CN106275406A - A kind of safe and reliable energy-saving unmanned plane - Google Patents
A kind of safe and reliable energy-saving unmanned plane Download PDFInfo
- Publication number
- CN106275406A CN106275406A CN201610806341.7A CN201610806341A CN106275406A CN 106275406 A CN106275406 A CN 106275406A CN 201610806341 A CN201610806341 A CN 201610806341A CN 106275406 A CN106275406 A CN 106275406A
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- Prior art keywords
- unmanned plane
- blast
- driven
- safe
- unit
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Classifications
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C25/00—Alighting gear
- B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface
- B64C25/58—Arrangements or adaptations of shock-absorbers or springs
- B64C25/62—Spring shock-absorbers; Springs
-
- 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
nullThe present invention relates to a kind of safe and reliable energy-saving unmanned plane，Including main body、Four horizontally disposed poles and two second driving motors，Being shaped as of the horizontal cross-section of described main body is back-shaped，Described pole is fixed at the corner of main body，Described pole be arranged over flying unit，The lower section of described pole is provided with buffer cell，Two described second both sides driving motor to be separately fixed at main body，Described second drives the two ends up and down of motor to be equipped with blast sensing unit，This safe and reliable energy-saving unmanned plane is by the wind-force direction in blast sensing unit detection flight course，According to direction regulation actively deep bead and the angle of driven deep bead，Thus change the blast active force to unmanned plane，Reduce energy resource consumption speed，Improve flying power，Moreover，By the buffer stopper in support unit、Piston、First spring and trachea make level Four buffered，Thus the buffer capacity of unmanned plane is greatly improved，Ensure the landing of equipment safety smoothly.
Description
Technical field
The present invention relates to a kind of safe and reliable energy-saving unmanned plane.
Background technology
Along with the technology of automation field develops, in recent years, unmanned plane with its simple structure, easily operation and
The features such as autonomous operation are more and more paid attention to, and unmanned plane is exhibited one's skill to the full in all trades and professions, progress into ordinary consumption
In the production management of the daily life of person, work entertainment and enterprise.
Unmanned plane is as an electrical equipment, owing to disconnecting with external power source in flight course, at its flight course
In need to consume continuously electric energy needed for satisfied flight, and existing unmanned plane typically requires when flight and overcomes wind
A series of active force such as power, air drag, thus further speeded up the power consumption speed of itself, cause the device flight time
Short, flying power is poor, moreover, needs landing, and due to the buffer structure of unmanned plane own at the end of unmanned plane during flying
Simply, buffer capacity when causing unmanned plane to land is limited, it is impossible to ensures unmanned plane safe falling, there are still in landing mission
Certain potential safety hazard.
Summary of the invention
The technical problem to be solved in the present invention is: in order to overcome the deficiencies in the prior art, it is provided that a kind of safe and reliable joint
Can type unmanned plane.
The technical solution adopted for the present invention to solve the technical problems is: a kind of safe and reliable energy-saving unmanned plane, bag
Including main body, four horizontally disposed poles and two second and drive motor, being shaped as of the horizontal cross-section of described main body is back-shaped, institute
State pole and be fixed at the corner of main body, described pole be arranged over flying unit, it is single that the lower section of described pole is provided with buffering
Unit, two described second both sides driving motor to be separately fixed at main body, described second drives the two ends up and down of motor to be equipped with
Blast sensing unit；
Described buffer cell includes a vertically arranged stay tube, vertically arranged piston, buffer stopper and some tracheas, described
Propping up stay tube and be fixed on the lower section of pole, be provided with barometer in described stay tube, the top of described piston is arranged in a stay tube, institute
Stating buffer stopper and be fixed on the bottom of piston, described trachea circumference is evenly distributed on the periphery of a stay tube and connects with a stay tube, institute
Stating trachea Open Side Down and arrange, described tracheal strips is provided with valve；
Both sides in described main body are equipped with groove, are provided with conveyer belt in described groove, and the inner side of described conveyer belt is provided with
Some driven tooth, described driven tooth is evenly distributed on the inner side of conveyer belt；
Being provided with the unit that actively keeps out the wind in described main body, described second drives motor to be in transmission connection with the unit that actively keeps out the wind, institute
Stating the unit that actively keeps out the wind and include actively deep bead and two active drive assemblies, described active drive assembly is arranged on deep bead
Both sides, described active drive assembly includes the second drive shaft and drives gear, and one end of described second drive shaft is fixed on actively
On deep bead, the other end of described second drive shaft is through driving gear and the second driving motor-driven connection, described driving tooth
In wheel is arranged on conveyer belt and engage with the driven tooth on conveyer belt；
The described both sides actively keeping out the wind unit are provided with some driven unit that keeps out the wind, and the described driven unit that keeps out the wind includes driven gear
Aerofoil and two driven driving assemblies, described driven driving assembly is arranged on the both sides of driven deep bead, described driven driving group
Part includes that transverse axis and driven gear, one end of described transverse axis are fixed on driven deep bead, described transverse axis through driven gear and
The other end of transverse axis is arranged on the bottom of groove, in described driven gear is arranged on conveyer belt and nibbles with the driven tooth on conveyer belt
Close；
As preferably, in order to monitor blast direction, described blast sensing unit includes that sleeve pipe, described sleeve pipe are fixed on second
Drive on motor, the vertical cross-section of described sleeve pipe be shaped as U-shaped and outward opening, be provided with in described sleeve pipe pressure transducer,
Second spring and bead, described pressure transducer is fixed on the bottom in sleeve pipe, and described pressure transducer passes through the second spring
It is connected with bead.
As preferably, in order to increase the blast active area to blast sensing unit active force, thus improve blast sensing
The sensitivity of unit, described blast sensing unit also includes that pillar and blast stressed plate, described pillar and blast stressed plate are all provided with
Putting the outside at sleeve pipe, described bead is connected with blast stressed plate by pillar.
As preferably, in order to increase the blast active area to blast sensing unit active force further, thus improve wind
Pressure sensing unit sensitivity, described blast stressed plate be shaped as hemisphere face shape.
As preferably, utilize the feature that foam is light, in order to reduce blast stressed plate pair, the material of described blast stressed plate
Matter is foam.
As preferably, in order to realize the flight function of unmanned plane, described flying unit includes the first driving motor, vertically sets
The first drive shaft put and some blades, described first drives motor to be fixed on the top of pole, described first drive motor with
First drive shaft is in transmission connection, and described blade circumference is evenly distributed on the periphery of the first drive shaft.
As preferably, in order to improve the buffer capacity of a stay tube further, in described stay tube, it is additionally provided with the first spring, institute
State barometer to be connected with piston by the first spring.
As preferably, by limiting the pore size of tracheostomy, thus ensure the gas velocity of ejection at tracheostomy
Degree, improves buffer capacity, and the aperture of the opening of described trachea is 1mm.
The invention has the beneficial effects as follows, this safe and reliable energy-saving unmanned plane was flown by the detection of blast sensing unit
Wind-force direction in journey, according to direction regulation actively deep bead and the angle of driven deep bead, thus changes blast to unmanned plane
Active force, reduce energy resource consumption speed, improve flying power, moreover, by the buffer stopper in support unit, piston,
First spring and trachea make level Four buffered, thus the buffer capacity of unmanned plane is greatly improved, and have ensured that equipment is smooth
The landing of safety.
Accompanying drawing explanation
The present invention is further described with embodiment below in conjunction with the accompanying drawings.
Fig. 1 is the structural representation of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 2 is the structural representation of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 3 is the structural representation of the buffer cell of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 4 is the structural representation of the buffer cell of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 5 is the structural representation of the blast sensing unit of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 6 is the structural representation of the wind-blocking mechanism of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 7 is the structural representation of the unit that actively keeps out the wind of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 8 is the structural representation of the driven unit that keeps out the wind of the safe and reliable energy-saving unmanned plane of the present invention；
In figure: 1. main body, 2. pole, 3. first drive motor, 4. the first drive shaft, 5. blade, 6. second drive motor,
7. blast sensing unit, 8. a stay tube, 9. piston, 10. buffer stopper, 11. tracheas, 12. valves, 13. barometers, 14. first bullets
Spring, 15. sleeve pipes, 16. pressure transducers, 17. second springs, 18. beades, 19. pillars, 20. blast stressed plates, 21. flights
Unit, 22. actively keep out the wind unit, the 23. driven unit that keep out the wind, 24. conveyer belts, 25. driven tooth, and 26. drive gears, and 27. second
Drive shaft, 28. driven gears, 29. transverse axis, 30. driven deep beads, 31. active deep beads, 33. grooves.
Detailed description of the invention
In conjunction with the accompanying drawings, the present invention is further detailed explanation.These accompanying drawings are the schematic diagram of simplification, only with
The basic structure of the illustration explanation present invention, therefore it only shows the composition relevant with the present invention.
As Figure 1-Figure 8, a kind of safe and reliable energy-saving unmanned plane, including 1, four horizontally disposed poles of main body
2 and two second drive motors 6, being shaped as of the horizontal cross-section of described main body 1 is back-shaped, and described pole 2 is fixed on the four of main body 1
At angle, described pole 2 be arranged over flying unit, the lower section of described pole 2 is provided with buffer cell, two described second drive
Motor 6 is separately fixed at the both sides of main body 1, and described second drives the two ends up and down of motor 6 to be equipped with blast sensing unit 7；
Described buffer cell includes a vertically arranged stay tube 8, vertically arranged piston 9, buffer stopper 10 and some tracheas
11, described stay tube 8 is fixed on the lower section of pole 2, is provided with barometer 13 in described stay tube 8, and the top of described piston 9 is arranged
In a stay tube 8, described buffer stopper 10 is fixed on the bottom of piston 9, and described trachea 11 circumference is evenly distributed on outside a stay tube 8
Week and connecting with stay tube 8, Open Side Down arranges for described trachea 11, is provided with valve 12 in described trachea 11；
Both sides in described main body 1 are equipped with groove 33, are provided with conveyer belt 24 in described groove 33, described conveyer belt 24
Inner side is provided with some driven tooth 25, and described driven tooth 25 is evenly distributed on the inner side of conveyer belt 24；
Being provided with the unit 22 that actively keeps out the wind in described main body 1, described second drives motor 6 and actively keeps out the wind unit 22 transmission even
Connecing, the described unit 22 that actively keeps out the wind includes actively deep bead 31 and two active drive assemblies, and described active drive assembly is arranged
In the both sides of deep bead 31, described active drive assembly includes the second drive shaft 27 and drives gear 26, described second drive shaft
One end of 27 is fixed on active deep bead 31, and the other end of described second drive shaft 27 is through driving gear 26 and the second driving
Motor 6 is in transmission connection, and in described driving gear 26 is arranged on conveyer belt 24 and engages with the driven tooth 25 on conveyer belt 24；
The described both sides actively keeping out the wind unit 22 are provided with some driven unit 23 that keeps out the wind, the described driven unit that keeps out the wind include from
Dynamic deep bead 30 and two driven driving assemblies, described driven driving assembly is arranged on the both sides of driven deep bead 30, described from
Dynamic driving assembly includes that transverse axis 29 and driven gear 28, one end of described transverse axis 29 are fixed on driven deep bead 30, described horizontal stroke
The other end that axle 29 passes driven gear 28 and transverse axis 29 is arranged on the bottom of groove 33, and described driven gear 28 is arranged on transmission
With in 24 and engaging with the driven tooth 25 on conveyer belt 24；
As preferably, in order to monitor blast direction, described blast sensing unit 7 includes that sleeve pipe 15, described sleeve pipe 15 are fixed
Drive on motor 6 second, the vertical cross-section of described sleeve pipe 15 be shaped as U-shaped and outward opening, be provided with in described sleeve pipe 15
Pressure transducer the 16, second spring 17 and bead 18, described pressure transducer 16 is fixed on the bottom in sleeve pipe 15, described pressure
Force transducer 15 is connected with bead 18 by the second spring 17.
As preferably, in order to increase the blast active area to blast sensing unit 7 active force, thus improve blast sensing
The sensitivity of unit 7, described blast sensing unit 7 also includes that pillar 19 and blast stressed plate 20, described pillar 19 and blast are subject to
Power plate 20 is arranged at the outside of sleeve pipe 15, and described bead 18 is connected with blast stressed plate 20 by pillar 19.
As preferably, in order to increase the blast active area to blast sensing unit 7 active force further, thus improve wind
Pressure sensing unit 7 sensitivity, described blast stressed plate 20 be shaped as hemisphere face shape.
As preferably, utilize the feature that foam is light, right in order to reduce blast stressed plate 20, described blast stressed plate 20
Material be foam.
As preferably, in order to realize the flight function of unmanned plane, described flying unit 21 includes the first driving motor 3, erects
To the first drive shaft 4 arranged and some blades 5, described first drives motor 3 to be fixed on the top of pole 2, and described first drives
Galvanic electricity machine 3 is in transmission connection with the first drive shaft 4, and described blade 5 circumference is evenly distributed on the periphery of the first drive shaft 4.
As preferably, in order to improve the buffer capacity of a stay tube 8 further, in described stay tube 8, it is additionally provided with the first spring
14, described barometer 13 is connected with piston 9 by the first spring 14.
As preferably, by limiting the pore size of trachea 11 opening, thus ensure the gas from the ejection of trachea 11 opening part
Flow Velocity, improves buffer capacity, and the aperture of the opening of described trachea 11 is 1mm.
During unmanned plane during flying, in order to improve the flying power of unmanned plane, it is ensured that the sufficient flight time, by main body
The driven unit 23 that keeps out the wind of actively keep out the wind unit 22 and both sides in 1 utilizes blast and air drag, reduces power consumption, reduces
Energy resource consumption thus improve the flight time.First driven the blast sensing unit 7 at motor about 6 two ends to detect by second to fly
Wind-force direction in journey, utilizes the hemispherical design of blast stressed plate 20 to improve the active area of blast, when second drives electricity
When the pressure transducer 16 in blast sensing unit 7 below machine 6 detects pressure data, show that now wind direction is upwards, utilize
Actively keep out the wind in unit 22 second driving motor 6 rotate, drive driving gear 28 rotate, recycling conveyer belt 24 on driven
Tooth 25 engages with driven gear 28, makes the active deep bead 31 actively keeping out the wind in unit 22 and both sides are driven keeps out the wind in unit 23
Driven deep bead 30 turns to level angle, thus increases blast and actively deep bead 31, the contact area of driven deep bead 30,
Improve the active force of blast, thus reduce in flying unit 21 by the first power consumption driving motor 3, with second driving electricity
When the pressure transducer 16 in blast sensing unit 7 above machine 6 detects pressure data, show that now wind direction is downward, now
By second drive motor 6 make the active deep bead 31 actively keeping out the wind in unit 22 and both sides driven keep out the wind in unit 23 driven
Deep bead 30 turns to vertical angle, thus reduces blast and actively deep bead 31, the contact area of driven deep bead 30, reduces
The active force of blast, the resistance making unmanned plane during flying be overcome reduces, and then reduces power consumption.This is safe and reliable energy-conservation
Type unmanned plane detects the wind-force direction in flight course by blast sensing unit 7, according to direction regulation actively deep bead 31 He
The angle of driven deep bead 30, thus change the blast active force to unmanned plane, reduce energy resource consumption speed, improve continuation of the journey energy
Power.
In order to ensure that the safety and steady of unmanned plane lands, in buffer cell, utilize buffer stopper 10 to make first-level buffer and process,
Along with unmanned plane height reduction, the air compression in a stay tube 8 is processed after contacting ground by piston 9, overcomes air drag, makes nothing
Man-machine level 2 buffering of making processes, and makees three pole buffered, afterwards entering along with air compression at the first spring 14 utilizing compression
OK, after barometer 13 detects that the air pressure in a stay tube 8 reaches certain value, open the valve 12 in a stay tube 8 circumference trachea 11,
The air of compression is discharged from the outlet that trachea 11 is downward, forms air-flow, unmanned plane is produced active force upwards, thus completes four
Level buffered, it is ensured that the landing of unmanned plane safety smoothly.This safe and reliable energy-saving unmanned plane is by support unit
Buffer stopper 10, piston the 9, first spring 14 and trachea 11 make level Four buffered, thus the buffering of unmanned plane is greatly improved
Ability, has ensured the landing of equipment safety smoothly.
Compared with prior art, this safe and reliable energy-saving unmanned plane detects flight course by blast sensing unit 7
In wind-force direction, according to direction regulation actively deep bead 31 and the angle of driven deep bead 30, thus change blast to unmanned
The active force of machine, reduces energy resource consumption speed, improves flying power, moreover, by the buffer stopper 10 in support unit, lives
Plug the 9, first spring 14 and trachea 11 make level Four buffered, thus the buffer capacity of unmanned plane is greatly improved, and ensure
The landing of equipment safety smoothly.
With the above-mentioned desirable embodiment according to the present invention for enlightenment, by above-mentioned description, relevant staff is complete
Entirely can carry out various change and amendment in the range of without departing from this invention technological thought.The technology of this invention
The content that property scope is not limited in description, it is necessary to determine its technical scope according to right.
Claims (8)
1. a safe and reliable energy-saving unmanned plane, it is characterised in that include main body (1), four horizontally disposed poles (2)
Driving motor (6) with two second, being shaped as of the horizontal cross-section of described main body (1) is back-shaped, and described pole (2) is fixed on main body
(1) at corner, described pole (2) be arranged over flying unit, the lower section of described pole (2) is provided with buffer cell, two
Described second drives motor (6) to be separately fixed at the both sides of main body (1), and described second drives the two ends up and down of motor (6) to be all provided with
There is blast sensing unit (7)；
Described buffer cell include vertically arranged stay tube (8), vertically arranged piston (9), buffer stopper (10) and if dry gas
Pipe (11), described stay tube (8) is fixed on the lower section of pole (2), is provided with barometer (13), described work in described stay tube (8)
The top of plug (9) is arranged in a stay tube (8), and described buffer stopper (10) is fixed on the bottom of piston (9), described trachea (11) week
To being evenly distributed on the periphery of stay tube (8) and connect with a stay tube (8), described trachea (11) Open Side Down setting, described
Valve (12) it is provided with in trachea (11)；
Both sides in described main body (1) are equipped with groove (33), are provided with conveyer belt (24), described conveyer belt in described groove (33)
(24) inner side is provided with some driven tooth (25), and described driven tooth (25) is evenly distributed on the inner side of conveyer belt (24)；
Being provided with the unit that actively keeps out the wind (22) in described main body (1), described second drives motor (6) and unit (22) biography of actively keeping out the wind
Being dynamically connected, the described unit (22) that actively keeps out the wind includes actively deep bead (31) and two active drive assemblies, described active drive
Assembly is arranged on the both sides of deep bead (31), and described active drive assembly includes the second drive shaft (27) and drives gear (26),
One end of described second drive shaft (27) is fixed in active deep bead (31), and the other end of described second drive shaft (27) passes
Drive gear (26) to drive motor (6) to be in transmission connection with second, described driving gear (26) be arranged on conveyer belt (24) interior and with
Driven tooth (25) engagement on conveyer belt (24)；
The described both sides actively keeping out the wind unit (22) are provided with some driven unit that keeps out the wind (23), the described driven unit that keeps out the wind include from
Dynamic deep bead (30) and two driven driving assemblies, described driven driving assembly is arranged on the both sides of driven deep bead (30), institute
Stating driven driving assembly and include transverse axis (29) and driven gear (28), one end of described transverse axis (29) is fixed on driven deep bead
(30), on, described transverse axis (29) is arranged on the bottom of groove (33), institute through the other end of driven gear (28) and transverse axis (29)
State in driven gear (28) is arranged on conveyer belt (24) and engage with the driven tooth (25) on conveyer belt (24)；
The most safe and reliable energy-saving unmanned plane, it is characterised in that described blast sensing unit (7)
Including sleeve pipe (15), described sleeve pipe (15) is fixed on the second driving motor (6), the shape of the vertical cross-section of described sleeve pipe (15)
For U-shaped and outward opening, in described sleeve pipe (15), it is provided with pressure transducer (16), the second spring (17) and bead (18), institute
Stating the bottom that pressure transducer (16) is fixed in sleeve pipe (15), described pressure transducer (15) passes through the second spring (17) and glass
Glass pearl (18) connects.
The most safe and reliable energy-saving unmanned plane, it is characterised in that described blast sensing unit (7)
Also include that pillar (19) and blast stressed plate (20), described pillar (19) and blast stressed plate (20) are arranged at sleeve pipe (15)
Outside, described bead (18) is connected with blast stressed plate (20) by pillar (19).
The most safe and reliable energy-saving unmanned plane, it is characterised in that described blast stressed plate (20)
It is shaped as hemisphere face shape.
The most safe and reliable energy-saving unmanned plane, it is characterised in that described blast stressed plate (20)
Material is foam.
The most safe and reliable energy-saving unmanned plane, it is characterised in that described flying unit (21) includes
First drives motor (3), vertically arranged the first drive shaft (4) and some blades (5), and described first drives motor (3) to fix
In the top of pole (2), described first drives motor (3) to be in transmission connection with the first drive shaft (4), and described blade (5) circumference is all
The even periphery being distributed in the first drive shaft (4).
The most safe and reliable energy-saving unmanned plane, it is characterised in that also set in described stay tube (8)
Having the first spring (14), described barometer (13) is connected with piston (9) by the first spring (14).
The most safe and reliable energy-saving unmanned plane, it is characterised in that the opening of described trachea (11)
Aperture is 1mm.
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| CN201610806341.7A CN106275406B (en) | 2016-09-05 | 2016-09-05 | A kind of safe and reliable energy-saving unmanned plane |
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| CN201610806341.7A CN106275406B (en) | 2016-09-05 | 2016-09-05 | A kind of safe and reliable energy-saving unmanned plane |
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Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN106892099A (en) * | 2017-03-15 | 2017-06-27 | 深圳市雷凌广通技术研发有限公司 | A kind of strong energy-saving unmanned plane of endurance |
| CN107117315A (en) * | 2017-05-16 | 2017-09-01 | 广州鼎飞航空科技有限公司 | One kind is airborne to penetrate net riot gear and unmanned plane |
| CN107284670A (en) * | 2017-06-05 | 2017-10-24 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for being used to pour with shock-absorbing function |
| CN107284680A (en) * | 2017-06-05 | 2017-10-24 | 深圳市雷凌广通技术研发有限公司 | A kind of intelligent unmanned machine for fire-fighting based on Internet of Things |
| CN107972868A (en) * | 2017-11-28 | 2018-05-01 | 深圳市雷凌广通技术研发有限公司 | A kind of vehicle-mounted unmanned aerial vehicle for being used for meteorological detection based on Internet of Things |
| CN108128445A (en) * | 2017-12-22 | 2018-06-08 | 中交遥感载荷（安徽）科技有限公司 | A kind of unmanned machine automatic drive hovering system |
| CN108557092A (en) * | 2018-03-15 | 2018-09-21 | 清远市巨劲科技有限公司 | One kind take photo by plane unmanned plane decline deceleration device |
| CN109131915A (en) * | 2018-09-20 | 2019-01-04 | 广州大学 | A kind of wind resistance unmanned plane with wind direction identification function |
| CN109367780A (en) * | 2018-11-30 | 2019-02-22 | 国网河南省电力公司偃师市供电公司 | A kind of Electric Power Patrol unmanned plane |
| WO2019077963A1 (en) * | 2017-10-16 | 2019-04-25 | ローム株式会社 | Unmanned aerial vehicle and control method therefor |
| CN111498094A (en) * | 2020-04-23 | 2020-08-07 | 杭州流富科技有限公司 | Unmanned aerial vehicle descending buffer device based on gear transmission |
| CN113856093A (en) * | 2021-09-17 | 2021-12-31 | 重庆齐伶科贸有限公司 | Fire extinguishing method for forest fire control and fire extinguishing unmanned aerial vehicle |
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