CN202190661U - Natural enemy releaser for aircraft - Google Patents
Natural enemy releaser for aircraft Download PDFInfo
- Publication number
- CN202190661U CN202190661U CN2011203282459U CN201120328245U CN202190661U CN 202190661 U CN202190661 U CN 202190661U CN 2011203282459 U CN2011203282459 U CN 2011203282459U CN 201120328245 U CN201120328245 U CN 201120328245U CN 202190661 U CN202190661 U CN 202190661U
- Authority
- CN
- China
- Prior art keywords
- natural enemy
- casing
- rotating disc
- releaser
- aircraft
- 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
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Abstract
The utility model relates to a releaser, in particular to a natural enemy releaser for an aircraft, which resolves the problem that an existing releaser cannot meet large-area releasing and is low in releasing efficiency. The natural enemy releaser for the aircraft comprises a box arranged on the aircraft, a releasing opening is arranged at the bottom of the box and provided with a rotating impeller matching with the releasing opening, the lower side of the rotating impeller is provided with a conveying belt, the position of one end of the conveying belt corresponds to that of the rotating impeller, a natural enemy spraying barrel located below the conveying belt is arranged below the other end of the conveying belt, a rotating disc is disposed below the natural enemy spraying barrel, and motors are arranged at axle centers of the rotating disc and the rotating impeller. The natural enemy releaser is reasonable and reliable in structural design, realizes large-area natural enemy releasing, simultaneously is complete and uniform in releasing effect, greatly improves utilization rate of natural enemies, and has the advantages of simple structure, convenience in operation and low cost.
Description
Technical field
The utility model relates to releasing device, is specially a kind of aircraft and uses the natural enemy release.
Background technology
Adopting the natural enemy prevention and elimination of disease and pests to have outstanding feature free from environmental pollution, can lasting stability control pest disaster, is the developing direction of the present extermination of disease and insect pest.What the method for natural enemy release at present adopted all is artificial method for releasing.The conventional artificial method for releasing adopts every strain tree or a few strain, tens strains tree to discharge the method for natural enemy respectively; Release efficiency is very low; Can only be applied on the little extermination of disease and insect pest of city trees and shrubs seeds or generation area, when running into the pest disaster of large tracts of land outburst, traditional natural enemy releasing device release efficiency is low can't realize the effective control to pest disaster; Can only use chemical pesticide to prevent and treat in a large number, thereby environment has been caused serious pollution and destruction.
Summary of the invention
The utility model can't satisfy large tracts of land release and the low problem of release efficiency in order to solve existing releasing device, provides a kind of aircraft to use the natural enemy release.
The utility model is to adopt following technical scheme to realize: aircraft is used the natural enemy release; Comprise setting casing aboard, bottom half has liberation port, and the liberation port place is provided with the rotary blade that is mated; The rotary blade below is provided with the end conveyer belt corresponding with its position; The other end below of conveyer belt is provided with the natural enemy spray tube that is positioned at its below, and natural enemy spray tube below is provided with rotating disc, and the axle center of rotating disc and rotary blade is equipped with motor.During use, natural enemy is inserted in the casing, regulate motor speed control rotary blade and rotate; And then natural enemy at the uniform velocity delivered to conveyer belt; Transmission at conveyer belt falls into natural enemy spray tube, drops on through natural enemy spray tube and leans on the motor-driven rotating disc, relies on action of centrifugal force; Natural enemy is thrown away, and release efficiency is higher when satisfying large tracts of land release.
Be supported with two turning cylinders that are positioned at the rotary blade left and right sides between the both sides before and after in the casing, wherein be wound with gauze on a turning cylinder, the other end of gauze is wrapped on another root turning cylinder, all is fixed with motor on two turning cylinders.During use, do not have on it that root turning cylinder of gauze to rotate through motor-driven, and constantly on gauze, spread natural enemy; Thereby with natural enemy being involved in the gauze from level to level; During release, the position of two turning cylinders is exchanged, rotated through the motor-driven turning cylinder; Thereby reasonably control the rate of release and the quantity of natural enemy, release efficiency further improves.
Natural enemy spray tube comprises anti-high-pressure plastic outer tube, is provided with the inner metal sleeve pipe that has high-tension electricity in the anti-high-pressure plastic outer tube.When natural enemy sprayed tube through natural enemy, under the effect of inner metal sleeve pipe, natural enemy can have static, and plant is had good suction-operated, can not get off from landing on the plant, improved and prevented and treated efficient.
The rotating disc upper surface is laid with some radially-arranged baffle plates, and is with the back-up ring that is supported on the rotating disc on the baffle plate.Improved the suffered centrifugal force of natural enemy through setting up baffle plate and back-up ring, be scattered when flying out more comprehensively evenly.
Casing is with shell outward, is fixed with pole between shell and the casing, and pole is provided with separation layer.Through additional isolation layer on pole, prevent the natural enemy escape.
The utility model reasonable in design is reliable, and when realizing that the natural enemy large tracts of land discharges, releasing effect is even comprehensively, and the availability of natural enemy significantly promotes, and has advantage simple in structure, easy to operate and with low cost.
Description of drawings
Fig. 1 is the structural representation of the utility model.
Among the figure: the 1-casing, the 2-liberation port, the 3-rotary blade, the 4-conveyer belt, 5-natural enemy spray tube, the 6-rotating disc, the 7-turning cylinder, the 8-gauze, 9-prevents high-pressure plastic outer tube, 10-inner metal sleeve pipe, 11-baffle plate, 12-back-up ring, 13-shell, 14-pole, 15-motor.
Embodiment
Aircraft is used the natural enemy release; Comprise setting casing 1 aboard, casing 1 bottom has liberation port 2, and liberation port 2 places are provided with the rotary blade 3 that is mated; Rotary blade 3 belows are provided with the end conveyer belt corresponding with its position 4; The other end below of conveyer belt 4 is provided with the natural enemy spray tube 5 that is positioned at its below, and natural enemy spray tube 5 belows are provided with rotating disc 6, and the axle center of rotating disc 6 and rotary blade 3 is equipped with motor.Be supported with two turning cylinders 7 that are positioned at rotary blade 3 left and right sides between the both sides before and after in the casing 1, wherein be wound with gauze 8 on a turning cylinder 7, the other end of gauze 8 is wrapped on another root turning cylinder 7, all is fixed with motor on two turning cylinders 7; Natural enemy spray tube 5 comprises anti-high-pressure plastic outer tube 9, is provided with the inner metal sleeve pipe 10 that has high-tension electricity in the anti-high-pressure plastic outer tube 9; Rotating disc 6 upper surfaces are laid with some radially-arranged baffle plates 11, and are with the back-up ring 12 that is supported on the rotating disc 6 on the baffle plate 11; Be with shell 13 outside the casing 1, be fixed with pole 14 between shell 13 and the casing 1, pole 14 is provided with separation layer.In the practical implementation process, casing 1 bottom is cone structure, and used motor is stepper motor.
Claims (7)
1. an aircraft is used the natural enemy release; It is characterized in that: comprise setting casing (1) aboard; Casing (1) bottom has liberation port (2); Liberation port (2) locates to be provided with the rotary blade (3) that is mated, and rotary blade (3) below is provided with the end conveyer belt corresponding with its position (4), and the other end below of conveyer belt (4) is provided with the natural enemy spray tube (5) that is positioned at its below; Natural enemy spray tube (5) below is provided with rotating disc (6), and the axle center of rotating disc (6) and rotary blade (3) is equipped with motor.
2. aircraft according to claim 1 is used the natural enemy release; It is characterized in that: be supported with two turning cylinders (7) that are positioned at rotary blade (3) left and right sides between the both sides before and after in the casing (1); Wherein be wound with gauze (8) on the turning cylinder (7); The other end of gauze (8) is wrapped on another root turning cylinder (7), all is fixed with motor on two turning cylinders (7).
3. aircraft according to claim 1 and 2 is used the natural enemy release, it is characterized in that: natural enemy spray tube (5) comprises anti-high-pressure plastic outer tube (9), is provided with the inner metal sleeve pipe (10) that has high-tension electricity in the anti-high-pressure plastic outer tube (9).
4. aircraft according to claim 1 and 2 is used the natural enemy release, it is characterized in that: rotating disc (6) upper surface is laid with some radially-arranged baffle plates (11), and is with the back-up ring (12) that is supported on the rotating disc (6) on the baffle plate (11).
5. aircraft according to claim 3 is used the natural enemy release, it is characterized in that: rotating disc (6) upper surface is laid with some radially-arranged baffle plates (11), and is with the back-up ring (12) that is supported on the rotating disc (6) on the baffle plate (11).
6. aircraft according to claim 1 and 2 is used the natural enemy release, it is characterized in that: casing (1) is outer to be with shell (13), is fixed with pole (14) between shell (13) and the casing (1), and pole (14) is provided with separation layer.
7. aircraft according to claim 5 is used the natural enemy release, it is characterized in that: casing (1) is outer to be with shell (13), is fixed with pole (14) between shell (13) and the casing (1), and pole (14) is provided with separation layer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011203282459U CN202190661U (en) | 2011-09-03 | 2011-09-03 | Natural enemy releaser for aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011203282459U CN202190661U (en) | 2011-09-03 | 2011-09-03 | Natural enemy releaser for aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202190661U true CN202190661U (en) | 2012-04-18 |
Family
ID=45945596
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011203282459U Expired - Fee Related CN202190661U (en) | 2011-09-03 | 2011-09-03 | Natural enemy releaser for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202190661U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103238568A (en) * | 2013-05-13 | 2013-08-14 | 广东省农业科学院植物保护研究所 | Trichogramma releasing solution and releasing method thereof |
| CN105394025A (en) * | 2015-09-21 | 2016-03-16 | 江苏大学 | Degradable ball automatic dropping device used for unmanned plane |
| CN105613483A (en) * | 2015-11-30 | 2016-06-01 | 沈阳金丰春航空科技有限公司 | Trichogramma dispenser |
| CN106516116A (en) * | 2016-09-26 | 2017-03-22 | 江苏大学 | Natural enemy release device used for aircraft |
| CN107372366A (en) * | 2017-08-29 | 2017-11-24 | 遵义市林业科学研究所 | A kind of insect delivery device |
| CN107889798A (en) * | 2017-12-16 | 2018-04-10 | 李竑靓 | A kind of Natural Enemies of Insects delivery device |
-
2011
- 2011-09-03 CN CN2011203282459U patent/CN202190661U/en not_active Expired - Fee Related
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103238568A (en) * | 2013-05-13 | 2013-08-14 | 广东省农业科学院植物保护研究所 | Trichogramma releasing solution and releasing method thereof |
| CN103238568B (en) * | 2013-05-13 | 2015-04-22 | 广东省农业科学院植物保护研究所 | Trichogramma releasing solution and releasing method thereof |
| CN105394025A (en) * | 2015-09-21 | 2016-03-16 | 江苏大学 | Degradable ball automatic dropping device used for unmanned plane |
| WO2017049746A1 (en) * | 2015-09-21 | 2017-03-30 | 江苏大学 | Automatic degradable sphere dropping device for unmanned aerial vehicle |
| GB2558828A (en) * | 2015-09-21 | 2018-07-18 | Univ Jiangsu | Automatic degradable sphere dropping device for unmanned aerial vehicle |
| US10773803B2 (en) | 2015-09-21 | 2020-09-15 | Jiangsu University | Automatic degradable sphere distributing device for unmanned aerial vehicle |
| GB2558828B (en) * | 2015-09-21 | 2021-06-30 | Univ Jiangsu | Automatic degradable sphere distributing device for unmanned aerial vehicle |
| CN105613483A (en) * | 2015-11-30 | 2016-06-01 | 沈阳金丰春航空科技有限公司 | Trichogramma dispenser |
| CN106516116A (en) * | 2016-09-26 | 2017-03-22 | 江苏大学 | Natural enemy release device used for aircraft |
| CN107372366A (en) * | 2017-08-29 | 2017-11-24 | 遵义市林业科学研究所 | A kind of insect delivery device |
| CN107889798A (en) * | 2017-12-16 | 2018-04-10 | 李竑靓 | A kind of Natural Enemies of Insects delivery device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120418 Termination date: 20130903 |