CN107521692A - A kind of intelligent unmanned machine with self-protection function - Google Patents
A kind of intelligent unmanned machine with self-protection function Download PDFInfo
- Publication number
- CN107521692A CN107521692A CN201710586068.6A CN201710586068A CN107521692A CN 107521692 A CN107521692 A CN 107521692A CN 201710586068 A CN201710586068 A CN 201710586068A CN 107521692 A CN107521692 A CN 107521692A
- Authority
- CN
- China
- Prior art keywords
- main body
- operational amplifier
- resistance
- self
- protection
- 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.)
- Pending
Links
- 230000007246 mechanism Effects 0.000 claims abstract description 13
- 239000011324 bead Substances 0.000 claims description 11
- 230000003321 amplification Effects 0.000 claims description 9
- 238000003199 nucleic acid amplification method Methods 0.000 claims description 9
- 230000005236 sound signal Effects 0.000 claims description 7
- 238000005259 measurement Methods 0.000 claims description 2
- 230000009545 invasion Effects 0.000 abstract description 7
- 230000006870 function Effects 0.000 description 17
- 230000008859 change Effects 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 230000033001 locomotion Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 230000018199 S phase Effects 0.000 description 1
- 241000269400 Sirenidae Species 0.000 description 1
- 241000486406 Trachea Species 0.000 description 1
- 238000004458 analytical method Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 229940079593 drug Drugs 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000009993 protective function Effects 0.000 description 1
- 239000013589 supplement Substances 0.000 description 1
- 230000009897 systematic effect Effects 0.000 description 1
- 210000003437 trachea Anatomy 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M29/00—Scaring or repelling devices, e.g. bird-scaring apparatus
- A01M29/06—Scaring or repelling devices, e.g. bird-scaring apparatus using visual means, e.g. scarecrows, moving elements, specific shapes, patterns or the like
- A01M29/10—Scaring or repelling devices, e.g. bird-scaring apparatus using visual means, e.g. scarecrows, moving elements, specific shapes, patterns or the like using light sources, e.g. lasers or flashing lights
-
- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01M—CATCHING, TRAPPING OR SCARING OF ANIMALS; APPARATUS FOR THE DESTRUCTION OF NOXIOUS ANIMALS OR NOXIOUS PLANTS
- A01M29/00—Scaring or repelling devices, e.g. bird-scaring apparatus
- A01M29/16—Scaring or repelling devices, e.g. bird-scaring apparatus using sound waves
-
- 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
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/02—Arrangements or adaptations of signal or lighting devices
-
- 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
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D2045/0095—Devices specially adapted to avoid bird strike
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Landscapes
- Engineering & Computer Science (AREA)
- Life Sciences & Earth Sciences (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pest Control & Pesticides (AREA)
- Birds (AREA)
- Insects & Arthropods (AREA)
- Wood Science & Technology (AREA)
- Zoology (AREA)
- Environmental Sciences (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Mechanical Engineering (AREA)
- Toys (AREA)
Abstract
The present invention relates to a kind of intelligent unmanned machine with self-protection function,Including main body,Some support units being arranged on below main body,Some signal gathering units being arranged in main body,Some flying units,The adjusted device and protection mechanism being arranged on above main body,The signal gathering unit is circumferentially evenly distributed in main body,The signal gathering unit includes camera and wind direction measuring unit,The flying unit is circumferentially evenly distributed on the outside of main body,There is the intelligent unmanned machine of self-protection function to detect wind direction by wind direction measuring unit for this,According to flight demand,Flat board is adjusted to correct position using adjusted device,Coordinate wind-force direction,Reduce the energy of flight consumption,Improve the practicality of equipment,Moreover,Detect whether birds close to invasion and attack by camera,And flash lamp is rotated by protection location and is directed at birds progress group flashing light,So as to draw back birds with fear,Ensure the normal flight of unmanned plane.
Description
Technical field
The present invention relates to unmanned plane field, more particularly to a kind of intelligent unmanned machine with self-protection function.
Background technology
UAV, abbreviation unmanned plane（UAV）, it is a kind of new concept weapon equipment being in developing rapidly, its
The advantages of low is required with maneuverability, rapid reaction, unmanned flight, operation.Unmanned plane, can by carrying multiclass sensor
It is the strong supplement of satellite remote sensing and traditional air remote sensing to realize image real-time Transmission, high-risk areas detecting function.At present,
The use range of unmanned plane has widened military affairs, scientific research, civilian three big field, specifically in electric power, communication, meteorology, agricultural, sea
Ocean, he explores, photographs, preventing and reducing natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the field application such as public security anti-terrorism it is very wide.
Existing unmanned plane is in flight course, easily by various birds birds as invader, therefore, unmanned plane during flying
Often perplex by the invasion and attack of all kinds of flying birds, when meeting with the bird of prey as eagle, unmanned plane is easier to be destroyed, and causes
It can not continue to navigate by water, moreover, can not be according to sky when causing unmanned plane during flying due to the single fixation of unmanned plane self structure
Airflow direction and itself heading in gas effectively utilize wind-force, so that unmanned plane during flying needs to consume substantial amounts of energy
Source, thus the practicality of equipment is reduced, meanwhile, during audio signal analysis controls, due to lacking signal enhancing, going
The function such as make an uproar, so as to greatly reduce the reliability of audio frequency process, reduce further the reliability of system.
The content of the invention
The technical problem to be solved in the present invention is：For overcome the deficiencies in the prior art, there is provided one kind has self-protection
The intelligent unmanned machine of function.
The technical solution adopted for the present invention to solve the technical problems is：A kind of intelligent nothing with self-protection function
It is man-machine, if including main body, be arranged on below main body some support units, be arranged in main body some signal gathering units,
Dry run unit, the adjusted device and protection mechanism being arranged on above main body, the signal gathering unit are circumferentially evenly distributed on
In main body, the signal gathering unit includes camera and wind direction measuring unit, and the flying unit is circumferentially evenly distributed on master
The outside of body；
The protection mechanism includes some protection locations, and the quantity of the protection location is equal with the quantity of camera and one a pair
Should, the protection location is circumferentially evenly distributed in main body, the protection location include the second motor, driving wheel, framework,
Fixed block, contiguous block and flash lamp, second motor are fixed in main body and are connected with driving wheel, the fixation
Block is fixed on the drive wheel and is arranged in framework, and the framework is fixedly connected by contiguous block with flash lamp, the contiguous block
It is hinged with main body；
The adjusted device includes driver element, driven gear and flat board, and the driver element is connected with driven gear, institute
State flat board to be fixed on driven gear, the driver element includes air pump, tracheae, cylinder and piston, and the cylinder and air pump are equal
It is fixed in main body, the air pump is connected by tracheae with cylinder, and one end of the piston is arranged in cylinder, the piston
The other end is provided with bar shaped tooth close to the side of flat board, and the bar shaped tooth on the piston engages with driven gear, is set in the cylinder
Limited position mechanism, the position-limit mechanism include the collar and are arranged on the gag lever post of collar both sides, and the collar is set on piston,
The collar is fixedly connected by gag lever post with the inwall of cylinder；
The lower section of the main body is provided with siren, and signal amplification module is provided with the siren, and the audio signal amplifies mould
Block includes amplifier circuit for sound frequency signal, the amplifier circuit for sound frequency signal include the first operational amplifier, the second operational amplifier,
First resistor, second resistance, 3rd resistor, the 4th resistance, the 5th resistance, the 6th resistance, the 7th resistance, the 8th resistance, first
Electric capacity, the second electric capacity, inductance and buzzer, the model OPA27 of first operational amplifier, second operational amplifier
Model OPA502, the in-phase input end of first operational amplifier is grounded by first resistor, and first computing is put
The inverting input of big device is connected by the first electric capacity with the output end of the first operational amplifier, first operational amplifier
Output end is connected with the in-phase input end of the second operational amplifier, and the inverting input of first operational amplifier passes through the 3rd
Resistance is connected with the output end of the second operational amplifier, and the inverting input of second operational amplifier passes through the 5th electricity respectively
Resistance and the second electric capacity are connected with the output end of the second operational amplifier, and the inverting input of second operational amplifier passes through the
Four resistance eutral groundings, the first compensating end of second operational amplifier pass through the 6th resistance and the series circuit of the 7th resistance composition
Be connected with the second compensating end of the second operational amplifier, the output end of second operational amplifier respectively with the 6th resistance and
Seven resistance are connected, and the output end of second operational amplifier is connected by the 8th resistance and one end of inductance and buzzer respectively
Connect, the other end ground connection of the buzzer.
Preferably, in order to detect the wind-force size of all directions, so that it is determined that overall wind direction, the wind direction measuring unit
Including first sleeve, pressure sensor, the first spring and deep bead, the first sleeve is fixed in main body, and the pressure passes
Sensor is fixed on the bottom in first sleeve, and one end of first spring is fixedly connected with pressure sensor, first bullet
The other end of spring is fixedly connected with deep bead.
Preferably, in order to increase wind-force receiving area, the vertical cross-section of the deep bead is shaped as circular arc,
The center of circle of the circular section is located in first sleeve.
Preferably, in order to realize the flight performance of unmanned plane, the flying unit includes connecting bracket, the first driving electricity
Machine, the first drive shaft and some blades, one end of the connecting bracket are fixed in main body, and first motor is with being connected
The other end of support is fixedly connected, and the blade is circumferentially evenly distributed on the outside of the first drive shaft, first motor
It is connected by the first drive shaft and blade.
Preferably, using DC servo motor driving force it is strong the characteristics of, in order to ensure the flight performance of flying unit, institute
It is DC servo motor to state the first motor.
Preferably, in order to improve the intelligence degree of unmanned plane, central control unit is provided with the main body, in described
Control device is entreated to include central control module, the protection control module being connected with central control module, air pump control module, motor
Control module and signal acquisition module, the flash lamp electrically connect with protection control module, the air pump and air pump control module
Electrical connection, first motor and the second motor electrically connect with motor control module, the pressure sensor with
Camera electrically connects with signal acquisition module.
Preferably, in order to when ensureing that unmanned plane declines support unit play cushioning effect, the support unit includes the
Two sleeve pipes, second spring and buffer stopper, second sleeve pipe is fixed on the lower section of main body and Open Side Down, the second spring
Bottom is fixed on the top in the second sleeve pipe, and the bottom of the second spring is fixedly connected with buffer stopper.
Preferably, using the characteristic of sponge excellent spring, it is described in order to further increase the buffer capacity of support unit
Buffer stopper is sponge.
Preferably, in order to ensure the coverage of camera, the focal length of the camera is 15mm.
The invention has the advantages that it should be examined with the intelligent unmanned machine of self-protection function by wind direction measuring unit
Determine the wind direction, according to flight demand, adjust flat board to correct position using adjusted device, coordinate wind-force direction, reduce flight and disappear
The energy of consumption, the practicality of equipment is improved, moreover, birds have been detected whether close to invasion and attack by camera, and pass through
Protection location rotates flash lamp alignment birds and carries out group flashing light, so as to draw back birds with fear, ensures the normal flight of unmanned plane, audio
In signal amplification circuit, ultra-low noise and high-accuracy characteristic by the first integrated circuit, audio signal not only ensure that
Reliable amplification, the reliability of audio output is also improved, so as to improve the reliability of system.
Brief description of the drawings
The present invention is further described with reference to the accompanying drawings and examples.
Fig. 1 is the structural representation of the intelligent unmanned machine with self-protection function of the present invention；
Fig. 2 is the structural representation of the protection location of the intelligent unmanned machine with self-protection function of the present invention；
Fig. 3 is the structural representation of the adjusted device of the intelligent unmanned machine with self-protection function of the present invention；
Fig. 4 is the structural representation of the wind direction measuring unit of the intelligent unmanned machine with self-protection function of the present invention；
Fig. 5 is the structural representation of the support unit of the intelligent unmanned machine with self-protection function of the present invention；
Fig. 6 is the systematic schematic diagram of the intelligent unmanned machine with self-protection function of the present invention；
Fig. 7 is the circuit theory of the amplifier circuit for sound frequency signal of the intelligent unmanned machine with self-protection function of the present invention
Figure；
In figure：1. main body, 2. adjusted devices, 3. sirens, 4. support units, 5. protection locations, 6. cameras, the measurement of 7. wind directions
Unit, 8. connecting brackets, 9. first motors, 10. first drive shafts, 11. blades, 12. second motors, 13. drivings
Wheel, 14. frameworks, 15. fixed blocks, 16. contiguous blocks, 17. flash lamps, 18. driven gears, 19. flat boards, 20. bar shaped teeth, 21. live
Plug, 23. gag lever posts, 24. collars, 25. cylinders, 26. air pumps, 27. tracheaes, 28. first sleeves, 29. pressure sensors, 30. the
One spring, 31. deep beads, 32. second sleeve pipes, 33. second springs, 34. buffer stoppers, 35. central control modules, 36. protection controls
Molding block, 37. air pump control modules, 38. motor control modules, 39. signal acquisition modules.
Embodiment
In conjunction with the accompanying drawings, the present invention is further explained in detail.These accompanying drawings are simplified schematic diagram, only with
Illustration illustrates the basic structure of the present invention, therefore it only shows the composition relevant with the present invention.
As shown in Fig. 1-Fig. 7, a kind of intelligent unmanned machine with self-protection function, including main body 1, it is arranged on main body
Some support units 4 of 1 lower section, some signal gathering units on the body 1, some flying units are set, are arranged on main body 1
The adjusted device 2 and protection mechanism of top, the signal gathering unit are circumferentially uniformly distributed on the body 1, the signal acquisition
Unit includes camera 6 and wind direction measuring unit 7, and the flying unit is circumferentially evenly distributed on the outside of main body 1；
The protection mechanism includes some protection locations 5, and the quantity of the protection location 5 is equal with the quantity of camera 6 and one
One correspondence, the protection location 5 is circumferential to be uniformly distributed on the body 1, and the protection location 5 includes the second motor 12, driven
Driving wheel 13, framework 14, fixed block 15, contiguous block 16 and flash lamp 17, second motor 12 fix on the body 1 and with
Driving wheel 13 is connected, and the fixed block 15 is fixed on driving wheel 13 and is arranged in framework 14, and the framework 14 passes through
Contiguous block 16 is fixedly connected with flash lamp 17, and the contiguous block 16 is be hinged with main body 1；
The adjusted device 2 includes driver element, driven gear 18 and flat board 19, and the driver element is driven with driven gear 18
Connection, the flat board 19 are fixed on driven gear 18, and the driver element includes air pump 26, tracheae 27, cylinder 25 and piston
21, the cylinder 25 and air pump 26 are each attached in main body 1, and the air pump 26 is connected by tracheae 27 with cylinder 25, the work
One end of plug 21 is arranged in cylinder 25, and the other end of the piston 21 is provided with bar shaped tooth 20 close to the side of flat board 19, described
Bar shaped tooth 20 on piston 21 engages with driven gear 18, is provided with position-limit mechanism in the cylinder 25, the position-limit mechanism includes
The collar 24 and the gag lever post 23 for being arranged on the both sides of the collar 24, the collar 24 are set on piston 21, and the collar 24 passes through limit
Position bar 23 is fixedly connected with the inwall of cylinder 25；
The lower section of the main body 1 is provided with siren 3, and audio signal amplification module, the audio signal are provided with the siren 3
Amplification module includes amplifier circuit for sound frequency signal, and the amplifier circuit for sound frequency signal includes the first operational amplifier U1, the second fortune
Calculate amplifier U2, first resistor R1, second resistance R2,3rd resistor R3, the 4th resistance R4, the 5th resistance R5, the 6th resistance R6,
7th resistance R7, the 8th resistance R8, the first electric capacity C1, the second electric capacity C2, inductance L1 and buzzer BL, first operation amplifier
Device U1 model OPA27, the second operational amplifier U2 model OPA502, the first operational amplifier U1's is same
Phase input is grounded by first resistor R1, and the inverting input of the first operational amplifier U1 passes through the first electric capacity C1 and
One operational amplifier U1 output end connection, the output end of the first operational amplifier U1 are same with the second operational amplifier U2's
Phase input connects, and the inverting input of the first operational amplifier U1 passes through 3rd resistor R3 and the second operational amplifier U2
Output end connection, the inverting input of the second operational amplifier U2 respectively by the 5th resistance R5 and the second electric capacity C2 with
Second operational amplifier U2 output end connection, the inverting input of the second operational amplifier U2 are connect by the 4th resistance R4
Ground, the first compensating end of the second operational amplifier U2 by the series circuit that the 6th resistance R6 and the 7th resistance R7 is formed with
Second operational amplifier U2 the second compensating end connection, the output end of the second operational amplifier U2 respectively with the 6th resistance R6
Connected with the 7th resistance R7, the output end of the second operational amplifier U2 passes through the 8th resistance R8 and inductance L1 and buzzing respectively
Device BL one end connection, the other end ground connection of the buzzer BL.
Preferably, in order to detect the wind-force size of all directions, so that it is determined that overall wind direction, the wind direction measuring unit
7 include first sleeve 28, pressure sensor 29, the first spring 30 and deep bead 31, and the first sleeve 28 is fixed on main body 1
On, the pressure sensor 29 is fixed on the bottom in first sleeve 28, one end of first spring 30 and pressure sensor
29 are fixedly connected, and the other end of first spring 30 is fixedly connected with deep bead 31.
Preferably, in order to increase wind-force receiving area, the vertical cross-section of the deep bead 31 is shaped as circular arc
Shape, the center of circle of the circular section are located in first sleeve 28.
Preferably, in order to realize the flight performance of unmanned plane, the flying unit drives including connecting bracket 8, first
Motor 9, the first drive shaft 10 and some blades 11, one end of the connecting bracket 8 are fixed on the body 1, first driving
Motor 9 is fixedly connected with the other end of connecting bracket 8, the circumferential outside for being evenly distributed on the first drive shaft 10 of blade 11,
First motor 9 is connected by the first drive shaft 10 with blade 11.
Preferably, using DC servo motor driving force it is strong the characteristics of, in order to ensure the flight performance of flying unit, institute
It is DC servo motor to state the first motor 9.
Preferably, in order to improve the intelligence degree of unmanned plane, central control unit is provided with the main body 1, it is described
Central control unit includes central control module 35, the protection control module 36 being connected with central control module 35, air pump control
Module 37, motor control module 38 and signal acquisition module 39, the flash lamp 17 electrically connects with protection control module 36, described
Air pump 26 electrically connects with the control module 37 of air pump 37, and the motor 12 of the first motor 9 and second is and motor control
Module 38 electrically connects, and the pressure sensor 29 and camera 6 electrically connect with signal acquisition module 39.Wherein, center control
Module 35, for the module of the intelligent operation of modules in control system, herein, central control module 35 is not only
PLC, single-chip microcomputer is can also be, so as to improve the intelligence degree of unmanned plane operation；Control module 36 is protected, is dodged to control
Light lamp 17 is run, when find unmanned plane attacked by birds, draw back birds with fear using the group flashing light of flash lamp 17, play a protective role；
Air pump control module 37, control air pump 26 to change air pressure in cylinder 25, make the movement of piston 21 drive driven gear 18 to rotate,
So as to adjust the angle of flat board 19；The fortune of major control the first motor 9 of motor control module 38 and the second motor 12
OK, the first motor 9 is run, and can drive unmanned plane during flying, and the second motor 12 drives driving wheel 13 to rotate, Neng Gougai
Become the angle of flash lamp 17, facilitate the birds of the alignment invasion and attack of flash lamp 17；Signal acquisition module 39, it is responsible for reception camera 6 and claps
The pressure data that the image and pressure sensor 29 taken the photograph receive, determine whether that birds attack by the image of collection, utilize
The pressure data of pressure sensor 29 determines the component of wind-force in all directions, so that it is determined that wind direction.
Preferably, in order to ensure unmanned plane decline when support unit 4 play cushioning effect, the support unit 4 includes
Second sleeve pipe 32, second spring 33 and buffer stopper 34, second sleeve pipe 32 is fixed on the lower section of main body 1 and Open Side Down, institute
The bottom for stating second spring 33 is fixed on top in the second sleeve pipe 32, and bottom and the buffer stopper 34 of the second spring 33 are fixed
Connection.
Preferably, using the characteristic of sponge excellent spring, in order to further increase the buffer capacity of support unit 4, institute
It is sponge to state buffer stopper 34.
Preferably, in order to ensure the coverage of camera 6, the focal length of the camera 6 is 15mm.
During the unmanned plane during flying, in order to reduce the energy of flight consumption, by each wind direction measuring unit 7 in main body 1
Detect wind-force in all directions and, to the blast of deep bead 31, wind data is detected by pressure sensor 29, so that it is determined that each side
Upward wind-force size, so that it is determined that wind-force direction, when unmanned plane downwind, by flat board rotating unit 2 by flat board 19
Turn to wind direction vertical direction, by the flat board 19 of wind blows unmanned plane so as to reduce unmanned plane move ahead needed for power；When inverse
During wind flight, by flat board 19 turn to wind direction parallel direction, so as to reduce the resistance of wind, so as to reduce flight needed for consume
The energy, when the rotating unit of flat board 2 is run, change by tracheae 27 air pressure in cylinder 25 by air pump 26, send out piston 21
Raw movement, in the moving process of piston 21, the bar shaped tooth 20 on piston 21 engages with driven gear 18, so that bar shaped gear 18
Rotate, drive the angle of flat board 19 to change, so as to have adjusted the angle of flat board 19 according to unmanned plane during flying.Should have and self protect
The intelligent unmanned machine of protective function detects wind direction by wind direction measuring unit 7, according to flight demand, is adjusted using adjusted device 2
Flat board 19 coordinates wind-force direction, reduces the energy of flight consumption, improve the practicality of equipment to correct position.
In order to ensure unmanned plane safe flight, avoid being attacked by each middle birds, each camera 6 on the body 1
Detect the flight environment of vehicle of surrounding, when some camera 6 detect by birds close to when, in main body 1 therewith to protection location 5 transport
OK, used second motor 12 rotates, and drives center axis thereof of the fixed block 15 along driving wheel 13, makes framework 14 that angle occur
Degree rotates, and drives flash lamp 17 to rotate, is directed at close birds, using the group flashing light 17 of flash lamp 17, makes close bird
Class is temporarily lost with observation ability, prevents the tracked invasion and attack of unmanned plane, when running into the large birds such as eagle, can also pass through main body
The siren 3 of 1 lower section sends the sound, so as to frighten birds, increases deterrent capability, birds is further prevented away from unmanned plane
Unmanned plane is invaded and harassed, and ensure that the normal flight of unmanned plane.There is the intelligent unmanned machine of self-protection function to pass through shooting for this
First 6 have detected whether birds close to invasion and attack, and rotate flash lamp 17 by protection location 5 and be directed at birds progress group flashing light, from
And draw back birds with fear, ensure the normal flight of unmanned plane.
The first integrated circuit U1 has used ultra-low noise precision amplifier OPA27 to be put before being used as in amplifier circuit for sound frequency signal
Greatly.When power output is 50W, under conditions of frequency is 20kHz, its total harmonic distortion is 0.02%, under the conditions of 1kHz,
Its total harmonic distortion is 0.002%, so as to the ultra-low noise by the first integrated circuit U1 and high-accuracy characteristic, is not only ensured
The reliable amplification of audio signal, the reliability of audio output is also improved, so as to improving the reliability of system.
Compared with prior art, should be detected with the intelligent unmanned machine of self-protection function by wind direction measuring unit 7
Wind direction, according to flight demand, flat board 19 is adjusted to correct position using adjusted device 2, coordinates wind-force direction, reduces flight and disappear
The energy of consumption, the practicality of equipment is improved, moreover, birds have been detected whether close to invasion and attack by camera 6, and pass through
Protection location 5 rotates flash lamp 17 and is directed at birds progress group flashing light, so as to draw back birds with fear, ensures the normal flight of unmanned plane,
In amplifier circuit for sound frequency signal, ultra-low noise and high-accuracy characteristic by the first integrated circuit, it not only ensure that audio is believed
Number reliable amplification, the reliability of audio output is also improved, so as to improve the reliability of system.
It is complete by above-mentioned description, relevant staff using the above-mentioned desirable embodiment according to the present invention as enlightenment
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 scope is not limited to the content on specification, it is necessary to determines its technical scope according to right.
Claims (9)
1. a kind of intelligent unmanned machine with self-protection function, it is characterised in that including main body（1）, be arranged on main body（1）
Some support units of lower section（4）, be arranged on main body（1）On some signal gathering units, some flying units, be arranged on master
Body（1）The adjusted device of top（2）And protection mechanism, the signal gathering unit are circumferentially evenly distributed on main body（1）On, it is described
Signal gathering unit includes camera（6）With wind direction measuring unit（7）, the flying unit is circumferentially evenly distributed on main body（1）
Outside；
The protection mechanism includes some protection locations（5）, the protection location（5）Quantity and camera（6）Quantity phase
Deng and correspond, the protection location（5）Circumferentially it is evenly distributed on main body（1）On, the protection location（5）Driven including second
Dynamic motor（12）, driving wheel（13）, framework（14）, fixed block（15）, contiguous block（16）And flash lamp（17）, second driving
Motor（12）It is fixed on main body（1）Upper and and driving wheel（13）Drive connection, the fixed block（15）It is fixed on driving wheel（13）
Go up and be arranged on framework（14）It is interior, the framework（14）Pass through contiguous block（16）With flash lamp（17）It is fixedly connected, the connection
Block（16）With main body（1）It is be hinged；
The adjusted device（2）Including driver element, driven gear（18）And flat board（19）, the driver element and driven gear
（18）Drive connection, the flat board（19）It is fixed on driven gear（18）On, the driver element includes air pump（26）, tracheae
（27）, cylinder（25）And piston（21）, the cylinder（25）And air pump（26）It is each attached to main body（1）On, the air pump（26）
Pass through tracheae（27）With cylinder（25）Connection, the piston（21）One end be arranged on cylinder（25）It is interior, the piston（21）'s
The other end is close to flat board（19）Side be provided with bar shaped tooth（20）, the piston（21）On bar shaped tooth（20）With driven gear
（18）Engagement, the cylinder（25）Interior to be provided with position-limit mechanism, the position-limit mechanism includes the collar（24）Be arranged on the collar（24）
The gag lever post of both sides（23）, the collar（24）It is set in piston（21）On, the collar（24）Pass through gag lever post（23）With gas
Cylinder（25）Inwall be fixedly connected；
The main body（1）Lower section be provided with siren（3）, the siren（3）It is interior to be provided with audio signal amplification module, the sound
Frequency signal amplification module includes amplifier circuit for sound frequency signal, and the amplifier circuit for sound frequency signal includes the first operational amplifier
（U1）, the second operational amplifier（U2）, first resistor（R1）, second resistance（R2）, 3rd resistor（R3）, the 4th resistance（R4）、
5th resistance（R5）, the 6th resistance（R6）, the 7th resistance（R7）, the 8th resistance（R8）, the first electric capacity（C1）, the second electric capacity
（C2）, inductance（L1）And buzzer（BL）, first operational amplifier（U1）Model OPA27, second computing puts
Big device（U2）Model OPA502, first operational amplifier（U1）In-phase input end pass through first resistor（R1）Connect
Ground, first operational amplifier（U1）Inverting input pass through the first electric capacity（C1）With the first operational amplifier（U1）It is defeated
Go out end connection, first operational amplifier（U1）Output end and the second operational amplifier（U2）In-phase input end connection,
First operational amplifier（U1）Inverting input pass through 3rd resistor（R3）With the second operational amplifier（U2）Output
End connection, second operational amplifier（U2）Inverting input pass through the 5th resistance respectively（R5）With the second electric capacity（C2）With
Second operational amplifier（U2）Output end connection, second operational amplifier（U2）Inverting input pass through the 4th resistance
（R4）Ground connection, second operational amplifier（U2）The first compensating end pass through the 6th resistance（R6）With the 7th resistance（R7）Composition
Series circuit and the second operational amplifier（U2）The second compensating end connection, second operational amplifier（U2）Output end
Respectively with the 6th resistance（R6）With the 7th resistance（R7）Connection, second operational amplifier（U2）Output end pass through respectively
Eight resistance（R8）And inductance（L1）With buzzer（BL）One end connection, the buzzer（BL）The other end ground connection.
2. there is the intelligent unmanned machine of self-protection function as claimed in claim 1, it is characterised in that the wind direction measurement
Unit（7）Including first sleeve（28）, pressure sensor（29）, the first spring（30）And deep bead（31）, the first sleeve
（28）It is fixed on main body（1）On, the pressure sensor（29）It is fixed on first sleeve（28）Interior bottom, first spring
（30）One end and pressure sensor（29）It is fixedly connected, first spring（30）The other end and deep bead（31）It is fixed to connect
Connect.
3. there is the intelligent unmanned machine of self-protection function as claimed in claim 2, it is characterised in that the deep bead
（31）Vertical cross-section be shaped as circular arc, the center of circle of the circular section is located at first sleeve（28）It is interior.
4. there is the intelligent unmanned machine of self-protection function as claimed in claim 1, it is characterised in that the flying unit
Including connecting bracket（8）, the first motor（9）, the first drive shaft（10）With some blades（11）, the connecting bracket（8）
One end be fixed on main body（1）On, first motor（9）With connecting bracket（8）The other end be fixedly connected, the oar
Leaf（11）Circumferentially it is evenly distributed on the first drive shaft（10）Outside, first motor（9）Pass through the first drive shaft
（10）With blade（11）Drive connection.
5. there is the intelligent unmanned machine of self-protection function as claimed in claim 1, it is characterised in that first driving
Motor（9）For DC servo motor.
6. there is the intelligent unmanned machine of self-protection function as claimed in claim 1, it is characterised in that the main body（1）
Interior to be provided with central control unit, the central control unit includes central control module（35）With central control module（35）Even
The protection control module connect（36）, air pump control module（37）, motor control module（38）And signal acquisition module（39）, it is described
Flash lamp（17）With protecting control module（36）Electrical connection, the air pump（26）With air pump（37）Control module（37）Electrical connection,
First motor（9）With the second motor（12）And motor control module（38）Electrical connection, the pressure sensing
Device（29）And camera（6）And signal acquisition module（39）Electrical connection.
7. there is the intelligent unmanned machine of self-protection function as claimed in claim 1, it is characterised in that the support unit
（4）Including the second sleeve pipe（32）, second spring（33）And buffer stopper（34）, second sleeve pipe（32）It is fixed on main body（1）'s
Lower section and Open Side Down, the second spring（33）Bottom be fixed on the second sleeve pipe（32）Interior top, the second spring
（33）Bottom and buffer stopper（34）It is fixedly connected.
8. there is the intelligent unmanned machine of self-protection function as claimed in claim 1, it is characterised in that the buffer stopper
（34）For sponge.
9. there is the intelligent unmanned machine of self-protection function as claimed in claim 1, it is characterised in that the camera
（6）Focal length be 15mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710586068.6A CN107521692A (en) | 2017-07-18 | 2017-07-18 | A kind of intelligent unmanned machine with self-protection function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710586068.6A CN107521692A (en) | 2017-07-18 | 2017-07-18 | A kind of intelligent unmanned machine with self-protection function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN107521692A true CN107521692A (en) | 2017-12-29 |
Family
ID=60749000
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710586068.6A Pending CN107521692A (en) | 2017-07-18 | 2017-07-18 | A kind of intelligent unmanned machine with self-protection function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN107521692A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109823538A (en) * | 2019-01-22 | 2019-05-31 | 广州林电科技有限公司 | A kind of unmanned flight's transport device with anti-interference function for logistics |
| JPWO2019168047A1 (en) * | 2018-02-28 | 2020-08-20 | 株式会社ナイルワークス | Drone, drone control method, and drone control program |
-
2017
- 2017-07-18 CN CN201710586068.6A patent/CN107521692A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPWO2019168047A1 (en) * | 2018-02-28 | 2020-08-20 | 株式会社ナイルワークス | Drone, drone control method, and drone control program |
| CN109823538A (en) * | 2019-01-22 | 2019-05-31 | 广州林电科技有限公司 | A kind of unmanned flight's transport device with anti-interference function for logistics |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106769241B (en) | Unmanned aerial vehicle for atmosphere sampling detection and toxic and harmful gas early warning monitoring | |
| CN107054626B (en) | A kind of energy-saving unmanned plane with defencive function | |
| CN203819497U (en) | Fire-fighting unmanned aerial vehicle system based on 3G network | |
| WO2015100899A1 (en) | Intelligent cruise robot based on wireless charging odd-shaft aircraft | |
| CN107521692A (en) | A kind of intelligent unmanned machine with self-protection function | |
| CN106586009A (en) | Unmanned aerial vehicle | |
| CN104443380A (en) | Splay-track flapping wing mechanism and miniature flapping wing air vehicle | |
| CN205931243U (en) | Alert unmanned aerial vehicle that uses | |
| CN107336830A (en) | It is a kind of to irrigate the intelligent unmanned machine for being accurately used for agricultural production | |
| CN108020635A (en) | A kind of environment protection digital device for quick collecting | |
| CN209634726U (en) | Unmanned plane is used in a kind of monitoring of agricultural plant protection | |
| CN207157525U (en) | A kind of unmanned plane propeller protection device | |
| CN206494135U (en) | A kind of unmanned plane | |
| CN208593494U (en) | Unmanned road conditions reconnaissance plane | |
| CN106240818B (en) | Unmanned plane grabs object device | |
| CN107089334A (en) | A kind of unmanned plane | |
| CN203510240U (en) | Mechanical arm of explosive-handling robot | |
| CN205090877U (en) | Portable guided missile follow -up emitter | |
| CN204323688U (en) | A kind of Eight characters track flapping wing mechanism and micro flapping wing air vehicle | |
| CN218112987U (en) | Special highway patrol unmanned aerial vehicle for group fog weather | |
| CN208165258U (en) | A kind of AGV unmanned plane of laser radar positioning function | |
| CN208602704U (en) | A kind of construction quality evidence obtaining photo taking type unmanned plane | |
| CN206322024U (en) | One kind arrests unmanned plane | |
| CN206664919U (en) | A kind of unmanned plane | |
| CN205365118U (en) | Land, water and air investigation robot |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20171229 |