CN208344542U - For surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane - Google Patents
For surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane Download PDFInfo
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- CN208344542U CN208344542U CN201820913314.4U CN201820913314U CN208344542U CN 208344542 U CN208344542 U CN 208344542U CN 201820913314 U CN201820913314 U CN 201820913314U CN 208344542 U CN208344542 U CN 208344542U
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Abstract
The utility model provides the two sided Anti-bumping protection mechanism for surveying and drawing unmanned plane, including side guard plate, interior nut head and nut；Two U-shaped folder backplate inner ends are oppositely arranged, and are pressed from both sides both ends on the side wall of backplate outer end and be symmetrically arranged two aviation aluminium support columns；The outer end of the aviation aluminium support column is respectively fixedly connected on side guard plate medial surface；It is respectively provided at the top and bottom of the folder backplate there are two the tight jam plate, and is respectively provided on tight jam plate there are two symmetrical clamping screw and is fixed together two tight jam plates by the nut that end thread connects.The setting of the utility model side guard plate, it is the arc plate structure of semicircle shape by side guard plate, the setting of arc plate structure can provide safety coefficient higher Anticollision Measures for unmanned plane two sides, it can especially ensure the safety of data box to greatest extent after encountering shock, on the other hand, the setting of curved plate-like structure can reduce windage, and the influence to unmanned plane during flying is reduced in utmostly range.
Description
Technical field
The utility model belongs to mapping unmanned plane, protection technical field of structures, and more particularly, to mapping unmanned plane is double
Side Anti-bumping protection mechanism.
Background technique
Unmanned plane take photo by plane, rescue, forest fire protection, security protection, many fields such as mapping are widely used, especially exist
When mapping, unmanned plane needs topography by various complexity and precipitous gully and jungle, and unmanned plane is hit because of itself and justice
The case where business shock damage, is more, and use cost is caused to increase.
Based on above-mentioned, the inventors discovered that, the rack installed on unmanned plane generally without installing damping anticollision device, collision-prevention device additional, therefore
Unmanned plane landing or aerial catastrophic failure and when falling, rack cannot rush with buffering well in face of the shock of unmanned aerial vehicle body
It hits, causes unmanned plane damage serious, and the unmanned plane that usually frequently lands, can fuselage be made by droping to ground every time in addition
At certain shock, therefore, traditional unmanned plane service life is generally shorter, and the maintenance period is shorter, and use cost is long
Phase is high, and on the other hand, in flight, for foreign matter high in the air to the shock of unmanned plane, damage is larger, can not only make nothing
Man-machine crash and the integrality for being more difficult to ensure surveying and mapping data, directly increase dual cost.
Then, it in view of this, being studied improvement for existing structure and missing, provides for surveying and drawing the double of unmanned plane
Side Anti-bumping protection mechanism, to achieve the purpose that with more more practical value.
Utility model content
In order to solve the above-mentioned technical problem, the utility model provides the two sided Anti-bumping protection machine for surveying and drawing unmanned plane
Structure awing lacks the anti-collision protection structure of two sided and lacks protection to surveying and mapping data collecting cassette to solve existing unmanned plane
The problem of.
The utility model is used to survey and draw the purpose and effect of the two sided Anti-bumping protection mechanism of unmanned plane, by skill in detail below
Art means are reached:
For surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane, including side guard plate, backplate is pressed from both sides, tight jam plate, clamping screw,
Aviation aluminium support column, damping, buffering spring break aerofoil, lighten the burden hole, buffer layer, interior nut head and nut；Two U-shaped folders
Backplate inner end is oppositely arranged, and is pressed from both sides both ends on the side wall of backplate outer end and be symmetrically arranged two aviation aluminium support columns；The boat
The outer end of empty aluminium support column is respectively fixedly connected on side guard plate medial surface；There are two being respectively provided at the top and bottom of the folder backplate
The tight jam plate, and be respectively provided with two on tight jam plate there are two symmetrical clamping screw and by the nut of end thread connection
Tight jam plate is fixed together；The outer end of the clamping screw is the structure of interior nut hair style；The side guard plate and folder backplate
Between the front end portion position parallel with aviation aluminium support column at be provided with and all have 39 degree of angle inclined surface up and down
Broken aerofoil.
Further, the side guard plate is the arc plate structure of semicircle shape, and two side guard plate inner concaves are opposite, just
It can make up a complete cylinder-like structure well, and the inner concave bottom of side guard plate is provided perpendicular to the small flat of horizontal plane
Platform.
Further, the tight jam plate and folder backplate offer several transparent Reduction of Students' Study Load holes in the horizontal plane.
Further, one layer of buffer layer with several through-holes is equipped in the folder backplate upright inner side walls.
Further, the aviation aluminium support column has the cambered surface groove there are six semicircle shape, and two aviation aluminium support columns
Between be provided with damping, buffering spring with aviation aluminium support column equivalent diameter size, the special construction of aviation aluminium support column increases
Stress supporting surface.
Compared with prior art, the utility model has the following beneficial effects:
The setting of side guard plate is the arc plate structure of semicircle shape, and two side guard plate inner concave phases by side guard plate
It is right, it can make up a complete cylinder-like structure just, and the inner concave bottom of side guard plate is provided perpendicular to horizontal plane
Chain-wales, and the outer end of aviation aluminium support column is respectively fixedly connected on side guard plate medial surface, the setting energy of arc plate structure
It enough provides safety coefficient higher Anticollision Measures for unmanned plane two sides, especially can ensure number to greatest extent after encountering shock
According to the safety of box, on the other hand, the setting of curved plate-like structure can reduce windage, reduce in utmostly range to nobody
The influence of machine flight.
The setting of aviation aluminium support column, by aviation aluminium support column tool, there are six the cambered surface grooves of semicircle shape, and two are navigated
The damping, buffering spring with aviation aluminium support column equivalent diameter size, the spy of aviation aluminium support column are provided between empty aluminium support column
Different structure increases stress supporting surface, can realize stronger support force in limited quality, and damping, buffering spring can be
It can play the role of damping reset after being hit, reduce the damage to unmanned plane in maximum.
The setting of buffer layer and Reduction of Students' Study Load hole, it is slow with several through-holes by being equipped with one layer in folder backplate upright inner side walls
Rush layer, can to unmanned aerial vehicle body during clamping and flight during play the role of it is antiwear, can be to nothing
Man-machine fuselage plays the role of antiwear the clamping during and during flight, can ensure structural integrity
Meanwhile and weight bearing can be mitigated for unmanned plane.
Detailed description of the invention
Fig. 1 is the right front axis view structural schematic diagram of the utility model.
Fig. 2 is the left back square shaft view structural schematic diagram of the utility model.
Fig. 3 is the schematic view of the front view of the utility model.
Fig. 4 is the overlooking structure diagram of the utility model.
Fig. 5 is the schematic cross-sectional view of the utility model.
In figure: 1- side guard plate, 2- press from both sides backplate, the tight jam plate of 3-, 4- clamping screw, 5- aviation aluminium support column, 6- damping, buffering
Spring, 7- break aerofoil, and 8- lightens the burden hole, 9- buffer layer, nut head in 401-, 402- nut.
Specific embodiment
The utility model is described further below in conjunction with attached drawing:
Embodiment:
As shown in attached drawing 1 to attached drawing 5:
The utility model provides the two sided Anti-bumping protection mechanism for surveying and drawing unmanned plane, including side guard plate 1, presss from both sides backplate 2,
Tight jam plate 3, clamping screw 4, aviation aluminium support column 5, damping, buffering spring 6 break aerofoil 7, hole 8 of lightening the burden, buffer layer 9, interior nut
First 401 and nut 402；Two U-shaped 2 inner ends of folder backplate are oppositely arranged, and it is right respectively to press from both sides both ends on 2 outer end side wall of backplate
Title is provided with two aviation aluminium support columns 5；The outer end of the aviation aluminium support column 5 is respectively fixedly connected in 1 medial surface of side guard plate
On；It is respectively provided at the top and bottom of the folder backplate 2 there are two the tight jam plate 3, and is respectively provided with that there are two symmetrical on tight jam plate 3
Two tight jam plates 3 are simultaneously fixed together by the nut 402 that end thread connects by clamping screw 4；The clamping screw 4
Outer end be interior 401 formula of nut head structure；Front end portion and aviation aluminium support column 5 between the side guard plate 1 and folder backplate 2
The broken aerofoil 7 for all having 39 degree of angle inclined surface up and down is provided at parallel position.
Wherein, the side guard plate 1 is the arc plate structure of semicircle shape, and two 1 inner concaves of side guard plate are opposite, just
It can make up a complete cylinder-like structure, and the inner concave bottom of side guard plate 1 is provided perpendicular to the small flat of horizontal plane
The setting of platform, arc plate structure can provide safety coefficient higher Anticollision Measures for unmanned plane two sides, especially encounter shock
It can ensure the safety of data box to greatest extent afterwards, on the other hand, the setting of curved plate-like structure can reduce windage, most
The influence to unmanned plane during flying is reduced in big extent and scope.
Wherein, the tight jam plate 3 and folder backplate 2 offer several transparent Reduction of Students' Study Load holes 8 in the horizontal plane, can
While ensureing structural integrity, and weight bearing can be mitigated for unmanned plane.
Wherein, it is equipped with one layer of buffer layer 9 with several through-holes in folder 2 upright inner side walls of backplate, it can be to nothing
Man-machine fuselage plays the role of antiwear during clamping and during flight.
Wherein, the aviation aluminium support column 5 tool is there are six the cambered surface groove of semicircle shape, and two aviation aluminium support columns 5 it
Between be provided with damping, buffering spring 6 with 5 equivalent diameter size of aviation aluminium support column, the special construction of aviation aluminium support column 5 increases
Stress supporting surface is added, can realize that stronger support force, damping, buffering spring 6 can hit in limited quality
It can play the role of damping reset afterwards, reduce the damage to unmanned plane in maximum.
The specifically used mode and effect of the present embodiment:
In the utility model, when in use, the clamping screw 4 on tight jam plate 3 is unclamped by spanner first, so that tight lock
Plate 3 separates, and two U-shaped folder backplates 2 are wrapped on unmanned aerial vehicle body, is passing through clamping screw 4 and nut 402 for two parts
It fits together, side guard plate 1 is the arc plate structure of semicircle shape, and two 1 inner concaves of side guard plate are opposite, just being capable of group
The chain-wales of horizontal plane, arc are provided perpendicular at the inner concave bottom of a complete cylinder-like structure, and side guard plate 1
The setting of hardened structure can provide safety coefficient higher Anticollision Measures for unmanned plane two sides, especially can be most after encountering shock
The safety of the guarantee data box of limits, on the other hand, the setting of curved plate-like structure can reduce windage, in utmostly model
Influence of the interior reduction to unmanned plane during flying is enclosed, tight jam plate 3 and folder backplate 2 offer several transparent subtract in the horizontal plane
Negative hole 8 can mitigate weight bearing while ensureing structural integrity for unmanned plane, press from both sides 2 upright inner side walls upper berth of backplate
Buffer layer 9 equipped with one layer with several through-holes, can be to unmanned aerial vehicle body during clamping and during flight
Play the role of it is antiwear, the tool of aviation aluminium support column 5 there are six the cambered surface groove of semicircle shape, and two aviation aluminium support columns 5 it
Between be provided with damping, buffering spring 6 with 5 equivalent diameter size of aviation aluminium support column, the special construction of aviation aluminium support column 5 increases
Stress supporting surface is added, can realize that stronger support force, damping, buffering spring 6 can hit in limited quality
It can play the role of damping reset afterwards, the damage to unmanned plane be reduced in maximum, between side guard plate 1 and folder backplate 2
The front end portion position parallel with aviation aluminium support column 5 at be provided with and all have breaking for 39 degree angle inclined surface up and down
Aerofoil 7 can reduce anti-collision structure and give unmanned plane bring windage, and the flight resistance of unmanned plane is reduced in side.
The opening in technical solutions of the utility model using technical solution described in the utility model or those skilled in the art
It gives, designs similar technical solution, and reach above-mentioned technical effect, be to fall into the protection scope of the utility model.
Claims (5)
1. the two sided Anti-bumping protection mechanism for surveying and drawing unmanned plane, it is characterised in that: this is used to survey and draw the two sided of unmanned plane
Anti-bumping protection mechanism includes side guard plate, presss from both sides backplate, tight jam plate, clamping screw, aviation aluminium support column, damping, buffering spring, broken wind
Plate, lighten the burden hole, buffer layer, interior nut head and nut；Two U-shaped folder backplate inner ends are oppositely arranged, and press from both sides backplate outer end
Both ends have been symmetrically arranged two aviation aluminium support columns on side wall；The outer end of the aviation aluminium support column is respectively fixedly connected with
On side guard plate medial surface；It is respectively provided at the top and bottom of the folder backplate there are two the tight jam plate, and is provided on tight jam plate
Two tight jam plates are simultaneously fixed together by the nut that end thread connects by two symmetrical clamping screws；The locking
The outer end of bolt is the structure of interior nut hair style；Front end portion and aviation aluminium support column phase between the side guard plate and folder backplate
The broken aerofoil for all having 39 degree of angle inclined surface up and down is provided at parallel position.
2. as described in claim 1 for surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane, it is characterised in that: the side guard plate
For the arc plate structure of semicircle shape, and two side guard plate inner concaves are opposite, can make up just one it is complete cylindric
Structure, and the inner concave bottom of side guard plate is provided perpendicular to the chain-wales of horizontal plane.
3. as described in claim 1 for surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane, it is characterised in that: the tight jam plate
Several transparent Reduction of Students' Study Load holes are offered in the horizontal plane with folder backplate.
4. as described in claim 1 for surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane, it is characterised in that: the folder backplate
One layer of buffer layer with several through-holes is equipped in upright inner side walls.
5. as described in claim 1 for surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane, it is characterised in that: the aviation aluminium
There are six the cambered surface grooves of semicircle shape for support column tool, and are provided between two aviation aluminium support columns same with aviation aluminium support column
The special construction of the damping, buffering spring of diameter, aviation aluminium support column increases stress supporting surface.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820913314.4U CN208344542U (en) | 2018-06-13 | 2018-06-13 | For surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820913314.4U CN208344542U (en) | 2018-06-13 | 2018-06-13 | For surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208344542U true CN208344542U (en) | 2019-01-08 |
Family
ID=64883690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820913314.4U Active CN208344542U (en) | 2018-06-13 | 2018-06-13 | For surveying and drawing the two sided Anti-bumping protection mechanism of unmanned plane |
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| CN (1) | CN208344542U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113086179A (en) * | 2021-04-27 | 2021-07-09 | 桂林天经地纬遥感信息技术有限公司 | Double-side anti-collision protection device for aerial photography unmanned aerial vehicle |
| CN113844646A (en) * | 2021-10-13 | 2021-12-28 | 云南交通运输职业学院(云南交通技师学院、云南省交通高级技工学校) | Damage-proof unmanned aerial vehicle for training |
-
2018
- 2018-06-13 CN CN201820913314.4U patent/CN208344542U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN113086179A (en) * | 2021-04-27 | 2021-07-09 | 桂林天经地纬遥感信息技术有限公司 | Double-side anti-collision protection device for aerial photography unmanned aerial vehicle |
| CN113086179B (en) * | 2021-04-27 | 2022-09-23 | 桂林天经地纬遥感信息技术有限公司 | Double-side anti-collision protection device for aerial photography unmanned aerial vehicle |
| CN113844646A (en) * | 2021-10-13 | 2021-12-28 | 云南交通运输职业学院(云南交通技师学院、云南省交通高级技工学校) | Damage-proof unmanned aerial vehicle for training |
| CN113844646B (en) * | 2021-10-13 | 2023-12-29 | 云南交通运输职业学院(云南交通技师学院、云南省交通高级技工学校) | Damage-preventing unmanned aerial vehicle for training |
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