CN105818970A - Upper air unmanned paint sprayer - Google Patents
Upper air unmanned paint sprayer Download PDFInfo
- Publication number
- CN105818970A CN105818970A CN201610201459.7A CN201610201459A CN105818970A CN 105818970 A CN105818970 A CN 105818970A CN 201610201459 A CN201610201459 A CN 201610201459A CN 105818970 A CN105818970 A CN 105818970A
- Authority
- CN
- China
- Prior art keywords
- propeller
- carbon fiber
- unmanned
- shower nozzle
- downside
- 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.)
- Granted
Links
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; ARRANGEMENTS 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
Abstract
The invention belongs to the field of unmanned aerial vehicle manufacturing and particularly relates to an upper air unmanned paint sprayer. The upper air unmanned paint sprayer comprises a rectangular center board. Four aileron rods in two sets are symmetrically arranged on the two sides of the center board. Propellers are arranged at the end portions of the aileron rods. A butterfly-shaped anti-collision device is arranged outside the four aileron rods and comprises multiple hollow insulation carbon fiber pipes. Every two hollow insulation carbon fiber pipes are connected through a connecting board to form a peripheral structure so as to achieve a protecting effect. The diameter of each carbon fiber pipe ranges from 40 cm to 50 cm. The multiple carbon fiber pipes communicate with one another and are internally provided with inflation air bags. The distance between propeller tips of the propellers on the same side is not smaller than 50 cm, and the distance between propeller tips of the propellers on the two sides is not smaller than 50 cm. The upper air unmanned paint sprayer is reasonable in structural arrangement and low in total weight; and the upper and low propellers and motors are arranged, so that the power consumption generated in the flight process is reduced, and the flight time is prolonged.
Description
Technical field
The invention belongs to unmanned plane preparation field, particularly relate to the unmanned paint spraying machine in a kind of high-altitude.
Background technology
Unmanned plane sprays in conventional agricultural and other altitude effect, but causes weight the heaviest owing to unmanned plane to carry sufficiently bulky spray paint can, and power consumption is high in-flight, the serious flight time that have impact on unmanned plane.
Summary of the invention
The technical problem to be solved is to provide a kind of high-altitude unmanned paint spraying machine, the problem solving the own wt weight of unmanned plane in prior art.
The present invention is achieved in that the unmanned paint spraying machine in a kind of high-altitude, and this unmanned plane includes: rectangular central plate, and the lateral symmetry at central plate is provided with two groups of totally four aileron horns, and the end of aileron horn is provided with propeller；The anticollision device, collision-prevention device of buttferfly-type it is provided with in the outside of four aileron horns, described anticollision device, collision-prevention device includes multiple hollow insulative carbon fiber pipe, it is connected as peripheral structure by connecting plate two-by-two between hollow insulative carbon fiber pipe, play protective action, carbon pipe a diameter of 40～50cm, many carbon fiber pipe intercommunications, it is built-in with aerating gasbag, distance between the propeller blade tip of homonymy cannot be less than 50cm, and the distance between the propeller blade tip of both sides must not be less than 50cm.
Further, central plate includes upper plate and lower plate, symmetrical above and below along center between the two-layer being made up of upper plate and lower plate on central plate length direction two cavitys are set, a cavity is used for placing control system wherein, placing battery and storage paint pressurized tank in another cavity, by stablizing of the placement location center-of-gravity regulating of battery.
Further, being respectively arranged with electron speed regulator in the symmetrical both sides of each cavity, electron speed regulator is connected for the propeller motor with closing on.
Further, louvre is set in the upper plate position of two cavitys corresponding with in lower plate and the position of electron speed regulator.
Further, the end of described aileron horn connects motor fixing seat, the two sides up and down of motor fixing seat are respectively arranged with two motors, it is respectively connected with propeller on each motor output shaft, wherein, towards on the upside of the conduct of upper side during flight, downward side is downside, the rotating speed of the motor being positioned at upside is more than the rotating speed of downside motor, is positioned at the propeller length length less than the propeller being positioned at downside of upside.
Further, the rotating speed of upside motor is 0～9900 rev/min, and downside is 0-5940 rev/min.
Further, 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 between 1:1.5～1:2.
Further, end side in central plate length installs carbon fiber hollow shower nozzle pole, video camera is installed in the end of pole and fixes seat, video camera is arranged on fixing seat, shower nozzle fixed plate is stretched out along fixing seat, it is bolted shower nozzle, the oil pipe that described shower nozzle connects is connected through hollow shower nozzle pole is internal with the storage paint pressurized tank in central plate interlayer, the trachea of described shower nozzle, internal through hollow shower nozzle pole and in the middle of central plate adapter is connected, and the airway connected by adapter leads to bottom surface.
The present invention compared with prior art, has the beneficial effects that: present configuration arranges rationally, and overall weight is clear, and the power consumption that the setting of the propeller up and down that arranges and motor reduces in flight course, improves the time of flight.
Accompanying drawing explanation
Fig. 1 is the equipment upper side structural representation that the embodiment of the present invention provides；
Fig. 2 is the equipment downside structural representation that the embodiment of the present invention provides.
Detailed description of the invention
In order to make the purpose of the present invention, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the present invention is further elaborated.Should be appreciated that specific embodiment described herein, only in order to explain the present invention, is not intended to limit the present invention.
Seeing Fig. 1 and combine Fig. 2, the unmanned paint spraying machine in high-altitude, this unmanned plane includes: rectangular central plate, and the lateral symmetry at central plate 3 is provided with two groups of totally four aileron horns 11, is provided with propeller (9.10) in the end of aileron horn；The anticollision device, collision-prevention device of buttferfly-type it is provided with in the outside of four aileron horns, support bar 8 is set between buttferfly-type waist and central plate, anticollision device, collision-prevention device includes multiple hollow insulative carbon fiber pipe 1, it is connected as peripheral structure by connecting plate 2 between hollow insulative carbon fiber pipe 1 two-by-two, plays protective action, carbon pipe a diameter of 40～50cm, many carbon fiber pipe intercommunications, being built-in with aerating gasbag, the distance between the propeller blade tip of homonymy cannot be less than 50cm, and the distance between the propeller blade tip of both sides must not be less than 50cm.According to master control system requirement, the distance between blade tip is set.
Central plate 3 includes upper plate and lower plate, central plate includes upper plate and lower plate, symmetrical above and below along center between the two-layer being made up of upper plate and lower plate on central plate length direction two cavitys are set, first cavity 4 and the second cavity 5, first cavity 4 is used for placing control system wherein, placing battery and storage paint pressurized tank in second cavity 5, stablizing of center of gravity is ensured by the placement location of battery, it is respectively arranged with two electron speed regulators in the symmetrical both sides of cavity, electron speed regulator is connected for the propeller motor with closing on, upper plate with lower plate are symmetrical arranged louvre 6, louvre is arranged on two cavitys and position corresponding to electron speed regulator.
The end of aileron horn 11 connects motor fixing seat 7, the two sides up and down of motor fixing seat 7 are respectively arranged with two motors, propeller (9,10) it is respectively connected with on each motor output shaft, wherein, towards on the upside of the conduct of upper side during flight, side is downside downwards, and the rotating speed of the motor being positioned at upside is more than the rotating speed of downside motor, is positioned at propeller 9 length length less than the propeller 10 being positioned at downside of upside.
The rotating speed of upside motor is 0～9900 rev/min, and downside is 0-5940 rev/min.
The propeller 9 of upside and propeller 10 length ratio 16:20～15:25 of downside；The width ratio of the widest part of the propeller 9 of upside and the propeller 10 of downside is between 1:1.5～1:2.Advantage is, the high rotating speed in upside, the wind-force that the downside slow-speed of revolution is upper and lower, and upper cross force is big, and lower cross force is little, propeller on the downside of the wind blows that the propeller of upside produces so that downside propeller motor discharge coefficient declines, thus improves lift.Upper propeller is less than minor spiral oar, the certain space provided to the air inlet of lower propeller, thus ensure that the entrance of lower propeller is unimpeded, due to upper oar height rotating speed small size, bring the wind-force blown downwards more than lower oar, lower oar width and lower oar ratio absorb the kinetic energy of oar at 1:1.5～1:2 by the length and width of lower oar so that lower oar power consumption is few, it is provided that the substantial amounts of wind-force blown downwards.
Carbon fiber hollow shower nozzle pole 12 is installed in side in central plate length, video camera is installed in the end of pole and fixes seat 13, video camera 16 is arranged on fixing seat 13, shower nozzle fixed plate 17 is stretched out along fixing seat, by bolt 14 stationary nozzle 15, seeing Fig. 2, the oil pipe 18 that shower nozzle 5 connects is connected through hollow shower nozzle pole is internal with the storage paint pressurized tank in central plate interlayer.The trachea 19 of shower nozzle, internal through hollow shower nozzle pole and in the middle of central plate adapter 20 is connected, and the airway connected by adapter leads to bottom surface.Thus by the air pump on ground to gas, it is achieved high-altitude is sprayed.
The foregoing is only presently preferred embodiments of the present invention, not in order to limit the present invention, all any amendment, equivalent and improvement etc. made within the spirit and principles in the present invention, should be included within the scope of the present invention.
Claims (8)
1. the unmanned paint spraying machine in high-altitude, it is characterised in that this unmanned plane includes: rectangular central plate, the lateral symmetry at central plate is provided with two groups of totally four aileron horns, the end of aileron horn is provided with propeller；The anticollision device, collision-prevention device of buttferfly-type it is provided with in the outside of four aileron horns, described anticollision device, collision-prevention device includes multiple hollow insulative carbon fiber pipe, it is connected as peripheral structure by connecting plate two-by-two between hollow insulative carbon fiber pipe, play protective action, carbon pipe a diameter of 40～50cm, many carbon fiber pipe intercommunications, it is built-in with aerating gasbag, distance between the propeller blade tip of homonymy cannot be less than 50cm, and the distance between the propeller blade tip of both sides must not be less than 50cm.
2. according to the unmanned paint spraying machine in the high-altitude described in claim 1, it is characterized in that, central plate includes upper plate and lower plate, symmetrical above and below along center between the two-layer being made up of upper plate and lower plate on central plate length direction two cavitys are set, a cavity is used for placing control system wherein, placing battery and storage paint pressurized tank in another cavity, by stablizing of the placement location center-of-gravity regulating of battery.
3., according to the unmanned paint spraying machine in the high-altitude described in claim 2, it is characterised in that be respectively arranged with electron speed regulator in the symmetrical both sides of each cavity, electron speed regulator is connected for the propeller motor with closing on.
4. according to the unmanned paint spraying machine in the high-altitude described in claim 3, it is characterised in that arrange louvre in the upper plate position of two cavitys corresponding with in lower plate and the position of electron speed regulator.
5. according to the unmanned paint spraying machine in the high-altitude described in claim 1, it is characterized in that, the end of described aileron horn connects motor fixing seat, the two sides up and down of motor fixing seat are respectively arranged with two motors, each motor output shaft are respectively connected with propeller, wherein, towards on the upside of the conduct of upper side during flight, side is downside downwards, and the rotating speed of the motor being positioned at upside is more than the rotating speed of downside motor, is positioned at the propeller length length less than the propeller being positioned at downside of upside.
6. according to the unmanned paint spraying machine in the high-altitude described in claim 5, it is characterised in that the rotating speed of upside motor is 0～9900 rev/min, and downside is 0-5940 rev/min.
7. according to the unmanned paint spraying machine in the 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 between 1:1.5～1:2.
8. according to the unmanned paint spraying machine in the high-altitude described in claim 1, it is characterized in that, end side in central plate length installs carbon fiber hollow shower nozzle pole, video camera is installed in the end of pole and fixes seat, video camera is arranged on fixing seat, shower nozzle fixed plate is stretched out along fixing seat, it is bolted shower nozzle, the oil pipe that described shower nozzle connects is connected through hollow shower nozzle pole is internal with the storage paint pressurized tank in central plate interlayer, the trachea of described shower nozzle, internal through hollow shower nozzle pole and in the middle of central plate adapter is connected, the airway connected by adapter leads to bottom surface.
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 true CN105818970A (en) | 2016-08-03 |
| CN105818970B 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 |
|---|---|
| CN (1) | CN105818970B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| JP2019064581A (en) * | 2017-10-02 | 2019-04-25 | 株式会社プロドローン | Rotor craft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090283629A1 (en) * | 2008-05-15 | 2009-11-19 | Aeryon Labs Inc. | Hovering aerial vehicle with removable rotor arm assemblies |
| 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 |
-
2016
- 2016-04-01 CN CN201610201459.7A patent/CN105818970B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090283629A1 (en) * | 2008-05-15 | 2009-11-19 | Aeryon Labs Inc. | Hovering aerial vehicle with removable rotor arm assemblies |
| 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 |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019064581A (en) * | 2017-10-02 | 2019-04-25 | 株式会社プロドローン | Rotor craft |
| 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 |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105818970B (en) | 2017-09-22 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103238513B (en) | Airborne device suitable for pollination work of unmanned aerial vehicle and pollination method thereof | |
| US7581381B2 (en) | Ducted air power plant | |
| CN109319109B (en) | Traction energy transmission type ducted rotor wing flying crane and control method thereof | |
| CN204916161U (en) | No rotorcraft multiaxis aircraft | |
| US10669026B2 (en) | Lift cell modules and lift pods | |
| CN203612209U (en) | Agricultural aircraft | |
| CN107021235B (en) | A kind of low-to-medium altitude aircraft driving device, driving method and low-to-medium altitude aircraft | |
| CN104260875A (en) | Collision-resistant structure of agricultural plant protection unmanned aerial vehicle | |
| CN108284949B (en) | Foldable staggered six-rotor aircraft | |
| CN105818970A (en) | Upper air unmanned paint sprayer | |
| CN107176301A (en) | Fixed-wing fuel cell plant protection unmanned plane | |
| CN205524947U (en) | Unmanned paint spraying machine in high altitude | |
| CN206456566U (en) | Applied to Multi-axis aircraft without rotor air generation plants | |
| CN106379534A (en) | Spin control system and aircraft | |
| CN101580127B (en) | Movement device | |
| CN104986323B (en) | One kind fan wing aircraft | |
| CN111516859A (en) | Low-temperature invisible multi-nozzle aircraft | |
| CN107618647A (en) | Dirigible | |
| CN206900647U (en) | A kind of more rotors of combined type are tethered at UAS | |
| CN104875887A (en) | Vertical lifting component and fan wing aircraft with same | |
| CN202666408U (en) | Six-arm model aerial propeller | |
| CN105438475A (en) | Agricultural unmanned aerial vehicle capable of pressurizing and spraying pesticides | |
| CN205499376U (en) | V type flight mode plant protection unmanned aerial vehicle | |
| CN114275157A (en) | Composite wing unmanned aerial vehicle and pneumatic balancing method | |
| CN104843191A (en) | Non-contact type intelligent rainproof device for unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |