CN106275406B - 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
- CN106275406B CN106275406B CN201610806341.7A CN201610806341A CN106275406B CN 106275406 B CN106275406 B CN 106275406B CN 201610806341 A CN201610806341 A CN 201610806341A CN 106275406 B CN106275406 B CN 106275406B
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- wind
- unmanned plane
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- safe
- unit
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- 210000000515 tooth Anatomy 0.000 claims description 14
- 239000011324 bead Substances 0.000 claims description 8
- 239000006260 foam Substances 0.000 claims description 5
- 239000000463 material Substances 0.000 claims description 3
- 239000011521 glass Substances 0.000 claims 2
- 238000005265 energy consumption Methods 0.000 abstract description 5
- 238000010586 diagram Methods 0.000 description 9
- 230000006835 compression Effects 0.000 description 4
- 238000007906 compression Methods 0.000 description 4
- 230000035945 sensitivity Effects 0.000 description 4
- 230000003139 buffering effect Effects 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 230000005611 electricity Effects 0.000 description 2
- 230000006698 induction Effects 0.000 description 2
- 239000011148 porous material Substances 0.000 description 2
- 241000486406 Trachea Species 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000025518 detection of mechanical stimulus involved in sensory perception of wind Effects 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 210000003437 trachea Anatomy 0.000 description 1
Classifications
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- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Remote Sensing (AREA)
- Wind Motors (AREA)
Abstract
The present invention relates to a kind of safe and reliable energy-saving unmanned planes,Including main body,Four horizontally disposed struts and two the first driving motors,The shape of the horizontal cross-section of the main body is back-shaped,The strut is fixed on the four corners of main body,The top of the strut is equipped with flying unit,The lower section of the strut is equipped with buffer cell,Two first driving motors are separately fixed at the both sides of main body,The upper and lower ends of first driving motor are equipped with wind pressure sensing unit,The safe and reliable energy-saving unmanned plane detects the wind-force direction in flight course by wind pressure sensing unit,The angle of active wind shield and driven wind shield is adjusted according to direction,To change active force of the wind pressure to unmanned plane,Reduce energy consumption speed,Improve cruising ability,Moreover,Pass through the buffer stopper in support unit,Piston,Second spring and tracheae make level Four buffered,To which the buffer capacity of unmanned plane be greatly improved,The landing of the smooth safety of equipment is ensured.
Description
Technical field
The present invention relates to a kind of safe and reliable energy-saving unmanned planes.
Background technology
Develop with the technology of automation field, in recent years, unmanned plane with its simple structure, convenient operation and
The features such as autonomous operation, is more and more paid attention to, and unmanned plane is exhibited one's skill to the full in all trades and professions, progresses into ordinary consumption
In the production management of the daily life of person, work entertainment and enterprise.
Unmanned plane is as an electrical equipment, due to being disconnected with external power supply in flight course, in its flight course
In need continuously to consume electric energy to meet needed for flight, and existing unmanned plane usually requires to overcome wind in flight
A series of active forces such as power, air drag lead to the device flight time to further speed up the power consumption speed of itself
It is short, cruising ability is poor, moreover, need to land at the end of unmanned plane during flying, and due to the buffer structure of unmanned plane itself
Simply, buffer capacity when causing unmanned plane to land is limited, can not ensure unmanned plane safe falling, in landing mission there are still
Some potential safety problems.
Invention content
The technical problem to be solved by the present invention is to：For overcome the deficiencies in the prior art, a kind of safe and reliable section is provided
It can type unmanned plane.
The technical solution adopted by the present invention to solve the technical problems is：A kind of safe and reliable energy-saving unmanned plane, packet
Main body, four horizontally disposed struts and two the first driving motors are included, the shape of the horizontal cross-section of the main body is back-shaped, institute
The four corners that strut is fixed on main body are stated, the top of the strut is equipped with flying unit, and the lower section of the strut is equipped with buffering list
Member, two first driving motors are separately fixed at the both sides of main body, and the upper and lower ends of first driving motor are equipped with
Wind pressure sensing unit；
The buffer cell includes vertically arranged support tube, vertically arranged piston, buffer stopper and several tracheae, described
Support tube is fixed on the lower section of strut, and barometer is equipped in the support tube, and the top of the piston is arranged in support tube, institute
The bottom end that buffer stopper is fixed on piston is stated, the tracheae is circumferentially evenly distributed on the periphery of support tube and is connected to support tube, institute
Tracheae is stated Open Side Down setting, the tracheal strips are equipped with valve；
Both sides in the main body are all provided with fluted, conveyer belt are equipped in the groove, the inside of the conveyer belt is equipped with
Several driven tooths, the driven tooth are evenly distributed on the inside of conveyer belt；
The unit that actively keeps out the wind, first driving motor and unit drive connection of actively keeping out the wind, institute are equipped in the main body
It includes active wind shield and two active drive components to state the unit that actively keeps out the wind, and the active drive component setting is actively being kept out the wind
The both sides of plate, the active drive component include the first drive shaft and driving gear, and one end of first drive shaft is fixed on
On active wind shield, the other end of first drive shaft passes through driving gear and the first driving motor to be sequentially connected, the drive
Moving gear be arranged in conveyer belt and with the driven tooth engagement on conveyer belt；
The both sides of the unit that actively keeps out the wind are equipped with several driven units that keep out the wind, and the driven unit that keeps out the wind includes driven gear
Aerofoil and two driven drive components, the driven drive component are arranged in the both sides of driven wind shield, the driven driving group
Part includes horizontal axis and driven gear, and one end of the horizontal axis is fixed on driven wind shield, the horizontal axis pass through driven gear and
The other end of horizontal axis is arranged in the bottom of groove, and the driven gear is arranged in conveyer belt and is nibbled with the driven tooth on conveyer belt
It closes；
Preferably, in order to monitor wind pressure direction, the wind pressure sensing unit includes casing, and described sleeve pipe is fixed on first
On driving motor, the shape of the vertical cross-section of described sleeve pipe is U-shaped and outward opening, be equipped in described sleeve pipe pressure sensor,
First spring and bead, the pressure sensor are fixed on the bottom in casing, and the pressure sensor passes through the first spring
It is connect with bead.
Preferably, in order to increase active area of the wind pressure to wind pressure sensing unit active force, to improve wind pressure induction
The sensitivity of unit, the wind pressure sensing unit further include pillar and wind pressure stressed plate, and the pillar and wind pressure stressed plate are all provided with
It sets in the outside of casing, the bead is connect by pillar with wind pressure stressed plate.
Preferably, in order to further increase active area of the wind pressure to wind pressure sensing unit active force, to improve wind
The sensitivity of sensing unit is pressed, the shape of the wind pressure stressed plate is hemisphere face shape.
Preferably, using the light feature of foam, in order to reduce wind pressure stressed plate pair, the material of the wind pressure stressed plate
Matter is foam.
Preferably, in order to realize that the flight function of unmanned plane, the flying unit include the second driving motor, vertically set
The second drive shaft set and several blades, second driving motor are fixed on the top of strut, second driving motor with
Second drive shaft is sequentially connected, and the blade is circumferentially evenly distributed on the periphery of the second drive shaft.
Preferably, in order to further increase the buffer capacity of support tube, second spring, institute are additionally provided in the support tube
Barometer is stated to connect with piston by second spring.
Preferably, the pore size by limiting tracheostomy, to ensure the gas velocity sprayed from tracheostomy
Degree improves buffer capacity, and the aperture of the opening of the tracheae is 1mm.
The invention has the advantages that the safe and reliable energy-saving unmanned plane was flown by the detection of wind pressure sensing unit
Wind-force direction in journey adjusts the angle of active wind shield and driven wind shield according to direction, to change wind pressure to unmanned plane
Active force, reduce energy consumption speed, improve cruising ability, moreover, by buffer stopper in support unit, piston,
Second spring and tracheae make level Four buffered, to which the buffer capacity of unmanned plane be greatly improved, have ensured that equipment is smooth
The landing of safety.
Description of the drawings
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 2 is the structural schematic diagram of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 3 is the structural schematic diagram of the buffer cell of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 4 is the structural schematic diagram of the buffer cell of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 5 is the structural schematic diagram of the wind pressure sensing unit of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 6 is the structural schematic diagram of the wind-blocking mechanism of the safe and reliable energy-saving unmanned plane of the present invention；
Fig. 7 is the structural schematic diagram 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 schematic diagram 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. struts, 3. second driving motors, 4. second drive shafts, 5. blades, 6. first driving motors,
7. wind pressure sensing unit, 8. support tubes, 9. pistons, 10. buffer stoppers, 11. tracheaes, 12. valves, 13. barometers, 14. second bullets
Spring, 15. casings, 16. pressure sensors, 17. first springs, 18. beades, 19. pillars, 20. wind pressure stressed plates, 21. flights
Unit, 22. actively keep out the wind unit, the 23. driven units that keep out the wind, 24. conveyer belts, 25. driven tooths, 26. driving gears, and 27. first
Drive shaft, 28. driven gears, 29. horizontal axis, 30. driven wind shields, 31. active wind shields, 33. grooves.
Specific implementation mode
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates the basic structure of the present invention, therefore it only shows the composition relevant to the invention.
As Figure 1-Figure 8, a kind of safe and reliable energy-saving unmanned plane, including 1, four horizontally disposed strut of main body
2 and two the first driving motors 6, the shape of the horizontal cross-section of the main body 1 is back-shaped, and the strut 2 is fixed on the four of main body 1
At angle, the top of the strut 2 is equipped with flying unit, and the lower section of the strut 2 is equipped with buffer cell, two first drivings
Motor 6 is separately fixed at the both sides of main body 1, and the upper and lower ends of first driving motor 6 are equipped with wind pressure sensing unit 7；
The buffer cell includes vertically arranged support tube 8, vertically arranged piston 9, buffer stopper 10 and several tracheae
11, the support tube 8 is fixed on the lower section of strut 2, and barometer 13 is equipped in the support tube 8, and the top of the piston 9 is arranged
In support tube 8, the buffer stopper 10 is fixed on the bottom end of piston 9, and the tracheae 11 is circumferential to be evenly distributed on the outer of support tube 8
Week and be connected to support tube 8, Open Side Down the setting of the tracheae 11, equipped with valve 12 in the tracheae 11；
Both sides in the main body 1 are all provided with fluted 33, and conveyer belt 24 is equipped in the groove 33, the conveyer belt 24
Inside is equipped with several driven tooths 25, and the driven tooth 25 is evenly distributed on the inside of conveyer belt 24；
The unit 22 that actively keeps out the wind is equipped in the main body 1, first driving motor 6 and the transmission of unit 22 of actively keeping out the wind connect
It connects, the unit 22 that actively keeps out the wind includes active wind shield 31 and two active drive components, the active drive component setting
In the both sides of active wind shield 31, the active drive component includes the first drive shaft 27 and driving gear 26, and described first drives
One end of moving axis 27 is fixed on active wind shield 31, and the other end of first drive shaft 27 passes through driving gear 26 and first
Driving motor 6 is sequentially connected, and the driving gear 26 is arranged in conveyer belt 24 and is engaged with the driven tooth 25 on conveyer belt 24；
The both sides of the unit 22 that actively keeps out the wind be equipped with several driven units 23 that keep out the wind, the driven unit that keeps out the wind include from
Dynamic wind shield 30 and two driven drive components, the driven drive component are arranged in the both sides of driven wind shield 30, it is described from
Dynamic drive component includes horizontal axis 29 and driven gear 28, and one end of the horizontal axis 29 is fixed on driven wind shield 30, the cross
Axis 29 passes through the other end of driven gear 28 and horizontal axis 29 to be arranged in the bottom of groove 33, and the setting of the driven gear 28 is transmitting
With being engaged in 24 and with the driven tooth 25 on conveyer belt 24.
Preferably, in order to monitor wind pressure direction, the wind pressure sensing unit 7 includes casing 15, and described sleeve pipe 15 is fixed
On the first driving motor 6, the shape of the vertical cross-section of described sleeve pipe 15 is U-shaped and outward opening, is equipped in described sleeve pipe 15
Pressure sensor 16, the first spring 17 and bead 18, the pressure sensor 16 are fixed on the bottom in casing 15, the pressure
Force snesor 16 is connect by the first spring 17 with bead 18.
Preferably, in order to increase active area of the wind pressure to 7 active force of wind pressure sensing unit, to improve wind pressure induction
The sensitivity of unit 7, the wind pressure sensing unit 7 further include pillar 19 and wind pressure stressed plate 20, the pillar 19 and wind pressure by
Power plate 20 is arranged at the outside of casing 15, and the bead 18 is connect by pillar 19 with wind pressure stressed plate 20.
Preferably, in order to further increase active area of the wind pressure to 7 active force of wind pressure sensing unit, to improve wind
The sensitivity of sensing unit 7 is pressed, the shape of the wind pressure stressed plate 20 is hemisphere face shape.
Preferably, using the light feature of foam, the wind pressure stressed plate 20 right in order to reduce wind pressure stressed plate 20
Material be foam.
Preferably, in order to realize that the flight function of unmanned plane, the flying unit 21 include the second driving motor 3, erect
To the second drive shaft 4 and several blades 5 of setting, second driving motor 3 is fixed on the top of strut 2, and described second drives
3 and second drive shaft 4 of dynamic motor is sequentially connected, the circumferential periphery for being evenly distributed on the second drive shaft 4 of the blade 5.
Preferably, in order to further increase the buffer capacity of support tube 8, second spring is additionally provided in the support tube 8
14, the barometer 13 is connect by second spring 14 with piston 9.
Preferably, the pore size being open by limiting tracheae 11, to ensure the gas sprayed from 11 opening of tracheae
Flow velocity degree improves buffer capacity, and the aperture of the opening of the tracheae 11 is 1mm.
During unmanned plane during flying, in order to improve the cruising ability of unmanned plane, ensure the sufficient flight time, by main body
Actively keep out the wind unit 22 and driven keep out the wind unit 23 utilization wind pressure and the air drag of both sides in 1, reduce power consumption, reduce
Energy consumption is to improve the flight time.It was flown first by the detection of the wind pressure sensing unit 7 of 6 upper and lower ends of the first driving motor
Wind-force direction in journey improves the active area of wind pressure using the hemispherical design of wind pressure stressed plate 20, when the first driving electricity
When pressure sensor 16 in the wind pressure sensing unit 7 of 6 lower section of machine detects pressure data, shows that wind direction is upward at this time, utilize
The first driving motor 6 rotation actively kept out the wind in unit 22, drives driving gear 28 to rotate, and recycles driven on conveyer belt 24
Tooth 25 is engaged with driven gear 28, in the driven unit 23 that keeps out the wind of active wind shield 31 and both sides in the unit 22 that makes actively to keep out the wind
Driven wind shield 30 turns to level angle, to increase the contact area of wind pressure and active wind shield 31, driven wind shield 30,
The active force for improving wind pressure together should the first driving electricity to reduce the power consumption of the second driving motor 3 in flying unit 21
When pressure sensor 16 in the wind pressure sensing unit 7 of 6 top of machine detects pressure data, show that wind direction is downward at this time, at this time
It is driven in the driven unit 23 that keeps out the wind of active wind shield 31 and both sides for making actively to keep out the wind by the first driving motor 6 in unit 22
Wind shield 30 turns to vertical angle, to reduce the contact area of wind pressure and active wind shield 31, driven wind shield 30, reduces
The active force of wind pressure makes the resistance that unmanned plane during flying is overcome reduce, thereby reduces power consumption.This is safe and reliable energy saving
Type unmanned plane detects the wind-force direction in flight course by wind pressure sensing unit 7, and 31 He of active wind shield is adjusted according to direction
The angle of driven wind shield 30 reduces energy consumption speed to change active force of the wind pressure to unmanned plane, improves continuation of the journey energy
Power.
In order to ensure unmanned plane safety and steady landing, in buffer cell, make first-level buffer processing using buffer stopper 10,
As unmanned plane height reduces, to the air compression processing in support tube 8 behind the contact of piston 9 ground, overcomes air drag, make nothing
It is man-machine to make level 2 buffering processing, using compression second spring 14 make three pole buffereds, later with air compression into
Row after barometer 13 detects that the air pressure in support tube 8 reaches certain value, opens the valve 12 in 8 circumferential direction tracheae 11 of support tube,
The air of compression is discharged from the downward outlet of tracheae 11, forms air-flow, upward active force is generated to unmanned plane, to complete four
Grade buffered ensures the landing of the smooth safety of unmanned plane.The safe and reliable energy-saving unmanned plane passes through in support unit
Buffer stopper 10, piston 9, second spring 14 and tracheae 11 make level Four buffered, to which the buffering of unmanned plane be greatly improved
Ability has ensured the landing of the smooth safety of equipment.
Compared with prior art, which detects flight course by wind pressure sensing unit 7
In wind-force direction, the angle of active wind shield 31 and driven wind shield 30 is adjusted according to direction, to change wind pressure to nobody
The active force of machine reduces energy consumption speed, improves cruising ability, moreover, passes through the buffer stopper 10 in support unit, work
Plug 9, second spring 14 and tracheae 11 make level Four buffered, to which the buffer capacity of unmanned plane be greatly improved, ensure
The landing of the smooth safety of equipment.
It is enlightenment with above-mentioned desirable embodiment according to the present invention, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to determine its technical scope according to right.
Claims (8)
1. a kind of safe and reliable energy-saving unmanned plane, which is characterized in that including main body (1), four horizontally disposed struts (2)
Shape with two the first driving motors (6), the horizontal cross-section of the main body (1) is back-shaped, and the strut (2) is fixed on main body
(1) four corners, the top of the strut (2) are equipped with flying unit, and the lower section of the strut (2) is equipped with buffer cell, two
First driving motor (6) is separately fixed at the both sides of main body (1), and the upper and lower ends of first driving motor (6) are all provided with
There is wind pressure sensing unit (7)；
The buffer cell includes vertically arranged support tube (8), vertically arranged piston (9), buffer stopper (10) and if dry gas
It manages (11), the support tube (8) is fixed on the lower section of strut (2), and barometer (13), the work are equipped in the support tube (8)
The top setting of (9) is filled in support tube (8), and the buffer stopper (10) is fixed on the bottom end of piston (9), tracheae (11) week
Be connected to the periphery for being evenly distributed on support tube (8) and with support tube (8), the tracheae (11) Open Side Down setting, it is described
Valve (12) is equipped in tracheae (11)；
Both sides in the main body (1) are all provided with fluted (33), and conveyer belt (24), the conveyer belt are equipped in the groove (33)
(24) inside is equipped with several driven tooths (25), and the driven tooth (25) is evenly distributed on the inside of conveyer belt (24)；
The unit (22) that actively keeps out the wind, first driving motor (6) and unit (22) biography of actively keeping out the wind are equipped in the main body (1)
Dynamic connection, the unit (22) that actively keeps out the wind includes active wind shield (31) and two active drive components, the active drive
In the both sides of active wind shield (31), the active drive component includes the first drive shaft (27) and driving gear for component setting
(26), one end of first drive shaft (27) is fixed on active wind shield (31), first drive shaft (27) it is another
End is sequentially connected across driving gear (26) and the first driving motor (6), and the driving gear (26) is arranged in conveyer belt (24)
It is interior and engaged with the driven tooth (25) on conveyer belt (24)；
The both sides of the unit (22) that actively keeps out the wind be equipped with several driven units that keep out the wind (23), the driven unit that keeps out the wind include from
Dynamic wind shield (30) and two driven drive components, the driven drive component are arranged in the both sides of driven wind shield (30), institute
It includes horizontal axis (29) and driven gear (28) to state driven drive component, and one end of the horizontal axis (29) is fixed on driven wind shield
(30) on, the horizontal axis (29) passes through the other end of driven gear (28) and horizontal axis (29) to be arranged in the bottom of groove (33), institute
Driven gear (28) setting is stated to engage in conveyer belt (24) and with the driven tooth (25) on conveyer belt (24).
2. safe and reliable energy-saving unmanned plane as described in claim 1, which is characterized in that the wind pressure sensing unit (7)
Including casing (15), described sleeve pipe (15) is fixed on the first driving motor (6), the shape of the vertical cross-section of described sleeve pipe (15)
For U-shaped and outward opening, described sleeve pipe (15) is interior to be equipped with pressure sensor (16), the first spring (17) and bead (18), institute
The bottom that pressure sensor (16) is fixed in casing (15) is stated, the pressure sensor (16) passes through the first spring (17) and glass
Glass pearl (18) connects.
3. safe and reliable energy-saving unmanned plane as claimed in claim 2, which is characterized in that the wind pressure sensing unit (7)
Further include pillar (19) and wind pressure stressed plate (20), the pillar (19) and wind pressure stressed plate (20) are arranged at casing (15)
Outside, the bead (18) are connect by pillar (19) with wind pressure stressed plate (20).
4. safe and reliable energy-saving unmanned plane as claimed in claim 3, which is characterized in that the wind pressure stressed plate (20)
Shape is hemisphere face shape.
5. safe and reliable energy-saving unmanned plane as claimed in claim 3, which is characterized in that the wind pressure stressed plate (20)
Material is foam.
6. safe and reliable energy-saving unmanned plane as described in claim 1, which is characterized in that the flying unit (21) includes
Second driving motor (3), vertically arranged the second drive shaft (4) and several blades (5), second driving motor (3) are fixed
Top in strut (2), second driving motor (3) are sequentially connected with the second drive shaft (4), and the blade (5) is circumferential
The even periphery for being distributed in the second drive shaft (4).
7. safe and reliable energy-saving unmanned plane as described in claim 1, which is characterized in that also set in the support tube (8)
There are second spring (14), the barometer (13) to be connect with piston (9) by second spring (14).
8. safe and reliable energy-saving unmanned plane as described in claim 1, which is characterized in that the opening of the tracheae (11)
Aperture is 1mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610806341.7A CN106275406B (en) | 2016-09-05 | 2016-09-05 | A kind of safe and reliable energy-saving unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610806341.7A CN106275406B (en) | 2016-09-05 | 2016-09-05 | A kind of safe and reliable energy-saving unmanned plane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106275406A CN106275406A (en) | 2017-01-04 |
| CN106275406B true CN106275406B (en) | 2018-07-24 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610806341.7A Expired - Fee Related CN106275406B (en) | 2016-09-05 | 2016-09-05 | A kind of safe and reliable energy-saving unmanned plane |
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| CN (1) | CN106275406B (en) |
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| CN109131915B (en) * | 2018-09-20 | 2023-08-29 | 广州大学 | A wind-resistant UAV with wind direction recognition 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 unmanned aerial vehicle for electric patrol |
| CN111498094B (en) * | 2020-04-23 | 2021-12-03 | 江苏翔龙智能装备科技有限公司 | 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 |
| CN117163343A (en) * | 2023-09-27 | 2023-12-05 | 亿航智能设备（广州）有限公司 | A kind of lifting and landing auxiliary device for maritime drones |
| CN117401195A (en) * | 2023-10-08 | 2024-01-16 | 南京华设云信息技术有限公司 | An RPA intelligent assistance system for power supply station construction |
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| CN202464124U (en) * | 2012-01-13 | 2012-10-03 | 安徽理工大学 | Four-rotor aircraft |
| US20160059958A1 (en) * | 2014-08-19 | 2016-03-03 | Tau Emerald Rotors Inc. | Controlling Rotary Wing Aircraft |
| CN104787309B (en) * | 2015-05-12 | 2016-11-09 | 厦门大学 | Unmanned rotorcraft undercarriage |
| CN205113695U (en) * | 2015-11-21 | 2016-03-30 | 长沙学院 | Four rotors aircraft of taking photo by plane |
| CN105882966B (en) * | 2016-03-30 | 2018-08-07 | 浙江聚楼信息科技有限公司 | A kind of novel unmanned plane based on Internet of Things |
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