CN206218246U - Portable full landform multi-rotor unmanned aerial vehicle landing platform - Google Patents
Portable full landform multi-rotor unmanned aerial vehicle landing platform Download PDFInfo
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- CN206218246U CN206218246U CN201621273493.7U CN201621273493U CN206218246U CN 206218246 U CN206218246 U CN 206218246U CN 201621273493 U CN201621273493 U CN 201621273493U CN 206218246 U CN206218246 U CN 206218246U
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- aerial vehicle
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- rotor unmanned
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Abstract
The utility model discloses the portable full landform multi-rotor unmanned aerial vehicle landing platform of one kind, including tripod, support and table top, the tripod includes pedestal and telescopic supporting leg, the support includes multiple poles and chuck, the chuck is fixed on one end of pole, and the table top is removably mounted on chuck, and the pole other end is provided with buckle, the pedestal is provided with multiple draw-in grooves fastened with the buckle, is connected with each other by buckle and draw-in groove between the pole and pedestal.Portable full landform multi-rotor unmanned aerial vehicle landing platform of the present utility model, constituted using detachability part, assembling is simple, it is easy to carry, can be used in abrupt slope, stone riprap, the shrub complicated landform such as weedy, shorten the landing distance of multi-rotor unmanned aerial vehicle, while the airborne dust rolled when avoiding landing, withered grass, corrosive substance enter in multi-rotor unmanned aerial vehicle, extension multi-rotor unmanned aerial vehicle service life, reduces the maintenance cost of multi-rotor unmanned aerial vehicle.
Description
Technical field
The utility model is related to power industry unmanned plane landing positioner, and in particular to revolved a kind of portable full landform more
Wing unmanned plane landing platform.
Background technology
With the development of science and technology application of the multi-rotor unmanned aerial vehicle in transmission line of electricity maintenance work is more extensive, however it is high
Pressure transmission line is generally high mountain high hill or mountain region by way of region, and transmission line of electricity high mountain high hill region accounting surpasses in southern some areas
Cross 70%, unmanned plane apply at the scene in there are the following problems：
1st, current multi-rotor unmanned aerial vehicle provides power by battery more, its endurance between 15-20min, power transmission line
Approach region is generally the complicated landform such as abrupt slope, stone riprap, shrub be weedy, and most operation fields do not possess unmanned plane landing bar
Part, takes off will greatly shorten the effective operation time of unmanned plane at a distance, or even its endurance cannot meet operation development and want
Ask.
2nd, multi-rotor unmanned aerial vehicle before take-off, need to switch on power and be calibrated, self-inspection, and the process of self-inspection need to ensure equipment
Horizontal positioned, is otherwise likely to occur the phenomenons such as calibration, initialization mistake, and then triggers unmanned plane to fall machine event, but in the wild
Under the conditions of be difficult to meet the requirement of unmanned plane horizontal positioned.
3rd, airborne dust, withered grass, corrosive substance rolled during unmanned plane ground landing in the wild etc. is easily caused unmanned plane
Motor or fault, are unfavorable for the maintaining of equipment.
According to investigations, most of unmanned planes fall machine event is occurred in landing link, therefore badly natural in transmission line of electricity
Under the conditions of ensure unmanned plane landing needed for condition be particularly important.
Therefore prior art has much room for improvement and develops.
Utility model content
The purpose of this utility model is to overcome above-mentioned the deficiencies in the prior art, there is provided a kind of portable complete many rotors of landform
Unmanned plane landing platform, makes multi-rotor unmanned aerial vehicle landing operation not influenceed by orographic condition, improves operational security, to greatest extent
Improve the effective operation time of unmanned plane, reduce unmanned plane failure and spoilage.
To realize object above, the technical solution adopted in the utility model is：
A kind of portable full landform multi-rotor unmanned aerial vehicle landing platform, including tripod, support and table top, the tripod
It is accordion structure, including pedestal and telescopic supporting leg, the support includes multiple poles and chuck, and the chuck is fixed
In one end of pole, the table top is removably mounted on chuck, and the pole other end is provided with buckle, and the pedestal is provided with
Multiple draw-in grooves fastened with the buckle, are connected with each other between the pole and pedestal by buckle and draw-in groove.
The pole is circular pin, and the buckle is the bearing pin being radially arranged, and the pedestal is provided with multiple for the pole
The patchhole of insertion, the draw-in groove is the annular groove for being arranged on the patchhole inwall.
The table top includes the tablecloth and group frame, and the group frame includes multiple connecting rods, multiple connectors and extremely
A few regulating part, the edge of the tablecloth is provided with the spacing hole passed through for connecting rod, and the connecting rod is removable with the chuck
Unload connection.
The table top is square structure, and the connector is rigging-angle connector, and the regulating part is for adjusting the tablecloth
The adjusting screw of tightness.
The tripod also includes counterweight hook, and the counterweight hook is arranged on the bottom of the pedestal.
The beneficial effects of the utility model are：
1st, selectivity of the multi-rotor unmanned aerial vehicle to operating environment is reduced, shortens landing distance, increasing multi-rotor unmanned aerial vehicle has
The effect activity duration, raising machine patrols operating efficiency；
2nd, multi-rotor unmanned aerial vehicle landing operating environment is optimized, reduction is fallen machine, device damage event and occurred；
3rd, multi-rotor unmanned aerial vehicle operation landing link difficulty is reduced, shortens the training time that multi-rotor unmanned aerial vehicle flies hand；
4th, the airborne dust produced during multi-rotor unmanned aerial vehicle landing is reduced, extends multi-rotor unmanned aerial vehicle service life, reduced
The maintenance cost of multi-rotor unmanned aerial vehicle.
Brief description of the drawings
Fig. 1 is the overall structure figure of landing platform of the present utility model；
Fig. 2 is the decomposing schematic representation of landing platform of the present utility model；
Fig. 3 is the assembling schematic diagram of pedestal and support；
Fig. 4 is the decomposing schematic representation of group frame；
Fig. 5 is the assembling schematic diagram of rigging-angle connector and connecting rod；
Fig. 6 is the assembling schematic diagram of adjusting screw and connecting rod
Description of reference numerals：1- tripods；11- pedestals；111- annular grooves；12- supporting legs；13- counterweight hooks；2- supports；
21- poles；211- bearing pins；22- chucks；3- table tops；The 31- tablecloths；311- spacing holes；312- breach；32- group frames；321-
Connecting rod；322- rigging-angle connectors；323- adjusting screws.
Specific embodiment
Content of the present utility model is described in further details with reference to the accompanying drawings and detailed description.
Embodiment：
Refer to shown in Fig. 1 to Fig. 6, a kind of portable full landform multi-rotor unmanned aerial vehicle landing platform, including tripod 1,
Support 2 and table top 3.
Wherein, tripod 1 stands on ground, including pedestal 11, supporting leg 12 and counterweight hook 13.Pedestal 11 is located at tripod 1
Top, its underpart and supporting leg 12 rotate and be connected, and its top is provided with the boss being connected with support 2.Supporting leg 12 is telescopic
Structure, platform holding level under the landform of out-of-flatness can be made by adjusting supporting leg 12.Counterweight hook 13 by screw thread coordinate with
The bottom surface connection of pedestal 11, can on the spot take the weights such as stone and is suspended on counterweight hook 13, to increase platform according to actual needs
Resistance to overturning, prevents because center of gravity transfer causes platform to be toppled over when unmanned plane drops to platform edges.
Wherein, support 2 is made up of four poles of circle 21 and four chucks 22, and chuck 22 is fixed on the one of pole 21
End, the other end of pole 21 is provided with the bearing pin 211 of radial direction.Correspondingly, patchhole is provided with four sides of the boss of pedestal 11,
Annular groove 111 is provided with the bottom of patchhole, is inserted in the hole and is rotated to an angle by the way that pole 21 is inserted into, so that it may so that
Bearing pin 211 is fastened in annular groove 111, realizes the quick connection of pole 21 and pedestal 11, and its simple structure is easy for installation.
Wherein, table top 3 includes the tablecloth 31 and group frame 32, and group frame 32 includes multiple connecting rods 321, multiple connections
Part and at least one regulating part, the edge sewing limited location hole 311 of the tablecloth 31, the connecting rod 321 is located in spacing hole 311
In, breach 312 is designed with the middle part of each spacing hole 311, it is connected with connecting rod 321 for chuck 22.
In the present embodiment, connecting rod 321 is connecting rod 321A, two connecting rod 321B and a connecting rod
321C, and circular pin is, connector is two rigging-angle connectors 322, and regulating part is two adjusting screws 323.Connecting rod
321A two ends are provided with the bearing pin 211 of radial direction, and one end of connecting rod 321B is provided with the bearing pin 211 of radial direction, and the other end is provided with
Hole clipping, connecting rod 321C two ends are equipped with the screwed hole of radial direction.Two ends of rigging-angle connector 322 are equipped with and bearing pin 211
The annular groove 111 being engaged.Adjusting screw 323 has the threaded portion coordinated with screwed hole, and the insertion section coordinated with hole clipping.
The two ends of connecting rod 321A are connected with rigging-angle connector 322 respectively, and one end of connecting rod 321B is connected with rigging-angle connector 322,
Its other end is connected with connecting rod 321C by adjusting screw 323, by adjusting the screw-in distance of adjusting screw 323, makes the tablecloth
31 are in tensioned state.
Portable full landform multi-rotor unmanned aerial vehicle landing platform of the present utility model, it is overall to use detachability component structure
Into, assemble simple and convenient, can be used in abrupt slope, stone riprap, the shrub complicated landform such as weedy, thus shorten many rotors without
Man-machine landing distance, increases effective operation time, and raising machine patrols operating efficiency；The airborne dust that can avoid being rolled during landing,
Withered grass, corrosive substance enter in multi-rotor unmanned aerial vehicle, extend multi-rotor unmanned aerial vehicle service life, reduce multi-rotor unmanned aerial vehicle
Maintenance cost.
Above-listed detailed description is directed to illustrating for the utility model possible embodiments, and the embodiment is simultaneously not used to limitation
Protection domain of the present utility model, all equivalence enforcements or change without departing from carried out by the utility model are intended to be limited solely by this case
In protection domain.
Claims (5)
1. a kind of portable full landform multi-rotor unmanned aerial vehicle landing platform, it is characterised in that including tripod (1), support (2) and
Table top (3), the tripod (1) is accordion structure, including pedestal (11) and telescopic supporting leg (12), the support
(2) including multiple poles (21) and chuck (22), the chuck (22) is fixed on one end of pole (21), and the table top (3) can
Releasably be arranged on chuck (22), pole (21) other end is provided with buckle, the pedestal (11) be provided with it is multiple with it is described
The draw-in groove that buckle fastens, is connected with each other between the pole (21) and pedestal (11) by buckle and draw-in groove.
2. portable full landform multi-rotor unmanned aerial vehicle landing platform according to claim 1, it is characterised in that the pole
(21) it is circular pin, the buckle is the bearing pin (211) being radially arranged, the pedestal (11) is provided with multiple for the pole (21)
The patchhole of insertion, the draw-in groove is the annular groove (111) for being arranged on the patchhole inwall.
3. portable full landform multi-rotor unmanned aerial vehicle landing platform according to claim 1, it is characterised in that the table top
(3) including the tablecloth (31) and group frame (32), the group frame (32) includes multiple connecting rods (321), multiple connectors
With at least one regulating part, the edge of the tablecloth (31) is provided with the spacing hole (311) passed through for connecting rod (321), the company
Extension bar (321) is detachably connected with the chuck (22).
4. portable full landform multi-rotor unmanned aerial vehicle landing platform according to claim 3, it is characterised in that the table top
(3) it is square structure, the connector is rigging-angle connector (322), and the regulating part is for adjusting the tablecloth (31) rate of tension
Adjusting screw (323).
5. according to any described portable full landform multi-rotor unmanned aerial vehicle landing platforms of claim 1-4, it is characterised in that institute
Stating tripod (1) also includes counterweight hook (13), and the counterweight hook (13) is arranged on the bottom of the pedestal (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621273493.7U CN206218246U (en) | 2016-11-25 | 2016-11-25 | Portable full landform multi-rotor unmanned aerial vehicle landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621273493.7U CN206218246U (en) | 2016-11-25 | 2016-11-25 | Portable full landform multi-rotor unmanned aerial vehicle landing platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206218246U true CN206218246U (en) | 2017-06-06 |
Family
ID=58785753
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621273493.7U Active CN206218246U (en) | 2016-11-25 | 2016-11-25 | Portable full landform multi-rotor unmanned aerial vehicle landing platform |
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| CN (1) | CN206218246U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108238275A (en) * | 2018-02-10 | 2018-07-03 | 清远韶兴新能源科技有限公司 | A kind of unmanned plane lifting gear |
| CN109229407A (en) * | 2018-08-24 | 2019-01-18 | 国家电网有限公司 | Portable unmanned machine hoistable platform |
| CN110254735A (en) * | 2019-05-07 | 2019-09-20 | 国网吉林省电力有限公司长春供电公司 | The full landform self-balancing landing platform of multi-rotor unmanned aerial vehicle |
| CN112722309A (en) * | 2021-02-25 | 2021-04-30 | 刘晓梅 | Agricultural unmanned aerial vehicle carries on platform |
| CN112722309B (en) * | 2021-02-25 | 2024-05-31 | 源沅(深圳)技术转移有限责任公司 | Agricultural unmanned aerial vehicle carries on platform |
-
2016
- 2016-11-25 CN CN201621273493.7U patent/CN206218246U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108238275A (en) * | 2018-02-10 | 2018-07-03 | 清远韶兴新能源科技有限公司 | A kind of unmanned plane lifting gear |
| CN109229407A (en) * | 2018-08-24 | 2019-01-18 | 国家电网有限公司 | Portable unmanned machine hoistable platform |
| CN110254735A (en) * | 2019-05-07 | 2019-09-20 | 国网吉林省电力有限公司长春供电公司 | The full landform self-balancing landing platform of multi-rotor unmanned aerial vehicle |
| CN112722309A (en) * | 2021-02-25 | 2021-04-30 | 刘晓梅 | Agricultural unmanned aerial vehicle carries on platform |
| CN112722309B (en) * | 2021-02-25 | 2024-05-31 | 源沅(深圳)技术转移有限责任公司 | Agricultural unmanned aerial vehicle carries on platform |
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