CN105383698A - Fog-dissipation unmanned aerial vehicle with flexible wings - Google Patents
Fog-dissipation unmanned aerial vehicle with flexible wings Download PDFInfo
- Publication number
- CN105383698A CN105383698A CN201510928752.9A CN201510928752A CN105383698A CN 105383698 A CN105383698 A CN 105383698A CN 201510928752 A CN201510928752 A CN 201510928752A CN 105383698 A CN105383698 A CN 105383698A
- Authority
- CN
- China
- Prior art keywords
- fog
- aerial vehicle
- antifogging agent
- baffle
- unmanned aerial
- 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.)
- Pending
Links
- 238000007599 discharging Methods 0.000 abstract 4
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 239000003795 chemical substances by application Substances 0.000 description 14
- 239000013078 crystal Substances 0.000 description 4
- 239000003595 mist Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- ATUOYWHBWRKTHZ-UHFFFAOYSA-N Propane Chemical compound CCC ATUOYWHBWRKTHZ-UHFFFAOYSA-N 0.000 description 2
- 239000003054 catalyst Substances 0.000 description 2
- 238000004891 communication Methods 0.000 description 2
- 230000008030 elimination Effects 0.000 description 2
- 238000003379 elimination reaction Methods 0.000 description 2
- JKFYKCYQEWQPTM-UHFFFAOYSA-N 2-azaniumyl-2-(4-fluorophenyl)acetate Chemical compound OC(=O)C(N)C1=CC=C(F)C=C1 JKFYKCYQEWQPTM-UHFFFAOYSA-N 0.000 description 1
- CURLTUGMZLYLDI-UHFFFAOYSA-N Carbon dioxide Chemical compound O=C=O CURLTUGMZLYLDI-UHFFFAOYSA-N 0.000 description 1
- 229910021612 Silver iodide Inorganic materials 0.000 description 1
- 235000011089 carbon dioxide Nutrition 0.000 description 1
- 238000012512 characterization method Methods 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000001704 evaporation Methods 0.000 description 1
- 230000008020 evaporation Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000010899 nucleation Methods 0.000 description 1
- 239000001294 propane Substances 0.000 description 1
- 229940045105 silver iodide Drugs 0.000 description 1
- 238000009331 sowing Methods 0.000 description 1
Classifications
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/30—Wings comprising inflatable structural components
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Catching Or Destruction (AREA)
Abstract
The invention relates to a fog-dissipation unmanned aerial vehicle with flexible wings. The fog-dissipation unmanned aerial vehicle with the flexible wings comprises an aerial vehicle body, wherein flexible ram air parachutes are arranged on two sides of the aerial vehicle body; an antifogging agent box is arranged in the aerial vehicle body; a generator assembly is arranged on one side of the inside of the aerial vehicle body; an outputting end of the generator assembly is connected with a propeller; a feeding cover plate is arranged at the upper end of the antifogging agent box; a discharging hole is formed in the lower end of the antifogging agent box; a first baffle and a second baffle are arranged in the antifogging agent box and are distributed in a staggered manner; a discharging leaf disc is arranged in the antifogging agent box; and a plurality of discharging grooves are formed in the discharging leaf disc in the peripheral direction. The fog-dissipation unmanned aerial vehicle is low in cost and wide in using range, and is suitable for dissipating fog of local scopes, for example, the fog-dissipation unmanned aerial vehicle can be used for improving a traffic environment of a road, dissipating dense fog of an airport, improving the microclimate of a disaster relief region, and the like.
Description
Technical field
This
inventionrelate to unmanned air vehicle technique field, particularly relate to
the soft wing unmanned vehicle of a kind of fog dispersal.
Background technology
Robot airplane is called for short " unmanned plane ", and english abbreviation is " UAV ", is the not manned aircraft utilizing radio robot to handle with the process controller provided for oneself.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 scout and target drone.The sector application of unmanned plane is the real firm need of unmanned plane.At present taking photo by plane, agricultural plant protection, the field such as mapping application, expanded the purposes of unmanned plane itself greatly.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 visbility by the mode of artificial affecting.Specifically, with certain equipment, the catalyst such as silver iodide, dry ice, liquid propane are sowed in mist, produce a large amount of ice crystal, steam in fog-zone is sublimated on numerous ice crystals, impels over cooling water-drop evaporation, and the moisture that namely ice crystal captures former droplet is constantly grown up, ice crystal drops to ground after growing up, thus 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 arrange multiple catalyst to sow a man power and material consumed huge in fog-zone.
Summary of the invention
This
inventionobject be to overcome the deficiencies in the prior art, provide
the soft wing unmanned vehicle of a kind of fog dispersal.
This
inventionbe achieved through the following technical solutions:
the soft wing unmanned vehicle of a kind of fog dispersal, comprise aircraft body, described aircraft body both sides are provided with flexible ram air parachute, described aircraft body inside is provided with antifogging agent case, the inner side of described aircraft body is provided with generator assembly, described generator assembly mouth is connected with screw propeller, 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 first baffle plate, alternative arrangement between second baffle, described antifogging agent case inside is provided with discharge leaf dish, described discharge leaf dish is circumferentially provided with several discharge grooves.
As this
inventionoptimal technical scheme, described first baffle plate lower end position is in second baffle upper end.
As this
inventionoptimal technical scheme, described first baffle plate, second baffle are in being in tilted layout.
As this
inventionoptimal technical scheme, for key is connected between described antifogging agent case with discharge leaf dish.
Compared with prior art, originally
inventionbeneficial effect be: this
inventionby arranging induction opening, sowing assembly and external fog dispersal equipment, during such use, unmanned plane during flying is to aerial, now flexible ram air parachute is opened, unmanned plane is generator assembly carrying screws High Rotation Speed in flight course, be convenient to the flight of unmanned plane, in flight course, antifogging agent is discharged and is realized falling mist to air by discharge leaf dish High Rotation Speed, such cost is low, range of use is wide, everyly relates to the situation needing subrange disperse fog, the environment that such as improves highway communication, elimination airport thick fog, improve disaster relief region micrclimate etc., all can be suitable for.
Accompanying drawing explanation
fig. 1for this
inventionstructural representation
figure;
fig. 2for
fig. 1middle A place partial enlargement
figure.
Detailed description of the invention
In order to make this
inventionobject, technical scheme and advantage clearly understand, below in conjunction with
accompanying drawingand embodiment, to this
inventionbe further elaborated.Should be appreciated that specific embodiment described herein only in order to explain this
invention, and be not used in restriction originally
invention.
Refer to
fig. 1,
fig. 2,
fig. 1for this
inventionstructural representation
figure;
fig. 2for
fig. 1middle A place partial enlargement
figure.
the soft wing unmanned vehicle of a kind of fog dispersal, comprise aircraft body 1, described aircraft body 1 both sides are provided with flexible ram air parachute 2, described aircraft body 1 inside is provided with antifogging agent case 3, the described inner side of aircraft body 1 is provided with generator assembly 4, described generator assembly 4 mouth is connected with screw propeller 5, described antifogging agent case 3 upper end is provided with charging cover plate 301, lower end is provided with relief hole 302, described antifogging agent case 3 inside is provided with the first baffle plate 6, second baffle 7, wherein said first baffle plate 6 lower end is positioned at second baffle 7 upper end, and described first baffle plate 6, second baffle 7 is in being in tilted layout, be convenient to the smooth discharge of antifogging agent like this.
Alternative arrangement between described first baffle plate 6, second baffle 7, described antifogging agent case 3 inside is provided with discharge leaf dish 8, for key is connected between wherein said antifogging agent case 3 with discharge leaf dish 8, described discharge leaf dish 8 is circumferentially provided with several discharge grooves 801, antifogging agent is discharged by such discharge leaf dish 8 High Rotation Speed, realizes fog dispersal.
Its detailed description of the invention is: when using like this, unmanned plane during flying is to aerial, now flexible ram air parachute 2 is opened, unmanned plane is generator assembly 4 carrying screws 5 High Rotation Speed in flight course, be convenient to the flight of unmanned plane, in flight course, antifogging agent is discharged and is realized falling mist to air by discharge leaf dish 8 High Rotation Speed, such cost is low, range of use is wide, everyly relate to the situation needing subrange to disperse fog, such as improve highway communication environment, elimination airport thick fog, improves disaster relief region micrclimate etc., all can be suitable for.
At this
inventiondescription in, it is to be appreciated that term " orientation of the instruction such as " center ", " top ", " end ", " interior ", " outward " or position relationship be based on
accompanying drawing institutethe orientation shown or position relationship are only for convenience of description originally
inventionand simplified characterization, instead of instruction or hint indication device or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as to this
inventionrestriction.
The foregoing is only this
inventionpreferred embodiment, not in order to restriction this
invention, all at this
inventionspirit and principle within do any amendment, equivalent to replace and improvement etc., all should be included in this
inventionprotection domain within.
Claims (4)
1. the soft wing unmanned vehicle of fog dispersal, comprise aircraft body (1), described aircraft body (1) both sides are provided with flexible ram air parachute (2), described aircraft body (1) inside is provided with antifogging agent case (3), described aircraft body (1) inner side is provided with generator assembly (4), described generator assembly (4) mouth is connected with screw propeller (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 first baffle plate (6), alternative arrangement between second baffle (7), described antifogging agent case (3) inside is provided with discharge leaf dish (8), described discharge leaf dish (8) is circumferentially provided with several discharge grooves (801).
2. the soft wing unmanned vehicle of fog dispersal according to claim 1, is characterized in that: described 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 first baffle plate (6), second baffle (7) are in being in tilted layout.
4. the soft wing unmanned vehicle of fog dispersal according to claim 1, is characterized in that: described antifogging agent case (3) with between discharge leaf dish (8) for key is connected.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510928752.9A CN105383698A (en) | 2015-12-15 | 2015-12-15 | Fog-dissipation unmanned aerial vehicle with flexible wings |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510928752.9A CN105383698A (en) | 2015-12-15 | 2015-12-15 | Fog-dissipation unmanned aerial vehicle with flexible wings |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105383698A true CN105383698A (en) | 2016-03-09 |
Family
ID=55416597
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510928752.9A Pending CN105383698A (en) | 2015-12-15 | 2015-12-15 | Fog-dissipation unmanned aerial vehicle with flexible wings |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105383698A (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2696295Y (en) * | 2004-02-17 | 2005-05-04 | 王晓望 | Automatic fertilizing machine |
| CN101195994A (en) * | 2007-12-13 | 2008-06-11 | 辛忻 | Airborne defogging equipment |
| CN102612917A (en) * | 2012-03-20 | 2012-08-01 | 郭继高 | Fertilizer water flushing device |
| CN102910288A (en) * | 2012-10-31 | 2013-02-06 | 襄阳宏伟航空器有限责任公司 | Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil |
| CN202818936U (en) * | 2012-10-09 | 2013-03-27 | 宁夏农林科学院 | Adjustable seeding fertilizing constant weight feeder |
| CN202984114U (en) * | 2012-11-29 | 2013-06-12 | 酒泉奥凯种子机械股份有限公司 | Grass seed cleaning and discharging device |
| CN103241377A (en) * | 2013-05-27 | 2013-08-14 | 襄阳宏伟航空器有限责任公司 | Soft-wing unmanned aerocraft with automatic fog dispersal function |
| CN103611622A (en) * | 2013-11-27 | 2014-03-05 | 辽宁福犇食品有限公司 | Fresh corn kernel drift sorter |
| CN203638594U (en) * | 2014-01-13 | 2014-06-11 | 大连理工大学 | Anti-blocking star-shaped discharge device |
| CN205256678U (en) * | 2015-12-15 | 2016-05-25 | 谷家菊 | Gentle wing unmanned vehicles of fog dispersal |
-
2015
- 2015-12-15 CN CN201510928752.9A patent/CN105383698A/en active Pending
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2696295Y (en) * | 2004-02-17 | 2005-05-04 | 王晓望 | Automatic fertilizing machine |
| CN101195994A (en) * | 2007-12-13 | 2008-06-11 | 辛忻 | Airborne defogging equipment |
| CN102612917A (en) * | 2012-03-20 | 2012-08-01 | 郭继高 | Fertilizer water flushing device |
| CN202818936U (en) * | 2012-10-09 | 2013-03-27 | 宁夏农林科学院 | Adjustable seeding fertilizing constant weight feeder |
| CN102910288A (en) * | 2012-10-31 | 2013-02-06 | 襄阳宏伟航空器有限责任公司 | Multifunctional unmanned aerial vehicle provided with flexible stamping parafoil |
| CN202984114U (en) * | 2012-11-29 | 2013-06-12 | 酒泉奥凯种子机械股份有限公司 | Grass seed cleaning and discharging device |
| CN103241377A (en) * | 2013-05-27 | 2013-08-14 | 襄阳宏伟航空器有限责任公司 | Soft-wing unmanned aerocraft with automatic fog dispersal function |
| CN103611622A (en) * | 2013-11-27 | 2014-03-05 | 辽宁福犇食品有限公司 | Fresh corn kernel drift sorter |
| CN203638594U (en) * | 2014-01-13 | 2014-06-11 | 大连理工大学 | Anti-blocking star-shaped discharge device |
| CN205256678U (en) * | 2015-12-15 | 2016-05-25 | 谷家菊 | Gentle wing unmanned vehicles of fog dispersal |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160309 |