CN207791138U - A kind of unmanned plane landing platform - Google Patents
A kind of unmanned plane landing platform Download PDFInfo
- Publication number
- CN207791138U CN207791138U CN201820045725.6U CN201820045725U CN207791138U CN 207791138 U CN207791138 U CN 207791138U CN 201820045725 U CN201820045725 U CN 201820045725U CN 207791138 U CN207791138 U CN 207791138U
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- CN
- China
- Prior art keywords
- bottom end
- unmanned plane
- drone body
- right sides
- middle position
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Abstract
It is disclosed by the utility model to belong to air vehicle technique field,Specially a kind of unmanned plane landing platform,The middle position on the drone body top is provided with wireless transmitter,It is both provided with mounting base at left and right sides of the drone body bottom end,The left and right sides of the mounting base is connected by fixing bolt with drone body,The middle position of the mounting base bottom end is welded with arc bracket,Middle position below the drone body is provided with blower device,By the way that arc bracket is arranged,So that it is more uniformly stressed,Good supporting role is played during landing,By the way that blower device is arranged,It is obliquely installed discharge pipe,Wind direction outer ring dissipates,So that unmanned plane is not easy to shake in landing,Improve stability when its landing,By the way that elastic shock attenuation block and damping spring is arranged,Effectively reduce vibrations of the unmanned plane in landing,Effectively reduce the damage to ontology and equipment.
Description
Technical field
The utility model is related to air vehicle technique field, specially a kind of unmanned plane landing platform.
Background technology
Unmanned plane be by radio robot or airborne computer tele-control system manipulated it is not manned fly
Row device, nowadays more and more people like carrying out high-altitude with unmanned plane taking photo by plane, the picture and image taken, currently, mostly
Unmanned plane landing when due to inertia active force so that the stability of unmanned plane and safety are low, and landing when can produce
Raw violent vibrations, can lead to the damage of ontology and its equipment, for this purpose, it is proposed that a kind of unmanned plane landing platform.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane landing platforms, to solve to propose in above-mentioned background technology
Before, most unmanned plane is in landing due to the active force of inertia so that the stability of unmanned plane and safety are low, and are dropping
The problem of will produce violent vibrations when falling, the damage of ontology and its equipment can be caused.
To achieve the above object, the utility model provides the following technical solutions：A kind of unmanned plane landing platform, including nothing
The middle position of man-machine ontology, the drone body top is provided with wireless transmitter, the drone body bottom end
The left and right sides is both provided with mounting base, and the left and right sides of the mounting base is connected by fixing bolt with drone body,
The middle position of the mounting base bottom end is welded with arc bracket, and the middle position below the drone body is provided with air blast
The left and right sides of device, the blower device top is welded with supporting leg, and the top of the supporting leg is connected to drone body
The air outlet of bottom end, the blower device bottom end is equipped with wind-collecting cover, and the outer ring of the wind-collecting cover bottom end is evenly arranged with outlet air
Pipe, the bottom end of the arc bracket are equipped with trapezoidal connecting plate, and the bottom end of the trapezoidal connecting plate is provided with upper backup pad, described
It is provided with lower supporting plate below upper backup pad, motion bar, the work are both provided at left and right sides of the upper backup pad bottom end
The bottom end of lever is socketed with sleeve, and the bottom end of sleeve is mounted on the top of lower supporting plate, the upper backup pad and lower supporting plate
Between middle position be provided with elastic shock attenuation block, be both provided with damping spring at left and right sides of the elastic shock attenuation block, it is described
The top and bottom end of damping spring are respectively supported at the bottom end of upper backup pad and the top of lower supporting plate.
Preferably, the discharge pipe is obliquely installed to far from the side at wind-collecting cover center.
Preferably, the bottom end of the outlet air tube cavity is provided with strainer.
Preferably, the bottom end of the motion bar is provided with limited block.
Compared with prior art, the utility model has the beneficial effects that：The utility model proposes a kind of unmanned planes with falling
Ground platform, by the way that arc bracket is arranged so that it is more uniformly stressed, and good supporting role is played during landing,
By the way that blower device is arranged, it is obliquely installed discharge pipe, the diverging of wind direction outer ring so that unmanned plane is not easy to shake in landing, improves
Stability when it is landed, the utility model is reasonable for structure, easy to use, by the way that elastic shock attenuation block and damping spring is arranged, has
Effect reduces vibrations of the unmanned plane in landing, effectively reduces the damage to ontology and equipment.
Description of the drawings
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the portions the utility model A enlarged drawing.
In figure：1 drone body, 2 wireless transmitters, 3 mounting bases, 4 fixing bolts, 5 arc brackets, 6 supporting legs, 7 drums
Wind apparatus, 8 wind-collecting covers, 9 discharge pipes, 10 trapezoidal connecting plates, 11 upper backup pads, 12 lower supporting plates, 13 universal wheels, 14 motion bars,
15 fixed links, 16 elastic shock attenuation blocks, 17 damping springs.
Specific implementation mode
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
The every other embodiment obtained, shall fall within the protection scope of the present invention.
- 2 are please referred to Fig.1, the utility model provides a kind of technical solution：A kind of unmanned plane landing platform, including nobody
The middle position of machine ontology 1,1 top of the drone body is provided with wireless transmitter 2,1 bottom end of the drone body
The left and right sides be both provided with mounting base 3, the left and right sides of the mounting base 3 passes through fixing bolt 4 and 1 phase of drone body
The middle position of connection, 3 bottom end of the mounting base is welded with arc bracket 5, and the middle position of 1 lower section of the drone body is set
It is equipped with blower device 7, the left and right sides on 7 top of the blower device is welded with supporting leg 6, and the top of the supporting leg 6 is connected to
The bottom end of drone body 1, the air outlet of 7 bottom end of the blower device are equipped with wind-collecting cover 8,8 bottom end of the wind-collecting cover it is outer
Circle is evenly arranged with discharge pipe 9, and the bottom end of the arc bracket 5 is equipped with trapezoidal connecting plate 10, the trapezoidal connecting plate 10
Bottom end is provided with upper backup pad 11, and the lower section of the upper backup pad 11 is provided with lower supporting plate 12,11 bottom end of the upper backup pad
The left and right sides be both provided with motion bar 14, the bottom end of the motion bar 14 is socketed with sleeve 15, and the bottom end installation of sleeve 15
Middle position between the top of lower supporting plate 12, the upper backup pad 11 and lower supporting plate 12 is provided with elastic shock attenuation block
16, the left and right sides of the elastic shock attenuation block 16 is both provided with damping spring 17, the top and bottom end point of the damping spring 17
It is not supported on the top of the bottom end and lower supporting plate 12 of upper backup pad 11.
Wherein, the discharge pipe 9 is obliquely installed to far from the side at 8 center of wind-collecting cover so that wind direction periphery is blown out, institute
The bottom end for stating 9 inner cavity of discharge pipe is provided with strainer, effectively prevent sundries to enter the inner cavity of discharge pipe 9, the bottom of the motion bar 14
End is provided with limited block.
Operation principle：Before work, mounting base 3 is fixed on to the bottom end of drone body 1 by fixing bolt 4, installed
The bottom end of seat 3 is welded with arc bracket 5 so that it is more uniformly stressed, during unmanned plane lands so that arc bracket
5 are not easily broken when by impact force, play good support effect, and letter is received and transmitted by wireless transmitter 2
Number remote control is carried out, blower device 7 is connected to by supporting leg 6 in drone body 1, when unmanned plane lands soon close to ground
When, blower device 7 is opened, wind aggregation in wind-collecting cover 8 is dissipated by discharge pipe 9, by being obliquely installed discharge pipe 9,
So that the diverging of wind direction outer ring so that it is not easy to shake, and effectively improves stability of the drone body 1 in landing, after landing,
Pass through and universal wheel 13 be set so that unmanned plane slides forward according to inertia, by be arranged upper backup pad 11 and lower supporting plate 12 into
Row support, by be arranged elastic shock attenuation block 16, effectively improve buffering effect when landing, to mitigate unmanned plane landing when
Vibrations further mitigate vibrations when its landing, by the way that motion bar 14 and fixed link is arranged by the way that two groups of damping springs 17 are arranged
15 so that during landing, motion bar 14 moves up and down in the inner cavity of fixed link 15 for it, and the utility model structure is closed
Reason, it is easy to use.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is appreciated that can these embodiments be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaiied
Change, replace and modification, the scope of the utility model are defined by the appended claims and the equivalents thereof.
Claims (4)
1. a kind of unmanned plane landing platform, including drone body (1), it is characterised in that：Drone body (1) top
Middle position be provided with wireless transmitter (2), be both provided with mounting base at left and right sides of drone body (1) bottom end
(3), the left and right sides of the mounting base (3) is connected by fixing bolt (4) with drone body (1), the mounting base
(3) middle position of bottom end is welded with arc bracket (5), and the middle position below the drone body (1) is provided with air blast
The left and right sides of device (7), blower device (7) top is welded with supporting leg (6), and the top of the supporting leg (6) is connected to
The air outlet of the bottom end of drone body (1), blower device (7) bottom end is equipped with wind-collecting cover (8), the wind-collecting cover (8)
The outer ring of bottom end is evenly arranged with discharge pipe (9), and the bottom end of the arc bracket (5) is equipped with trapezoidal connecting plate (10), described
The bottom end of trapezoidal connecting plate (10) is provided with upper backup pad (11), and lower supporting plate is provided with below the upper backup pad (11)
(12), motion bar (14), the bottom end set of the motion bar (14) are both provided at left and right sides of upper backup pad (11) bottom end
It is connected to sleeve (15), and the bottom end of sleeve (15) is mounted on the top of lower supporting plate (12), the upper backup pad (11) and lower branch
Middle position between fagging (12) is provided with elastic shock attenuation block (16), is respectively provided at left and right sides of the elastic shock attenuation block (16)
There are damping spring (17), the top and bottom end of the damping spring (17) to be respectively supported at the bottom end of upper backup pad (11) and lower branch
The top of fagging (12).
2. a kind of unmanned plane according to claim 1 landing platform, it is characterised in that：The discharge pipe (9) is to separate
Side at wind-collecting cover (8) center is obliquely installed.
3. a kind of unmanned plane according to claim 1 landing platform, it is characterised in that：Discharge pipe (9) inner cavity
Bottom end is provided with strainer.
4. a kind of unmanned plane according to claim 1 landing platform, it is characterised in that：The bottom end of the motion bar (14)
It is provided with limited block.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820045725.6U CN207791138U (en) | 2018-01-11 | 2018-01-11 | A kind of unmanned plane landing platform |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820045725.6U CN207791138U (en) | 2018-01-11 | 2018-01-11 | A kind of unmanned plane landing platform |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207791138U true CN207791138U (en) | 2018-08-31 |
Family
ID=63271405
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820045725.6U Expired - Fee Related CN207791138U (en) | 2018-01-11 | 2018-01-11 | A kind of unmanned plane landing platform |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207791138U (en) |
-
2018
- 2018-01-11 CN CN201820045725.6U patent/CN207791138U/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: 20180831 Termination date: 20190111 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |