CN204937494U - A kind of remote control plant protection aircraft - Google Patents
A kind of remote control plant protection aircraft Download PDFInfo
- Publication number
- CN204937494U CN204937494U CN201520708534.XU CN201520708534U CN204937494U CN 204937494 U CN204937494 U CN 204937494U CN 201520708534 U CN201520708534 U CN 201520708534U CN 204937494 U CN204937494 U CN 204937494U
- Authority
- CN
- China
- Prior art keywords
- support arm
- rotor support
- rotor
- fixed
- fixed link
- 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.)
- Active
Links
Abstract
A kind of remote control plant protection aircraft, comprise alighting gear, alighting gear is provided with branched rotor support arm, one end of each rotor support arm is fixed on the top center of alighting gear, the other end is dispersed to surrounding, end is dispersed in formation, the end top of dispersing of each rotor support arm is provided with rotor, the rotor support arm top of alighting gear top center is provided with spider, the engine petrol identical with rotor quantity is provided with in spider, every platform engine petrol correspondence is connected with a rotor, often prop up rotor support arm top and be equipped with fixed link, often prop up bottom rotor support arm and be equipped with lower fixed link, what one end of upper fixed link was fixed on rotor support arm disperses end, the other end of upper fixed link is fixed on the sidewall of spider, what one end of lower fixed link was fixed on rotor support arm disperses end, the other end of lower fixed link is fixed on the top center of alighting gear.The utility model flight time is long, and load-carrying capacity is strong, and rotor support arm can be avoided to rock, and makes aircraft more stable in the process of flight.
Description
Technical field
The utility model relates to a kind of remote control plant protection aircraft.
Background technology
Remote control plant protection aircraft is a kind ofly specifically designed to the aircraft of spraying insecticide to ground crops, and its type is petite and powerful, sprays insecticide in low latitude, and per minute can complete the operation of 0.07 hectare, and its spraying efficiency is 30 times of Traditional Man.This aircraft adopts Intelligent control, and operator is implemented to control to it by ground remote control device.It is low that remote control distributor fog machine has operation height; drift is few; can hovering; without the need to special landing airport; the downdraft that its rotor produces contributes to increasing spray to the penetrance of crop, and prevention effect is good, simultaneously; spraying operation personnel avoid the danger close to agricultural chemicals, and remote control dispenser substantially increases the safety of pesticide spraying.
At present, existing remote control plant protection aircraft adopts electrical motor as the propulsion source of rotor mostly, supportingly on aircraft is equipped with as electrical motor provides the battery system of power supply.Because battery system charge capacity is very limited, the time that this type remote control plant protection is aloft flown after taking off is shorter, and the disposable time of spraying insecticide is also shorter; Meanwhile, load-carrying capacity is also poor.
Meanwhile, when remote control plant protection aircraft adopts many rotors, the rotor support arm of remote control plant protection aircraft easily rocks, and flight course may cause and rocks.
Utility model content
Technical problem to be solved in the utility model is, overcomes the deficiency of above-mentioned background technology, provides a kind of flight time long, the remote control plant protection aircraft that load-carrying capacity is strong.
The technical scheme that the utility model solves the employing of its technical matters is, a kind of remote control plant protection aircraft, comprise alighting gear, described alighting gear is provided with branched rotor support arm, one end of each rotor support arm is fixed on the top center of alighting gear, the other end is dispersed to surrounding, end is dispersed in formation, the end top of dispersing of each rotor support arm is provided with rotor, the rotor support arm top of described alighting gear top center is provided with spider, the engine petrol identical with rotor quantity is provided with in described spider, every platform engine petrol correspondence is connected with a rotor, often prop up rotor support arm top and be equipped with fixed link, often prop up bottom rotor support arm and be equipped with lower fixed link, what one end of fixed bar was fixed on rotor support arm disperses end, the other end of upper fixed link is fixed on the sidewall of spider, what one end of described lower fixed link was fixed on rotor support arm disperses end, the other end of lower fixed link is fixed on the top center of alighting gear.
Further, be provided with anticollision device outside described rotor, described anticollision device is fixed on rotor support arm.
Further, the quantity of described rotor support arm is that even number props up.
Further, the quantity of described rotor support arm is 6.
Further, described engine petrol is EFI two-cycle gasoline engine.
Compared with prior art, advantage of the present utility model is as follows:
(1) be provided with engine petrol in spider, adopt engine petrol as the propulsion source of rotor, comparing traditional electrical motor is that rotor is powered rotation, and the flight time of the present utility model is longer, and the disposable time of spraying insecticide is also longer; Meanwhile, load-carrying capacity is also stronger.
(2) rotor support arm top is provided with fixed link, and bottom is provided with lower fixed link, and rotor support arm can be avoided to rock, and makes aircraft more stable in the process of flight.
Accompanying drawing explanation
Fig. 1 is the structural representation of the utility model embodiment.
Fig. 2 is front view embodiment illustrated in fig. 1.
In figure: 1-alighting gear, 2-rotor support arm, 3-upper fixed link, 4-rotor, 5-spider, 6-engine petrol, 7-anticollision device, 8-lower fixed link.
Detailed description of the invention
Below in conjunction with drawings and the specific embodiments, the utility model is described in further detail.
With reference to Fig. 1, Fig. 2, the present embodiment comprises alighting gear 1, alighting gear 1 is provided with 6 rotor support arms 2, one end of each rotor support arm 2 is fixed on the top center of alighting gear 1, the other end is dispersed to surrounding, end is dispersed in formation, the end top of dispersing of each rotor support arm 2 is provided with rotor 4, rotor support arm 2 top of alighting gear 1 top center is provided with spider 5,6 engine petroies 6 are provided with in spider 5, every platform engine petrol 6 correspondence is connected with a rotor 4, and for rotor 4 provides power, described engine petrol 6 adopts EFI two-cycle gasoline engine; In order to avoid rotor support arm 2 rocks, make aircraft more stable in the process of flight, often prop up rotor support arm 2 top and be equipped with fixed link 3, often prop up bottom rotor support arm 2 and be equipped with lower fixed link 8, what one end of upper fixed link 3 was fixed on rotor support arm 2 disperses end, the other end of upper fixed link 3 is fixed on the sidewall of spider 5, and what one end of lower fixed link 8 was fixed on rotor support arm 2 disperses end, and the other end of lower fixed link 8 is fixed on the top center of alighting gear 1; Anticollision device 7 is installed outside rotor 4; anticollision device 7 is fixed on rotor support arm 2; anticollision device 7 utilizes cushioning principle; when aircraft flight runs into obstacle on the way or is born; described anticollision device 7 can play a protective role to rotor support arm 2 and rotor 4; reduce the probability of rotor support arm 2 and rotor 4 damage, also can ensure the safety of aircraft in operation process, in order to avoid the High Rotation Speed of rotor 4 damages to personnel simultaneously.
The utility model adopts engine petrol 6 as the propulsion source of rotor 4, and comparing traditional electrical motor is that rotor 4 power supply rotates, and the flight time of the present utility model is longer, and the disposable time of spraying insecticide is also longer; Meanwhile, load-carrying capacity is also stronger.
Those skilled in the art can carry out various modifications and variations to the utility model embodiment; if these amendments and modification are within the scope of the utility model claim and equivalent technologies thereof, then these revise and modification also within protection domain of the present utility model.
The prior art that the content do not described in detail in specification sheets is known to the skilled person.
Claims (7)
1. a remote control plant protection aircraft, comprise alighting gear (1), described alighting gear (1) is provided with branched rotor support arm (2), one end of each rotor support arm (2) is fixed on the top center of alighting gear (1), the other end is dispersed to surrounding, end is dispersed in formation, the end top of dispersing of each rotor support arm (2) is provided with rotor (4), rotor support arm (2) top of described alighting gear (1) top center is provided with spider (5), it is characterized in that: in described spider (5), be provided with the engine petrol (6) identical with rotor (4) quantity, every platform engine petrol (6) correspondence is connected with a rotor (4), often prop up rotor support arm (2) top and be equipped with fixed link (3), often prop up rotor support arm (2) bottom and be equipped with lower fixed link (8), what one end of fixed bar (3) was fixed on rotor support arm (2) disperses end, the other end of upper fixed link (3) is fixed on the sidewall of spider (5), what one end of described lower fixed link (8) was fixed on rotor support arm (2) disperses end, the other end of lower fixed link (8) is fixed on the top center of alighting gear (1).
2. remote control plant protection aircraft as claimed in claim 1, is characterized in that: described rotor (4) outside is provided with anticollision device (7), and described anticollision device (7) is fixed on rotor support arm (2).
3. remote control plant protection aircraft as claimed in claim 1 or 2, is characterized in that: the quantity of described rotor support arm (2) is that even number props up.
4. remote control plant protection aircraft as claimed in claim 3, is characterized in that: the quantity of described rotor support arm (2) is 6.
5. remote control plant protection aircraft as claimed in claim 1 or 2, is characterized in that: described engine petrol (6) is EFI two-cycle gasoline engine.
6. remote control plant protection aircraft as claimed in claim 3, is characterized in that: described engine petrol (6) is EFI two-cycle gasoline engine.
7. remote control plant protection aircraft as claimed in claim 4, is characterized in that: described engine petrol (6) is EFI two-cycle gasoline engine.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520708534.XU CN204937494U (en) | 2015-09-15 | 2015-09-15 | A kind of remote control plant protection aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520708534.XU CN204937494U (en) | 2015-09-15 | 2015-09-15 | A kind of remote control plant protection aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204937494U true CN204937494U (en) | 2016-01-06 |
Family
ID=55004939
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520708534.XU Active CN204937494U (en) | 2015-09-15 | 2015-09-15 | A kind of remote control plant protection aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204937494U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106477037A (en) * | 2016-12-05 | 2017-03-08 | 北京猎鹰无人机科技有限公司 | A kind of unmanned plane |
| CN107380416A (en) * | 2017-07-25 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of new unmanned plane for forest fire protection monitoring |
-
2015
- 2015-09-15 CN CN201520708534.XU patent/CN204937494U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106477037A (en) * | 2016-12-05 | 2017-03-08 | 北京猎鹰无人机科技有限公司 | A kind of unmanned plane |
| CN107380416A (en) * | 2017-07-25 | 2017-11-24 | 芜湖超源力工业设计有限公司 | A kind of new unmanned plane for forest fire protection monitoring |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN105539852A (en) | Multi-rotor UAV (unmanned aerial vehicle) as well as control system and method thereof | |
| CN204399482U (en) | The electronic unmanned fog machine of a kind of DCB Specimen close coupled type anticollision | |
| CN204399473U (en) | A kind of folding many rotor unmanned aircrafts of fast disassembly type | |
| CN203876984U (en) | Novel remote control pesticide spraying helicopter | |
| CN105882985B (en) | A kind of electronic unmanned fog machine of DCB Specimen close coupled type anticollision | |
| CN104554724A (en) | Low-cost and high-load specialized plant-protection unmanned aerial vehicle and driving method | |
| CN205554597U (en) | Intelligence pesticide sprays helicopter | |
| CN206012966U (en) | A kind of standard device for administration of drugs for plant protection unmanned plane | |
| CN204937494U (en) | A kind of remote control plant protection aircraft | |
| CN204157524U (en) | A kind of light and handy formula efficient remote control plant protection machine | |
| CN205418119U (en) | Agricultural plant protection unmanned aerial vehicle of rotor | |
| CN203199180U (en) | Four-propeller airship with wired energy supply infusion for pesticide spraying and fertilization of crops | |
| CN205256661U (en) | From rotor agricultural plant protection unmanned aerial vehicle | |
| CN107554746A (en) | Energy-saving type (plant protection, fire-fighting, remote measurement) unmanned aerial vehicle | |
| CN204979220U (en) | But agricultural many rotor unmanned aerial vehicle of automatic adjustment flight height | |
| CN205273856U (en) | Multiaxis horn pesticide sprinkling system | |
| CN204916172U (en) | Unmanned train's aircraft of integrated circuit debugging control system | |
| CN207045676U (en) | The more rotor plant protection unmanned planes of Y types | |
| CN204507273U (en) | A kind of agricultural unmanned vehicle spraying atomizing | |
| CN207029556U (en) | Multipurpose self-insurance unmanned plane | |
| CN206900643U (en) | A kind of agricultural spraying unmanned plane | |
| CN105292489A (en) | Unmanned aerial vehicle having pesticide spraying function | |
| CN206776573U (en) | Unmanned plane for pesticide spraying | |
| CN206165605U (en) | Unmanned aerial vehicle dusts | |
| CN205345344U (en) | Eight plant protection machines |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210416 Address after: No. 204, building 5, phase I, China Power Software Park, No. 39, Jianshan Road, Changsha high tech Development Zone, Changsha City, Hunan Province, 410205 Patentee after: HUNAN ZHONGDIAN JINJUN SOFTWARE TECHNOLOGY Co.,Ltd. Address before: 410217, No. 2, building 132 of electromechanical building materials market, Lei Feng Town, hi tech Development Zone, Hunan, Changsha Patentee before: CHANGSHA WANGCHENG HUANENG AGRICULTURAL MACHINERY TECHNOLOGY Co.,Ltd. |
|
| TR01 | Transfer of patent right | ||
| CP03 | Change of name, title or address |
Address after: No.204, building 5, phase I, Zhongdian Software Park, No.39, Jianshan Road, high tech Development Zone, Changsha, Hunan 410000 Patentee after: Hunan Zhongdian Jinjun Technology Group Co.,Ltd. Address before: No. 204, building 5, phase I, China Power Software Park, No. 39, Jianshan Road, Changsha high tech Development Zone, Changsha City, Hunan Province, 410205 Patentee before: HUNAN ZHONGDIAN JINJUN SOFTWARE TECHNOLOGY CO.,LTD. |
|
| CP03 | Change of name, title or address |