CN208278309U - A kind of mapping unmanned plane with high stability - Google Patents
A kind of mapping unmanned plane with high stability Download PDFInfo
- Publication number
- CN208278309U CN208278309U CN201820334646.7U CN201820334646U CN208278309U CN 208278309 U CN208278309 U CN 208278309U CN 201820334646 U CN201820334646 U CN 201820334646U CN 208278309 U CN208278309 U CN 208278309U
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- CN
- China
- Prior art keywords
- unmanned plane
- moving assembly
- fixedly installed
- high stability
- drone body
- 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
The utility model discloses a kind of mapping unmanned plane with high stability, including metal edge frame, rubber layer, dismounting screw, steady brace, guiding wing leaf and moving assembly, the metal edge frame outboard bonds have rubber layer, steady brace is installed on the inside of the dismounting screw, moving assembly is installed below the guiding wing leaf, the utility model is scientific and reasonable for structure, safe and convenient to use, and being provided with metal edge frame makes unmanned plane have higher mechanical strength and service life；Being provided with rubber layer avoids unmanned plane body from being corroded by the acid rain etc. in air；Dismounting screw is provided with convenient for the installation and removal between unmanned plane composition component；Being provided with steady brace keeps the connection between unmanned aerial vehicle rack stronger；It is provided with the direct contact-impact that guiding wing leaf avoids unmanned plane and air draught etc., improves stability of the unmanned plane in flight or mapping process；Keep movement of the unmanned plane after landing more convenient using moving assembly.
Description
Technical field
The utility model relates to air vehicle technique field, specially a kind of mapping unmanned plane with high stability.
Background technique
With the continuous development of present science and technology, it is gradually increased the use scope of unmanned plane also therewith, unmanned plane, again
Claim UAV, have many advantages, such as maneuverability, be swift in response, unmanned flight, remote control, and surveys and draws unmanned plane, it is main
The plotting board that include unmanned plane and be mounted on unmanned plane, traditional mapping unmanned plane is because it is in flight course, often
The direct contact-impact of Chang Yinwei unmanned plane body and air draught etc., causes unmanned plane body extremely unstable, and make its
Reduce the mapping quality of unmanned plane in mapping process because of shaking, existing unmanned plane after landing because of its bottom on the ground
Lack moving assembly, causes it to become not moved, reduce the flexibility of unmanned plane, in addition existing unmanned plane is because of it
Lack the components such as reinforcing and protection in use, leads to its not only shadow vulnerable to dirt in air and acid rain etc. when in use
It rings, while reducing the service life of unmanned plane.
Utility model content
The utility model provides a kind of mapping unmanned plane with high stability, can effectively solve in above-mentioned background technique
The traditional mapping unmanned plane proposed is because it is in flight course, usually because unmanned plane body connects with the direct of air draught etc.
Touching is hit, and causes unmanned plane body extremely unstable, and it is made to reduce the mapping of unmanned plane because of shaking in mapping process
Quality, existing unmanned plane, because its bottom lacks moving assembly on the ground, cause it to become not moved after landing,
The flexibility of unmanned plane is reduced, in addition existing unmanned plane is led because it lacks the components such as reinforcing and protection in use
Its not only influence vulnerable to dirt in air and acid rain etc. when in use is caused, while the service life etc. for reducing unmanned plane is asked
Topic.
To achieve the above object, the utility model provides the following technical solutions: a kind of mapping with high stability nobody
Machine, including drone body, metal edge frame, rubber layer, casing, rack, dismounting screw, shaft, rotation wing, steady brace,
Ventilative board, air inlet, support arch bar, wind deflector, guiding wing leaf, oblique rib plate, support column, moving assembly, installation screw and system
Device is moved, edge is fixedly installed with metal edge frame on the outside of the drone body, and edge is fixed viscous on the outside of the metal edge frame
Rubber layer is had, each vertex of drone body is obliquely extended installation organic frame, the fixed peace in one side end of rack
Equipped with dismounting screw, the rack end side is rotatably connected to shaft, is rotatably connected to rotation wing above the shaft,
Steady brace is fixedly installed on the outside of two edge of drone body, edge is fixedly installed with below the drone body
Ventilative board offers air inlet inside the ventilative board, and the drone body bottom part down fixation is supported by support arch bar,
Wind deflector is fixedly installed with above the support arch bar, the wind deflector inside is diagonally-installed guiding wing leaf, the wind deflector
Two sides edge is oblique to be fixedly installed with oblique rib plate upwards, and fixation is supported by support column, the branch below the support arch bar
It is fixedly installed with moving assembly below dagger, the moving assembly includes pressure reductor, side securing plate, movable pulley and buffer layer,
It is fixedly installed with side securing plate below the pressure reductor both side ends, side-lower is fixedly installed in the side securing plate
Movable pulley, the mobile wheel outer surface are bonded with buffer layer, and the moving assembly side is fixedly installed with brake.
Preferably, casing is coated on the outside of the rubber layer.
Preferably, the dismounting screw is convenient for the installation and removal between rack and drone body.
Preferably, the quantity of the steady brace is two.
Preferably, connection is fixedly mounted by installation screw between the moving assembly and support column.
Preferably, the drone body and metal edge frame are a kind of component of aluminum alloy material.
Compared with prior art, the utility model has the beneficial effects that the utility model is scientific and reasonable for structure, secure side is used
Just, being provided with metal edge frame makes unmanned plane have higher mechanical strength and service life；It is provided with rubber layer and avoids unmanned plane
Body is corroded by the acid rain etc. in air；Dismounting screw is provided with convenient for the installation and removal between unmanned plane composition component；
Being provided with steady brace keeps the connection between unmanned aerial vehicle rack stronger, further improves the stability of unmanned plane；Setting
There is guiding wing leaf to avoid the direct contact-impact of unmanned plane and air draught etc., improves unmanned plane in flight or mapping process
Stability；Keep movement of the unmanned plane after landing more convenient using moving assembly.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this
Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention.
In the accompanying drawings:
Fig. 1 is the structural schematic diagram of the utility model；
Fig. 2 is the utility model main view；
Fig. 3 is the mounting structure schematic diagram of the utility model moving assembly；
Fig. 4 is the mounting structure schematic diagram of the utility model brake；
Figure label: 1, drone body；2, metal edge frame；3, rubber layer；4, casing；5, rack；6, screw is dismounted；7,
Shaft；8, wing is rotated；9, steady brace；10, ventilative board；11, air inlet；12, arch bar is supported；13, wind deflector；14, it is oriented to
Wing leaf；15, oblique rib plate；16, support column；17, moving assembly；18, pressure reductor；19, side securing plate；20, movable pulley；21,
Buffer layer；22, screw is installed；23, brake.
Specific embodiment
It is illustrated below in conjunction with preferred embodiment of the attached drawing to the utility model, it should be understood that described herein excellent
It selects embodiment to be only used for describing and explaining the present invention, is not used to limit the utility model.
Embodiment: as shown in Figs 1-4, the utility model provides a kind of technical solution, a kind of mapping with high stability
Unmanned plane, including drone body 1, metal edge frame 2, rubber layer 3, casing 4, rack 5, dismounting screw 6, shaft 7, rotation wing
8, steady brace 9, ventilative board 10, air inlet 11, support arch bar 12, wind deflector 13, guiding wing leaf 14, oblique rib plate 15, support
Column 16, moving assembly 17, installation screw 22 and brake 23,1 outside edge of drone body are fixedly installed with metal edge frame
2,2 outside edge of metal edge frame is fixed to be bonded with rubber layer 3, and it is organic that each vertex of drone body 1 is obliquely extended installation
Frame 5,5 one side end of rack are fixedly installed with dismounting screw 6, and 5 end side of rack is rotatably connected to shaft 7,7 top of shaft
It is rotatably connected to rotation wing 8, is fixedly installed with steady brace 9 on the outside of 1 liang of edge of drone body, under drone body 1
Square edge is fixedly installed with ventilative board 10, and air inlet 11 is offered inside ventilative board 10, and 1 bottom part down of drone body is solid
Surely it is supported by support arch bar 12, supports and is fixedly installed with wind deflector 13 above arch bar 12,13 inside of wind deflector is diagonally-installed to lead
To wing leaf 14,13 two sides edge of wind deflector is oblique to be fixedly installed with oblique rib plate 15 upwards, supports fixed branch below arch bar 12
Support has support column 16, and moving assembly 17 is fixedly installed with below support column 16, and moving assembly 17 includes pressure reductor 18, side reinforcing
Plate 19, movable pulley 20 and buffer layer 21,18 both side ends of pressure reductor lower section are fixedly installed with side securing plate 19, and side reinforces
Side-lower is fixedly installed with movable pulley 20 in plate 19, and 20 outer surface of movable pulley is bonded with buffer layer 21,17 side of moving assembly
It is fixedly installed with brake 23.
In order to further increase the mechanical strength of drone body 1, in the present embodiment, it is preferred that coated on the outside of rubber layer 3
There is casing 4.
For the ease of the fixed installation and disassembly between rack 5, shaft 7 and rotation wing 8 and drone body 1, this reality
It applies in example, it is preferred that dismounting screw 6 is convenient for the installation and removal between rack 5 and unmanned plane body 1.
In order to keep 1 side frame 5 of drone body more stable, in the present embodiment, it is preferred that the quantity of steady brace 9
It is two.
For the ease of being fixedly connected between moving assembly 17 and support column 16, in the present embodiment, it is preferred that moving assembly
Connection is fixedly mounted by installation screw 22 between 17 and support column 16.
In order to reduce the overall weight of unmanned plane body, in the present embodiment, it is preferred that drone body 1 and metal edge frame 2
It is a kind of component of aluminum alloy material.
The working principle and process for using of the utility model: mapping unmanned plane is in practical flight mapping process, body
The metal edge frame 2 and casing 4 of inside can effectively prevent the generations such as the dirt to suspend in unmanned plane and air from colliding, and avoid nothing
Man-machine face generates abrasion, and rubber layer 3 can prevent the dirts such as dust, aqueous vapor in air from entering in unmanned plane, in it
Portion's component impacts, and the flights component such as rack 5, shaft 7 and rotation wing 8 provides stable flight performance for unmanned plane,
Screw 6 is dismounted convenient for fixed installation and activity disassembly between rack 5 and drone body 1, makes unmanned plane after flight
Cleaning and maintenance become more convenient, steady brace 9 makes connection between unmanned aerial vehicle rack 5 and is more firmly mounted, ventilative
Plate 10 and its internal air inlet 11 are convenient for the transmission of air draught, wind deflector 13, the guiding groups such as wing leaf 14 and oblique rib plate 15
Part makes unmanned plane in flight course, and when body and air draught etc. directly contact, wind deflector 13 can pass through air draught
Guiding wing leaf 14 dredges it to 13 liang of upper sides of wind deflector, and then further dredging by oblique rib plate 15, makes air gas
The air-flow for forming spiral below shaft 7 is flowed, contact-impact between unmanned plane and air draught is avoided and generates biased, make nothing
It is man-machine more stable in flight or mapping process, improve the mapping quality of unmanned plane, the movable pulley 20 of 17 lower section of moving assembly
Movement of the unmanned plane after landing is set to become easier, while brake 23 makes unmanned plane can be consolidated after movement
Fixed, in addition the pressure reductor 18 of moving assembly 17 and buffer layer 21 make unmanned plane when contacting between ground in descent, energy
The anti-force between unmanned plane and ground is enough effectively eliminated, keeps unmanned plane more stable in landing.
Finally, it should be noted that being not limited to this reality the foregoing is merely the preferred embodiment of the utility model
With novel, although the utility model is described in detail with reference to the foregoing embodiments, come for those skilled in the art
Say, it is still possible to modify the technical solutions described in the foregoing embodiments, or to part of technical characteristic into
Row equivalent replacement.Within the spirit and principle of the utility model, any modification, equivalent replacement, improvement and so on, should all
It is included within the scope of protection of this utility model.
Claims (6)
1. a kind of mapping unmanned plane with high stability, including drone body (1), metal edge frame (2), rubber layer (3), machine
Shell (4), rack (5), dismounting screw (6), shaft (7), rotation wing (8), steady brace (9), ventilative board (10), air inlet
(11), arch bar (12), wind deflector (13), guiding wing leaf (14), oblique rib plate (15), support column (16), moving assembly are supported
(17), screw (22) and brake (23) are installed, it is characterised in that: edge is fixedly mounted on the outside of the drone body (1)
Have metal edge frame (2), edge fixation is bonded with rubber layer (3) on the outside of the metal edge frame (2), the drone body (1)
Each vertex is obliquely extended installation organic frame (5), and (5) one side end of rack is fixedly installed with dismounting screw (6), described
Rack (5) end side is rotatably connected to shaft (7), and rotation wing (8) is rotatably connected to above the shaft (7), described
It is fixedly installed with steady brace (9) on the outside of (1) two edge of drone body, edge is fixed below the drone body (1)
It is equipped with ventilative board (10), is offered air inlet (11) inside the ventilative board (10), under drone body (1) bottom
Side is fixed to be supported by support arch bar (12), is fixedly installed with wind deflector (13), the wind deflector above the support arch bar (12)
(13) it is internal it is diagonally-installed have guiding wing leaf (14), wind deflector (13) two sides edge it is oblique be fixedly installed with upwards it is oblique
Rib plate (15), support arch bar (12) lower section fixation are supported by support column (16), are fixedly mounted below the support column (16)
Have moving assembly (17), the moving assembly (17) includes pressure reductor (18), side securing plate (19), movable pulley (20) and buffering
Layer (21), pressure reductor (18) the both side ends lower section are fixedly installed with side securing plate (19), the side securing plate
(19) interior side-lower is fixedly installed with movable pulley (20), and movable pulley (20) outer surface is bonded with buffer layer (21), described
Moving assembly (17) side is fixedly installed with brake (23).
2. a kind of mapping unmanned plane with high stability according to claim 1, it is characterised in that: the rubber layer
(3) outside is coated with casing (4).
3. a kind of mapping unmanned plane with high stability according to claim 1, it is characterised in that: the dismounting screw
(6) convenient for the installation and removal between rack (5) and drone body (1).
4. a kind of mapping unmanned plane with high stability according to claim 1, it is characterised in that: the steady brace
(9) quantity is two.
5. a kind of mapping unmanned plane with high stability according to claim 1, it is characterised in that: the moving assembly
(17) connection is fixedly mounted by installation screw (22) between support column (16).
6. a kind of mapping unmanned plane with high stability according to claim 1, it is characterised in that: the unmanned plane sheet
Body (1) and metal edge frame (2) are a kind of component of aluminum alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820334646.7U CN208278309U (en) | 2018-03-12 | 2018-03-12 | A kind of mapping unmanned plane with high stability |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820334646.7U CN208278309U (en) | 2018-03-12 | 2018-03-12 | A kind of mapping unmanned plane with high stability |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208278309U true CN208278309U (en) | 2018-12-25 |
Family
ID=64748925
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820334646.7U Expired - Fee Related CN208278309U (en) | 2018-03-12 | 2018-03-12 | A kind of mapping unmanned plane with high stability |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208278309U (en) |
-
2018
- 2018-03-12 CN CN201820334646.7U patent/CN208278309U/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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20181225 Termination date: 20200312 |