CN205256679U - Gentle wing unmanned vehicles of fog dispersal function has - Google Patents
Gentle wing unmanned vehicles of fog dispersal function has Download PDFInfo
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- CN205256679U CN205256679U CN201521039080.8U CN201521039080U CN205256679U CN 205256679 U CN205256679 U CN 205256679U CN 201521039080 U CN201521039080 U CN 201521039080U CN 205256679 U CN205256679 U CN 205256679U
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Abstract
The utility model relates to a gentle wing unmanned vehicles of fog dispersal function has, including airframe, be provided with the stationary vane on the airframe both sides, the inside one side of airframe is provided with generator assembly, the generator assembly output is connected with the screw, the airframe upside is connected with flexible punching press parafoil, be equipped with a plurality of inlet port on the airframe lateral wall, the subassembly is scattered to inside being equipped with of airframe, be provided with external fog dispersal equipment on each stationary vane. The utility model discloses with low costs, application range is wide, every condition that needs the subrange fog dispersal that relates to, for example improve road traffic environment, eliminate the airport thick fog, improve the regional local conditions etc. Of providing disaster relief, all can be suitable for.
Description
Technical field
The utility model relates to unmanned plane technical field, relates in particular to one and has the soft wing unmanned vehicle of fog dispersal function.
Background technology
UAV is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft that utilizes radio robot and the presetting apparatus of providing for oneself to handle. Can be divided into from technical standpoint definition: depopulated helicopter, unmanned fixed-wing aircraft, unmanned multi-rotor aerocraft, unmanned airship, unmanned parasol etc.
Unmanned plane, by application, can be divided into military and civilian. Military aspect, unmanned plane is divided into reconnaissance plane and target drone. The sector application of unmanned plane is the real firm need of unmanned plane. At present taking photo by plane, the application in the field such as agricultural plant protection, mapping, expanded greatly the purposes of unmanned plane itself. In addition, many model telecontrolled aircrafts are also referred to as unmanned plane.
In aircraft field, so-called arrtificial fog dissipation refers to eliminates droplet in regional area to improve the method for visibility by the mode of artificial affecting. Particularly, with certain equipment, the catalyst such as silver iodide, dry ice, liquefied propane are sowed in mist, produce a large amount of ice crystals, steam in fog-zone is sublimated on numerous ice crystals, impels supercooling water droplet evaporation, and the moisture that ice crystal is captured former droplet is constantly grown up, ice crystal drops to ground after growing up, thereby mist is disappeared. General direct employing aircraft seeding cost is high, if adopt shell to sow and can be subject to wind direction and air speed influence, and multiple catalyst are set in fog-zone, and to sow the man power and material of a consumption huge.
Utility model content
The purpose of this utility model is in order to overcome the deficiencies in the prior art, provides one to have the soft wing unmanned vehicle of fog dispersal function.
The utility model is to be achieved through the following technical solutions:
One has the soft wing unmanned vehicle of fog dispersal function, comprise aircraft body, described aircraft body is provided with fixed-wing on both sides, described aircraft internal body one side is provided with generator assembly, described generator assembly output is connected with screw, and described aircraft body upside is connected with flexible ram air parachute, and described aircraft organism sidewall is provided with several air admission holes, described aircraft internal body is provided with sows assembly, is provided with external fog dispersal equipment on described each fixed-wing.
As optimal technical scheme of the present utility model, described air admission hole reduces gradually from outside to inner side area of section.
As optimal technical scheme of the present utility model, described in sow assembly and comprise rotating shaft, sow blade, described in sow blade and be evenly distributed in rotating shaft.
As optimal technical scheme of the present utility model, between described external fog dispersal equipment and each fixed-wing for removably connecting.
Compared with prior art, the beneficial effects of the utility model are: the utility model is by arranging air admission hole, sow assembly and external fog dispersal equipment, while use like this, unmanned plane during flying is to aerial, now flexible ram air parachute is opened, unmanned plane air in flight course enters internal body from air admission hole, drive is sowed assembly rotation antifogging agent is sowed in air, external fog dispersal equipment is also sowed simultaneously, realize mist is fallen in atmosphere, cost is low like this, the scope of application is wide, every situation that needs subrange fog dispersal that relates to, environment for example improves highway communication, eliminate airport thick fog, improve disaster relief region miniclimate etc., all can be suitable for.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the utility model is further elaborated. Should be appreciated that specific embodiment described herein is only in order to explain the utility model, and be not used in restriction the utility model.
Refer to Fig. 1, Fig. 1 is structural representation of the present utility model.
One has the soft wing unmanned vehicle of fog dispersal function, comprise aircraft body 1, described aircraft body is provided with fixed-wing 2 on 1 both sides, the inner side of described aircraft body 1 is provided with generator assembly 3, described generator assembly 3 outputs are connected with screw 4, described aircraft body 1 upside is connected with flexible ram air parachute 7, described aircraft body 1 sidewall is provided with several air admission holes 101, wherein said air admission hole 101 reduces gradually from outside to inner side area of section, like this can air enter.
Described aircraft body 1 inside is provided with sows assembly 5, and the wherein said assembly 5 of sowing comprises rotating shaft 501, sows blade 502, described in sow blade 502 and be evenly distributed in rotating shaft 501, sow like this assembly 5 and can realize the discharge of antifogging agent. On described each fixed-wing 2, be provided with external fog dispersal equipment 6, between wherein said external fog dispersal equipment 6 and each fixed-wing 2 for removably connecting, the installation and removal of external like this fog dispersal equipment 6.
Its detailed description of the invention is: while use like this, unmanned plane during flying is to aerial, now flexible ram air parachute 7 is opened, unmanned plane air in flight course enters internal body from air admission hole 101, drive is sowed assembly 5 and is rotated antifogging agent is sowed in air, external fog dispersal equipment 6 is also sowed simultaneously, realize mist is fallen in atmosphere, cost is low like this, the scope of application is wide, every situation that needs subrange fog dispersal that relates to, the environment that for example improves highway communication, elimination airport thick fog, improve disaster relief region miniclimate etc., all can be suitable for.
In description of the present utility model, it will be appreciated that, term " orientation or the position relationship of the instruction such as " center ", " top ", " end ", " interior ", " outward " be based on orientation shown in the drawings or position relationship; be only the utility model and simplified characterization for convenience of description; instead of the device of instruction or hint indication or element must have specific orientation, with specific orientation structure with operate, therefore can not be interpreted as restriction of the present utility model.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all any amendments of doing within spirit of the present utility model and principle, be equal to and replace and improvement etc., within all should being included in protection domain of the present utility model.
Claims (4)
1. one kind has the soft wing unmanned vehicle of fog dispersal function, comprise aircraft body (1), described aircraft body (1) is provided with fixed-wing (2) on both sides, the inner side of described aircraft body (1) is provided with generator assembly (3), described generator assembly (3) output is connected with screw (4), described aircraft body (1) upside is connected with flexible ram air parachute (7), it is characterized in that: described aircraft body (1) sidewall is provided with several air admission holes (101), described aircraft body (1) inside is provided with sows assembly (5), on described each fixed-wing (2), be provided with external fog dispersal equipment (6).
2. according to claim 1 have a soft wing unmanned vehicle of fog dispersal function, it is characterized in that: described air admission hole (101) reduces gradually from outside to inner side area of section.
3. according to claim 1 have a soft wing unmanned vehicle of fog dispersal function, it is characterized in that: described in sow assembly (5) and comprise rotating shaft (501), sow blade (502), described in sow blade (502) and be evenly distributed in rotating shaft (501).
4. according to claim 1 have a soft wing unmanned vehicle of fog dispersal function, it is characterized in that: between described external fog dispersal equipment (6) and each fixed-wing (2) for removably connecting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521039080.8U CN205256679U (en) | 2015-12-15 | 2015-12-15 | Gentle wing unmanned vehicles of fog dispersal function has |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521039080.8U CN205256679U (en) | 2015-12-15 | 2015-12-15 | Gentle wing unmanned vehicles of fog dispersal function has |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205256679U true CN205256679U (en) | 2016-05-25 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521039080.8U Expired - Fee Related CN205256679U (en) | 2015-12-15 | 2015-12-15 | Gentle wing unmanned vehicles of fog dispersal function has |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205256679U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105366055A (en) * | 2015-12-15 | 2016-03-02 | 谷家菊 | Flexible-wing unmanned aerial vehicle with fog dispersal function |
-
2015
- 2015-12-15 CN CN201521039080.8U patent/CN205256679U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105366055A (en) * | 2015-12-15 | 2016-03-02 | 谷家菊 | Flexible-wing unmanned aerial vehicle with fog dispersal function |
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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: 20160525 Termination date: 20161215 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |