CN207173945U - A kind of plant protection unmanned plane - Google Patents
A kind of plant protection unmanned plane Download PDFInfo
- Publication number
- CN207173945U CN207173945U CN201720903024.7U CN201720903024U CN207173945U CN 207173945 U CN207173945 U CN 207173945U CN 201720903024 U CN201720903024 U CN 201720903024U CN 207173945 U CN207173945 U CN 207173945U
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- China
- Prior art keywords
- unmanned plane
- fixed seat
- support bar
- plant protection
- undercarriage
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Abstract
It the utility model is related to a kind of plant protection unmanned plane, belong to agricultural production equipment technical field, described plant protection unmanned plane mainly includes frame main body, undercarriage, support bar I, support bar II, rotating shaft, micromachine, rotor, device for quickly disassembling, clip, frame main body is arranged at the top of undercarriage, device for quickly disassembling is symmetrically installed with undercarriage, described device for quickly disassembling includes support rail, tight locking button, sleeving connecting rod, described clip includes fixed seat I, fixed seat II, junction button, buckle, neck, the utility model provides a kind of novel plant protection unmanned plane, the transport of unmanned plane can be facilitated, increase substantially transition efficiency, increase unmanned plane rotor intensity, ensure its flight stability, simultaneously, the quick-replaceable that different operating environments carries out medicine-chest can be directed to, increase operating efficiency, realize a tractor serves several purposes.
Description
Technical field
It the utility model is related to agricultural production equipment technical field, and in particular to a kind of novel plant protection unmanned plane.
Background technology
Plant protection unmanned plane, is the UAV for agriculture and forestry plant protection operation, and the type unmanned aerial vehicle is flat by flying
Platform（Fixed-wing, helicopter, Multi-axis aircraft）, navigation fly control, spraying mechanism three parts composition, by ground remote control or navigation fly
Control, to realize spraying operation, can spray medicament, seed, pulvis etc..
Existing plant protection unmanned aerial vehicle body space-consuming is larger, and transport is more difficult, and transition is less efficient, and fuselage itself
Less stable, the intensity of connector is relatively low, it is impossible to meets more atrocious weather situation；Carried out simultaneously to different pharmaceutical
When changing medicine-chest, the fixed effect of medicine-chest is poor, easily occurs the phenomenon rocked in flight course, influences the flight of unmanned plane, needs
Devote a tremendous amount of time adjustment medicine-chest angle and position, operating efficiency decrease, plant protection unmanned plane when being sprayed,
Need to ask larger stability, existing plant protection unmanned plane rotor is less, and stability is poor, it is impossible to meet to require.
Therefore, it is necessary to existing plant protection unmanned plane being improved so that the structure of plant protection unmanned plane is more perfect,
On the premise of not increasing a large amount of production costs, the practicality for improving plant protection unmanned plane is maximized, increases its flight stability, increased
Operating efficiency.
The content of the invention
In order to overcome problem present in background technology, the utility model provides a kind of novel plant protection unmanned plane, can
Facilitate the transport of unmanned plane, increase substantially transition efficiency, increase unmanned plane rotor intensity, ensure its flight stability, meanwhile,
The quick-replaceable that different operating environments carries out medicine-chest can be directed to, increases operating efficiency, realizes a tractor serves several purposes.
To reach above-mentioned purpose, the utility model is implemented by following technical scheme：
Described plant protection unmanned plane mainly includes frame main body, undercarriage, support bar I, support bar II, rotating shaft, micro electric
Machine, rotor, device for quickly disassembling, clip, frame main body are arranged at the top of undercarriage, and device for quickly disassembling is symmetrically installed with undercarriage,
Described device for quickly disassembling includes support rail, tight locking button, sleeving connecting rod, and support rail is arranged on undercarriage by tight locking button, supports
Cross bar rear and front end is respectively welded sleeving connecting rod, and front end sleeving connecting rod is provided with screw thread, and described frame main body surrounding is uniformly provided with
Four support bars I, support bar I are bolted with frame main body, and the right-hand end of support bar I is connected with branch by clip
Strut II, support bar II are hinged with rotating shaft, and rotating shaft upper end is provided with micromachine, and micromachine is connected with rotor, described fixation
Button includes fixed seat I, fixed seat II, junction button, buckle, neck, and fixed seat I is welded on the right-hand end of support bar I, fixed seat
I one end is provided with neck, and the other end and the one end of fixed seat II of fixed seat I are hinged, and fixed seat II is welded on a left side for support bar II
Side end face, the other end of fixed seat II are provided with groove, and described junction button is arranged in groove, and junction button one end is cut with scissors with fixed seat II
Connect, the junction button other end is hinged with the buckle that neck matches.
Further, the described length of support bar II is more than rotor length.
Further, described undercarriage and frame main body junction angle are 125 ° -135 °.
Further, the location external that lands of described undercarriage is provided with cushion, and cushion is made up of silica-gel sponge.
Further, described buckle end face tilts in certain taper.
The beneficial effects of the utility model：
The utility model provides a kind of novel plant protection unmanned plane, simple and compact for structure, by changing to unmanned plane frame
Enter, improve the load-carrying of unmanned plane, the stability of unmanned plane during flying can be increased substantially, increase of rotor on each support frame
Number, realize the stability during sprinkling；Using special tight locking button structure design, in the case of without using unmanned plane, subtract
Its few floor space, and can be more convenient in transportation, transition efficiency is improved, increases its practicality, increases it and use model
Enclose；Meanwhile designed using fast disassembly type, can arbitrarily change suspension and adjust ginseng, for different working environment carry out medicine-chest it is quick more
Change, increase substantially operating efficiency, and accomplish a tractor serves several purposes.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model；
Fig. 2 is tight locking button dimensional structure diagram of the present utility model；
In figure, 1- frame main bodies, 2- undercarriages, 3- support bars I, 4- support bars II, 5- rotating shafts, 6- micromachines, 7- rotations
The wing, 8- support rails, 9- tight locking buttons, 10- sleeving connecting rods, 11- clips, 12- fixed seats I, 13- fixed seats II, 14- junction buttons,
15- buckles, 16- necks.
Embodiment
In order that the purpose of this utility model, technical scheme and beneficial effect are clearer, below in conjunction with accompanying drawing, to this
The preferred embodiment of utility model is described in detail, to facilitate the technical staff to understand.
As shown in Figure 1-2, described plant protection unmanned plane mainly includes frame main body 1, undercarriage 2, support bar I 3, support bar
II 4, rotating shaft 5, micromachine 6, rotor 7, device for quickly disassembling, clip 11.
Frame main body 1 is arranged on the top of undercarriage 2, and device for quickly disassembling, described device for quickly disassembling are symmetrically installed with undercarriage 2
Including support rail 8, tight locking button 9, sleeving connecting rod 10, support rail 8 is arranged on undercarriage 2, undercarriage 2 and machine by tight locking button 9
The junction angle of frame body 1 is 125 ° -135 °, and the location external that lands of undercarriage 2 is provided with cushion, and cushion is by silica-gel sponge
It is made, the rear and front end of support rail 8 is respectively welded sleeving connecting rod 10, and front end sleeving connecting rod 10 is provided with screw thread, set using fast disassembly type
Meter, it can arbitrarily change suspension and adjust ginseng, the quick-replaceable of medicine-chest is carried out for different working environments, increase substantially work effect
Rate, and accomplish a tractor serves several purposes.The described surrounding of frame main body 1 is uniformly provided with four support bars I 3, support bar I 3 and frame master
Body 1 is bolted, and the right-hand end of support bar I 3 is connected with support bar II 4, support bar II 4 and rotating shaft by clip 11
5 is be hinged, and the upper end of rotating shaft 5 is provided with micromachine 6, and micromachine 6 is connected with rotor 7, and each micromachine 6 connects with two panels rotor 7
Connecing, the described length of support bar II 4 is more than the length of rotor 7, by the improvement to unmanned plane frame, improves the load-carrying of unmanned plane,
The stability of unmanned plane during flying can be increased substantially, increases the number of rotor 7 on each support frame, is realized during spraying
Stability.
Described clip 11 includes fixed seat I 12, fixed seat II 13, junction button 14, buckle 15, neck 16, fixed seat I
12 are welded on the right-hand end of support bar I 3, and one end of fixed seat I 12 is provided with neck 16, the other end of fixed seat I 12 and fixation
II 13 one end of seat are hinged, and fixed seat II 13 is welded on the left end face of support bar II 4, and the other end of fixed seat II 13 is provided with groove,
Described junction button 14 is arranged in groove, and the one end of junction button 14 is be hinged with fixed seat II 13, the other end of junction button 14 and neck
16 buckles 15 to match are be hinged, and the end face of buckle 15 tilts in certain taper, using the special structure design of tight locking button 9, not
In the case of using unmanned plane, its floor space is reduced, and can be more convenient in transportation, improve transition efficiency, increase
Its practicality, increase its use range.
The course of work of the present utility model：
When carrying out agricultural plant protection using the utility model, support bar I 3 and support bar II 4 are pulled, buckle 15 is fixed on
In neck 16, you can fixed support bar I 3 and support bar II 4, when completing plant protection, the buckle 15 being locked in neck 16 is opened,
Support bar I 3 and support bar II 4 are pulled, clip 11 is opened, and fastens adjacent supports bar with double buckle, is completed to fog machine
Storage.
The utility model provides a kind of novel plant protection unmanned plane, simple and compact for structure, by changing to unmanned plane frame
Enter, improve the load-carrying of unmanned plane, the stability of unmanned plane during flying can be increased substantially, increase of rotor on each support frame
Number, realize the stability during sprinkling；Using special tight locking button structure design, in the case of without using unmanned plane, subtract
Its few floor space, and can be more convenient in transportation, transition efficiency is improved, increases its practicality, increases it and use model
Enclose；Meanwhile designed using fast disassembly type, can arbitrarily change suspension and adjust ginseng, for different working environment carry out medicine-chest it is quick more
Change, increase substantially operating efficiency, and accomplish a tractor serves several purposes.
Finally illustrate, preferred embodiment above is merely to illustrate the technical solution of the utility model and unrestricted, to the greatest extent
The utility model has been described in detail by above preferred embodiment for pipe, but those skilled in the art should manage
Solution, can make various changes, without departing from the utility model claims book institute to it in the form and details
Limit.
Claims (5)
- A kind of 1. plant protection unmanned plane, it is characterised in that：Described plant protection unmanned plane mainly includes frame main body, undercarriage, support Bar I, support bar II, rotating shaft, micromachine, rotor, device for quickly disassembling, clip, frame main body are arranged at the top of undercarriage, risen and fallen Device for quickly disassembling is symmetrically installed with frame, described device for quickly disassembling includes support rail, tight locking button, sleeving connecting rod, and support rail passes through Tight locking button is arranged on undercarriage, and support rail rear and front end is respectively welded sleeving connecting rod, and front end sleeving connecting rod is provided with screw thread, described Frame main body surrounding be uniformly provided with four support bars I, support bar I is bolted with frame main body, the right side of support bar I End is connected with support bar II by clip, and support bar II is hinged with rotating shaft, and rotating shaft upper end is provided with micromachine, micromachine It is connected with rotor, described clip includes fixed seat I, fixed seat II, junction button, buckle, neck, and fixed seat I is welded on branch The right-hand end of strut I, one end of fixed seat I are provided with neck, and the other end and the one end of fixed seat II of fixed seat I are hinged, fixed Seat II is welded on the left end face of support bar II, and the other end of fixed seat II is provided with groove, and described junction button is arranged in groove, Junction button one end is be hinged with fixed seat II, and the junction button other end is hinged with the buckle that neck matches.
- A kind of 2. plant protection unmanned plane according to claim 1, it is characterised in that：The described length of support bar II is more than rotor Length.
- A kind of 3. plant protection unmanned plane according to claim 1, it is characterised in that：Described undercarriage is connected with frame main body It is 125 ° -135 ° to locate angle.
- A kind of 4. plant protection unmanned plane according to claim 1, it is characterised in that：The location external that lands of described undercarriage Provided with cushion, cushion is made up of silica-gel sponge.
- A kind of 5. plant protection unmanned plane according to claim 1, it is characterised in that：Incline in certain taper described buckle end face Tiltedly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720903024.7U CN207173945U (en) | 2017-07-25 | 2017-07-25 | A kind of plant protection unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720903024.7U CN207173945U (en) | 2017-07-25 | 2017-07-25 | A kind of plant protection unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207173945U true CN207173945U (en) | 2018-04-03 |
Family
ID=61737363
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720903024.7U Expired - Fee Related CN207173945U (en) | 2017-07-25 | 2017-07-25 | A kind of plant protection unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207173945U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382561A (en) * | 2018-04-17 | 2018-08-10 | 珠海市双捷科技有限公司 | Folded unmanned plane and its application method |
| CN110877726A (en) * | 2019-11-12 | 2020-03-13 | 徐州迪沃通讯工程有限公司 | Foldable unmanned aerial vehicle |
-
2017
- 2017-07-25 CN CN201720903024.7U patent/CN207173945U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108382561A (en) * | 2018-04-17 | 2018-08-10 | 珠海市双捷科技有限公司 | Folded unmanned plane and its application method |
| CN108382561B (en) * | 2018-04-17 | 2024-03-12 | 珠海市双捷科技有限公司 | Folding unmanned aerial vehicle and application method thereof |
| CN110877726A (en) * | 2019-11-12 | 2020-03-13 | 徐州迪沃通讯工程有限公司 | Foldable unmanned aerial vehicle |
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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: 20180403 Termination date: 20200725 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |