CN109592024A - A kind of Intelligent unattended machine - Google Patents
A kind of Intelligent unattended machine Download PDFInfo
- Publication number
- CN109592024A CN109592024A CN201811429480.8A CN201811429480A CN109592024A CN 109592024 A CN109592024 A CN 109592024A CN 201811429480 A CN201811429480 A CN 201811429480A CN 109592024 A CN109592024 A CN 109592024A
- Authority
- CN
- China
- Prior art keywords
- drive shaft
- driving motor
- ontology
- fixed
- buffer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 22
- 230000003139 buffering effect Effects 0.000 claims description 15
- 239000003990 capacitor Substances 0.000 claims description 10
- 230000005611 electricity Effects 0.000 claims description 6
- 239000007787 solid Substances 0.000 claims description 3
- 230000005540 biological transmission Effects 0.000 claims description 2
- 238000004519 manufacturing process Methods 0.000 abstract description 6
- 238000004891 communication Methods 0.000 abstract description 2
- 238000010586 diagram Methods 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000010355 oscillation Effects 0.000 description 2
- 238000002604 ultrasonography Methods 0.000 description 2
- 241000272814 Anser sp. Species 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
Classifications
-
- 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
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/30—Aircraft characterised by electric power plants
- B64D27/35—Arrangements for on-board electric energy production, distribution, recovery or storage
- B64D27/353—Arrangements for on-board electric energy production, distribution, recovery or storage using solar cells
-
- G—PHYSICS
- G08—SIGNALLING
- G08C—TRANSMISSION SYSTEMS FOR MEASURED VALUES, CONTROL OR SIMILAR SIGNALS
- G08C23/00—Non-electrical signal transmission systems, e.g. optical systems
- G08C23/02—Non-electrical signal transmission systems, e.g. optical systems using infrasonic, sonic or ultrasonic waves
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Toys (AREA)
Abstract
The present invention relates to a kind of Intelligent unattended machines, it is based on Internet of Things and has the function of remote-control communication, including ontology, aviation mechanism square on the body is set, device of solar generating and the buffer gear being arranged in below ontology, the ontology is equipped with several indicator lights, the Intelligent unattended machine based on Internet of Things drives sliding panel mobile by sliding equipment, the first through hole on the second through-hole opposing clamping plate on sliding panel is set to misplace, to change the air drag of each balancing unit, adjusting unmanned plane can steady safe falling, in ultrasonic wave transmitting circuit, using conventional discrete component, the production cost of circuit is also reduced while realizing wireless signal transmitting.
Description
Technical field
The present invention relates to a kind of Intelligent unattended machines.
Background technique
As the technology of automation field develops, 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, in order to realize distant control function, often needs to emit ultrasonic signal, be believed by ultrasonic wave in flight course
It number is communicated with remote control equipment, but existing ultrasonic wave transmitting circuit process structure is relative complex, production cost is higher, makes
The big heavy discount of its market competitiveness, moreover, the landing protection structure of unmanned plane are simply single, especially in descent
In, unmanned plane is generally in heeling condition, and it is excessive with ground contact portion local pressure when leading to its landing, to cause nobody
Machine damage, further reduced the practicability of unmanned plane.
Summary of the invention
The technical problem to be solved by the present invention is for overcome the deficiencies in the prior art, provide a kind of based on Internet of Things
Intelligent unattended machine.
The technical solution adopted by the present invention to solve the technical problems is: a kind of Intelligent unattended machine based on Internet of Things, packet
It includes ontology, square on the body aviation mechanism, device of solar generating and the buffer gear being arranged in below ontology is set, it is described
Ontology is equipped with several indicator lights；
The buffer gear includes several Buffer Units, and the Buffer Unit is circumferentially evenly distributed on the periphery of ontology, described slow
Rushing component includes support frame, range sensor and two buffer cells, and support frame as described above is fixed on the lower section of ontology, the distance
The bottom end of support frame is arranged in sensor, and the buffer cell is arranged in the bottom end of support frame and is located at the two sides of support frame；
The buffer cell includes third driving motor and two balance mechanisms, and the third driving motor is fixed on support frame
On, the balance mechanism includes third drive shaft and balancing unit, and the third driving motor passes through third drive shaft and balance
Unit transmission connection；
The balancing unit includes that sliding panel, sliding equipment, two clamping plates and two pillars, the both ends of the pillar are fixed on folder
On plate, the first clamping plate is located at the top of second clamping plate, and the sliding panel and sliding equipment are respectively positioned between two clamping plates, institute
The first pillar is stated to be fixed in third drive shaft, the sliding panel and sliding equipment be arranged at the first pillar and the second pillar it
Between, the clamping plate is equipped with several first through hole, and the sliding panel is equipped with several second through-holes, the quantity of the first through hole
And one-to-one correspondence equal with the quantity of the second through-hole；
The sliding equipment includes the 4th driving motor, the 4th drive shaft and casing, and the 4th driving motor is fixed on first
On pillar, the 4th driving motor is connect with 4 wheel driven driving-axle gearing, and the 4th drive shaft is set in casing, and described
The periphery of four drive shafts is equipped with external screw thread, is equipped with internal screw thread in described sleeve pipe, the external screw thread of the 4th drive shaft and casing
Internal screw thread matches, and described sleeve pipe is fixed on sliding panel；
Central processing unit and ultrasonic wave transmitting module are equipped in the ontology, the third driving motor and the 4th driving motor are equal
It is electrically connected with central processing unit, ultrasonic wave transmitting circuit, the ultrasound wave transmitting circuit is equipped in the ultrasonic wave transmitting module
Including supersonic generator, the first triode, the second triode, first resistor, second resistance, switch, diode and capacitor, institute
The emitter of the emitter and the second triode of stating the first triode is grounded, the base stage of first triode and diode
Cathode connection, the plus earth of the diode, the cathode of the diode pass through supersonic generator and, the second triode
Collector connection, the external 9V direct current of series circuit that the collector of first triode passes through first resistor and switch composition
The collector of voltage source, first triode is connect with the base stage of the second triode, and the collector of second triode is logical
Cross the external 9V DC voltage power supply of series circuit of second resistance and switch composition, one end ground connection of the capacitor, the capacitor
The other end by switching external 9V DC voltage power supply.
Preferably, the flight performance in order to guarantee aviation mechanism, the aviation mechanism includes several flying units, described
Flying unit is circumferentially evenly distributed on the periphery of ontology, and the flying unit includes bracket and flight component, and the one of the bracket
End is fixed, and the other end and the flight component of the bracket are fixed on the body, and the flight component includes the first driving motor, erects
The first drive shaft and several blades to setting, first driving motor are fixed on bracket, and the blade is circumferential uniformly to be divided
On the periphery of the first drive shaft, first driving motor is sequentially connected cloth by the first drive shaft and each blade.
Preferably, in order to improve the generating efficiency of device of solar generating, the device of solar generating includes second
Driving motor, the second drive shaft, link block, connecting shaft and solar panels, second driving motor and link block are each attached to
On ontology, second drive shaft is arranged between the second driving motor and link block, and second driving motor and second drives
Driving-axle gearing connection, one end of the connecting shaft are fixed in the second drive shaft, and the other end of the connecting shaft is fixed on the sun
On energy plate.
Preferably, being additionally provided with level 2 buffering below the balancing unit to reinforce the buffer capacity of balancing unit
Mechanism, the level 2 buffering mechanism include two level 2 buffering units, and the two sides of clamping plate, institute is arranged in the level 2 buffering unit
Stating level 2 buffering unit includes second spring and buffer stopper, and one end of the second spring is fixed in second clamping plate, and described
The other end of two springs is fixed on buffer stopper.
Preferably, the buffer capacity in order to guarantee buffer stopper, the material of the buffer stopper is rubber block.
Preferably, in order to accurately control the sliding distance of sliding panel, the sliding panel far from third driving motor one
End is equipped with the first spring and pressure sensor, and the sliding panel is connect by the first spring with pressure sensor, and the pressure passes
Sensor is fixed on the second pillar.
Preferably, in order to improve ultrasonic wave transmitting circuit to the anti-interference ability of temperature, the first resistor and second
The temperature drift coefficient of resistance is 5%ppm.
Preferably, the model T-40-16 of the supersonic generator.
Sliding panel is driven to move the invention has the advantages that the Intelligent unattended machine based on Internet of Things of being somebody's turn to do passes through sliding equipment
It is dynamic, so that the first through hole on the second through-hole opposing clamping plate on sliding panel is misplaced, to change the air of each balancing unit
Resistance, adjust unmanned plane can steady safe falling, moreover, in ultrasonic wave transmitting circuit, using conventional point
Vertical component realizes the production cost for being also greatly reduced circuit while wireless signal transmitting, improves its practical value.
Detailed description of the invention
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of the Intelligent unattended machine of the invention based on Internet of Things；
Fig. 2 is the structural schematic diagram of the Intelligent unattended machine of the invention based on Internet of Things；
Fig. 3 is the structural schematic diagram of the device of solar generating of the Intelligent unattended machine of the invention based on Internet of Things；
Fig. 4 is the structural schematic diagram of the buffer cell of the Intelligent unattended machine of the invention based on Internet of Things；
Fig. 5 is the structural schematic diagram of the balancing unit of the Intelligent unattended machine of the invention based on Internet of Things；
Fig. 6 is the circuit diagram of the ultrasonic wave transmitting circuit of the Intelligent unattended machine of the invention based on Internet of Things；
In figure: 1. ontologies, 2. indicator lights, 3. device of solar generating, 4. brackets, 5. first driving motors, 6. first drive shafts,
7. blade, 8. support frames, 9. range sensors, 10. buffer cells, 11. solar panels, 12. connecting shafts, 13. second driving electricity
Machine, 14. second drive shafts, 15. link blocks, 16. third driving motors, 17. third drive shafts, 18. balancing units, 19. clamping plates,
20. first through hole, 21. pillars, 22. second through-holes, 23. sliding panels, 24. first springs, 25. pressure sensors, 26. 4 wheel drivens
Dynamic motor, 27. the 4th drive shafts, 28. casings, 29. second springs, 30. buffer stoppers, P1. ultrasonic transmitter, Q1. the one or three
Pole pipe, the second triode of Q2., R1. first resistor, R2. second resistance, S1. switch, VD1. diode, C1. capacitor.
Specific embodiment
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 basic structure of the invention, therefore it only shows the composition relevant to the invention.
As shown in figs 1 to 6, including ontology 1,1 top of ontology is arranged in a kind of Intelligent unattended machine based on Internet of Things
Aviation mechanism, device of solar generating 3 and the buffer gear being arranged in below ontology 1, the ontology 1 are equipped with several indicator lights
2；
The buffer gear includes several Buffer Units, and the Buffer Unit is circumferentially evenly distributed on the periphery of ontology 1, described slow
Rushing component includes support frame 8, range sensor 9 and two buffer cells 10, and support frame as described above 8 is fixed on the lower section of ontology 1, institute
The bottom end that support frame 8 is arranged in range sensor 9 is stated, the buffer cell 10 is arranged in the bottom end of support frame 8 and is located at support
The two sides of frame 8；
The buffer cell 10 includes third driving motor 16 and two balance mechanisms, and the third driving motor 16 is fixed on branch
On support 8, the balance mechanism includes third drive shaft 17 and balancing unit 18, and the third driving motor 16 is driven by third
Moving axis 17 and balancing unit 18 are sequentially connected；
The balancing unit 18 include sliding panel 23, sliding equipment, two clamping plates 19 and two pillars 21, the two of the pillar 21
End is fixed on clamping plate 19, and the first clamping plate 19 is located at the top of second clamping plate 19, and the sliding panel 23 and sliding equipment are equal
Between two clamping plates 19, first pillar 21 is fixed in third drive shaft 17, the sliding panel 23 and sliding equipment
It is arranged between the first pillar 21 and the second pillar 21, the clamping plate 19 is equipped with several first through hole 20, the sliding panel
23 are equipped with several second through-holes 22, and the quantity of the first through hole 20 is equal with the quantity of the second through-hole 22 and corresponds；
The sliding equipment includes the 4th driving motor 26, the 4th drive shaft 27 and casing 28, and the 4th driving motor 26 is solid
It being scheduled on the first pillar 21, the 4th driving motor 26 and the 4th drive shaft 27 are sequentially connected, and described 27 sets of 4th drive shaft
It being located in casing 28, the periphery of the 4th drive shaft 27 is equipped with external screw thread, it is equipped with internal screw thread in described sleeve pipe 28, the described 4th
The external screw thread of drive shaft 27 and the internal screw thread of casing 28 match, and described sleeve pipe 28 is fixed on sliding panel 23；
Central processing unit and ultrasonic wave transmitting module, the third driving motor 16 and the 4th driving electricity are equipped in the ontology 1
Machine 26 is electrically connected with central processing unit, and ultrasonic wave transmitting circuit, the ultrasonic wave hair are equipped in the ultrasonic wave transmitting module
Transmit-receive radio road includes supersonic generator P1, the first triode Q1, the second triode Q2, first resistor R1, second resistance R2, switch
S1, diode VD1 and capacitor C1, the emitter of the first triode Q1 and the emitter of the second triode Q2 are grounded, institute
The base stage for stating the first triode Q1 is connect with the cathode of diode VD1, the plus earth of the diode VD1, the diode
The cathode of VD1 is connect by supersonic generator P1 with the collector of, the second triode Q2, the current collection of the first triode Q1
Series circuit external 9V DC voltage power supply of the pole by first resistor R1 and switch S1 composition, the collection of the first triode Q1
Electrode is connect with the base stage of the second triode Q2, and the collector of the second triode Q2 passes through second resistance R2 and switch S1 group
At the external 9V DC voltage power supply of series circuit, one end ground connection of the capacitor C1, the other end of the capacitor C1 is by opening
Close the external 9V DC voltage power supply of S1.
Preferably, the flight performance in order to guarantee aviation mechanism, the aviation mechanism includes several flying units, described
Flying unit is circumferentially evenly distributed on the periphery of ontology 1, and the flying unit includes bracket 4 and flight component, the bracket 4
One end is fixed on ontology 1, and the other end and the flight component of the bracket 4 are fixed, and the flight component includes the first driving electricity
Machine 5, the first vertically arranged drive shaft 6 and several blades 7, first driving motor 5 are fixed on bracket 4, the blade 7
It is circumferentially evenly distributed on the periphery of the first drive shaft 6, first driving motor 5 is passed by the first drive shaft 6 with each blade 7
Dynamic connection.
Preferably, in order to improve the generating efficiency of device of solar generating 3, the device of solar generating 3 includes the
Two driving motors 13, the second drive shaft 14, link block 15, connecting shaft 12 and solar panels 11,13 He of the second driving motor
Link block 15 is each attached on ontology 1, and second drive shaft 14 is arranged between the second driving motor 13 and link block 15, institute
It states the second driving motor 13 and the second drive shaft 14 is sequentially connected, one end of the connecting shaft 12 is fixed on the second drive shaft 14
On, the other end of the connecting shaft 12 is fixed on solar panels 11.
Preferably, in order to reinforce the buffer capacity of balancing unit 18, the lower section of the balancing unit 18 is additionally provided with second level
Buffer gear, the level 2 buffering mechanism include two level 2 buffering units, and clamping plate 19 is arranged in the level 2 buffering unit
Two sides, the level 2 buffering unit include second spring 29 and buffer stopper 30, and one end of the second spring 29 is fixed on second
On clamping plate 19, the other end of the second spring 29 is fixed on buffer stopper 30.
Preferably, the buffer capacity in order to guarantee buffer stopper 30, the material of the buffer stopper 30 is rubber block.
Preferably, the sliding panel 23 is far from third driving motor in order to accurately control the sliding distance of sliding panel 23
26 one end is equipped with the first spring 24 and pressure sensor 25, and the sliding panel 23 passes through the first spring 24 and pressure sensor 25
Connection, the pressure sensor 25 are fixed on the second pillar 21.
Preferably, in order to improve ultrasonic wave transmitting circuit to the anti-interference ability of temperature, the first resistor R1 and
The temperature drift coefficient of two resistance R2 is 5%ppm.
Preferably, the model T-40-16 of the supersonic generator P1.
The unmanned plane is in flight course, in order to realize remote-control communication function, is sent out by the ultrasonic wave transmitting module in ontology 1
Ultrasonic signal is penetrated, in ultrasonic wave transmitting circuit, supersonic generator P1 is as the first triode in feedback element and circuit
Q1, the second triode Q2 constitute strong positive feedback frequency oscillator, and electric oscillation signal is converted to ultrasonic signal, oscillation
Frequency is equal to the centre frequency 40kHz of ultrasound transmitter device T-40-16.When circuit works, the both ends T-40-16 generate waveform
It is similar to pulse square wave, voltage amplitude sends voltage close to electricity.When pressing lower switch S1, it can launch a series of 40kHz's
Ultrasonic signal emits to receiver.Electric wild goose+the 9V of circuit work, operating current 25mA, remote control distance is up to 8m or so.It should
In circuit, using conventional discrete component, the transmitting of wireless signal is not only realized, while being also greatly reduced circuit
Production cost improves its practical value.
When unmanned plane landing, the safe landing of unmanned plane is realized by the buffer gear of 1 lower section of ontology.In Buffer Unit
In, first with the rotation of third driving motor 16, so that original vertically arranged balancing unit 18 is become horizontally disposed, so have
Conducive to when increasing unmanned plane landing and the contact area of air slows down the speed of unmanned plane landing to increase the resistance of air,
It plays a certain protective role.After the completion of balancing unit 18 turns to, detected by the range sensor 9 of each 8 bottom end of support frame
Height of each support frame 8 apart from ground indicates that unmanned plane is in a horizontal position, without carrying out angle when highly all equal
Adjustment.It when altitude information is inconsistent, is rotated using the 4th driving motor 26 in balancing unit 18, drives the 4th drive shaft 27
It is rotated along own axes, so that casing 28 be made to be translated between two clamping plates 19, drives sliding panel 23 mobile.On sliding panel 23
The quantity of second through-hole 22 is equal with the quantity of first through hole 20 on clamping plate 19 and corresponds, former when sliding panel 23 is mobile
The second through-hole 22 being first aligned with first through hole 20 changes position at this time, so that air is logical by first through hole 20 and second
The part in hole 22 is reduced, and then increases the resistance of air, strengthens the buffer function of the balancing unit 18, single by each balance
First 18 different degrees of bufferings make unmanned plane keep equilibrium state, make its stable landing.The Intelligent unattended machine based on Internet of Things
It drives sliding panel 23 mobile by sliding equipment, makes the first through hole 20 on 22 opposing clamping plate 19 of the second through-hole on sliding panel 23
It misplaces, to change the air drag of each balancing unit 18, adjusting unmanned plane can steady safe falling.
Compared with prior art, it is somebody's turn to do the Intelligent unattended machine based on Internet of Things and drives sliding panel 23 mobile by sliding equipment,
The first through hole 20 on 22 opposing clamping plate 19 of the second through-hole on sliding panel 23 is set to misplace, to change each balancing unit 18
Air drag, adjust unmanned plane can steady safe falling moreover in ultrasonic wave transmitting circuit, use normal
The discrete component of rule realizes the production cost for being also greatly reduced circuit while wireless signal transmitting, it is practical to improve its
Value.
Taking the above-mentioned ideal embodiment according to the present invention as inspiration, 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 which the technical scope thereof is determined according to the scope of the claim.
Claims (4)
1. a kind of buffer gear, which is characterized in that including several Buffer Units, the Buffer Unit is circumferentially evenly distributed on ontology
(1) periphery, the Buffer Unit include support frame (8), range sensor (9) and two buffer cells (10), the support
Frame (8) is fixed on the lower section of ontology (1), and the range sensor (9) is arranged in the bottom end of support frame (8), the buffer cell
(10) bottom end in support frame (8) is set and is located at the two sides of support frame (8)；
The buffer cell (10) includes third driving motor (16) and two balance mechanisms, and the third driving motor (16) is solid
It is scheduled on support frame (8), the balance mechanism includes third drive shaft (17) and balancing unit (18), the third driving motor
(16) it is sequentially connected by third drive shaft (17) and balancing unit (18)；
The balancing unit (18) includes sliding panel (23), sliding equipment, two clamping plates (19) and two pillars (21), the branch
The both ends of column (21) are fixed on clamping plate (19), and the first clamping plate (19) is located at the top of second clamping plate (19), the sliding
Plate (23) and sliding equipment are respectively positioned between two clamping plates (19), and first pillar (21) is fixed on third drive shaft (17)
On, the sliding panel (23) and sliding equipment are arranged between the first pillar (21) and the second pillar (21), the clamping plate
(19) several first through hole (20) are equipped with, the sliding panel (23) is equipped with several second through-holes (22), the first through hole
(20) quantity is equal with the quantity of the second through-hole (22) and corresponds.
2. a kind of Intelligent unattended machine based on Internet of Things, which is characterized in that including ontology (1), setting flying above ontology (1)
Row mechanism, device of solar generating (3) and the buffer gear being arranged below ontology (1), the ontology (1) are equipped with several fingers
Show lamp (2)；
The buffer gear includes several Buffer Units, and the Buffer Unit is circumferentially evenly distributed on the periphery of ontology (1), described
Buffer Unit includes that support frame (8), range sensor (9) and two buffer cells (10), support frame as described above (8) are fixed on ontology
(1) lower section, in the bottom end of support frame (8), the buffer cell (10) is arranged in support frame for range sensor (9) setting
(8) bottom end and the two sides positioned at support frame (8)；
The buffer cell (10) includes third driving motor (16) and two balance mechanisms, and the third driving motor (16) is solid
It is scheduled on support frame (8), the balance mechanism includes third drive shaft (17) and balancing unit (18), the third driving motor
(16) it is sequentially connected by third drive shaft (17) and balancing unit (18)；
The balancing unit (18) includes sliding panel (23), sliding equipment, two clamping plates (19) and two pillars (21), the branch
The both ends of column (21) are fixed on clamping plate (19), and the first clamping plate (19) is located at the top of second clamping plate (19), the sliding
Plate (23) and sliding equipment are respectively positioned between two clamping plates (19), and first pillar (21) is fixed on third drive shaft (17)
On, the sliding panel (23) and sliding equipment are arranged between the first pillar (21) and the second pillar (21), the clamping plate
(19) several first through hole (20) are equipped with, the sliding panel (23) is equipped with several second through-holes (22), the first through hole
(20) quantity is equal with the quantity of the second through-hole (22) and corresponds；
The sliding equipment includes the 4th driving motor (26), the 4th drive shaft (27) and casing (28), the 4th driving electricity
Machine (26) is fixed on the first pillar (21), and the 4th driving motor (26) and the 4th drive shaft (27) are sequentially connected, described
4th drive shaft (27) is set in casing (28), and the periphery of the 4th drive shaft (27) is equipped with external screw thread, described sleeve pipe
(28) internal screw thread is equipped in, the internal screw thread of the external screw thread and casing (28) of the 4th drive shaft (27) matches, described sleeve pipe
(28) it is fixed on sliding panel (23)；
Central processing unit and ultrasonic wave transmitting module, the third driving motor (16) and 4 wheel driven are equipped in the ontology (1)
Dynamic motor (26) are electrically connected with central processing unit, and ultrasonic wave transmitting circuit is equipped in the ultrasonic wave transmitting module, described super
Sonic wave transmitting circuit include supersonic generator (P1), the first triode (Q1), the second triode (Q2), first resistor (R1),
Second resistance (R2), switch (S1), diode (VD1) and capacitor (C1), the emitter and second of first triode (Q1)
The emitter of triode (Q2) is grounded, and the base stage of first triode (Q1) is connect with the cathode of diode (VD1), described
The plus earth of diode (VD1), the cathode of the diode (VD1) pass through supersonic generator (P1) and, the second triode
(Q2) collector connection, the string that the collector of first triode (Q1) passes through first resistor (R1) and switch (S1) composition
Join the external 9V DC voltage power supply of circuit, the collector of first triode (Q1) and the base stage of the second triode (Q2) connect
It connects, the collector of second triode (Q2) is straight by the external 9V of series circuit of second resistance (R2) and switch (S1) composition
The other end of galvanic electricity voltage source, one end ground connection of the capacitor (C1), the capacitor (C1) passes through switch (S1) external 9V direct current
Voltage source；
The aviation mechanism includes several flying units, and the flying unit is circumferentially evenly distributed on the periphery of ontology (1), described
Flying unit includes bracket (4) and flight component, and one end of the bracket (4) is fixed on ontology (1), the bracket (4)
The other end is fixed with flight component, and the flight component includes the first driving motor (5), vertically arranged the first drive shaft (6)
With several blades (7), first driving motor (5) is fixed on bracket (4), and the blade (7) is circumferentially evenly distributed on the
On the periphery of one drive shaft (6), first driving motor (5) is sequentially connected by the first drive shaft (6) and each blade (7)；
The device of solar generating (3) includes the second driving motor (13), the second drive shaft (14), link block (15), connection
Axis (12) and solar panels (11), second driving motor (13) and link block (15) are each attached on ontology (1), and described the
Two drive shafts (14) are arranged between the second driving motor (13) and link block (15), second driving motor (13) and second
Drive shaft (14) transmission connection, one end of the connecting shaft (12) are fixed on the second drive shaft (14), the connecting shaft (12)
The other end be fixed on solar panels (11).
3. the Intelligent unattended machine based on Internet of Things as claimed in claim 2, which is characterized in that under the balancing unit (18)
Side is additionally provided with level 2 buffering mechanism, and the level 2 buffering mechanism includes two level 2 buffering units, and the level 2 buffering unit is set
The two sides in clamping plate (19) are set, the level 2 buffering unit includes second spring (29) and buffer stopper (30), the second spring
(29) one end is fixed on second clamping plate (19), and the other end of the second spring (29) is fixed on buffer stopper (30).
4. the Intelligent unattended machine based on Internet of Things as claimed in claim 2, which is characterized in that the sliding panel (23) is far from the
One end of three driving motors (26) is equipped with the first spring (24) and pressure sensor (25), and the sliding panel (23) passes through the first bullet
Spring (24) is connect with pressure sensor (25), and the pressure sensor (25) is fixed on the second pillar (21).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811429480.8A CN109592024B (en) | 2016-07-05 | 2016-07-05 | Intelligent unmanned aerial vehicle |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811429480.8A CN109592024B (en) | 2016-07-05 | 2016-07-05 | Intelligent unmanned aerial vehicle |
| CN201610523034.8A CN106081076B (en) | 2016-07-05 | 2016-07-05 | A kind of Intelligent unattended machine based on Internet of Things |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610523034.8A Division CN106081076B (en) | 2016-07-05 | 2016-07-05 | A kind of Intelligent unattended machine based on Internet of Things |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN109592024A true CN109592024A (en) | 2019-04-09 |
| CN109592024B CN109592024B (en) | 2022-02-11 |
Family
ID=57212274
Family Applications (3)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610523034.8A Active CN106081076B (en) | 2016-07-05 | 2016-07-05 | A kind of Intelligent unattended machine based on Internet of Things |
| CN201811429480.8A Active CN109592024B (en) | 2016-07-05 | 2016-07-05 | Intelligent unmanned aerial vehicle |
| CN201811428621.4A Active CN109592023B (en) | 2016-07-05 | 2016-07-05 | Intelligent unmanned aerial vehicle capable of realizing remote control communication and working method thereof |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610523034.8A Active CN106081076B (en) | 2016-07-05 | 2016-07-05 | A kind of Intelligent unattended machine based on Internet of Things |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811428621.4A Active CN109592023B (en) | 2016-07-05 | 2016-07-05 | Intelligent unmanned aerial vehicle capable of realizing remote control communication and working method thereof |
Country Status (1)
| Country | Link |
|---|---|
| CN (3) | CN106081076B (en) |
Families Citing this family (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106892099B (en) * | 2017-03-15 | 2019-01-29 | 广东创意双星科技股份有限公司 | A kind of energy-saving unmanned plane that cruising ability is strong |
| CN107010210B (en) * | 2017-05-06 | 2019-12-17 | 广东电网有限责任公司电力科学研究院 | a intelligent unmanned aerial vehicle for electric power overhauls |
| CN107264785A (en) * | 2017-06-05 | 2017-10-20 | 深圳市雷凌广通技术研发有限公司 | A kind of Intelligent unattended machine for express transportation |
| CN107336835B (en) * | 2017-06-23 | 2019-10-29 | 张辉 | A kind of Intelligent unattended machine with air purification function based on Internet of Things |
| CN108583880A (en) * | 2018-04-03 | 2018-09-28 | 芜湖纵横智能制造产业技术研究有限公司 | A kind of sensorcraft with automatic regulating function |
| CN108423166B (en) * | 2018-05-14 | 2023-12-22 | 天长市星舟航空技术有限公司 | Multi-rotor unmanned aerial vehicle horizontal landing system |
| CN112533286A (en) * | 2020-11-30 | 2021-03-19 | 广西电网有限责任公司电力科学研究院 | Differential GPS positioning system of single ground base station to multiple mobile stations |
| CN112722257B (en) * | 2021-01-19 | 2024-05-03 | 南京誉葆科技股份有限公司 | Aircraft data link radio frequency combined system |
| CN116902246B (en) * | 2023-09-12 | 2023-12-12 | 成都庆龙航空科技有限公司 | Unmanned aerial vehicle investigation recognition device |
Citations (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB745915A (en) * | 1953-02-09 | 1956-03-07 | British Messier Ltd | Improvements in or relating to shock absorbers for aircraft |
| US4296897A (en) * | 1979-01-22 | 1981-10-27 | The Boeing Company | Brake torque limiter |
| CN1053401A (en) * | 1989-10-20 | 1991-07-31 | 国家工业宇航学会 | Be used for the rotatable visoelasticity device of the buffering of pulpboard track of rotor craft rotor paddle board and recovery of elasticity and comprise the rotor head of this device |
| US5890441A (en) * | 1995-09-07 | 1999-04-06 | Swinson Johnny | Horizontal and vertical take off and landing unmanned aerial vehicle |
| US6550715B1 (en) * | 2001-12-07 | 2003-04-22 | Lockheed Martin Corporation | Miniature vertical takeoff and landing aircraft |
| US20070007387A1 (en) * | 2005-07-05 | 2007-01-11 | The Boeing Company | Strut extender for landing gear snow skis |
| CN101687545A (en) * | 2007-06-15 | 2010-03-31 | 梅西耶-道提股份有限公司 | The bumper that is used for undercarriage |
| US20100320318A1 (en) * | 2009-06-18 | 2010-12-23 | Airbus Operations Gmbh | Decompression Device For An Aircraft |
| CN201856899U (en) * | 2010-10-14 | 2011-06-08 | 贺俊文 | Novel takeoff assisting device for plane |
| US20120097480A1 (en) * | 2009-04-16 | 2012-04-26 | Messier-Bugatti-Dowty | Device for reducing aerodynamic noise from an aircraft undercarriage |
| CN102501970A (en) * | 2011-11-15 | 2012-06-20 | 中国航空工业集团公司北京航空材料研究院 | Band type damper and preparation method thereof |
| CN102514711A (en) * | 2011-12-02 | 2012-06-27 | 叶洪新 | Multi-rotor fuel-electric hybrid aircraft |
| CN102602539A (en) * | 2012-04-06 | 2012-07-25 | 柴贵景 | Double spiral disc butterfly aircraft |
| CN103171762A (en) * | 2011-12-21 | 2013-06-26 | 尤洛考普特德国有限公司 | Landing gear vibration absorber for a helicopter and method of operating said landing gear vibration absorber |
| CN103192987A (en) * | 2013-04-07 | 2013-07-10 | 南京理工大学 | Amphibious robot capable of flying and climbing wall and control method of amphibious robot |
| US20130206915A1 (en) * | 2010-04-22 | 2013-08-15 | Jean-Marc (Joseph) Desaulniers | Vertical take-off and landing multimodal, multienvironment, gyropendular craft with compensatory propulsion and fluidic gradient collimation |
| CN103434640A (en) * | 2013-08-25 | 2013-12-11 | 西北工业大学 | High-altitude unmanned plane equipped with Magnus effect propulsion system |
| CN203461101U (en) * | 2013-09-13 | 2014-03-05 | 重庆金泰航空工业有限公司 | Quick-changing structure for undercarriage and body of four-axle agricultural aircraft |
| CN103625640A (en) * | 2013-10-25 | 2014-03-12 | 南京航空航天大学 | Multi-rotor unmanned aerial vehicle |
| CN103816671A (en) * | 2014-02-26 | 2014-05-28 | 中山市泰宝电子科技有限公司 | Infrared induction toy aircraft structure and application |
| CN104192303A (en) * | 2014-09-15 | 2014-12-10 | 沈阳飞机工业（集团）有限公司 | Small nose landing gear for unmanned aerial vehicle |
| US20140368765A1 (en) * | 2013-06-17 | 2014-12-18 | Lg Electronics Inc. | Display device |
| CN204250368U (en) * | 2014-11-14 | 2015-04-08 | 北华航天工业学院 | A kind of mini quadrotor of Intelligent aerial photography |
| CN104590556A (en) * | 2014-10-31 | 2015-05-06 | 湖北易瓦特科技有限公司 | Foldable unmanned aerial vehicle |
| CN104773296A (en) * | 2015-04-10 | 2015-07-15 | 武汉科技大学 | Aerial real-time tracking shooting micro unmanned plane |
| CN104787308A (en) * | 2015-04-08 | 2015-07-22 | 零度智控（北京）智能科技有限公司 | Aircraft undercarriage driving device, aircraft undercarriage and aircraft |
| CN204822065U (en) * | 2015-07-28 | 2015-12-02 | 河南大诚通用航空科技有限公司 | Unmanned aerial vehicle's undercarriage |
| CN105173068A (en) * | 2015-07-31 | 2015-12-23 | 广州极飞电子科技有限公司 | Unmanned plane |
| CN204916173U (en) * | 2015-06-19 | 2015-12-30 | 李永友 | Multiaxis aircraft with horn swing function |
| CN105217035A (en) * | 2015-10-20 | 2016-01-06 | 孙炳岐 | A kind of gas wing-type air-flow directional flying saucer and the optimal in structure formed thereof |
| CN205239901U (en) * | 2015-08-25 | 2016-05-18 | 吴会能 | Many rotor unmanned aerial vehicle and frame thereof |
Family Cites Families (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA2601056A1 (en) * | 2001-07-19 | 2003-01-19 | Burl A. Rogers | Airplane landing gear suspension and shock-absorbing device |
| US7377468B2 (en) * | 2003-08-29 | 2008-05-27 | Smiths Aerospace Llc | Active stabilization of a refueling drogue |
| US7946526B2 (en) * | 2004-11-05 | 2011-05-24 | Nachman Zimet | Rotary-wing vehicle system |
| CN101723093A (en) * | 2009-12-22 | 2010-06-09 | 航宇救生装备有限公司 | Landing cushion gasbag |
| CN202848037U (en) * | 2012-10-23 | 2013-04-03 | 成都纵横自动化技术有限公司 | Recovery device of cable-hanging type unmanned aerial vehicle |
| CN103150885B (en) * | 2013-01-30 | 2016-08-03 | 中国船舶重工集团公司第七一〇研究所 | A kind of underwater images method and be worth more decoding circuit |
| CN203381787U (en) * | 2013-05-09 | 2014-01-08 | 衡水众翔电子科技有限公司 | Electric multi-shaft unmanned aerial vehicle for checking electric transmission line |
| CN203652104U (en) * | 2013-12-30 | 2014-06-18 | 湖北易瓦特科技有限公司 | Damping landing gear of unmanned plane |
| CN103935522B (en) * | 2014-03-03 | 2016-06-15 | 浙江大学 | A kind of rotary wind type unmanned plane falling protecting device out of control and guard method |
| CN203946272U (en) * | 2014-05-13 | 2014-11-19 | 中国矿业大学徐海学院 | A kind of agriculture aircraft with multiaxis screw propeller |
| EP2944567B1 (en) * | 2014-05-13 | 2017-05-10 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Landing gear foa rotorcraft and method for the dissipation of ground resonance oscillations |
| CN104097787B (en) * | 2014-07-24 | 2017-01-18 | 郑州德莱孚科技有限公司 | Mooring grille, onboard mooring mast and quick mooring device |
| CN104670499B (en) * | 2015-02-28 | 2017-09-01 | 广州快飞计算机科技有限公司 | A kind of plant protection unmanned plane |
| CN204606224U (en) * | 2015-04-15 | 2015-09-02 | 广州快飞计算机科技有限公司 | A kind of unmanned plane landing damping device |
| CN104973243A (en) * | 2015-07-13 | 2015-10-14 | 龚伟民 | Spherical aircraft |
| CN204883224U (en) * | 2015-07-22 | 2015-12-16 | 河南科技学院 | Farming crop growth monitoring system based on thing networking |
| CN105292505B (en) * | 2015-12-03 | 2017-11-21 | 天津经天航空科技有限公司 | A kind of multi-rotor unmanned aerial vehicle Touchdown Protection device |
| CN105720649A (en) * | 2016-04-12 | 2016-06-29 | 张萍 | Internet of Things based intelligent searching and rescuing unmanned aerial vehicle |
-
2016
- 2016-07-05 CN CN201610523034.8A patent/CN106081076B/en active Active
- 2016-07-05 CN CN201811429480.8A patent/CN109592024B/en active Active
- 2016-07-05 CN CN201811428621.4A patent/CN109592023B/en active Active
Patent Citations (31)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB745915A (en) * | 1953-02-09 | 1956-03-07 | British Messier Ltd | Improvements in or relating to shock absorbers for aircraft |
| US4296897A (en) * | 1979-01-22 | 1981-10-27 | The Boeing Company | Brake torque limiter |
| CN1053401A (en) * | 1989-10-20 | 1991-07-31 | 国家工业宇航学会 | Be used for the rotatable visoelasticity device of the buffering of pulpboard track of rotor craft rotor paddle board and recovery of elasticity and comprise the rotor head of this device |
| US5890441A (en) * | 1995-09-07 | 1999-04-06 | Swinson Johnny | Horizontal and vertical take off and landing unmanned aerial vehicle |
| US6550715B1 (en) * | 2001-12-07 | 2003-04-22 | Lockheed Martin Corporation | Miniature vertical takeoff and landing aircraft |
| US20070007387A1 (en) * | 2005-07-05 | 2007-01-11 | The Boeing Company | Strut extender for landing gear snow skis |
| CN101687545A (en) * | 2007-06-15 | 2010-03-31 | 梅西耶-道提股份有限公司 | The bumper that is used for undercarriage |
| US20120097480A1 (en) * | 2009-04-16 | 2012-04-26 | Messier-Bugatti-Dowty | Device for reducing aerodynamic noise from an aircraft undercarriage |
| US20100320318A1 (en) * | 2009-06-18 | 2010-12-23 | Airbus Operations Gmbh | Decompression Device For An Aircraft |
| US20130206915A1 (en) * | 2010-04-22 | 2013-08-15 | Jean-Marc (Joseph) Desaulniers | Vertical take-off and landing multimodal, multienvironment, gyropendular craft with compensatory propulsion and fluidic gradient collimation |
| CN201856899U (en) * | 2010-10-14 | 2011-06-08 | 贺俊文 | Novel takeoff assisting device for plane |
| CN102501970A (en) * | 2011-11-15 | 2012-06-20 | 中国航空工业集团公司北京航空材料研究院 | Band type damper and preparation method thereof |
| CN102514711A (en) * | 2011-12-02 | 2012-06-27 | 叶洪新 | Multi-rotor fuel-electric hybrid aircraft |
| CN103171762A (en) * | 2011-12-21 | 2013-06-26 | 尤洛考普特德国有限公司 | Landing gear vibration absorber for a helicopter and method of operating said landing gear vibration absorber |
| CN102602539A (en) * | 2012-04-06 | 2012-07-25 | 柴贵景 | Double spiral disc butterfly aircraft |
| CN103192987A (en) * | 2013-04-07 | 2013-07-10 | 南京理工大学 | Amphibious robot capable of flying and climbing wall and control method of amphibious robot |
| US20140368765A1 (en) * | 2013-06-17 | 2014-12-18 | Lg Electronics Inc. | Display device |
| CN103434640A (en) * | 2013-08-25 | 2013-12-11 | 西北工业大学 | High-altitude unmanned plane equipped with Magnus effect propulsion system |
| CN203461101U (en) * | 2013-09-13 | 2014-03-05 | 重庆金泰航空工业有限公司 | Quick-changing structure for undercarriage and body of four-axle agricultural aircraft |
| CN103625640A (en) * | 2013-10-25 | 2014-03-12 | 南京航空航天大学 | Multi-rotor unmanned aerial vehicle |
| CN103816671A (en) * | 2014-02-26 | 2014-05-28 | 中山市泰宝电子科技有限公司 | Infrared induction toy aircraft structure and application |
| CN104192303A (en) * | 2014-09-15 | 2014-12-10 | 沈阳飞机工业（集团）有限公司 | Small nose landing gear for unmanned aerial vehicle |
| CN104590556A (en) * | 2014-10-31 | 2015-05-06 | 湖北易瓦特科技有限公司 | Foldable unmanned aerial vehicle |
| CN204250368U (en) * | 2014-11-14 | 2015-04-08 | 北华航天工业学院 | A kind of mini quadrotor of Intelligent aerial photography |
| CN104787308A (en) * | 2015-04-08 | 2015-07-22 | 零度智控（北京）智能科技有限公司 | Aircraft undercarriage driving device, aircraft undercarriage and aircraft |
| CN104773296A (en) * | 2015-04-10 | 2015-07-15 | 武汉科技大学 | Aerial real-time tracking shooting micro unmanned plane |
| CN204916173U (en) * | 2015-06-19 | 2015-12-30 | 李永友 | Multiaxis aircraft with horn swing function |
| CN204822065U (en) * | 2015-07-28 | 2015-12-02 | 河南大诚通用航空科技有限公司 | Unmanned aerial vehicle's undercarriage |
| CN105173068A (en) * | 2015-07-31 | 2015-12-23 | 广州极飞电子科技有限公司 | Unmanned plane |
| CN205239901U (en) * | 2015-08-25 | 2016-05-18 | 吴会能 | Many rotor unmanned aerial vehicle and frame thereof |
| CN105217035A (en) * | 2015-10-20 | 2016-01-06 | 孙炳岐 | A kind of gas wing-type air-flow directional flying saucer and the optimal in structure formed thereof |
Non-Patent Citations (2)
| Title |
|---|
| 冯飞等: "飞机柔性对前起落架摆振的影响分析", 《航空学报》 * |
| 豆清波等: "无人机全机着陆试验系统设计及应用", 《机械科学与技术》 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN106081076B (en) | 2019-01-22 |
| CN109592023A (en) | 2019-04-09 |
| CN109592023B (en) | 2022-01-07 |
| CN109592024B (en) | 2022-02-11 |
| CN106081076A (en) | 2016-11-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106081076B (en) | A kind of Intelligent unattended machine based on Internet of Things | |
| CN107416202B (en) | Miniature flapping wing aircraft | |
| CN203318676U (en) | Coaxial double-wing aircraft with moving centre-of-gravity ball | |
| CN201151485Y (en) | Coaxial counter-rotating flying saucer | |
| CN105813346A (en) | Internet of things based intelligent lighting system employing unmanned aerial vehicle | |
| CN105882946B (en) | A kind of unmanned plane with self-powered ability | |
| CN105799923A (en) | Four-rotor aircraft-based carrying manipulator | |
| CN205574270U (en) | Delivery manipulator based on four rotor crafts | |
| CN110001953A (en) | A kind of aerofoil profile unmanned plane and its flight control method | |
| CN106184728A (en) | A kind of rotary telescopic variable-torque quadrotor | |
| CN104691758B (en) | Linkage fixed-wing rotor electric vertical lifting unmanned plane | |
| CN206664920U (en) | A kind of telescopic energy-saving unmanned plane of support | |
| CN206544600U (en) | It is a kind of to can be used for the long-range unmanned plane for delivering article | |
| CN204776038U (en) | Miniature solar energy reconnaisance flight vehicle that combines ke enda effect | |
| CN204037899U (en) | Solar power vertically taking off and landing flyer during long boat | |
| CN109250095A (en) | A kind of VTOL fixed wing aircraft | |
| CN205602131U (en) | Small -size load compartment dispensing device of many rotor unmanned aerial vehicle | |
| CN205627087U (en) | Hand -thrown intelligence electronic toy aircraft | |
| CN209479965U (en) | A kind of solar power flight parasols | |
| CN207764615U (en) | A kind of electric butterfly valve controller | |
| CN208119408U (en) | A kind of scalable rotor and the aircraft based on the rotor | |
| CN107444638A (en) | A kind of unmanned actuation means of umbrella shape airflight | |
| CN202389598U (en) | Solar flying saucer capable of flying for long time | |
| CN205186530U (en) | Carry unmanned aerial vehicle of umbrella | |
| CN105909451B (en) | A kind of hydraulic turbine water guiding system with distant control function |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| TA01 | Transfer of patent application right | ||
| TA01 | Transfer of patent application right |
Effective date of registration: 20220119 Address after: 430040 room 01, No. 304, unit 1, building 3, new energy R & D base, No. 36, Tangxun Hubei Road, Donghu New Technology Development Zone, Wuhan, Hubei Province Applicant after: Wuhan Huinong UAV Technology Co.,Ltd. Address before: 213000 No. 33, Longxi Road, Longhutang street, Xinbei District, Changzhou City, Jiangsu Province Applicant before: Jin Fuzhen |
|
| GR01 | Patent grant | ||
| GR01 | Patent grant |