CN205239918U - Agricultural aviation ware - Google Patents
Agricultural aviation ware Download PDFInfo
- Publication number
- CN205239918U CN205239918U CN201520125497.XU CN201520125497U CN205239918U CN 205239918 U CN205239918 U CN 205239918U CN 201520125497 U CN201520125497 U CN 201520125497U CN 205239918 U CN205239918 U CN 205239918U
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- CN
- China
- Prior art keywords
- agricultural aviation
- rotor arm
- rotor
- aviation device
- led lamp
- 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.)
- Expired - Fee Related
Links
- 230000005540 biological transmission Effects 0.000 claims description 2
- 230000004888 barrier function Effects 0.000 abstract description 4
- 230000005622 photoelectricity Effects 0.000 abstract 1
- 239000007788 liquid Substances 0.000 description 6
- 230000004308 accommodation Effects 0.000 description 3
- 230000005611 electricity Effects 0.000 description 3
- 238000005507 spraying Methods 0.000 description 2
- 238000005406 washing Methods 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 1
- 206010008428 Chemical poisoning Diseases 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
- 239000002131 composite material Substances 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000003337 fertilizer Substances 0.000 description 1
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000575 pesticide Substances 0.000 description 1
- 230000010152 pollination Effects 0.000 description 1
- 230000005855 radiation Effects 0.000 description 1
- 230000000576 supplementary effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Landscapes
- Guiding Agricultural Machines (AREA)
Abstract
The utility model discloses an agricultural aviation ware aims at providing a simple structure, makes things convenient for dismantlement, convenient storage, has that photoelectricity shows, the agricultural aviation ware of operation is sprayed in imitative the more suitable farmland of flying and keeping away the barrier ability. The utility model discloses a two the rotor arm alternately rotates the design that sets up and be the cruciform symmetry, can be with two when transporting or accomodating the rotor arm is folding, the utility model discloses microwave radar and ultrasonic wave or laser rangefinder that the front and back end set up can realize the flight of face profile modeling everywhere well and avoid the obstacle, can be at the landmass of many barriers convenient to use. The utility model discloses be applied to agricultural aviation ware's technical field.
Description
Technical field
The utility model relates to a kind of aircraft, particularly a kind of agricultural aviation device.
Background technology
At present domestic cultivating received mechanization degree and improved year by year, but agricultural plant protection is still taking manually as main, and both dangerous, efficiency is low again. And the agricultural unmanned airborne vehicle of the one growing up gradually in recent years, apply at pesticide spraying, liquid fertilizer, the aspect such as crops supple-mentary pollination fully demonstrates advantage, peasant is freed from heavy plant protection operation, can solve a difficult problem that causes pesticide poisoning because manual operation is improper.
Publication number is the Chinese patent application of 103496446A, and it discloses the agricultural aircraft of a kind of four axle, and equipment compartment is positioned at centre position, and this equipment compartment is the cydariform of the uncovered lower end closed in upper end, and every stay pipe of undercarriage is connected with equipment compartment by two securing members; Be provided with four cantilevers that distribute by even circumferential in the periphery of equipment compartment, the inner and the equipment compartment of this cantilever are connected as a single entity, and are provided with motor bin in the outer end of each cantilever; Motor is housed in motor bin, and above this motor bin, is provided with screw. Because the size of agricultural aircraft is larger, and the inner of the cantilever of this patent application and equipment compartment be connected as a single entity, and inconvenience transport, uses, preserves. And current agricultural aircraft does not possess and has the ability of flying and keeping away barrier imitatively, can not meet well the operations such as farmland sprinkling.
Utility model content
Technical problem to be solved in the utility model is to overcome the deficiencies in the prior art, a kind of simple in structure, for convenience detach, convenient for collecting is provided, has photoelectric display, imitative fly and keep away the agricultural aviation device that is more suitable for farmland spraying operation of barrier ability.
The technical scheme that the utility model adopts is: the utility model comprises upper body and lower body, described upper body comprises several rotor arms, described in several, on rotor arm, be provided with rotor device, the quantity of described rotor arm is that 2, two described rotor arms intersections are rotated setting and are cross symmetry.
On described lower body, be provided with the movable securing member suitable with described rotor arm, described rotor arm is fixed on described lower body by described movable securing member.
Described lower body comprises main support, is arranged on the flusher of described main support below and at least three under-chassis that are fixedly connected with described main support.
Described flusher comprise be arranged on described main support below medicine-chest, be arranged on the pump housing of described medicine-chest below and arrange on described rotor arm and be positioned at the shower nozzle of the below of described rotor device, described shower nozzle is connected with the described pump housing by carrier pipe.
Described lower body also comprises around several power supplys that are arranged on described medicine-chest sidepiece, described upper body comprises the controller being arranged on described rotor arm, described controller top is vertically provided with LED lamppost, and the described pump housing, described power supply and described LED lamppost are all electrically connected with described controller.
The bottom of described under-chassis is made as deflection and below between two adjacent described rotor arms.
On described rotor arm, be provided with LED lamp band I, described LED lamp band I is electrically connected with described controller.
Be positioned on the described under-chassis at described main support rear and be provided with LED lamp band II, described LED lamp band II is electrically connected integral with described LED lamp band I.
Described rotor arm is pipe fitting, described rotor device comprises the motor cabinet being arranged on described pipe fitting, the screw that is arranged on the motor on described motor cabinet and is connected with described motor-driven, described motor cabinet is provided with the air vent suitable with described motor afterbody, and described air vent is connected with the inside of described pipe fitting.
Described agricultural aviation device also comprises the microwave radar and ultrasonic wave or the laser ranging system that are separately positioned on front and back end.
The beneficial effects of the utility model are: because the utility model has adopted dismountable design, the utility model comprises upper body and lower body, described upper body comprises several rotor arms, described in several, on rotor arm, be provided with rotor device, because the quantity of described rotor arm is 2, two described rotor arms intersections are rotated setting and are cross symmetry, so can two described rotor arms are folding in transport or storage, further ensure the safety of transport, also further saved accommodation space.
Meanwhile, on described lower body, be provided with the movable securing member suitable with described rotor arm, so described rotor arm is fixed on described lower body by described movable securing member, simple in structure, for convenience detach and storage, ensure transport safety, also greatly saved accommodation space.
And, due to described flusher comprise be arranged on described main support below medicine-chest, be arranged on the pump housing of described medicine-chest below and arrange on described rotor arm and be positioned at the shower nozzle of the below of described rotor device, described shower nozzle is connected with the described pump housing by carrier pipe, so, the utility model can make full use of the lower gas washing body of described rotor device, has increased the penetrability of liquid.
In addition, because described agricultural aviation device also comprises the microwave radar and ultrasonic wave or the laser ranging system that are separately positioned on front and back end, fly and avoid obstacle so the utility model can be realized well with ground profiling, can be easy to use in the plot of multi-obstacle avoidance.
Brief description of the drawings
Fig. 1 is perspective view of the present utility model;
Fig. 2 is side view of the present utility model;
Fig. 3 is top view of the present utility model;
Fig. 4 is the structural representation of described rotor arm 3.
Detailed description of the invention
Embodiment mono-:
As depicted in figs. 1 and 2, in the present embodiment, the utility model comprises upper body 1 and lower body 2, if described upper body 1 comprises two rotor arms 3, on two described rotor arms 3, be provided with rotor device 4, on described lower body 2, be provided with the movable securing member 5 suitable with described rotor arm 3, described rotor arm 3 is fixed on described lower body 2 by described movable securing member 5. In the present embodiment, described movable securing member 5 is clamping piece, and the bottom of described clamping piece is fixed on described lower body 2, and described clamping piece is being held described rotor arm 3 tightly, can be for convenience detach in the process of transport.
In the present embodiment, two described rotor arms 3 intersections are rotated and are arranged and be cross symmetry, thereby two described rotor arms 3 can fold, and save accommodation space.
In the present embodiment, four under-chassis 8 that described lower body 2 comprises main support 6, is arranged on the flusher 7 of described main support 6 belows and is fixedly connected with described main support 6.
In the present embodiment, described flusher 7 comprise be arranged on described main support 6 belows medicine-chest 9, be arranged on the pump housing 10 of described medicine-chest 9 belows and arrange on described rotor arm 3 and be positioned at the shower nozzle 11 of the below of described rotor device 4, described shower nozzle 11 is connected with the described pump housing 10 by carrier pipe, such design can make full use of the lower gas washing body of described rotor device 3, has increased the penetrability of liquid.
In the present embodiment, described lower body 2 also comprises that described upper body 1 comprises the controller 13 being arranged on described rotor arm 3 around several power supplys 12 that are arranged on described medicine-chest 9 sidepieces, and the described pump housing 10, described power supply 12 are all electrically connected with described controller 13.
In the present embodiment, the bottom of described under-chassis 8 is made as deflection and below between two adjacent described rotor arms 3, as shown in Figure 3, in top view, described rotor arm 3 becomes α angle with the bottom of described under-chassis 8, and α=30 ° in the present embodiment can effectively prevent the pollution of liquid like this.
Embodiment bis-:
The difference of the present embodiment and embodiment mono-is: in the present embodiment, described controller 13 tops are vertically provided with LED lamppost 19, and described LED lamppost 19 is electrically connected with described controller 13; On described rotor arm 3, be provided with LED lamp band I, described LED lamp band I is electrically connected with described controller 13, described LED lamp band I is full-color LED lamp band, by described LED lamppost 19 and the flicker variation of described LED lamp band I or the conversion of color, can point out the surplus of liquid, surplus and the environment temperature that electricity is adjusted etc. of power supply 12, simultaneously can also be by described LED lamppost 19 and the identification of described LED lamp band I flight attitude, flying quality and sprinkling data.
In the present embodiment, be positioned on the described under-chassis 8 at described main support 6 rears and be provided with LED lamp band II, described LED lamp band II is electrically connected integral, such design with described LED lamp band I and is easy to identify flight attitude.
Embodiment tri-:
The difference of the present embodiment and embodiment mono-and embodiment bis-is: as shown in Figure 4, described rotor arm 3 is pipe fitting, described pipe fitting is carbon fiber pipe or high strength composite pipe fitting, described rotor device 4 comprises the motor cabinet 14 being arranged on described pipe fitting, the screw 16 that is arranged on the motor 15 on described motor cabinet 14 and is in transmission connection with described motor 15, described motor cabinet 14 is provided with the air vent 17 suitable with described motor 15 afterbodys, described air vent 17 is connected with the inside of described pipe fitting, thereby the centrifugal wind that can produce by described motor 15 rotations is adjusted heat radiation to the electricity being placed in described pipe fitting. and described electricity arranges also can save space in described pipe fitting, after fulfiling assignment, directly water rinses clean.
In the present embodiment, as shown in Figure 3, described motor 15 is two circles and is distributed on described rotor arm 3, thereby has ensured the utlity model has enough power, and then can carry more liquid.
In the present embodiment, described a kind of agricultural aviation device also comprises and is separately positioned on microwave radar 18 or ultrasonic wave or laser ranging system front and back end and that be connected with controller 13 signals, thereby can realize profiling flight and avoid obstacle.
The utility model is applied to the technical field of agricultural aviation device.
Claims (9)
1. an agricultural aviation device, comprise upper body (1) and lower body (2), described upper body (1) comprises several rotor arms (3), described in several, on rotor arm (3), be provided with rotor device (4), it is characterized in that: the quantity of described rotor arm (3) is 2, two described rotor arms (3) intersection is rotated setting and is cross symmetry, described rotor arm (3) is pipe fitting, described rotor device (4) comprises the motor cabinet (14) being arranged on described pipe fitting, the screw (16) that is arranged on the motor (15) on described motor cabinet (14) and is in transmission connection with described motor (15), described motor cabinet (14) is provided with the air vent (17) suitable with described motor (15), described air vent (17) is connected with the inside of described pipe fitting.
2. a kind of agricultural aviation device according to claim 1, it is characterized in that: on described lower body (2), be provided with the movable securing member (5) suitable with described rotor arm (3), described rotor arm (3) is fixed on described lower body (2) by described movable securing member (5).
3. a kind of agricultural aviation device according to claim 1, is characterized in that: described lower body (2) comprises main support (6), is arranged on the flusher (7) of described main support (6) below and at least three under-chassis (8) that are fixedly connected with described main support (6).
4. a kind of agricultural aviation device according to claim 3, it is characterized in that: described flusher (7) comprise be arranged on described main support (6) below medicine-chest (9), be arranged on the pump housing (10) of described medicine-chest (9) below and be arranged on described rotor arm (3) upper and be positioned at the shower nozzle (11) of the below of described rotor device (4), described shower nozzle (11) is connected with the described pump housing (10) by carrier pipe.
5. a kind of agricultural aviation device according to claim 4, it is characterized in that: described lower body (2) also comprises around several power supplys (12) that are arranged on described medicine-chest (9) sidepiece, described upper body (1) comprises the controller (13) being arranged on described rotor arm (3), described controller (13) top is vertically provided with LED lamppost (19), and the described pump housing (10), described power supply (12) and described LED lamppost (19) are all electrically connected with described controller (13).
6. a kind of agricultural aviation device according to claim 3, is characterized in that: the bottom of described under-chassis (8) is made as deflection and is positioned at the below between adjacent two described rotor arms (3).
7. a kind of agricultural aviation device according to claim 5, is characterized in that: on described rotor arm (3), be provided with LED lamp band I, described LED lamp band I is electrically connected with described controller (13).
8. a kind of agricultural aviation device according to claim 7, is characterized in that: be positioned on the described under-chassis (8) at described main support (6) rear and be provided with LED lamp band II, described LED lamp band II is electrically connected integral with described LED lamp band I.
9. according to a kind of agricultural aviation device described in claim 4 to 7 any one, it is characterized in that: described a kind of agricultural aviation device also comprises the microwave radar (18) or ultrasonic wave or the laser ranging system that are separately positioned on front and back end.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520125497.XU CN205239918U (en) | 2015-03-04 | 2015-03-04 | Agricultural aviation ware |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520125497.XU CN205239918U (en) | 2015-03-04 | 2015-03-04 | Agricultural aviation ware |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205239918U true CN205239918U (en) | 2016-05-18 |
Family
ID=55938986
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520125497.XU Expired - Fee Related CN205239918U (en) | 2015-03-04 | 2015-03-04 | Agricultural aviation ware |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205239918U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106347626A (en) * | 2016-11-16 | 2017-01-25 | 北京韦加无人机科技股份有限公司 | Foldable multi-rotor plant protection unmanned aerial vehicle |
| CN106394907A (en) * | 2016-11-16 | 2017-02-15 | 北京韦加无人机科技股份有限公司 | Amphibious unmanned aerial vehicle |
| CN106477034A (en) * | 2016-11-16 | 2017-03-08 | 北京韦加无人机科技股份有限公司 | A kind of detachably many rotors plant protection unmanned plane |
-
2015
- 2015-03-04 CN CN201520125497.XU patent/CN205239918U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106347626A (en) * | 2016-11-16 | 2017-01-25 | 北京韦加无人机科技股份有限公司 | Foldable multi-rotor plant protection unmanned aerial vehicle |
| CN106394907A (en) * | 2016-11-16 | 2017-02-15 | 北京韦加无人机科技股份有限公司 | Amphibious unmanned aerial vehicle |
| CN106477034A (en) * | 2016-11-16 | 2017-03-08 | 北京韦加无人机科技股份有限公司 | A kind of detachably many rotors plant protection unmanned plane |
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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 |
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. |
|
| CP03 | Change of name, title or address | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160518 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |