CN204341400U - Fixed-wing unmanned plane carry formula atomizing cone - Google Patents
Fixed-wing unmanned plane carry formula atomizing cone Download PDFInfo
- Publication number
- CN204341400U CN204341400U CN201420677370.4U CN201420677370U CN204341400U CN 204341400 U CN204341400 U CN 204341400U CN 201420677370 U CN201420677370 U CN 201420677370U CN 204341400 U CN204341400 U CN 204341400U
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- CN
- China
- Prior art keywords
- aerofoil profile
- profile arm
- unmanned plane
- carry
- atomizing cone
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- 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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- Catching Or Destruction (AREA)
- Special Spraying Apparatus (AREA)
Abstract
The utility model relates to a kind of fixed-wing unmanned plane carry formula atomizing cone, is mainly used in fixed-wing unmanned plane and carries and carry out spraying operation.Be made up of casing (1), electrokinetic cell (2), motor-drive pump (3), remote speed regulating device (4), atomizer (5), aerofoil profile arm (6), carry frame (7) etc.The electrokinetic cell of this device is chargeable lithium cell, controls motor-drive pump by the liquid medicine press-in aerofoil profile arm in casing, realize the Long-distance Control to spray amount by remote speed regulating device; Liquid medicine, is mixed from the ejection of aerofoil profile arm trailing edge by the wake flow of aerofoil profile arm afterbody again by atomizer; The design of aerofoil profile arm can provide extra lift in flight way; Carry frame can realize the adjustment of the aerofoil profile arm angle of attack.
Description
Technical field
The utility model relates to a kind of fixed-wing unmanned plane carry formula atomizing cone, can adapt to multiple fixed-wing unmanned plane carry to realize spraying operation.
Background technology
The application of current unmanned plane is in the fast-developing stage, the flight operation of unmanned function well competent agricultural, forestry, animal husbandry, fish production and rescue and relief work.But in spraying operation, because the weight of atomising installation with the liquid medicine carried and can control to produce very large harmful effect to fixed-wing unmanned plane during flying, also there is no a Portable spray device being applicable to multiple fixed-wing unmanned plane carry at present.Existing atomising installation needs can carry through repacking to a certain degree unmanned plane.Therefore being badly in need of designing a kind of atomising installation that can be applicable to multiple fixed-wing UAV flight, well can realizing spraying operation, also without the need to reequiping unmanned plane.
Summary of the invention
The purpose of this utility model is to provide a kind of fixed-wing unmanned plane carry formula atomising installation, can the angle of attack of aerofoil profile arm be regulated to be suitable for different fixed-wing unmanned aerial vehicle lift-launchs by fast speed; Certain lift can be provided for atomising installation, reduce the weight of atomizing cone itself to the impact of unmanned plane; Atomizer is placed in aerofoil profile arm afterbody, utilizes the further mixing material medicine of its flow-disturbing; Remote speed regulating device to the remote real_time control of spraying flow velocity, can complete the spraying operation of high load-carrying.
Technical solutions of the utility model are such:
The utility model is made up of casing, electrokinetic cell, motor-drive pump, remote speed regulating device, atomizer, aerofoil profile arm, carry frame etc.
Carry frame is fixed on below the wing of unmanned plane, the angle of attack of quick adjustment aerofoil profile arm can adapt to different fixed-wing unmanned planes by regulating carry frame.
Adopt rechargeable lithium battary as electrokinetic cell for this device provides the energy.
Motor-drive pump is controlled by the liquid medicine press-in aerofoil profile arm in casing by remote speed regulating device, spray from aerofoil profile arm afterbody after liquid medicine is atomized by atomizer, again mixed by the wake flow of aerofoil profile arm afterbody, the design of aerofoil profile arm simultaneously can provide extra lift for unmanned plane in flight course.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model
Fig. 2 is the structural representation of aerofoil profile arm
Fig. 3 is the structural representation of the carry device of variable incidence
Fig. 4 is the schematic diagram of mechanism of the carry device of variable incidence
As in Fig. 1, casing (1), electrokinetic cell (2), motor-drive pump (3), long-range speed-controlling device (4), atomizer (5), aerofoil profile arm (6), carry frame (7).
Detailed description of the invention
Below in conjunction with accompanying drawing, the utility model is described in further detail with enforcement:
One, overall
Powered by electrokinetic cell (2), long-range speed-controlling device (4) is realized Long-distance Control motor-drive pump (3) and the liquid medicine in casing (1) is pressed into aerofoil profile arm (6) and is sprayed from aerofoil profile arm (6) trailing edge by atomizer (5).When atomising installation carry is installed, realized the quick adjustment of aerofoil profile arm (6) angle of attack by the graduated carry frame (7) of accommodation zone.
Two, each parts
As Fig. 2, the resistance of air-flow, in motion process, can be partially converted into lift by aerofoil profile arm (6), and liquid medicine can by some atomizers (5) ejection of the main support tube tail end of aerofoil profile arm (6) simultaneously.
As Fig. 4, the slide block of carry frame (7) 1. can move at the graduated support Linear of band, and 3. drivening rod rotates, and realizes the quick adjustment being arranged on aerofoil profile arm (6) angle of attack that 3. bar is gone up.
Claims (4)
1. fixed-wing unmanned plane carry formula atomizing cone, by casing (1), electrokinetic cell (2), motor-drive pump (3), remote speed regulating device (4), atomizer (5), aerofoil profile arm (6), carry frame (7) forms, atomizer is installed on aerofoil profile arm trailing edge, aerofoil profile arm is fixed on carry frame, powered by electrokinetic cell, remote speed regulating device is realized Long-distance Control motor-drive pump and the liquid medicine in casing is pressed into aerofoil profile arm and is sprayed from aerofoil profile arm trailing edge by atomizer, when atomizing cone carry is installed, the quick adjustment of the aerofoil profile arm angle of attack is realized by the graduated carry frame of accommodation zone, fixed-wing unmanned plane carry formula atomizing cone is a kind of atomizing cone adapting to the carry formula of multiple fixed-wing unmanned plane, realization can the spraying operation of long-range real-time adjustable spraying flow velocity.
2. atomizing cone according to claim 1, is characterized in that, aerofoil profile arm can provide lift in flight course, when unmanned plane power is enough, to a certain degree can offset the impact of atomizing cone weight on unmanned plane during flying.
3. atomizing cone according to claim 1, is characterized in that, atomizer is placed in aerofoil profile arm afterbody, while aerosolize liquid drug, utilizes wake flow mixing material medicine further.
4. atomizing cone according to claim 1, is characterized in that, the angle of attack of carry frame adjustable sprayer aerofoil profile arm, adapts to the angle of attack of different fixed-wing unmanned plane wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420677370.4U CN204341400U (en) | 2014-11-04 | 2014-11-04 | Fixed-wing unmanned plane carry formula atomizing cone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420677370.4U CN204341400U (en) | 2014-11-04 | 2014-11-04 | Fixed-wing unmanned plane carry formula atomizing cone |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204341400U true CN204341400U (en) | 2015-05-20 |
Family
ID=53224690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420677370.4U Expired - Fee Related CN204341400U (en) | 2014-11-04 | 2014-11-04 | Fixed-wing unmanned plane carry formula atomizing cone |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204341400U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892116A (en) * | 2017-02-27 | 2017-06-27 | 四川雷神空天科技有限公司 | For the flight instruments platform and its system and operational method of plant protection operation |
| CN107433235A (en) * | 2017-08-16 | 2017-12-05 | 市下控股有限公司 | A kind of Portable electric atomizer |
-
2014
- 2014-11-04 CN CN201420677370.4U patent/CN204341400U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892116A (en) * | 2017-02-27 | 2017-06-27 | 四川雷神空天科技有限公司 | For the flight instruments platform and its system and operational method of plant protection operation |
| CN107433235A (en) * | 2017-08-16 | 2017-12-05 | 市下控股有限公司 | A kind of Portable electric atomizer |
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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: 20150520 Termination date: 20161104 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |