CN105366055A - Flexible-wing unmanned aerial vehicle with fog dispersal function - Google Patents
Flexible-wing unmanned aerial vehicle with fog dispersal function Download PDFInfo
- Publication number
- CN105366055A CN105366055A CN201510928799.5A CN201510928799A CN105366055A CN 105366055 A CN105366055 A CN 105366055A CN 201510928799 A CN201510928799 A CN 201510928799A CN 105366055 A CN105366055 A CN 105366055A
- Authority
- CN
- China
- Prior art keywords
- aerial vehicle
- fog dispersal
- wing unmanned
- flexible
- wing
- 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
- 230000006698 induction Effects 0.000 claims description 9
- 239000013078 crystal Substances 0.000 description 4
- 239000003595 mist Substances 0.000 description 4
- 239000003795 chemical substances by application Substances 0.000 description 3
- 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
- 238000009331 sowing 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
- 238000009434 installation Methods 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
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
- 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
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention relates to a flexible-wing unmanned aerial vehicle with a fog dispersal function. The flexible-wing unmanned aerial vehicle comprises an aerial vehicle body, fixed wings are arranged on the two sides of the aerial vehicle body, a generator assembly is arranged on one side in the aerial vehicle body, and the output end of the generator assembly is connected with a propeller. The upper side of the aerial vehicle body is connected with a flexible ram air parachute, a plurality of air inlet holes are formed in the side wall of the aerial vehicle body, a scattering assembly is arranged in the aerial vehicle body, and each fixed wing is provided with external fog dispersal equipment. The flexible-wing unmanned aerial vehicle is low in cost and wide in use range, and the flexible-wing unmanned aerial vehicle can be suitable for the conditions needing fog dispersal within a local range, such as highway traffic environment improving, airport dense fog removing and disaster relief area microclimate improving.
Description
Technical field
This
inventionrelate to unmanned air vehicle technique field, particularly relate to
one has the soft wing unmanned vehicle of fog dispersal function.
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 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 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
one has the soft wing unmanned vehicle of fog dispersal function.
This
inventionbe achieved through the following technical solutions:
one has the soft wing unmanned vehicle of fog dispersal functioncomprise aircraft body, described aircraft body both sides are provided with fixed-wing, the inner side of described aircraft body is provided with generator assembly, described generator assembly mouth is connected with screw propeller, is connected on the upside of described aircraft body with flexible ram air parachute, and described aircraft body sidewall is provided with several induction openings, described aircraft body inside is provided with sows assembly, and each fixed-wing described is provided with external fog dispersal equipment.
As this
inventionoptimal technical scheme, described induction opening reduces gradually from outside to inside cross-sectional area.
As this
inventionoptimal technical scheme, described in sow assembly and comprise rotating shaft, sow blade, described in sow blade and be evenly distributed in rotating shaft.
As this
inventionoptimal technical scheme, for removably connecting between described external fog dispersal equipment and each fixed-wing.
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 air in flight course enters internal body from induction opening, drive is sowed assembly rotation and is sowed in atmosphere by antifogging agent, external fog dispersal equipment is also sowed simultaneously, realize falling mist to air, such cost is low, and 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.
Accompanying drawing explanation
fig. 1for this
inventionstructural representation
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. 1for this
inventionstructural representation
figure.
one has the soft wing unmanned vehicle of fog dispersal functioncomprise aircraft body 1, described aircraft body 1 both sides are provided with fixed-wing 2, the described inner side of aircraft body 1 is provided with generator assembly 3, described generator assembly 3 mouth is connected with screw propeller 4, is connected on the upside of described aircraft body 1 with flexible ram air parachute 7, and described aircraft body 1 sidewall is provided with several induction openings 101, wherein said induction opening 101 reduces gradually from outside to inside cross-sectional area, like this can the entering of air.
Described aircraft body 1 inside is provided with sows assembly 5, and 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 the discharge that assembly 5 can realize antifogging agent like this.Each fixed-wing 2 described is provided with external fog dispersal equipment 6, for removably connecting between wherein said external fog dispersal equipment 6 and each fixed-wing 2, the installation and removal of external like this fog dispersal equipment 6.
Its detailed description of the invention is: when using 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 induction opening 101, drive is sowed assembly 5 and is rotated and sow in atmosphere by antifogging agent, external fog dispersal equipment 6 is also sowed simultaneously, realize falling mist to air, 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.
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. one kind has the soft wing unmanned vehicle of fog dispersal function, comprise aircraft body (1), described aircraft body (1) both sides are provided with fixed-wing (2), described aircraft body (1) inner side is provided with generator assembly (3), described generator assembly (3) mouth is connected with screw propeller (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 induction openings (101), described aircraft body (1) inside is provided with sows assembly (5), described each fixed-wing (2) is provided with external fog dispersal equipment (6).
2. according to claim 1 have the soft wing unmanned vehicle of fog dispersal function, it is characterized in that: described induction opening (101) reduces gradually from outside to inside cross-sectional area.
3. according to claim 1 have the 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 the soft wing unmanned vehicle of fog dispersal function, it is characterized in that: for removably connecting between described external fog dispersal equipment (6) and each fixed-wing (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510928799.5A CN105366055A (en) | 2015-12-15 | 2015-12-15 | Flexible-wing unmanned aerial vehicle with fog dispersal function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510928799.5A CN105366055A (en) | 2015-12-15 | 2015-12-15 | Flexible-wing unmanned aerial vehicle with fog dispersal function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105366055A true CN105366055A (en) | 2016-03-02 |
Family
ID=55368800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510928799.5A Pending CN105366055A (en) | 2015-12-15 | 2015-12-15 | Flexible-wing unmanned aerial vehicle with fog dispersal function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105366055A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201195592Y (en) * | 2008-04-29 | 2009-02-18 | 邱志刚 | Light airplane planting apparatus |
| CN202541836U (en) * | 2012-06-26 | 2012-11-21 | 无锡汉和航空技术有限公司 | Novel unmanned air barrel duct-type aircraft for liquid sprinkling and grain sowing |
| 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 |
| 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 |
| CN204157260U (en) * | 2014-09-09 | 2015-02-18 | 湖南农业大学 | A kind of precision drilling operating system based on flying platform |
| CN204507275U (en) * | 2015-02-15 | 2015-07-29 | 新疆天山羽人农业航空科技有限公司 | A kind of unmanned vehicle sowed |
| CN204776007U (en) * | 2015-06-03 | 2015-11-18 | 中恒天信（天津）航空科技有限公司 | Many rotors of agricultural plant protection unmanned vehicles |
| CN205256679U (en) * | 2015-12-15 | 2016-05-25 | 谷家菊 | Gentle wing unmanned vehicles of fog dispersal function has |
-
2015
- 2015-12-15 CN CN201510928799.5A patent/CN105366055A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201195592Y (en) * | 2008-04-29 | 2009-02-18 | 邱志刚 | Light airplane planting apparatus |
| CN202541836U (en) * | 2012-06-26 | 2012-11-21 | 无锡汉和航空技术有限公司 | Novel unmanned air barrel duct-type aircraft for liquid sprinkling and grain sowing |
| 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 |
| 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 |
| CN204157260U (en) * | 2014-09-09 | 2015-02-18 | 湖南农业大学 | A kind of precision drilling operating system based on flying platform |
| CN204507275U (en) * | 2015-02-15 | 2015-07-29 | 新疆天山羽人农业航空科技有限公司 | A kind of unmanned vehicle sowed |
| CN204776007U (en) * | 2015-06-03 | 2015-11-18 | 中恒天信（天津）航空科技有限公司 | Many rotors of agricultural plant protection unmanned vehicles |
| CN205256679U (en) * | 2015-12-15 | 2016-05-25 | 谷家菊 | Gentle wing unmanned vehicles of fog dispersal function has |
Non-Patent Citations (1)
| Title |
|---|
| 梁吉艳: "环境工程学", 中国建材工业出版社, pages: 145 * |
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| 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: 20160302 |