CN203889063U - Artificial pollination aircraft - Google Patents
Artificial pollination aircraft Download PDFInfo
- Publication number
- CN203889063U CN203889063U CN201420332499.1U CN201420332499U CN203889063U CN 203889063 U CN203889063 U CN 203889063U CN 201420332499 U CN201420332499 U CN 201420332499U CN 203889063 U CN203889063 U CN 203889063U
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- frame
- pollination
- aircraft
- fuselage
- pollinating
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Abstract
The utility model relates to an artificial pollination device, in particular to an artificial pollination aircraft for agriculture. The artificial pollination aircraft comprises an aircraft body, a control system and a pollinating device, wherein rotor wing frames and foot stands are also arranged on the aircraft body, all the rotor wing frames and the aircraft body are positioned on a same horizontal plane, the rotor wing frames are circumferentially arranged by taking the aircraft body as the center, one end of each rotor wing frame is connected with the aircraft body, the other end of each rotor wing frame is provided with a screw propeller, the control system controls the operation time sequence of the screw propellers, the pollinating device comprises a pollinating frame and a support for connecting the pollinating frame and the aircraft body, one end of the support is connected onto the pollinating frame, the pollinating frame comprises one carbon fiber square tube at the top part of the pollinating frame, and two rows of PVC impact plates are arranged at the bottom surface of the carbon fiber square tube. The PVC impact plates are used for impacting flowers, so that pollen can be easily blown by airflow generated by the screw propellers and the artificial pollination effect is improved.
Description
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Technical field
The utility model relates to a kind of artificial pollination equipment, relates in particular in a kind of agricultural the aircraft for artificial pollination.
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Background technology
Agricultural, as infrastructural industries, more and more manifests its importance, and the quality of pollination has directly determined the output of crops.What the pollination of present most crops was leaned on is open-pollinated, such as corn, if run into some inclement weathers, can cause crop production reduction even to have no harvest.So, under given conditions, the artificial pollination necessity very that just seems.Although traditional pollinating device has played certain effect, itself exist some defects to restrict the effect of pollinating device.Human assistance is awarded in Different Crop not exclusively the same, is generally first from stamen, to gather pollen, then spreads on pistil stigma.On paddy rice, often pass through manpower, Yi Bian by the past method of pushing over of bamboo pole, the pollen in male parent is shaken to cause drop to female parent, height consuming time, efficiency is low.General pollinating device, design is complicated, and volume ratio is larger, or the carrying out of the pollination work of piece more longways, or pollinating device simplicity of design, cannot be applicable to the operation of large area plot.
Chinese invention patent ZL201310133972.3 discloses a kind of Y type non co axial multi-rotor aerocraft, comprises main body, and this main body is provided with the master arm being positioned on main body longitudinal median plane, and the rear end of this master arm is provided with a main rotor; The bilateral symmetry of the front end of this master arm is provided with two auxiliary hold-down arms, and each auxiliary hold-down arm is provided with at least 1 auxiliary rotor; Between each auxiliary hold-down arm and master arm, by hinged formation, be rotatably connected.But this aircraft relies on wind-force to carry out artificial pollination completely, and operating efficiency is lower, and be difficult to work for not wide-open flower, Applicable scope is limited, still has further improved space.
Utility model content
The purpose of this utility model is to provide a kind of artificial pollination aircraft simple in structure, applied widely.
To achieve these goals, the utility model adopts following technical scheme:
A kind of artificial pollination aircraft, comprise fuselage, the pollinating device that is arranged on the control system in described fuselage and is arranged on described fuselage below, on described fuselage, be also provided with four or more rotor wings frame, wherein on more than three or three described rotor wings frames, be provided with for parking the foot rest of pollination aircraft, described in each, rotor wings frame and described fuselage are positioned in same level, and become circumferential arrangement with centered by described fuselage, one end of described rotor wings frame is connected with described fuselage, the other end is provided with screw propeller, described control system is controlled the work schedule of described screw propeller, described foot rest one end is fixed on described rotor wings frame, the other end is also outward-dipping placement down, described pollinating device comprises pollination frame and the support that is connected described pollination frame and described fuselage, described support one end is connected on described pollination frame, the other end is directly connected with described fuselage or is indirectly connected with described fuselage by being connected on described rotor wings frame, described pollination frame comprises a carbon fiber square tube that is arranged on its top, described carbon fiber square tube bottom surface is provided with two row PVC striking plates, the described PVC striking plate of two rows is laterally chevron shaped arrangement, longitudinally being yi word pattern arranges.
Adopt such scheme, by control system, control screw propeller and carry out differential rotation, can not only provide the power that moves ahead and turn to for aircraft, and can below aircraft, produce air-flow, pollen is kicked up and carried out artificial pollination.Meanwhile, by PVC striking plate collision flower, the air-flow that pollen is more easily produced by screw propeller is blown afloat, improve the effect of artificial pollination.
As further improvement of the utility model, on described support, be provided with the shock absorption device of being made by soft spring.By the antagonistic force producing when shock absorption device can effectively be alleviated PVC striking plate collision flower is set, the stability of aircraft is impacted, light spring also can alleviate the weight of aircraft simultaneously, reduces power consumption.
As of the present utility model a kind of preferred, described rotor has six.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model artificial pollination aircraft.
In figure, corresponding sign is as follows:
1-fuselage; 2-pollinating device;
3-rotor wings frame; 4-foot rest;
5-screw propeller; The 21-frame of pollinating;
22-support; 23-carbon fiber square tube;
24-PVC striking plate.
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The specific embodiment
Below in conjunction with accompanying drawing, the specific embodiment of the present utility model is described further.
The artificial pollination Flight Vehicle Structure of the present embodiment as shown in Figure 1, comprise fuselage 1, the pollinating device 2 that is arranged on the control system in fuselage 1 and is arranged on fuselage below, on fuselage 1, be also provided with six rotor wings frames 3, wherein on three rotor wings frames 3, be provided with for parking the foot rest 4 of pollination aircraft, the quantity of rotor wings frame 3 can arrange according to the real work situation of pollination aircraft, but at least need to have four rotor wings frames could realize the function of pollination aircraft, the quantity of foot rest 4 can arrange according to practical service environment equally, but at least need the support pollination aircraft that three foot rests, 4 ability are stable.Each rotor wings frame 3 is positioned in same level with fuselage 1, and becomes circumferential arrangement with centered by fuselage 1.One end of rotor wings frame 3 is connected with fuselage 1, and the other end is provided with screw propeller 5, is controlled the work schedule of screw propeller 5 by control system, and control system can be remote control system common in prior art, no longer describes in detail herein.One end of foot rest 4 is fixed on rotor wings frame 3, and the other end is also outward-dipping placement down.
Pollinating device 2 comprises pollination frame 21 and is connected the support 22 of pollination frame 21 with fuselage 1, one end of support 22 is connected on pollination frame 21, the other end is connected with fuselage 1 indirectly by being connected on rotor wings frame 3, also can directly rotor wings frame 3 be directly connected with fuselage 1, but preferably as the indirect connection of the present embodiment, can increase the stability of pollination aircraft.Pollination frame 21 comprises a carbon fiber square tube 23 that is arranged on its top, and the bottom surface of carbon fiber square tube 23 is provided with two row PVC striking plate 24, two row PVC striking plates 24 and is laterally chevron shaped arrangement, is longitudinally yi word pattern and arranges.On support 22, be provided with the shock absorption device of being made by soft spring, this shock absorption device can be shock absorption device of the prior art, no longer describes in detail herein.
During use, the differential of controlling screw propeller 5 by control system rotates, as required controlled pollination aircraft turn to, the flare maneuver such as inclination or forward-reverse, by appropriate location, aircraft flight island, allow again PVC striking plate on pollinating device 2 collision flower gently, pollen on male parent flower is kicked up under the effect of the downwash flow of screw propeller 5 generations, and be transmitted to maternal flower, realize artificial pollination.
By reference to the accompanying drawings test tube stand of the present utility model has been done to detailed explanation above, but the utility model is not limited to above-mentioned embodiment, those skilled in the art can make various modification on this basis, and these all belong to protection domain of the present utility model.
Claims (3)
1. an artificial pollination aircraft, comprise fuselage, the pollinating device that is arranged on the control system in described fuselage and is arranged on described fuselage below, it is characterized in that, on described fuselage, be also provided with four or more rotor wings frame, wherein on more than three or three described rotor wings frames, be provided with for parking the foot rest of pollination aircraft, described in each, rotor wings frame and described fuselage are positioned in same level, and become circumferential arrangement with centered by described fuselage, one end of described rotor wings frame is connected with described fuselage, the other end is provided with screw propeller, described control system is controlled the work schedule of described screw propeller, described foot rest one end is fixed on described rotor wings frame, the other end is also outward-dipping placement down, described pollinating device comprises pollination frame and the support that is connected described pollination frame and described fuselage, described support one end is connected on described pollination frame, the other end is directly connected with described fuselage or is indirectly connected with described fuselage by being connected on described rotor wings frame, described pollination frame comprises a carbon fiber square tube that is arranged on its top, described carbon fiber square tube bottom surface is provided with two row PVC striking plates, the described PVC striking plate of two rows is laterally chevron shaped arrangement, longitudinally being yi word pattern arranges.
2. artificial pollination aircraft as claimed in claim 1, is characterized in that, is provided with the shock absorption device of being made by soft spring on described support.
3. artificial pollination aircraft as claimed in claim 1 or 2, is characterized in that, described rotor has six.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420332499.1U CN203889063U (en) | 2014-06-22 | 2014-06-22 | Artificial pollination aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420332499.1U CN203889063U (en) | 2014-06-22 | 2014-06-22 | Artificial pollination aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203889063U true CN203889063U (en) | 2014-10-22 |
Family
ID=51715498
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420332499.1U Expired - Fee Related CN203889063U (en) | 2014-06-22 | 2014-06-22 | Artificial pollination aircraft |
Country Status (1)
| Country | Link |
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| CN (1) | CN203889063U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354858A (en) * | 2014-11-10 | 2015-02-18 | 成都好飞机器人科技有限公司 | Agricultural multi-rotor unmanned machine |
| CN106069724A (en) * | 2016-06-29 | 2016-11-09 | 江苏红旗种业股份有限公司 | Many rotors remotely-piloted vehicle is applied to make hybrid paddy rice seed production and pollination method |
| WO2018133241A1 (en) * | 2017-01-23 | 2018-07-26 | 东莞理工学院 | Micro flying robot for autonomous agricultural pollination |
| JP2019508012A (en) * | 2017-01-23 | 2019-03-28 | トンクワン ユニバーシティ オブ テクノロジーＤｏｎｇｇｕａｎ Ｕｎｉｖｅｒｓｉｔｙ ｏｆ Ｔｅｃｈｎｏｌｏｇｙ | Automated pollination method for agriculture based on micro-flying robot |
-
2014
- 2014-06-22 CN CN201420332499.1U patent/CN203889063U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104354858A (en) * | 2014-11-10 | 2015-02-18 | 成都好飞机器人科技有限公司 | Agricultural multi-rotor unmanned machine |
| CN106069724A (en) * | 2016-06-29 | 2016-11-09 | 江苏红旗种业股份有限公司 | Many rotors remotely-piloted vehicle is applied to make hybrid paddy rice seed production and pollination method |
| WO2018133241A1 (en) * | 2017-01-23 | 2018-07-26 | 东莞理工学院 | Micro flying robot for autonomous agricultural pollination |
| JP2019508012A (en) * | 2017-01-23 | 2019-03-28 | トンクワン ユニバーシティ オブ テクノロジーＤｏｎｇｇｕａｎ Ｕｎｉｖｅｒｓｉｔｙ ｏｆ Ｔｅｃｈｎｏｌｏｇｙ | Automated pollination method for agriculture based on micro-flying robot |
| JP2019511974A (en) * | 2017-01-23 | 2019-05-09 | トンクワン ユニバーシティ オブ テクノロジーＤｏｎｇｇｕａｎ Ｕｎｉｖｅｒｓｉｔｙ ｏｆ Ｔｅｃｈｎｏｌｏｇｙ | Autonomous micro-flying robot for pollination for agriculture |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141022 Termination date: 20150622 |
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| EXPY | Termination of patent right or utility model |