CN109601208A - A kind of aircraft administration device - Google Patents
A kind of aircraft administration device Download PDFInfo
- Publication number
- CN109601208A CN109601208A CN201811386253.1A CN201811386253A CN109601208A CN 109601208 A CN109601208 A CN 109601208A CN 201811386253 A CN201811386253 A CN 201811386253A CN 109601208 A CN109601208 A CN 109601208A
- Authority
- CN
- China
- Prior art keywords
- deceleration
- administration device
- dispensing
- drug
- 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.)
- Withdrawn
Links
- 239000003814 drug Substances 0.000 claims abstract description 5
- 241000282470 Canis latrans Species 0.000 claims abstract description 4
- 239000000203 mixture Substances 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 3
- 238000012913 prioritisation Methods 0.000 description 2
- 241000607479 Yersinia pestis Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 201000010099 disease Diseases 0.000 description 1
- 208000037265 diseases, disorders, signs and symptoms Diseases 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000006187 pill Substances 0.000 description 1
- 239000002689 soil Substances 0.000 description 1
Classifications
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
- A01G13/00—Protecting plants
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/16—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Toxicology (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental Sciences (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Catching Or Destruction (AREA)
Abstract
The present invention relates to a kind of aircraft administration device, including dispensing kit, the dispensing kit bottom is connected with drug-feeding tube, and inclination baffle is provided in the drug-feeding tube；Administration device is connected with the medicine outlet end of drug-feeding tube, and the administration device includes outer housing and is made up of the dispensing shaft that central rotating shaft is connect with outer housing；Coyote hole is offered in the dispensing shaft；Impeller is connected with central rotating shaft one end.During use, after taking off by air push wheel rotation can driving device normal operation, do not need additional consumption energy.
Description
Technical field
The present invention relates to a kind of administration device, in particular to a kind of aircraft administration device.
Background technique
On large area soil pest and disease damage prevent usually using aircraft offer medicine, aircraft dispensing can either save human cost,
The time that dispensing can significantly be shortened again, it can greatly promote the efficiency of dispensing.
Administration device in the prior art usually needs to be equipped with driving device for administration device, can be consumed using driving device
Many aircraft energy.
Summary of the invention
Aiming at the shortcomings in the prior art, the present invention provide a kind of aircraft administration device solved it is existing in the prior art
Technical problem.
Not up to above-mentioned purpose, the present invention adopt the following technical scheme that:
A kind of aircraft administration device, including dispensing kit, the dispensing kit bottom are connected with drug-feeding tube, are provided in the drug-feeding tube
Tilt baffle；Administration device is connected with the medicine outlet end of drug-feeding tube, and the administration device includes outer housing and turned by center
The dispensing shaft composition that axis is connect with outer housing；Coyote hole is offered in the dispensing shaft；Impeller, with central rotating shaft one end phase
Connection.
Preferably, the dispensing shaft is connected with deceleration device far from impeller end.
Preferably, the deceleration device is made of deceleration shell and the deceleration turntable being arranged in deceleration shell, described to subtract
Fast turntable is connect with central rotating shaft.
Preferably, it opens up fluted on the deceleration turntable, deceleration block, described deceleration block one end is installed in the groove
It is hinged on deceleration turntable, the other end is connect with the spring being connected in deceleration turntable.
Preferably, the deceleration block on deceleration turntable is two.
Preferably, the dispensing kit bottom surface of the dispensing kit is taper.
Beneficial effects of the present invention:
During use, after taking off by air push wheel rotation can driving device normal operation, no
Need additional consumption energy.
Detailed description of the invention
Fig. 1 is the overall structure diagram of device；
Fig. 2 is the structural schematic diagram of administration device；
Fig. 3 is the structural schematic diagram of deceleration device；
Description of symbols:
100-dispensing kits, 110-dispensing kit bottom surfaces, 120-drug-feeding tubes, 130-inclination baffles,
200-administration devices, 210-outer housings, 220-dispensing shafts, 230-coyote holes, 240-central rotating shafts, 300-are slowed down
Device, 310-deceleration shells, 320-deceleration blocks, 330-springs, 340-deceleration turntables, 400-impellers.
Specific embodiment
To make those skilled in the art better understand technical solution of the present invention, specific embodiment is given below
The present invention is made further instructions.
A kind of aircraft administration device of the present invention, including dispensing kit 100,100 bottom of dispensing kit are connected with drug-feeding tube
120, inclination baffle 130 is provided in the drug-feeding tube 120；
Administration device 200 is connected with the medicine outlet end of drug-feeding tube 120, and the administration device 120 includes outer housing 210 and leads to
The dispensing shaft 220 that central rotating shaft 240 is connect with outer housing 210 is crossed to form；Coyote hole 230 is offered in the dispensing shaft 220；
Impeller 400 is connected with 240 one end of central rotating shaft.During use, pass through air push impeller after taking off
Rotation can driving device normal operation, do not need additional consumption energy.
As a kind of prioritization scheme of the invention, the dispensing shaft 240 is connected with deceleration device far from 400 end of impeller.
Further, the 300 deceleration shell 310 of deceleration device and the deceleration turntable 340 being arranged in deceleration shell 310 form, institute
Deceleration turntable 340 is stated to connect with central rotating shaft 240.Further, fluted, the groove is opened up on the deceleration turntable 340
Deceleration block 320 is inside installed, described 320 one end of deceleration block is hinged on deceleration turntable 340, the other end and is connected to deceleration turntable
Spring 330 in 340 connects.Deceleration block 320 on deceleration turntable 340 is two.After using deceleration device, work as wheel speed
When too fast, the inner wall of deceleration block meeting friction eceleration shell is timely adjusted under the influence of centrifugal force to reduce wheel speed
The quantity of dispensing.
As a kind of prioritization scheme of the invention, the dispensing kit bottom surface 110 of the dispensing kit 100 is taper.Using taper
Design structure the pill in dispensing kit can be made smoothly to flow out, avoid it from remaining in cabinet.
Embodiments of the present invention are explained in detail above in conjunction with attached drawing, but the present invention is not limited to above-mentioned implementations
Mode can also be made without departing from the purpose of the present invention within the knowledge of those skilled in the art
Various change.
Claims (6)
1. a kind of aircraft administration device, comprising:
Dispensing kit (100), dispensing kit (100) bottom are connected with drug-feeding tube (120), are provided in the drug-feeding tube (120)
It tilts baffle (130)；
Administration device (200) is connected with the medicine outlet end of drug-feeding tube (120), and the administration device (120) includes outer housing
(210) and by central rotating shaft (240) dispensing shaft (220) composition being connect with outer housing (210)；The dispensing shaft
(220) coyote hole (230) are offered on；
Impeller (400) is connected with central rotating shaft (240) one end.
2. aircraft administration device according to claim 1, it is characterised in that: the dispensing shaft (240) is far from impeller
(400) end is connected with deceleration device.
3. aircraft administration device according to claim 2, it is characterised in that: the deceleration device (300) is by deceleration shell
(310) it is formed with deceleration turntable (340) of the setting in deceleration shell (310), the deceleration turntable (340) and central rotating shaft
(240) it connects.
4. aircraft administration device according to claim 3, it is characterised in that: offered on the deceleration turntable (340) recessed
Slot is equipped with deceleration block (320) in the groove, and described deceleration block (320) one end is hinged on deceleration turntable (340), another
Hold and be connected to spring (330) connection in deceleration turntable (340).
5. aircraft administration device according to claim 4, it is characterised in that: the deceleration block (320) on deceleration turntable (340)
It is two.
6. aircraft administration device according to claim 1, it is characterised in that: the dispensing kit bottom surface of the dispensing kit (100)
It (110) is taper.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811386253.1A CN109601208A (en) | 2018-11-20 | 2018-11-20 | A kind of aircraft administration device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811386253.1A CN109601208A (en) | 2018-11-20 | 2018-11-20 | A kind of aircraft administration device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109601208A true CN109601208A (en) | 2019-04-12 |
Family
ID=66004513
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811386253.1A Withdrawn CN109601208A (en) | 2018-11-20 | 2018-11-20 | A kind of aircraft administration device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109601208A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110734103A (en) * | 2019-11-11 | 2020-01-31 | 佛山科学技术学院 | dosing device for water pollution treatment |
| CN112896515A (en) * | 2021-01-21 | 2021-06-04 | 深圳市爱速客自动化设备有限公司 | Unmanned aerial vehicle ware of jettisoninging |
-
2018
- 2018-11-20 CN CN201811386253.1A patent/CN109601208A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110734103A (en) * | 2019-11-11 | 2020-01-31 | 佛山科学技术学院 | dosing device for water pollution treatment |
| CN112896515A (en) * | 2021-01-21 | 2021-06-04 | 深圳市爱速客自动化设备有限公司 | Unmanned aerial vehicle ware of jettisoninging |
| CN112896515B (en) * | 2021-01-21 | 2022-07-05 | 深圳市爱速客自动化设备有限公司 | Unmanned aerial vehicle ware of jettisoninging |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20190412 |