 are not used.
In this embodiment, the protection sheet 205 and the leg 204 form an integrated structure, and the outer radius of the leg 204 is smaller than the outer radius of the protection sheet 205; during operation, the protection performance of the bottom end of the supporting leg 204 is better guaranteed through the integrated structure between the protection sheet 205 and the supporting leg 204.
In this embodiment, an adhesive structure is formed between the rubber pad 206 and the protection sheet 205, and the upper surface of the rubber pad 206 is attached to the lower surface of the protection sheet 205; when the anti-skid device works, the friction force between the support and the ground is increased through the adhesive structure between the rubber pad 206 and the protective sheet 205, and the anti-skid effect is achieved.
In this embodiment, the damping mechanism 3 is fixedly connected to the lower surface of the main body 1, the damping mechanism 3 includes a bottom plate 301, the lower surface of the bottom plate 301 is fixedly connected to a connecting block 302, a damping spring 303 is fixedly connected to the lower part of the connecting block 302, the damping spring 303 is welded to the bottom plate 301 through the connecting block 302, and the size of the damping spring 303 is smaller than that of the bottom plate 301; during operation, the shock absorption and buffering effects are achieved on the support through the welded connection between the shock absorption spring 303 and the bottom plate 301.
In this embodiment, a fixing bolt 4 is fixedly connected to the lower portion of the main body 1, a gasket 5 is movably connected to one side of the fixing bolt 4, the fixing bolt 4 is movably connected to the main body 1 through the gasket 5, and the fixing bolts 4 are distributed in parallel on the surface of the lower portion of the main body 1; during operation, the whole installation convenience of the support is better guaranteed through the movable connection between the fixing bolt 4 and the main body 1.
In this embodiment, a heat dissipation port 6 is formed in the surface of the main body 1, a heat dissipation net 7 is movably connected inside the heat dissipation port 6, a fixing frame 8 is fixedly connected to the outer side of the heat dissipation net 7, the heat dissipation net 7 is movably connected with the heat dissipation port 6 through the fixing frame 8, and the central axis of the heat dissipation net 7 coincides with the central axis of the heat dissipation port 6; during operation, through the swing joint between radiator-grid 7 and thermovent 6, better guarantee has been obtained to the unmanned aerial vehicle thermal diffusivity that needs the installation.
The working principle is that firstly a rubber pad 206 is adhered to the lower surface of a protective sheet 205, then the protective sheet 205 is fixedly arranged on the lower surface of a supporting leg 204, then the supporting leg 204 is movably arranged on the outer side surface of one end of an electric lifting sleeve rod 202 through an electric rotating shaft 203, then a damping spring 303 is fixedly arranged on the lower surface of a main body 1 through a connecting block 302 and a bottom plate 301 in a matching way, secondly the electric lifting sleeve rod 202 is fixedly arranged on the lower surface of the damping spring 303, then a heat radiating net 7 and a meal heating fixing frame 8 are movably arranged inside a heat radiating opening 6, and finally the main body 1 is fixedly arranged with an unmanned aerial vehicle through a fixing bolt 4, wherein the model of the electric lifting sleeve rod 202 is YS-NZ100-12A, and the model of the electric rotating shaft 203 is ND-P160.
In the description herein, references to the description of "one embodiment," "an example," "a specific example" or the like are intended to mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing shows and describes the general principles, essential features, and advantages of the utility model. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the utility model as claimed.
Claims (8)
1. The utility model provides an unmanned aerial vehicle is with descending buffering support which characterized in that: the device comprises a main body (1) and a supporting mechanism (2), wherein the supporting mechanism (2) comprises a base (201), an electric lifting loop bar (202) is fixedly connected to the surface below the base (201), and an electric rotating shaft (203) is fixedly connected to one side surface of one end of the electric lifting loop bar (202);
one side of the electric rotating shaft (203) is movably connected with a supporting leg (204), a protecting sheet (205) is fixedly connected below the supporting leg (204), and a rubber pad (206) is bonded on the surface below the protecting sheet (205).
2. A landing buffer support for unmanned aerial vehicles according to claim 1, wherein: the supporting legs (204) form a lifting structure through the electric lifting sleeve rods (202) and the base (201), and the electric lifting sleeve rods (202) are distributed in parallel below the main body (1).
3. A landing buffer support for unmanned aerial vehicles according to claim 1, wherein: the supporting legs (204) are movably connected with the electric lifting sleeve rod (202) through electric rotating shafts (203), and the sizes of the electric rotating shafts (203) are smaller than those of the supporting legs (204).
4. A landing buffer support for unmanned aerial vehicles according to claim 1, wherein: the protection sheet (205) and the supporting legs (204) form an integrated structure, and the outer radius of the supporting legs (204) is smaller than that of the protection sheet (205).
5. A landing buffer support for unmanned aerial vehicles according to claim 1, wherein: an adhesive structure is formed between the rubber pad (206) and the protective sheet (205), and the upper surface of the rubber pad (206) is attached to the lower surface of the protective sheet (205).
6. A landing buffer support for unmanned aerial vehicles according to claim 1, wherein: the damping mechanism (3) is fixedly connected with the lower surface of the main body (1), the damping mechanism (3) comprises a bottom plate (301), a connecting block (302) is fixedly connected with the lower surface of the bottom plate (301), a damping spring (303) is fixedly connected with the lower surface of the connecting block (302), the damping spring (303) is connected with the bottom plate (301) in a welding mode through the connecting block (302), and the size of the damping spring (303) is smaller than that of the bottom plate (301).
7. A landing buffer support for unmanned aerial vehicles according to claim 1, wherein: the fixing device is characterized in that a fixing bolt (4) is fixedly connected to the lower portion of the main body (1), a gasket (5) is movably connected to one side of the fixing bolt (4), the fixing bolt (4) is movably connected with the main body (1) through the gasket (5), and the fixing bolt (4) is distributed in parallel on the surface of the lower portion of the main body (1).
8. A landing buffer support for unmanned aerial vehicles according to claim 1, wherein: thermovent (6) have been seted up on the surface of main part (1), and the inside swing joint of thermovent (6) has radiator-grid (7), and the fixed frame (8) of the outside fixedly connected with of radiator-grid (7), and radiator-grid (7) constitute swing joint through between fixed frame (8) and thermovent (6), and coincide mutually between the axis of radiator-grid (7) and the axis of thermovent (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122758844.0U CN216360019U (en) | 2021-11-11 | 2021-11-11 | Landing buffering support for unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202122758844.0U CN216360019U (en) | 2021-11-11 | 2021-11-11 | Landing buffering support for unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN216360019U true CN216360019U (en) | 2022-04-22 |
Family
ID=81189755
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202122758844.0U Expired - Fee Related CN216360019U (en) | 2021-11-11 | 2021-11-11 | Landing buffering support for unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN216360019U (en) |
-
2021
- 2021-11-11 CN CN202122758844.0U patent/CN216360019U/en not_active Expired - Fee Related
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20220422 |
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| CF01 | Termination of patent right due to non-payment of annual fee |