CN205256678U - Gentle wing unmanned vehicles of fog dispersal - Google Patents
Gentle wing unmanned vehicles of fog dispersal Download PDFInfo
- Publication number
- CN205256678U CN205256678U CN201521038807.0U CN201521038807U CN205256678U CN 205256678 U CN205256678 U CN 205256678U CN 201521038807 U CN201521038807 U CN 201521038807U CN 205256678 U CN205256678 U CN 205256678U
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- China
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- fog dispersal
- baffle
- fog
- agent case
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Abstract
The utility model relates to a gentle wing unmanned vehicles of fog dispersal, including airframe, be provided with flexible punching press parafoil on the airframe both sides, the inside fog dispersal agent case that is equipped with of airframe, the inside one side of airframe is provided with generator assembly, the generator assembly output is connected with the screw, fog dispersal agent case upper end is equipped with the feed cap board, and the lower extreme is equipped with the relief hole, fog dispersal agent incasement portion is provided with first baffle, second baffle, staggered arrangement between first baffle, the second baffle, fog dispersal agent incasement portion is equipped with row material bladed disk, it arranges the silo to be equipped with a plurality of on row's material bladed disk circumferencial direction. 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 the soft wing unmanned vehicle of a kind of fog dispersal.
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 flexible ram air parachute machine, 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 a kind of fog dispersal soft wing unmanned vehicle.
The utility model is to be achieved through the following technical solutions:
The soft wing unmanned vehicle of a kind of fog dispersal, comprise aircraft body, described aircraft body is provided with flexible ram air parachute on both sides, described aircraft internal body is provided with antifogging agent case, described aircraft internal body one side is provided with generator assembly, described generator assembly output is connected with screw, described antifogging agent case upper end is provided with charging cover plate, lower end is provided with relief hole, described antifogging agent case inside is provided with the first baffle plate, second baffle, described the first baffle plate, interlaced arrangement between second baffle, described antifogging agent case inside is provided with discharge leaf dish, described discharge leaf dish circumferencial direction is provided with several discharge grooves.
As optimal technical scheme of the present utility model, described the first baffle plate lower end is positioned at second baffle upper end.
As optimal technical scheme of the present utility model, described the first baffle plate, second baffle are and are in tilted layout.
As optimal technical scheme of the present utility model, between described antifogging agent case and discharge leaf dish for key is connected.
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 generator assembly in flight course drives screw High Rotation Speed, be convenient to the flight of unmanned plane, in flight course, discharge leaf dish High Rotation Speed is discharged antifogging agent to 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;
Fig. 2 is A place partial enlarged drawing in Fig. 1.
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. 2, Fig. 1 is structural representation of the present utility model; Fig. 2 is A place partial enlarged drawing in Fig. 1.
The soft wing unmanned vehicle of a kind of fog dispersal, comprise aircraft body 1, described aircraft body is provided with flexible ram air parachute 2 on 1 both sides, described aircraft body 1 inside is provided with antifogging agent case 3, the inner side of described aircraft body 1 is provided with generator assembly 4, described generator assembly 4 outputs are connected with screw 5, described antifogging agent case 3 upper ends are provided with charging cover plate 301, lower end is provided with relief hole 302, described antifogging agent case 3 inside are provided with the first baffle plate 6, second baffle 7, wherein said the first baffle plate 6 lower ends are positioned at second baffle 7 upper ends, and described the first baffle plate 6, second baffle 7 is and is in tilted layout, be convenient to so the smooth discharge of antifogging agent.
Interlaced arrangement between described the first baffle plate 6, second baffle 7, described antifogging agent case 3 inside are provided with discharge leaf dish 8, between wherein said antifogging agent case 3 and discharge leaf dish 8 for key is connected, described discharge leaf dish 8 circumferencial directions are provided with several discharge grooves 801, discharge leaf dish 8 High Rotation Speeds are discharged antifogging agent like this, realize fog dispersal.
Its detailed description of the invention is: while use like this, unmanned plane during flying is to aerial, now flexible ram air parachute 2 is opened, unmanned plane generator assembly 4 in flight course drives screw 5 High Rotation Speeds, be convenient to the flight of unmanned plane, in flight course, discharge leaf dish 8 High Rotation Speeds are discharged antifogging agent to realize mist are fallen in atmosphere, cost is low like this, the scope of application is wide, every situation that needs subrange fog dispersal that relates to, for example improve highway communication environment, eliminate 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. the soft wing unmanned vehicle of fog dispersal, comprise aircraft body (1), described aircraft body (1) is provided with flexible ram air parachute (2) on both sides, described aircraft body (1) inside is provided with antifogging agent case (3), the inner side of described aircraft body (1) is provided with generator assembly (4), described generator assembly (4) output is connected with screw (5), described antifogging agent case (3) upper end is provided with charging cover plate (301), lower end is provided with relief hole (302), it is characterized in that: described antifogging agent case (3) inside is provided with the first baffle plate (6), second baffle (7), described the first baffle plate (6), interlaced arrangement between second baffle (7), described antifogging agent case (3) inside is provided with discharge leaf dish (8), described discharge leaf dish (8) circumferencial direction is provided with several discharge grooves (801).
2. the soft wing unmanned vehicle of fog dispersal according to claim 1, is characterized in that: described the first baffle plate (6) lower end is positioned at second baffle (7) upper end.
3. the soft wing unmanned vehicle of fog dispersal according to claim 1, is characterized in that: described the first baffle plate (6), second baffle (7) are and are in tilted layout.
4. the soft wing unmanned vehicle of fog dispersal according to claim 1, is characterized in that: between described antifogging agent case (3) and discharge leaf dish (8) for key is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521038807.0U CN205256678U (en) | 2015-12-15 | 2015-12-15 | Gentle wing unmanned vehicles of fog dispersal |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201521038807.0U CN205256678U (en) | 2015-12-15 | 2015-12-15 | Gentle wing unmanned vehicles of fog dispersal |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205256678U true CN205256678U (en) | 2016-05-25 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201521038807.0U Expired - Fee Related CN205256678U (en) | 2015-12-15 | 2015-12-15 | Gentle wing unmanned vehicles of fog dispersal |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205256678U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105383698A (en) * | 2015-12-15 | 2016-03-09 | 谷家菊 | Fog-dissipation unmanned aerial vehicle with flexible wings |
-
2015
- 2015-12-15 CN CN201521038807.0U patent/CN205256678U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105383698A (en) * | 2015-12-15 | 2016-03-09 | 谷家菊 | Fog-dissipation unmanned aerial vehicle with flexible wings |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160525 Termination date: 20161215 |