CN204979244U - External power source power supply remote control rotor flight seeder - Google Patents
External power source power supply remote control rotor flight seeder Download PDFInfo
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- CN204979244U CN204979244U CN201520723319.7U CN201520723319U CN204979244U CN 204979244 U CN204979244 U CN 204979244U CN 201520723319 U CN201520723319 U CN 201520723319U CN 204979244 U CN204979244 U CN 204979244U
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Abstract
External power source power supply remote control rotor flight seeder, including fuselage, the electronic rotor of a plurality of, state of flight computer control system, radio signal receiving process transmitting facilities and remote controller, state of flight computer control system includes satellite positioning terminal, accelerometer and communication module, characterized by flight seeder contains the power transmission line of being connected with external power source to contains a seeding facility, the seeding facility passes through interface circuit and state of flight computer control system signal connection, and the state of seeding facility is according to the change of state of flight computer control system state and the change. Adopt the power transmission line of being connected with external power source, make external power source pass through the power transmission line and last the supply the flying device electric energy can almost unrestrictedly strengthen flying device's stagnant empty ability.
Description
Technical field
The utility model relates to external power source remote controlled rotary-wing flight seeding apparatus.
Background technology
The agricultural sowing rotor craft of existing one, has the alternative advantage such as manually, but the storage battery flight owing to utilizing aircraft self-contained, the hang time is short, sometimes only has several minutes.
Summary of the invention
The purpose of this utility model is the agricultural flight seeding apparatus that the hang time will be provided longer.
The utility model realizes the technical scheme of its object: manufacture an external power source remote controlled rotary-wing flight seeding apparatus, comprise fuselage, several electronic rotors, state of flight computer control system, radio signal reception process launch facility and remote controller, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module.Described flight seeding apparatus adopts one group more than two to form the power transmission line in loop with the electricity consumption load of external power supply and described aircraft.External power supply continues the described flight seeding apparatus electric energy of supply by power transmission line.And adopt one to sow facility; Sowing facility is connected with state of flight computer control system signal by interface circuit, and the state of sowing facility changes according to the change of state of flight computer control system state.
Two frame rotor crafts can also be adopted namely to sow aircraft and assisting in flying device, and adopt a tracking dolly, follow the tracks of dolly and be mounted with automatic wire winding device, the automatic retraction device of seed transport tube, external power supply and storehouse cylinder; Described flight seeding apparatus adopts a seed transport tube, and seed transport tube two ends are communicated with storehouse cylinder with sowing facility respectively.
Two frame rotor crafts can also be adopted namely to sow aircraft and assisting in flying device, and adopt a tracking dolly; Containing an intermediate bin on sowing aircraft, follow the tracks of dolly and be mounted with the storehouse cylinder that automatic wire winding device, external power supply and band seed take out valve.
As required, the automatic retraction device that aircraft and assisting in flying device also can configure automatic wire winding device and seed transport tube is sowed.
The automatic retraction device of automatic wire winding device and seed transport tube can adopt one can the motorized pulleys of rotating make, and motorized pulleys reel power transmission line or seed transport tube.
Rotor craft comprises a post and multiaxis rotor craft, and a post comprises single-blade and double-vane.
The beneficial effects of the utility model: adopt one group more than two to form the power transmission line in loop with the electricity consumption load of external power supply and described flight instruments, make external power supply continue the described flight instruments electric energy of supply by power transmission line, almost unrestrictedly can strengthen the stagnant empty ability of described flight instruments.
Accompanying drawing explanation
Fig. 1 is the fundamental diagram of the external power source remote controlled rotary-wing flight seeding apparatus of a band seed transport tube.
Fig. 2 is the running orbit figure of the external power source remote controlled rotary-wing flight seeding apparatus of a band seed transport tube.
Fig. 3 is the fundamental diagram of the external power source remote controlled rotary-wing flight seeding apparatus of a band intermediate bin.
1. sowing aircraft in figure; 2. assisting in flying device; 3. follow the tracks of dolly; 4. fuselage; 5. electronic rotor; 6. external power supply; 7. power transmission line; 8. automatic wire winding device; 9. seed transport tube; 10. automatic retraction device; 11. storehouse cylinders; 12. choose high bar; 13. sowing facilities; 14. ridges; 15. intermediate bins; 16. seeds take out valve; 17. landing platforms.
Detailed description of the invention
Fig. 1 and Fig. 2 provides embodiment 1 jointly.
In embodiment 1, manufacture the external power source remote controlled rotary-wing flight seeding apparatus of a band seed transport tube, namely the sowing unit comprising two frame rotor craft compositions sows aircraft 1 and assisting in flying device 2, and adopts a tracking dolly 3.Sowing aircraft 1 and assisting in flying device 2 comprise fuselage 4, several electronic rotor 5, state of flight computer control system, radio signal reception process launch facility and remote controllers, and state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module.Described flight seeding apparatus adopts one group more than two to form the power transmission line 7 in loop with the electricity consumption load of external power supply 6 and aircraft 1,2.Follow the tracks of that dolly 3 is mounted with the automatic wire winding device 8 of power transmission line 7, the automatic retraction device 10 of seed transport tube 9, external power supply 6,11, one, storehouse cylinder choose high bar 12 and landing platform 17.Flight seeding apparatus configuration sowing facility also adopts the seed transport tube 9 that its two ends are communicated with storehouse cylinder 11 with sowing facility 13 respectively.Follow the tracks of dolly 3 from motion tracking assisting in flying device 2.External power supply 6 continues supply sowing unit electric energy by power transmission line 7.Storehouse cylinder 11 is configured with pneumatic seed conveying facility.Sowing facility 13 comprises and several seeders that sowing aircraft working direction is arranged vertically, level is installed.Sowing facility 13 is connected with state of flight computer control system signal by interface circuit, and the state of sowing facility 13 changes according to the change of state of flight computer control system state.
Automatic wire winding device 8 is for automatic deploying and retracting power transmission line 7.Automatic retraction device 10 is for automatic deploying and retracting seed folding and unfolding pipe.Pneumatic seed conveying facility is used for seed pump to eminence.Sowing facility is used for sowing.Automatic wire winding device, automatic retraction device, pneumatic seed conveying facility, sowing facility and sowing unit related content can with reference to prior art.The concrete form that these facilities described comprise sowing facility 13 can have multiple.
Choose high bar 12 upwards the highest stretch out 6 meters, stretch out at most 5 meters to side, choose high bar 12 and obviously can shorten power transmission line 7 and the skyborne length of delivery pipe assembly 9.Choose high bar 12 and have multiple robotic arm, its state can adjust, and comprises the aircraft of dodging absorption liquid.The content of robotic arm can with reference to the mechanical arm technology of existing robot.
Follow the tracks of on the ridge 14 of dolly 3 between Tanaka and move.Ridge 14 both sides need the farmland wide about 2*22 rice of sowing, often next width sowed back and forth about 4 meters.
The brief introduction of work principle of embodiment 1 is: the self-inspection of external power source remote controlled rotary-wing flight seeding apparatus system boot, and assisting in flying device 2 and sowing aircraft 1 successively stop from landing platform 17 hovering that rises; Then follow the tracks of dolly 3 to follow sowing unit and to reach the spot ridge 14 place, start pneumatic seed conveying facility and also implement seeding operation.Adopt resupply vehicle to supplement seed to storehouse cylinder 11 in good time.In operation process, automatic wire winding device 8 and automatic retraction device 10 automatic deploying and retracting power transmission line 7 and seed transport tube 9.Choose high bar 12 to rotate in the semicircle scope of such as Fig. 2 dotted line.
Due to the help of assisting in flying device 2, originally needed to spray the power transmission line of maximum 22 meters of horizontal span that aircraft 1 is born, and by choosing after high bar bears about 5 meters of spans, bears 12 meters of spans by assisting in flying device, only needing to spray aircraft 1 and bearing 5 meters of horizontal spans.Operating mode is greatly improved.And for assisting in flying device 2, the vector that pulling force suffered by its both sides represents as two solid arrows in Fig. 1 is superimposed, synthesizes dotted arrow.Obvious lateral pull total amount of cancelling out each other greatly reduces, and this makes the operating mode of assisting in flying device 2 in shape.
Operation completes, and unit aircraft to drop on landing platform 17 and recalls storehouse.
Obviously, on some hillside, only use a frame sowing aircraft and band to choose the tracking dolly 3 of high bar 12, and order is followed the tracks of dolly 3 and is positioned at higher position and also can implements seeding operation to lower.The many growths of wild Tiepi Fengdou on cliff, when cliff, when conveniently can sow plantation, can more be created the wealth.
Fig. 3 provides embodiment 2.
In embodiment 2, manufacture the external power source remote controlled rotary-wing flight seeding apparatus of a band intermediate bin, namely the sowing unit comprising two frame rotor craft compositions sows aircraft 1 and assisting in flying device 2, and adopts a tracking dolly 3.Sowing aircraft 1 and assisting in flying device 2 comprise fuselage 4, several electronic rotor 5, state of flight computer control system, radio signal reception process launch facility and remote controllers.Described flight seeding apparatus adopts one group more than two to form the power transmission line 7 in loop with the electricity consumption load of external power supply 6 and aircraft 1,2.Spray on aircraft 1 and be provided with sowing facility 13 and intermediate bin 15.Follow the tracks of 11, one, the storehouse cylinder that dolly 3 is mounted with the automatic wire winding device 8 of power transmission line 7, external power supply 6, band seed take out valve 16 and choose high bar 12 and landing platform 17.Follow the tracks of dolly 3 from motion tracking assisting in flying device 2.External power supply 6 continues supply sowing unit electric energy by power transmission line 7.
The brief introduction of work principle of embodiment 2 is: the self-inspection of external power source remote controlled rotary-wing flight seeding apparatus system boot, and assisting in flying device 2 and sowing aircraft 1 successively stop from landing platform 17 hovering that rises; Then follow the tracks of dolly 3 follow sowing unit reach the spot, sowing aircraft 1 all first flies to storehouse cylinder 11 front opening seed taking-up valve 16 at every turn and puts seed into intermediate bin 15, from then implementing seeding operation one back and forth, sowing 176(44*4 as described above) sq m; And again fly back and add storehouse, sow again ...In operation process, automatic wire winding device 8 automatic deploying and retracting power transmission line 7 coordinates.Operation completes, and unit aircraft to drop on landing platform 17 and recalls storehouse.
Due to can long-time continuous operation, the utility model than existing can only stagnant sky number minute much higher times of sowing aircraft work efficiency, the resource changing battery need not be configured.Again because seeding operation is not interrupted, neither broadcast leakage also not multicast, efficiency is high.
The weight of seed transport tube and power transmission line shared by assisting in flying device, realizes sowing aircraft and connect the degree of freedom that power transmission line adds sowing above its fuselage; The support of assisting in flying device effectively can increase the Distance geometry area of sowing aircraft operation.
Sowing aircraft requirements nap of the earth flight as far as possible, adopts assisting in flying device to make sowing aircraft can connect power transmission line from above, increases the flight degree of freedom of aircraft.Adopt and choose the power transmission line load that high bar can alleviate aircraft.
Claims (3)
1. external power source remote controlled rotary-wing flight seeding apparatus, comprise fuselage, several electronic rotors, state of flight computer control system, radio signal reception process launch facility and remote controller, state of flight computer control system comprises satellite positioning-terminal, accelerometer, magnetometer, baroceptor, gyroscope and communication module, it is characterized in that described flight seeding apparatus contains one group more than two and form the power transmission line in loop with the electricity consumption load of external power supply and described aircraft, and sow facility containing one; Sowing facility is connected with state of flight computer control system signal by interface circuit, and the state of sowing facility changes according to the change of state of flight computer control system state.
2. according to external power source remote controlled rotary-wing flight seeding apparatus according to claim 1, it is characterized in that namely comprise two frame rotor crafts sows aircraft and assisting in flying device, also comprise a tracking dolly, follow the tracks of dolly and be mounted with automatic wire winding device, the automatic retraction device of seed transport tube, external power supply and storehouse cylinder; Flight seeding apparatus contains a seed transport tube, and seed transport tube two ends are communicated with storehouse cylinder with sowing facility respectively.
3., according to external power source remote controlled rotary-wing flight seeding apparatus according to claim 1, it is characterized in that namely comprise two frame rotor crafts sows aircraft and assisting in flying device, also comprises a tracking dolly; Containing an intermediate bin on sowing aircraft; Follow the tracks of dolly and be mounted with the storehouse cylinder that automatic wire winding device, external power supply and band seed take out valve.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520723319.7U CN204979244U (en) | 2015-09-18 | 2015-09-18 | External power source power supply remote control rotor flight seeder |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520723319.7U CN204979244U (en) | 2015-09-18 | 2015-09-18 | External power source power supply remote control rotor flight seeder |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204979244U true CN204979244U (en) | 2016-01-20 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520723319.7U Expired - Fee Related CN204979244U (en) | 2015-09-18 | 2015-09-18 | External power source power supply remote control rotor flight seeder |
Country Status (1)
| Country | Link |
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| CN (1) | CN204979244U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105960905A (en) * | 2016-06-24 | 2016-09-28 | 河南沃野智能科技有限公司 | Multi-rotor sowing aircraft and method |
-
2015
- 2015-09-18 CN CN201520723319.7U patent/CN204979244U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105960905A (en) * | 2016-06-24 | 2016-09-28 | 河南沃野智能科技有限公司 | Multi-rotor sowing aircraft and method |
| CN105960905B (en) * | 2016-06-24 | 2018-10-26 | 河南沃野智能科技有限公司 | A kind of more rotors sowing aircraft and method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160120 Termination date: 20170918 |