CN204623846U - A kind of agricultural aviation device - Google Patents
A kind of agricultural aviation device Download PDFInfo
- Publication number
- CN204623846U CN204623846U CN201520187859.8U CN201520187859U CN204623846U CN 204623846 U CN204623846 U CN 204623846U CN 201520187859 U CN201520187859 U CN 201520187859U CN 204623846 U CN204623846 U CN 204623846U
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- China
- Prior art keywords
- rotor arm
- container part
- described rotor
- tighten
- vessel
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- 230000005611 electricity Effects 0.000 claims description 16
- 230000007704 transition Effects 0.000 claims description 13
- 239000011148 porous material Substances 0.000 claims description 12
- 208000002193 Pain Diseases 0.000 claims description 9
- 238000001816 cooling Methods 0.000 claims description 4
- 239000007921 spray Substances 0.000 abstract description 4
- 238000004519 manufacturing process Methods 0.000 abstract description 3
- 210000002683 foot Anatomy 0.000 description 6
- 239000000575 pesticide Substances 0.000 description 5
- 230000000694 effects Effects 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 241000607479 Yersinia pestis Species 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 238000009331 sowing Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000004917 carbon fiber Substances 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000004140 cleaning Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 238000005474 detonation Methods 0.000 description 1
- 238000003306 harvesting Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 238000003860 storage Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
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- Catching Or Destruction (AREA)
Abstract
The utility model discloses a kind of agricultural aviation device, aim to provide the agricultural aviation device that a kind of integral structure is simple, easy accessibility, cost of manufacture are low, good looking appearance spray area is large.The utility model comprises rotor arm section and container part, described container part is as the location of rotor arm section and fixed mount, described container part is integral structure, the annex that described container part comprises vessel (1) and is fixedly installed on described vessel (1), described vessel (1) and described annex are that integral moduleization is arranged, and described rotor arm section and described container part phase-splitting tighten up cooperation.The utility model is applied to the technical field of agricultural aviation device.
Description
Technical field
The utility model relates to a kind of aerocraft, particularly a kind of agricultural aviation device.
Background technology
Along with the development of science and technology, the level of mechanization of all trades and professions is more and more higher.Mechanization of agriculture also has development with rapid changepl. never-ending changes and improvements.In China, mechanization ploughing work, Mechanization sowing, mechanization pest control, mechanized harvest just progressively realizes throughout the country.And external Agricultural Mechanization Degree is higher.But with regard to Mechanization sowing, mechanization pest control aspect, but there is various deficiency, the production facilities as dropped into is expensive, and general medium and small plantation peasant household cannot bear; Equipment needs often to safeguard, equipment supplier is difficult to the service accomplishing thorough satisfaction, often needs to wait for the longer time; Need special technical personnel to drive mechanical equipment, cost of labor remains high.At present, some enterprises are also had to devise a kind of aircraft devices of carrying out pesticide spraying specially, as the agriculture unmanned plane that Japanese enterprises is produced.But these equipment prices are expensive, and general peasant household cannot bear at all.A problem is in addition, this aircraft devices complex structure, and the weight of equipment itself is comparatively large, cannot the more pesticide solution of splendid attire, and its area once sprayed is minimum, which again increases cost.
Utility model content
Technical problem to be solved in the utility model overcomes the deficiencies in the prior art, provides the agricultural aviation device that a kind of integral structure is simple, easy accessibility, cost of manufacture are low, good looking appearance, spraying efficiency are high.
The technical scheme that the utility model adopts is: the utility model comprises rotor arm section and container part, and described container part is as the location of rotor arm section and fixed mount, and described container part is integral structure.
Further, described container part comprises vessel and is fixedly installed on the annex on described vessel, and described vessel and described annex are that integral moduleization is arranged, and described rotor arm section and described container part phase-splitting tighten up cooperation.
Further, described container part is provided with and tightens up groove, described rotor arm section pass through described in tighten up groove and tighten up with described container part phase-splitting and coordinate.
Further, described rotor arm section comprises several rotor arms, and rotor arm described in several is provided with screw propeller, and described rotor arm is also provided with feet, and described screw propeller and described feet are separately positioned on the both sides of described rotor arm axle line.
Further, described rotor arm section comprises two described rotor arms, and two described rotor arms form intersection by attaching parts and are rotationally connected, described in tighten up groove be arranged in a crossed manner, two described rotor arms tighten up be engaged in arranged in a crossed manner described in tighten up in groove; The groove that tightens up on two described rotor arms and described container part all distributes in cruciform symmetry.
Further, described tighten up groove is provided with match with described rotor arm sting tight sheet, describedly sting tight sheet and be a scarce radian and the arc plate of hollow, the described outer wall stinging tight sheet is provided with outside thread, the described internal diameter stinging tight sheet is consistent with the external diameter of described rotor arm, the width dimensions of the described empty portions stung on tight sheet is less than the external diameter of described rotor arm, described rotor arm is provided with the transition plate consistent with the described empty portions stung on tight sheet, described tight sheet and the described transition plate stung forms a complete cylinder, described rotor arm is also arranged with tapped fixed cover, described fixed cover is set in by described that to sting cylinder that tight sheet and described transition plate form outer and tightened up by screw thread fit.
Further, described annex is power supply and the outlet valve being arranged on described vessel lower end, described vessel is provided with battery case, and described battery case comprises the first box body and the second box body, and described first box body and described second box body are the box-like connection of kinge-joint knot.
Further, in described vessel, be provided with the pump housing, on described rotor arm and the below being positioned at described screw propeller is provided with shower nozzle, described shower nozzle is connected with the described pump housing by conduit.
Further, described aerocraft also comprises distance measuring equipment (DME) and is arranged on the controller on described rotor arm, described distance measuring equipment (DME) is microwave radar, super sonic or laser ranging system, LED post is vertically provided with above described controller, described rotor arm is provided with LED, and described distance measuring equipment (DME), the described pump housing, described LED and described LED post are all electrically connected with described controller.
Further, described rotor arm is pipe fitting, in described rotor arm, be provided with electricity adjust, motor in the support of described screw propeller leaves the pore communicated with described rotor arm inside, the medium position of described rotor arm is provided with breather port, in the rotor arm that described electricity is transposed between described pore and described breather port, the motor of described screw propeller rotarily drives air and to enter in described rotor arm from described disposed at air vent and transfer in row cooling to described electricity, and hot blast is extracted out from described pore.
The beneficial effects of the utility model are: the utility model adopts modular design, whole aerocraft is divided into rotor arm section and container part in two sub-sections, described container part comprises vessel and is fixedly installed on the annex on described vessel, described vessel and described annex are that integral moduleization is arranged, described rotor arm section and described container part phase-splitting tighten up cooperation, so the utility model can carry out modularization dismounting and transport rapidly, can by two parts separately when transport or storage, this greatly reduces cost, integral structure is also simpler, attractive in appearance, compared with existing equipment, its deadweight is less, the aerocraft of same power, the pesticide solution that can carry is more, its area sprayed will be larger.
Simultaneously, described rotor arm section comprises two described rotor arms, two described rotor arms form intersection by attaching parts and are rotationally connected, described in tighten up groove be arranged in a crossed manner, two described rotor arms tighten up be engaged in arranged in a crossed manner described in tighten up in groove, so, the rotor arm section disassembled can realize folding, and can reduce further and take up room, convenient for collecting, ensure the safety of transport, also greatly save accommodation space and traffic cost.
And, due to described tighten up groove is provided with match with described rotor arm sting tight sheet, describedly sting tight sheet and be a scarce radian and the arc plate of hollow, the described outer wall stinging tight sheet is provided with outside thread, the described internal diameter stinging tight sheet is consistent with the external diameter of described rotor arm, the width dimensions of the described empty portions stung on tight sheet is less than the external diameter of described rotor arm, described rotor arm is provided with the transition plate consistent with the described empty portions stung on tight sheet, described tight sheet and the described transition plate stung forms a complete cylinder, described rotor arm is also arranged with tapped fixed cover, described fixed cover is set in by described that to sting cylinder that tight sheet and described transition plate form outer and tightened up by screw thread fit, so, the utility model can realize the dismounting of rotor arm section and container part rapidly, structure is simple.
In addition, because described annex is power supply and the outlet valve being arranged on described vessel lower end, described vessel is provided with battery case, described battery case comprises the first box body and the second box body, described first box body and described second box body are the box-like connection of kinge-joint knot, so this practicality power supply is arranged on moisture can be avoided to enter special battery box in, whole aircraft devices can be rinsed by direct water, be very easy to post-job cleaning, reduce the labour intensity of staff.
Owing to being provided with the pump housing in described vessel, on described rotor arm and the below being positioned at described screw propeller is provided with shower nozzle, described shower nozzle is connected with the described pump housing by conduit, so, the wind-force effect that the utility model can utilize the blade of described screw propeller to rotate, the pesticide spraying that shower nozzle sprays is obtained more even, improves spray effect further.
Also comprise distance measuring equipment (DME) due to described aerocraft and be arranged on the controller on described rotor arm, described distance measuring equipment (DME) is microwave radar, super sonic or laser ranging system, LED post is vertically provided with above described controller, described rotor arm is provided with LED, described distance measuring equipment (DME), the described pump housing, described LED and described LED post are all electrically connected with described controller, so, by described controller, realize unmanned flight, and microwave radar, the design of super sonic or laser ranging system, then can realize with ground profiling flight and avoid obstacle, can be easy to use in the plot of multi-obstacle avoidance, ensure that the safe flight of aerocraft, the design of described LED and described LED post, then according to its flashing state, can determine that the pesticide solution on aerocraft is how many, electric quantity of power supply how many and flight orientation, improve operator to the control of the overall condition of aerocraft, realize safe flight.
Because described rotor arm is pipe fitting, in described rotor arm, be provided with electricity adjust, motor in the support of described screw propeller leaves the pore communicated with described rotor arm inside, the medium position of described rotor arm is provided with breather port, in the rotor arm that described electricity is transposed between described pore and described breather port, the motor of described screw propeller rotarily drives air and to enter in described rotor arm from described disposed at air vent and transfer in row cooling to described electricity, hot blast is extracted out from described pore, so, being adjusted by electricity is arranged in rotor arm, make entirety more attractive in appearance, also the effect of screw propeller is taken full advantage of, save space.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model;
Fig. 2 is the structure for amplifying schematic diagram of part A in Fig. 1;
Fig. 3 is detonation configuration schematic diagram of the present utility model.
Detailed description of the invention
As shown in Figure 1 to Figure 3, in the present embodiment, the utility model comprises rotor arm section and container part, and described container part is as the location of rotor arm section and fixed mount, and described container part is integral structure.The annex that described container part comprises vessel 1 and is fixedly installed on described vessel 1, described vessel 1 and described annex are that integral moduleization is arranged, and described rotor arm section and described container part phase-splitting tighten up cooperation.Described container part is provided with and tightens up groove 2, described rotor arm section pass through described in tighten up groove 2 and tighten up with described container part phase-splitting and coordinate.In the present embodiment, described in tighten up groove 2 for orthogonal two grooves, the degree of depth of one of them groove and the external diameter of described rotor arm 3 in the same size, the degree of depth of a groove is in addition then that the external diameter sum of two described rotor arms 3 is in the same size.Described rotor arm section comprises several rotor arms 3, rotor arm 3 described in several is provided with screw propeller 4, and described rotor arm 3 is also provided with feet 5, and described screw propeller 4 and described feet 5 are separately positioned on the both sides of described rotor arm 3 axis.Wherein, described screw propeller 4 is installed upward, and described feet 5 is installed down.Each described rotor arm 3 is provided with two described feets 5.Described rotor arm 3 is pipe fitting, and described pipe fitting is carbon fiber pipe or high strength composite pipe fitting.
Described rotor arm section comprises two described rotor arms, 3, two described rotor arms 3 and forms intersection by attaching parts and be rotationally connected, described in tighten up groove 2 for arranged in a crossed manner, two described rotor arms 3 tighten up be engaged in arranged in a crossed manner described in tighten up in groove 2.The groove 2 that tightens up on two described rotor arms 3 and described container part all distributes in cruciform symmetry, thus two described rotor arms 3 can fold, and save accommodation space.
Described tighten up groove 2 is provided with match with described rotor arm 3 sting tight sheet 6, it is described that to sting tight sheet 6 be lack a radian and the arc plate of hollow, the described outer wall stinging tight sheet 6 is provided with outside thread, the described internal diameter stinging tight sheet 6 is consistent with the external diameter of described rotor arm 3, the width dimensions of the described empty portions stung on tight sheet 6 is less than the external diameter of described rotor arm 3, described rotor arm 3 is provided with the transition plate 7 consistent with the described empty portions stung on tight sheet 6, described tight sheet 6 and the described transition plate 7 stung forms a complete cylinder, described rotor arm 3 is also arranged with tapped fixed cover 8, described fixed cover 8 is set in by described that to sting cylinder that tight sheet 6 and described transition plate 7 form outer and tightened up by screw thread fit.Sting the cooperation of tight sheet, transition plate and described fixed cover described in utilization, the utility model can realize the dismounting of rotor arm section and container part rapidly, and structure is simple.
Described annex is power supply 13 and the outlet valve 9 being arranged on described vessel 1 lower end, described vessel 1 is provided with battery case 10, described battery case 10 comprises the first box body 101 and the second box body 102, and described first box body 101 and described second box body 102 are the box-like connection of kinge-joint knot.This battery case design, can avoid moisture to enter, thus make aircraft devices that water can be utilized directly to clean, facilitate maintenance.
In described vessel 1, be provided with the pump housing 11, on described rotor arm 3 and the below being positioned at described screw propeller 4 is provided with shower nozzle, described shower nozzle is connected with the described pump housing 11 by conduit.The described pump housing 11 is articulated on described rotor arm 3, and after installing the utility model, the described pump housing 11 is positioned at described vessel 1.Described shower nozzle is connected with the described pump housing 11 by delivery pipe, and such design can make full use of the lower gas washing body of described rotor arm 3, adds the penetrance of liquid.
Described aerocraft also comprises distance measuring equipment (DME) and is arranged on the controller 12 on described rotor arm 3, described distance measuring equipment (DME) is microwave radar, super sonic or laser ranging system, LED post is vertically provided with above described controller 12, described rotor arm 3 is provided with LED, and described distance measuring equipment (DME), the described pump housing 11, described LED and described LED post are all electrically connected with described controller 12.Described LED is all-colour LED light bar, by described LED post and the flicker change of described LED or the conversion of color, the ambient temperature etc. that the surplus of the surplus of liquid, power supply 13 and electricity are adjusted can be pointed out, simultaneously also by described LED post and described LED identification flight attitude with spray data.
Described rotor arm 3 is pipe fitting, in described rotor arm 3, be provided with electricity adjust, motor in the support of described screw propeller 4 leaves the pore communicated with described rotor arm 3 inside, the medium position of described rotor arm 3 is provided with breather port, in the rotor arm 3 that described electricity is transposed between described pore and described breather port, the motor of described screw propeller rotarily drives air and to enter in described rotor arm 3 from described disposed at air vent and transfer in row cooling to described electricity, and hot blast is extracted out from described pore.Thus the centrifugal wind of generation can be rotated to the heat radiation of the electricity be placed in described pipe fitting tune by the motor in described screw propeller.And described electricity arranges also can save space in described pipe fitting, can directly rinse clean after fulfiling assignment with water.
The utility model is applied to the technical field of agricultural aviation device.
Claims (10)
1. an agricultural aviation device, is characterized in that: it comprises rotor arm section and container part, and described container part is as the location of rotor arm section and fixed mount, and described container part is integral structure.
2. a kind of agricultural aviation device according to claim 1, it is characterized in that: the annex that described container part comprises vessel (1) and is fixedly installed on described vessel (1), described vessel (1) and described annex are that integral moduleization is arranged, and described rotor arm section and described container part tighten up cooperation mutually.
3. a kind of agricultural aviation device according to claim 2, is characterized in that: be provided with on described container part and tighten up groove (2), described rotor arm section pass through described in tighten up groove (2) and mutually tighten up with described container part and coordinate.
4. a kind of agricultural aviation device according to claim 3, it is characterized in that: described rotor arm section comprises several rotor arms (3), rotor arm (3) described in several is provided with screw propeller (4), described rotor arm (3) is also provided with feet (5), and described screw propeller (4) and described feet (5) are separately positioned on the both sides of described rotor arm (3) axis.
5. a kind of agricultural aviation device according to claim 4, it is characterized in that: described rotor arm section comprises two described rotor arms (3), two described rotor arms (3) form intersection by attaching parts and are rotationally connected, the described groove (2) that tightens up is for arranged in a crossed manner, two described rotor arms (3) tighten up be engaged in arranged in a crossed manner described in tighten up in groove (2), the groove (2) that tightens up on two described rotor arms (3) and described container part all distributes in cruciform symmetry.
6. a kind of agricultural aviation device according to claim 4 or 5, it is characterized in that: described tighten up groove (2) is provided with match with described rotor arm (3) sting tight sheet (6), described tight sheet (6) of stinging is for lacking a radian and the arc plate of hollow, the described outer wall stinging tight sheet (6) is provided with outside thread, the described internal diameter stinging tight sheet (6) is consistent with the external diameter of described rotor arm (3), the width dimensions of the described empty portions stung on tight sheet (6) is less than the external diameter of described rotor arm (3), described rotor arm (3) is provided with the transition plate (7) consistent with the described empty portions stung on tight sheet (6), described tight sheet (6) and the described transition plate (7) stung forms a complete cylinder, described rotor arm (3) is also arranged with tapped fixed cover (8), described fixed cover (8) is set in by described that to sting cylinder that tight sheet (6) and described transition plate (7) form outer and tightened up by screw thread fit.
7. a kind of agricultural aviation device according to claim 2, it is characterized in that: described annex is power supply (13) and the outlet valve (9) being arranged on described vessel (1) lower end, described vessel (1) is provided with battery case (10), described battery case (10) comprises the first box body (101) and the second box body (102), and described first box body (101) and described second box body (102) are the box-like connection of kinge-joint knot.
8. a kind of agricultural aviation device according to claim 6, it is characterized in that: in described vessel (1), be provided with the pump housing (11), described rotor arm (3) is upper and the below being positioned at described screw propeller (4) is provided with shower nozzle, described shower nozzle is connected with the described pump housing (11) by conduit.
9. a kind of agricultural aviation device according to claim 8, it is characterized in that: described aerocraft also comprises distance measuring equipment (DME) and is arranged on the controller (12) on described rotor arm (3), described distance measuring equipment (DME) is microwave radar, super sonic or laser ranging system, described controller (12) top is vertically provided with LED post, described rotor arm (3) is provided with LED, and described distance measuring equipment (DME), the described pump housing (11), described LED and described LED post are all electrically connected with described controller (12).
10. a kind of agricultural aviation device according to claim 9, it is characterized in that: described rotor arm (3) is pipe fitting, in described rotor arm (3), be provided with electricity adjust, motor in the support of described screw propeller (4) leaves the pore communicated with described rotor arm (3) inside, the medium position of described rotor arm (3) is provided with breather port, in the rotor arm (3) that described electricity is transposed between described pore and described breather port, the motor of described screw propeller rotarily drives air and to enter in described rotor arm (3) from described disposed at air vent and transfer in row cooling to described electricity, hot blast is extracted out from described pore.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520187859.8U CN204623846U (en) | 2015-03-31 | 2015-03-31 | A kind of agricultural aviation device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520187859.8U CN204623846U (en) | 2015-03-31 | 2015-03-31 | A kind of agricultural aviation device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204623846U true CN204623846U (en) | 2015-09-09 |
Family
ID=54042899
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520187859.8U Expired - Fee Related CN204623846U (en) | 2015-03-31 | 2015-03-31 | A kind of agricultural aviation device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204623846U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105966598A (en) * | 2016-05-17 | 2016-09-28 | 王勇 | Agricultural plant protection aircraft |
| CN106314797A (en) * | 2016-10-18 | 2017-01-11 | 韩振铎 | Different-propeller multi-axis aircraft structure and operation method |
| CN111051195A (en) * | 2017-09-09 | 2020-04-21 | 意造科技私人有限公司 | Non-planar frame structure of unmanned aerial vehicle |
-
2015
- 2015-03-31 CN CN201520187859.8U patent/CN204623846U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105966598A (en) * | 2016-05-17 | 2016-09-28 | 王勇 | Agricultural plant protection aircraft |
| CN106314797A (en) * | 2016-10-18 | 2017-01-11 | 韩振铎 | Different-propeller multi-axis aircraft structure and operation method |
| CN106314797B (en) * | 2016-10-18 | 2019-06-07 | 韩振铎 | Different paddle Multi-axis aircraft structure and operational method |
| CN111051195A (en) * | 2017-09-09 | 2020-04-21 | 意造科技私人有限公司 | Non-planar frame structure of unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 519090 Guangdong province Zhuhai city Zhuhai town of Red Bay area, Shuanghu Road West Road on the north side of No. 6 workshop two Patentee after: ZHUHAI YUREN AGRICULTURAL AVIATION Co.,Ltd. Address before: Green Bay Industrial Park Jinhu road 519041 Guangdong city of Zhuhai province Jinwan District No. 3 Patentee before: ZHUHAI YUREN AIRCRAFT Co.,Ltd. |
|
| 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: 20150909 |