CN105818970B - A kind of unmanned paint spraying machine in high-altitude - Google Patents
A kind of unmanned paint spraying machine in high-altitude Download PDFInfo
- Publication number
- CN105818970B CN105818970B CN201610201459.7A CN201610201459A CN105818970B CN 105818970 B CN105818970 B CN 105818970B CN 201610201459 A CN201610201459 A CN 201610201459A CN 105818970 B CN105818970 B CN 105818970B
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- CN
- China
- Prior art keywords
- propeller
- spraying machine
- carbon fiber
- paint spraying
- unmanned
- 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.)
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- 239000003973 paint Substances 0.000 title claims abstract description 21
- 238000005507 spraying Methods 0.000 title claims abstract description 14
- 229920000049 Carbon (fiber) Polymers 0.000 claims abstract description 15
- 239000004917 carbon fiber Substances 0.000 claims abstract description 15
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims abstract description 15
- 230000002093 peripheral effect Effects 0.000 claims abstract description 4
- 230000001681 protective effect Effects 0.000 claims abstract description 3
- 208000002925 dental caries Diseases 0.000 claims description 6
- 239000011229 interlayer Substances 0.000 claims description 3
- 239000010410 layer Substances 0.000 claims description 3
- 230000006641 stabilisation Effects 0.000 claims description 3
- 238000011105 stabilization Methods 0.000 claims description 3
- 230000005484 gravity Effects 0.000 claims description 2
- 239000007921 spray Substances 0.000 claims description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 abstract description 4
- 229910052799 carbon Inorganic materials 0.000 abstract description 4
- 238000002360 preparation method Methods 0.000 abstract description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000686 essence Substances 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/006—Safety devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- 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
- B64D1/18—Dropping or releasing powdered, liquid, or gaseous matter, e.g. for fire-fighting by spraying, e.g. insecticides
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Life Sciences & Earth Sciences (AREA)
- Pest Control & Pesticides (AREA)
- Remote Sensing (AREA)
- Application Of Or Painting With Fluid Materials (AREA)
- Nozzles (AREA)
Abstract
The invention belongs to unmanned plane preparation field, more particularly to a kind of unmanned paint spraying machine in high-altitude.Including rectangular central plate, two groups of totally four aileron horns are symmetrically arranged with the both sides of central plate, the end of aileron horn is provided with propeller；The outside of four aileron horns is provided with the anticollision device, collision-prevention device of buttferfly-type, the anticollision device, collision-prevention device includes multiple hollow insulative carbon fiber pipes, peripheral structure is connected as by connecting plate between hollow insulative carbon fiber pipe two-by-two, play protective action, carbon pipe diameter is 40~50cm, and many carbon fiber pipe intercommunications are built-in with air bag, the distance between propeller blade tip of homonymy cannot be less than 50cm, and the distance between both sides propeller blade tip must not be less than 50cm.Rationally, overall weight is clear for structure setting of the present invention, and the setting of the propeller up and down and motor set reduces power consumption in flight course, improves the time of flight.
Description
Technical field
The invention belongs to unmanned plane preparation field, more particularly to a kind of unmanned paint spraying machine in high-altitude.
Background technology
In the conventional agricultural of unmanned plane sprinkling and other altitude effects, but it is sufficiently bulky to be due to that unmanned plane will be carried
Spray paint can causes weight very heavy, and in-flight power consumption is high, the serious flight time that have impact on unmanned plane.
The content of the invention
The technical problems to be solved by the invention are to provide a kind of high-altitude unmanned paint spraying machine, solve in the prior art nobody
The problem of own wt weight of machine.
The present invention is achieved in that a kind of unmanned paint spraying machine in high-altitude, and the unmanned plane includes：Rectangular central plate, in
The both sides of core are symmetrically arranged with two groups of totally four aileron horns, and the end of aileron horn is provided with propeller；In four aileron horns
Outside be provided with the anticollision device, collision-prevention device of buttferfly-type, the anticollision device, collision-prevention device includes multiple hollow insulative carbon fiber pipes, two-by-two it is hollow absolutely
Peripheral structure is connected as by connecting plate between edge carbon fiber pipe, protective action is played, carbon pipe diameter is 40~50cm, many carbon
Fibre pipe intercommunication, is built-in with air bag, and the distance between the propeller blade tip of homonymy cannot be less than 50cm, both sides propeller oar
The distance between point must not be less than 50cm.
Further, central plate includes upper plate and lower plate, two be made up of on central plate length direction upper plate and lower plate
Two cavitys are set along center is symmetrical above and below between layer, a cavity is used to place control system wherein, in another cavity
Placing battery and storage paint pressurized tank, pass through the stabilization of the placement location center-of-gravity regulating of battery.
Further, electron speed regulator is respectively arranged with the symmetrical both sides of each cavity, electron speed regulator is used for
Propeller motor with closing on is connected.
Further, radiating is set in the position of upper plate two cavitys corresponding with lower plate and the position of electron speed regulator
Hole.
Further, the end connection motor fixing seat of the aileron horn, the two sides up and down of motor fixing seat are set respectively
It is equipped with two motors, each motor output shaft and is respectively connected with propeller, wherein, in the conduct of side during flight upwardly
Side, downward side is downside, and the rotating speed of downside motor, the propeller length positioned at upside are more than positioned at the rotating speed of the motor of upside
Less than the length of the propeller positioned at downside.
Further, the rotating speed of upside motor is 0~9900 rev/min, and downside is 0-5940 revs/min.
Further, upside propeller and downside propeller length ratio 16:20~15：25；Upside propeller and downside
The width ratio of the widest part of propeller is 1：1.5~1:Between 2.
Further, the hollow shower nozzle pole of carbon fiber is installed in the side in central plate length, pacifies in the end of pole
Video camera fixed seat is filled, video camera is arranged in fixed seat, is stretched out shower nozzle fixed plate along fixed seat, is bolted shower nozzle,
The oil pipe of the shower nozzle connection is connected through hollow shower nozzle pole inside with the storage paint pressurized tank in central plate interlayer, the shower nozzle
Tracheae, through being connected with the crossover sub in the middle of central plate inside hollow shower nozzle pole, the air guide connected by crossover sub
Pipe leads to bottom surface.
Compared with prior art, beneficial effect is the present invention：Rationally, overall weight is clear for structure setting of the present invention, and
The setting of the propeller up and down and motor that set reduces the power consumption in flight course, improves the time of flight.
Brief description of the drawings
Fig. 1 is equipment upper side structural representation provided in an embodiment of the present invention；
Fig. 2 is equipment downside provided in an embodiment of the present invention structural representation.
Embodiment
In order to make the purpose , technical scheme and advantage of the present invention be clearer, it is right below in conjunction with drawings and Examples
The present invention is further elaborated.It should be appreciated that the specific embodiments described herein are merely illustrative of the present invention, and
It is not used in the restriction present invention.
Referring to Fig. 1 combination Fig. 2, the unmanned paint spraying machine in high-altitude, the unmanned plane includes：Rectangular central plate, the two of central plate 3
Side is symmetrically arranged with two groups of totally four aileron horns 11, and propeller (9.10) is provided with the end of aileron horn；In four aileron horns
Outside be provided with the anticollision device, collision-prevention device of buttferfly-type, support bar 8 is set between buttferfly-type waist and central plate, and anticollision device, collision-prevention device includes many
Individual hollow insulative carbon fiber pipe 1, is connected as peripheral structure by connecting plate 2 between hollow insulative carbon fiber pipe 1 two-by-two, plays anti-
Shield is acted on, and carbon pipe diameter is 40~50cm, and many carbon fiber pipe intercommunications are built-in with air bag, the propeller blade tip of homonymy it
Between distance cannot be less than 50cm, the distance between both sides propeller blade tip must not be less than 50cm.Required according to master control system,
The distance between blade tip is set.
Central plate 3 include upper plate and lower plate, central plate include upper plate and lower plate, on central plate length direction by upper plate with
Two cavitys are set along center is symmetrical above and below between two layers of lower plate composition, the first cavity 4 and the second cavity 5, wherein first
Cavity 4 is used to place placing battery and storage paint pressurized tank in control system, the second cavity 5, is ensured by the placement location of battery
The stabilization of center of gravity, two electron speed regulators are respectively arranged with the symmetrical both sides of cavity, and electron speed regulator is used for the spiral shell with closing on
Revolve oar motor to be connected, be symmetrical arranged heat emission hole 6 on upper plate and lower plate, heat emission hole is arranged on two cavitys and electron speed regulator
Corresponding position.
The end connection motor fixing seat 7 of aileron horn 11, the two sides up and down of motor fixing seat 7 are respectively arranged with two electricity
Propeller (9,10) is respectively connected with machine, each motor output shaft, wherein, on the upside of the conduct of side during flight upwardly, to
Lower side is downside, and the rotating speed of downside motor is more than positioned at the rotating speed of the motor of upside, and the length of propeller 9 positioned at upside is less than
Positioned at the length of the propeller 10 of downside.
The rotating speed of upside motor is 0~9900 rev/min, and downside is 0-5940 revs/min.
The propeller 9 of upside and the length ratio 16 of propeller 10 of downside:20~15：25；The propeller 9 of upside and downside
Propeller 10 the widest part width ratio 1：1.5~1:Between 2.Advantage is, the high rotating speed in upside, above and below the slow-speed of revolution of downside
Wind-force, upper cross force is big, and lower cross force is small, propeller on the downside of the wind blows that the propeller of upside is produced so that downside spiral shell
Revolve oar motor discharge coefficient to decline, so as to improve lift.Upper propeller is smaller than minor spiral oar, and the air inlet to lower propeller is provided
Certain space, so as to ensure that the entrance of lower propeller is unimpeded, due to the high rotating speed small size of upper oar, bring the wind-force blown downwards
More than lower oar, lower oar width and lower oar ratio are 1：1.5~1:2 absorb the pneumatic of upper oar by the length and width of lower oar
Can so that lower oar power consumption is few, and there is provided the substantial amounts of wind-force blown downwards.
The hollow shower nozzle pole 12 of carbon fiber is installed in side in central plate length, installs video camera in the end of pole and consolidates
Reservation 13, video camera 16 is arranged in fixed seat 13, is stretched out shower nozzle fixed plate 17 along fixed seat, is passed through the stationary nozzle of bolt 14
15, referring to Fig. 2, the oil pipe 18 that shower nozzle 5 is connected connects through hollow shower nozzle pole inside and the storage paint pressurized tank in central plate interlayer
Connect.The tracheae 19 of shower nozzle, is connected with the crossover sub 20 in the middle of central plate through hollow shower nozzle pole inside, passes through crossover sub
The airway tube of connection leads to bottom surface.So as to gas, realize that high-altitude is sprayed by the air pump on ground.
The foregoing is merely illustrative of the preferred embodiments of the present invention, is not intended to limit the invention, all essences in the present invention
Any modifications, equivalent substitutions and improvements made within refreshing and principle etc., should be included in the scope of the protection.
Claims (7)
1. a kind of unmanned paint spraying machine in high-altitude, it is characterised in that the unmanned plane includes：Rectangular central plate, in the both sides of central plate
Two groups of totally four aileron horns are symmetrically arranged with, the end of aileron horn is provided with propeller；Set in four the outside of aileron horn
There is the anticollision device, collision-prevention device of buttferfly-type, the anticollision device, collision-prevention device includes multiple hollow insulative carbon fiber pipes, two-by-two hollow insulative carbon fiber pipe
Between peripheral structure is connected as by connecting plate, play protective action, a diameter of 40~50cm of carbon fiber pipe, many carbon fiber pipes
Intercommunication, is built-in with air bag, and the distance between the propeller blade tip of homonymy cannot be less than between 50cm, both sides propeller blade tip
Distance must not be less than 50cm, the hollow shower nozzle pole of carbon fiber is installed in a side in central plate length, in the end of pole
Video camera fixed seat is installed, video camera is arranged in fixed seat, is stretched out shower nozzle fixed plate along fixed seat, is bolted spray
Head, the oil pipe of the shower nozzle connection is connected through hollow shower nozzle pole inside with the storage paint pressurized tank in central plate interlayer, described
The tracheae of shower nozzle, is connected with the crossover sub in the middle of central plate through hollow shower nozzle pole inside, is connected by crossover sub
Airway tube leads to bottom surface.
2. according to the unmanned paint spraying machine in high-altitude described in claim 1, it is characterised in that central plate includes upper plate and lower plate, in
Two cavitys, wherein one are set along center is symmetrical above and below between two layers that upper plate and lower plate are constituted on core length direction
Cavity is used to place control system, and placing battery and storage paint pressurized tank, are adjusted by the placement location of battery in another cavity
The stabilization of center of gravity.
3. according to the unmanned paint spraying machine in high-altitude described in claim 2, it is characterised in that in the symmetrical both sides of each cavity point
Electron speed regulator is not provided with, and the propeller motor that electron speed regulator is used for closing on is connected.
4. according to the unmanned paint spraying machine in high-altitude described in claim 3, it is characterised in that in upper plate two cavitys corresponding with lower plate
Position and electron speed regulator position set heat emission hole.
5. according to the unmanned paint spraying machine in high-altitude described in claim 1, it is characterised in that the end connection motor of the aileron horn is consolidated
Reservation, the two sides up and down of motor fixing seat, which are respectively arranged with two motors, each motor output shaft, is respectively connected with propeller,
Wherein, on the upside of the conduct of side during flight upwardly, downward side is downside, and the rotating speed positioned at the motor of upside is more than downside
The rotating speed of motor, the propeller length positioned at upside is less than the length of the propeller positioned at downside.
6. according to the unmanned paint spraying machine in high-altitude described in claim 5, it is characterised in that the rotating speed of upside motor is 0~9900 turn/
Minute, downside is 0-5940 revs/min.
7. according to the unmanned paint spraying machine in high-altitude described in claim 5, it is characterised in that upside propeller and downside propeller length
Ratio 16:20~15：25；The width ratio of the widest part of upside propeller and downside propeller is 1：1.5~1:Between 2.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610201459.7A CN105818970B (en) | 2016-04-01 | 2016-04-01 | A kind of unmanned paint spraying machine in high-altitude |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610201459.7A CN105818970B (en) | 2016-04-01 | 2016-04-01 | A kind of unmanned paint spraying machine in high-altitude |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105818970A CN105818970A (en) | 2016-08-03 |
| CN105818970B true CN105818970B (en) | 2017-09-22 |
Family
ID=56525542
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610201459.7A Active CN105818970B (en) | 2016-04-01 | 2016-04-01 | A kind of unmanned paint spraying machine in high-altitude |
Country Status (1)
| Country | Link |
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| CN (1) | CN105818970B (en) |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP6721191B2 (en) * | 2017-10-02 | 2020-07-08 | 株式会社プロドローン | Rotorcraft |
| CN108999386A (en) * | 2018-10-24 | 2018-12-14 | 临海市天马装璜材料厂 | A kind of flight spray-painting plant |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204623829U (en) * | 2015-04-17 | 2015-09-09 | 何春旺 | Aircraft |
| CN105059526A (en) * | 2015-07-29 | 2015-11-18 | 北京中科遥数信息技术有限公司 | Slide rod type lightweight four-rotor unmanned aerial vehicle |
| CN204802080U (en) * | 2015-05-29 | 2015-11-25 | 刘琳 | Intelligent Mobile Terminal and intelligent flight system with flight function |
| CN204956914U (en) * | 2015-09-17 | 2016-01-13 | 广东中安金狮科创有限公司 | Automatic unmanned aerial vehicle of flight is dodged and passes through in three dimensions range finding |
| CN205524947U (en) * | 2016-04-01 | 2016-08-31 | 国网辽宁省电力有限公司辽阳供电公司 | Unmanned paint spraying machine in high altitude |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8322648B2 (en) * | 2008-05-15 | 2012-12-04 | Aeryon Labs Inc. | Hovering aerial vehicle with removable rotor arm assemblies |
-
2016
- 2016-04-01 CN CN201610201459.7A patent/CN105818970B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN204623829U (en) * | 2015-04-17 | 2015-09-09 | 何春旺 | Aircraft |
| CN204802080U (en) * | 2015-05-29 | 2015-11-25 | 刘琳 | Intelligent Mobile Terminal and intelligent flight system with flight function |
| CN105059526A (en) * | 2015-07-29 | 2015-11-18 | 北京中科遥数信息技术有限公司 | Slide rod type lightweight four-rotor unmanned aerial vehicle |
| CN204956914U (en) * | 2015-09-17 | 2016-01-13 | 广东中安金狮科创有限公司 | Automatic unmanned aerial vehicle of flight is dodged and passes through in three dimensions range finding |
| CN205524947U (en) * | 2016-04-01 | 2016-08-31 | 国网辽宁省电力有限公司辽阳供电公司 | Unmanned paint spraying machine in high altitude |
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| Publication number | Publication date |
|---|---|
| CN105818970A (en) | 2016-08-03 |
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