CN108583884A - A kind of flight instruments for finding the personnel that wander away that cruising ability is strong - Google Patents
A kind of flight instruments for finding the personnel that wander away that cruising ability is strong Download PDFInfo
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- CN108583884A CN108583884A CN201810505427.5A CN201810505427A CN108583884A CN 108583884 A CN108583884 A CN 108583884A CN 201810505427 A CN201810505427 A CN 201810505427A CN 108583884 A CN108583884 A CN 108583884A
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- Prior art keywords
- motor
- drive shaft
- fixed
- personnel
- finding
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- 230000007246 mechanism Effects 0.000 claims abstract description 38
- 238000010248 power generation Methods 0.000 claims abstract description 17
- 239000007787 solid Substances 0.000 claims description 5
- 230000005540 biological transmission Effects 0.000 claims description 3
- 230000001815 facial effect Effects 0.000 abstract description 6
- 230000000903 blocking effect Effects 0.000 abstract description 3
- 230000033001 locomotion Effects 0.000 description 7
- 238000005516 engineering process Methods 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000007812 deficiency Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 230000003752 improving hair Effects 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
Classifications
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- 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
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- 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
- B64D47/00—Equipment not otherwise provided for
- B64D47/08—Arrangements of cameras
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02S—GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRARED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, e.g. USING PHOTOVOLTAIC [PV] MODULES
- H02S20/00—Supporting structures for PV modules
- H02S20/30—Supporting structures being movable or adjustable, e.g. for angle adjustment
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/50—Photovoltaic [PV] energy
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Studio Devices (AREA)
Abstract
The present invention relates to a kind of strong flight instruments for finding the personnel that wander away of cruising ability,Including main body,Photographic unit,Power generation mechanism and several supporting mechanisms,Power generation mechanism includes the first photovoltaic panel and generation block,Recess there are four being set in generation block,Electrification component is equipped in recess,Electrification component includes telescopic unit,Slide plate,Lifting unit and the second photovoltaic panel,Supporting mechanism includes side plate,Flight component and support component,Support component includes fixed link,Support tube,Slide bar,Buffer board,Strut and translation unit,The strong flight instruments for finding the personnel that wander away of the cruising ability pass through power generation mechanism,Improve photovoltaic generation area,Increase generated energy,It flies for equipment,To strengthen cruising ability,Moreover,During execution task,By supporting mechanism so that support tube is rotated to side plate,It prevents from blocking camera,Ensure that camera can acquire large-scale facial image to lower section,People are helped to find the personnel that wander away,Improve the practicability of equipment.
Description
Technical field
The present invention relates to face recognition device field, more particularly to a kind of cruising ability it is strong wander away personnel's for finding
Flight instruments.
Background technology
Recognition of face is a kind of biological identification technology that the facial feature information based on people carries out identification.With camera shooting
Machine or camera acquire image or video flowing containing face, and automatic detect and track face in the picture, and then to detection
The face that arrives carries out a series of the relevant technologies of face, usually also referred to as Identification of Images, face recognition.
With the development of face recognition technology, recognition of face camera is usually installed on unmanned plane by people, utilizes nothing
Man-machine flight function carries out flight scanning, search missing child, old man and cyclothymic in crowd above crowd
Equal personnel, but since unmanned plane increases load, the duration flight of unmanned plane is caused to shorten, in operation one end time
Afterwards, unmanned plane needs return initial position to charge, while during unmanned plane during flying, and the supporting rack below unmanned plane holds
Camera easily is blocked, influences the shooting work of camera, the practicability of unmanned plane is caused to reduce.
Invention content
The technical problem to be solved by the present invention is to：For overcome the deficiencies in the prior art, it is strong to provide a kind of cruising ability
Flight instruments for finding the personnel that wander away.
The technical solution adopted by the present invention to solve the technical problems is：A kind of cruising ability it is strong for finding the people that wanders away
The flight instruments of member, including main body, photographic unit, power generation mechanism and several supporting mechanisms, the photographic unit and power generation mechanism
It is separately positioned on the following above and of main body, is equipped with PLC in the main body, the supporting mechanism is circumferentially evenly distributed on main body
Periphery, the power generation mechanism include the first photovoltaic panel and generation block, and first photovoltaic panel is fixed on main body by generation block
Top is set in the generation block from top to down there are four recess, and the opening of four recesses is located at four sides of generation block
On, electrification component is equipped in the recess；
The electrification component includes telescopic unit, slide plate, lifting unit, the second photovoltaic panel and two sliding units, described
The bottom in recess is arranged in telescopic unit, and the telescopic unit is sequentially connected with slide plate, and second photovoltaic panel is located at slide plate
Top, between slide plate and the second photovoltaic panel, the lifting unit and the second photovoltaic panel are sequentially connected the lifting unit,
Two sliding units are located at the both sides of slide plate；
The supporting mechanism includes side plate, flight component and support component, and one end of the side plate is fixed in main body, institute
It states flight component and the other end in side plate is set, the support component is located at the lower section of main body, and the support component includes fixing
The bottom end of bar, support tube, slide bar, buffer board, strut and translation unit, the fixed link is fixed on the lower section of main body, described solid
The bottom end of fixed pole is hinged with support tube, and the top of the slide bar is arranged in support tube, and the bottom end of the slide bar and buffer board are solid
Fixed connection, the translation unit are located at the lower section of side plate, one end drive connection of the translation unit and strut, the strut
The other end is hinged with support tube；
The translation unit includes first motor, the first drive shaft and casing, and the first motor is fixed under side plate
Side, the first motor be electrically connected with PLC, the first motor and the drive connection of the first drive shaft, and described sleeve pipe is set in the
In one drive shaft, described sleeve pipe with the junction of the first drive shaft be equipped with matched first screw thread of the first drive shaft, it is described
Casing is hinged with strut.
Preferably, in order to adjust the position of the second photovoltaic panel, the lifting unit includes the second motor and two adjustings
Unit, second motor are electrically connected with PLC, and two adjust the both sides that unit is located at the second motor, the adjusting unit
Including bearing, the second drive shaft, movable block and adjusting rod, the bearing and the second motor are each attached to the top of slide plate, described
One end of second motor and the second drive shaft is sequentially connected, and the other end of second drive shaft is arranged in bearing, the shifting
Motion block is set in the second drive shaft, and being equipped with the junction of the second drive shaft for the movable block is matched with the second drive shaft
Screw thread, the movable block are hinged by adjusting rod and the second photovoltaic panel.
Preferably, in order to realize that the movement of slide plate, the telescopic unit include third motor, first connecting rod and the second company
Bar, the third motor are fixed on the bottom in recess, and the third motor is electrically connected with PLC, the third motor and first
Link transmission connects, and the first connecting rod is hinged by second connecting rod and slide plate.
Preferably, in order to ensure that the steady movement of slide plate, the sliding unit include slideway and sliding block, the slideway is solid
It is scheduled on the inner wall of recess, the sliding block is fixed on slide plate, and the sliding block is slidably connected with slideway.
Preferably, sliding block is detached from slideway in order to prevent, the slideway is dovetail groove.
Preferably, in order to which Auxiliary support casing moves, the translation unit further includes fixed ring, and the fixed ring is fixed
In the lower section of side plate, the Fixing shrink ring is located on casing.
Preferably, in order to realize the flight function of equipment, the flight component include the 4th motor, the 4th drive shaft and
Several rotors, the 4th motor are fixed on side plate, and the 4th motor is electrically connected with PLC, and the rotor is circumferential uniformly to be divided
Cloth is connect by the 4th drive shaft with rotary-wing transmission in the periphery of the 4th drive shaft, the 4th motor.
Preferably, in order to realize the safe landing of equipment, the first magnet, spring and the second magnetic are equipped in the support tube
Iron, first magnet are fixed on the top in support tube, and first magnet is connect by spring with the second magnet, and described
Two magnet are fixedly connected with slide bar.
Preferably, in order to make slide bar be moved with fixed direction, spacing ring, the limit are additionally provided in the support tube
Ring is fixed on the inner wall of support tube, and the spacing ring is set on slide bar.
Preferably, in order to realize that the acquisition function of face, the photographic unit include the 5th motor, cross bar, the 6th electricity
Machine, buffer stopper, the 6th drive shaft and camera, the 5th motor are fixed on the lower section of main body, the 5th motor and cross bar
Drive connection, the 6th motor and buffer stopper are separately fixed at the both ends of cross bar, and the 6th drive shaft is located at the 6th motor
Between buffer stopper, the 6th motor and the 6th drive shaft are sequentially connected, and the camera is fixed in the 6th drive shaft, institute
The 5th motor, the 6th motor and camera is stated to be electrically connected with PLC.
The invention has the advantages that the flight instruments for finding the personnel that wander away of the cruising ability by force pass through generator
Structure improves photovoltaic generation area, increases generated energy, flies for equipment, to strengthen cruising ability, with existing generator
Structure is compared, which improves generating efficiency by increasing photovoltaic generation area, moreover, during execution task,
It by supporting mechanism so that support tube is rotated to side plate, prevents from blocking camera, it is a wide range of to ensure that camera can acquire lower section
Facial image, help people to find and wander away personnel, improve the practicability of equipment, compared with existing supporting mechanism, the branch
Support mechanism additionally aids the safe landing of equipment.
Description of the drawings
Present invention will be further explained below with reference to the attached drawings and examples.
Fig. 1 is the structural schematic diagram of the strong flight instruments for finding the personnel that wander away of the cruising ability of the present invention；
Fig. 2 is that the structure of the electrification component of the strong flight instruments for finding the personnel that wander away of the cruising ability of the present invention is shown
It is intended to；
Fig. 3 is that the structure of the lifting unit of the strong flight instruments for finding the personnel that wander away of the cruising ability of the present invention is shown
It is intended to；
Fig. 4 is that the structure of the supporting mechanism of the strong flight instruments for finding the personnel that wander away of the cruising ability of the present invention is shown
It is intended to；
Fig. 5 is that the structure of the photographic unit of the strong flight instruments for finding the personnel that wander away of the cruising ability of the present invention is shown
It is intended to；
In figure：1. main body, 2. first photovoltaic panels, 3. generation blocks, 4. slide plates, 5. second photovoltaic panels, 6. side plates, 7. supports
Pipe, 8. slide bars, 9. buffer boards, 10. struts, 11. first motors, 12. first drive shafts, 13. casings, 14. second motors, 15.
Bearing, 16. second drive shafts, 17. movable blocks, 18. adjusting rods, 19. third motors, 20. first connecting rods, 21. second connecting rods,
22. slideway, 23. sliding blocks, 24. fixed rings, 25. the 4th motors, 26. the 4th drive shafts, 27. rotors, 28. first magnet, 29. bullets
Spring, 30. second magnet, 31. spacing rings, 32. the 5th motors, 33. cross bars, 34. the 6th motors, 35. buffer stoppers, 36. the 6th drive
Moving axis, 37. cameras.
Specific implementation mode
In conjunction with the accompanying drawings, the present invention is further explained in detail.These attached drawings are simplified schematic diagram, only with
Illustration illustrates the basic structure of the present invention, therefore it only shows the composition relevant to the invention.
As shown in Figure 1, the flight instruments for finding the personnel that wander away that a kind of cruising ability is strong, including main body 1, camera
Structure, power generation mechanism and several supporting mechanisms, the photographic unit and power generation mechanism are separately positioned on the following above and of main body 1,
PLC is equipped in the main body 1, the supporting mechanism is circumferentially evenly distributed on the periphery of main body 1, and the power generation mechanism includes first
Photovoltaic panel 2 and generation block 3, first photovoltaic panel 2 are fixed on the top of main body 1 by generation block 3, in the generation block 3 from
It above divides into there are four recess, the opening of four recesses is located on four sides of generation block 3, and hair is equipped in the recess
Electrical component；
The flight instruments drive main body 1 to carry out in the air during execution is found and wanders away personnel by supporting mechanism
It is mobile, facial image is acquired using the photographic unit of 1 lower section of main body, to carry out recognition of face, determines that captured personnel are
No is the personnel that wander away, and so that equipment is carried out photovoltaic generation on sunny daytime by power generation mechanism, provides the energy of equipment flight, from
And the follow-on mission time of equipment is extended, cruising ability is strengthened, convenient for equipment for a long time into administrative staff's search, power generation
In mechanism, photovoltaic generation is carried out by the first photovoltaic panel 2, and the lower section of the first photovoltaic panel 2, the electrification component in four recesses is never
Same direction is stretched out, and four sides of the first photovoltaic panel 2 are moved to, and expands photovoltaic generation area, to reinforce generating capacity, Jin Erti
The high cruising ability of equipment.
As Figure 2-3, the electrification component includes telescopic unit, slide plate 4, lifting unit, the second photovoltaic panel 5 and two
The bottom in recess is arranged in sliding unit, the telescopic unit, and the telescopic unit is sequentially connected with slide plate 4, and described second
Photovoltaic panel 5 is located at the top of slide plate 4, and the lifting unit is located between slide plate 4 and the second photovoltaic panel 5, the lifting unit with
Second photovoltaic panel 5 is sequentially connected, and two sliding units are located at the both sides of slide plate 4；
When discharge assembly is run, slide plate 4 is driven to move by telescopic unit so that slide plate 4 drives in two sliding units
Under position-limiting action, smoothly moved to the outside of recess along fixed direction, and the top of tail skid 4, pass through lifting unit
The second photovoltaic panel 5 is driven to move up, the plane where making the second photovoltaic panel 5 is overlapped with the plane where the first photovoltaic panel 2, is prevented
Only generation block 3 and the first photovoltaic panel 2 block solar irradiation and are mapped to the second photovoltaic panel 5, and then make power generation mechanism in the first photovoltaic panel 2
Surrounding by stretching out the second photovoltaic panel 5, to expand photovoltaic generation area, to strengthen generating capacity, improve
The cruising ability of equipment.
As shown in figure 4, one end of the side plate 6 is fixed on the body 1, the flight component is arranged in the another of side plate 6
End, the support component are located at the lower section of main body 1, the support component include fixed link, support tube 7, slide bar 8, buffer board 9,
Strut 10 and translation unit, the bottom end of the fixed link are fixed on the lower section of main body 1, bottom end and the support tube 7 of the fixed link
Hinged, the top of the slide bar 8 is arranged in support tube 7, and the bottom end of the slide bar 8 is fixedly connected with buffer board 9, the translation
Unit is located at the lower section of side plate 6, and the translation unit and one end of strut 10 are sequentially connected, the other end and branch of the strut 10
Stay tube 7 is hinged；
The translation unit includes that first motor 11, the first drive shaft 12 and casing 13, the first motor 11 are fixed on
The lower section of side plate 6, the first motor 11 are electrically connected with PLC, and the first motor 11 and the first drive shaft 12 are sequentially connected, institute
Casing 13 is stated to be set in the first drive shaft 12, described sleeve pipe 13 be equipped with the junction of the first drive shaft 12 and the first driving
12 matched first screw thread of axis, described sleeve pipe 13 are hinged with strut 10.
In supporting mechanism, by the flight assembly operating of one end of the separate main body 1 of side plate 6, equipment can be driven vacantly to fly
Row execute search task, using support component convenient for equipment safety landing, simultaneously support component can flexible modulation form, prevent from hiding
It keeps off camera 37 and acquires image, PLC can control the first motor 11 in support component in translation unit to start, and drive the first driving
Axis 12 rotates, and the first drive shaft 12 is by the first threaded function on casing 13 so that casing 13 is along the first drive shaft 12
Axis moves, when casing 13 to main body 1 close to when, casing 13 drives support tube 7 time to rotate by strut 10, makes at support tube 7
In vertical angle, is landed convenient for equipment safety by buffer board 9 and slide bar 8, moved to the direction far from main body 1 when casing 13
When, casing 13 pulls support tube 7 to be rotated to side plate 6 by strut 10 so that the angle of two support tubes 7 increases, to convenient
Photographic unit shoots pedestrian's face image on road surface, carries out recognition of face, convenient for executing the searching the personnel that wander away of the task.
As shown in figure 3, the lifting unit include the second motor 14 and two adjusting units, second motor 14 with
PLC is electrically connected, and two adjust the both sides that unit is located at the second motor 14, and the adjusting unit includes that bearing 15, second drives
Moving axis 16, movable block 17 and adjusting rod 18, the bearing 15 and the second motor 14 are each attached to the top of slide plate 4, and described second
One end of motor 14 and the second drive shaft 16 is sequentially connected, and the other end of second drive shaft 16 is arranged in bearing 15, institute
Movable block 17 is stated to be set in the second drive shaft 16, the movable block 17 be equipped with the junction of the second drive shaft 16 and second
16 matched screw thread of drive shaft, the movable block 17 are hinged by adjusting rod 18 and the second photovoltaic panel 5.
PLC controls the second motor 14 and starts, and drives the second drive shaft 16 in the adjusting unit of both sides to rotate, the second drive shaft
16 by the second threaded function on movable block 17 so that movable block 17 is translated along the axis of the second drive shaft 16, into
And by adjusting rod 18 drive the second photovoltaic panel 5 movement, change the second photovoltaic panel 5 between slide plate 4 at a distance from, realize the second photovoltaic
The lifting of plate 5,
As shown in Fig. 2, the telescopic unit includes third motor 19, first connecting rod 20 and second connecting rod 21, the third
Motor 19 is fixed on the bottom in recess, and the third motor 19 is electrically connected with PLC, the third motor 19 and first connecting rod 20
It is sequentially connected, the first connecting rod 20 is hinged by second connecting rod 21 and slide plate 4.
PLC controls third motor 19 and starts, and first connecting rod 20 is driven to rotate, and first connecting rod 20 is acted on by second connecting rod 21
On slide plate 4 so that slide plate 4 moves.
Preferably, in order to ensure the steady movement of slide plate 4, the sliding unit includes slideway 22 and sliding block 23, described
Slideway 22 is fixed on the inner wall of recess, and the sliding block 23 is fixed on slide plate 4, and the sliding block 23 is slidably connected with slideway 22.
Since the position of slideway 22 is fixed, sliding block 23 is moved in slideway 22 along fixed direction, to secure slide plate 4
Moving direction makes slide plate 4 smoothly be moved.
Preferably, sliding block 23 is detached from slideway 22 in order to prevent, the slideway 22 is dovetail groove.
Preferably, in order to which Auxiliary support casing 13 moves, the translation unit further includes fixed ring 24, the fixed ring
24 are fixed on the lower section of side plate 6, and the fixed ring 24 is set on casing 13.Using 24 Auxiliary support casing 13 of fixed ring, prevent
When only the first drive shaft 12 rotates, casing 13 rotates, and then ensure that the steady movement of casing 13.
As shown in figure 4, the flight component includes the 4th motor 25, the 4th drive shaft 26 and several rotors 27, described the
Four motors 25 are fixed on side plate 6, and the 4th motor 25 is electrically connected with PLC, and the rotor 27 is circumferential to be evenly distributed on the 4th
The periphery of drive shaft 26, the 4th motor 25 are sequentially connected by the 4th drive shaft 26 with rotor 27.
PLC controls the 4th motor 25 and starts, and drives rotor 27 to rotate by the 4th drive shaft 26 so that rotor 27 generates gas
Stream drives 1 floating block of main body, and search task is executed convenient for flight.
As shown in figure 4, being equipped with the first magnet 28, spring 29 and the second magnet 30, first magnet in the support tube 7
28 are fixed on the top in support tube 7, and first magnet 28 is connect by spring 29 with the second magnet 30, second magnet
30 are fixedly connected with slide bar 8.When equipment is landed, buffer board 9 is against on the ground, by 30 compressed spring 29 of the second magnet,
Slow down the decrease speed of equipment, simultaneously because the distance between the first magnet 28 and the second magnet 30 increase, and the first magnet 28
Repel each other with the magnetism of the second magnet 30 so that the first magnet 28 generates elastic force to the second magnet 30, further slows down equipment
Decrease speed makes equipment carry out safe landing.
Preferably, in order to make slide bar 8 be moved with fixed direction, it is additionally provided with spacing ring 31 in the support tube 7, it is described
Spacing ring 31 is fixed on the inner wall of support tube 7, and the spacing ring 31 is set on slide bar 8.Cunning is secured using spacing ring 31
The moving direction of bar 8, so that the movement of 8 held stationary of slide bar.
As shown in figure 5, the photographic unit includes the 5th motor 32, cross bar 33, the 6th motor 34, buffer stopper the 35, the 6th
Drive shaft 36 and camera 37, the 5th motor 32 are fixed on the lower section of main body 1, and the 5th motor 32 is driven with cross bar 33
Connection, the 6th motor 34 and buffer stopper 35 are separately fixed at the both ends of cross bar 33, and the 6th drive shaft 36 is located at the 6th
Between motor 34 and buffer stopper 35, the 6th motor 34 and the 6th drive shaft 36 are sequentially connected, and the camera 37 is fixed on
In 6th drive shaft 36, the 5th motor 32, the 6th motor 34 and camera 37 are electrically connected with PLC.
PLC controls the operation of the 5th motor 32, adjusts the rotational angle of cross bar 33, and controls the 6th motor 34 and start, and drives
6th drive shaft 36 rotates so that camera 37 rotates, and to adjust the angle of camera 37, enables camera 37 to everywhere
Face is acquired, and facial image is uploaded to PLC so that PLC carries out recognition of face, missing convenient for being found in each face
The face of personnel, to help people to look for the personnel of wandering away.
The flight instruments drive slide plate 4 to move during the worker tasks that wander away are searched in execution, by telescopic unit, make slide plate
4 remove recesses, and by lifting unit make the second photovoltaic panel 5 rise to 2 sustained height position of the first photovoltaic panel, utilize first
Photovoltaic panel 2 and four the second photovoltaic panels 5 are carried out at the same time photovoltaic generation, due to expanding photovoltaic generation area, to improve hair
Electric energy caused by photovoltaic generation is flown for equipment and is used by electricity, long convenient for equipment to strengthen the cruising ability of equipment
Time executes search task, moreover, drives support tube 7 to be rotated to side plate 6 by translation unit, avoids support tube 7, slide bar
8 and buffer board 9 block camera 37, to facilitate camera 37 to carry out large-scale Image Acquisition to lower section, people is helped to exist
The personnel of wandering away are found in crowd, to improve the practicability of equipment.
Compared with prior art, the cruising ability it is strong for finding the flight instruments of the personnel that wander away by power generation mechanism,
Photovoltaic generation area is improved, generated energy is increased, is flown for equipment, to strengthen cruising ability, with existing power generation mechanism
It compares, which improves generating efficiency by increasing photovoltaic generation area, moreover, during execution task, leads to
Crossing supporting mechanism makes support tube 7 be rotated to side plate 6, prevents from blocking camera 37, and it is big to ensure that camera 37 can acquire lower section
The facial image of range helps people to find the personnel that wander away, improves the practicability of equipment, compared with existing supporting mechanism,
The supporting mechanism additionally aids the safe landing of equipment.
It is enlightenment with above-mentioned desirable embodiment according to the present invention, through the above description, relevant staff is complete
Various changes and amendments can be carried out without departing from the scope of the technological thought of the present invention' entirely.The technology of this invention
Property range is not limited to the contents of the specification, it is necessary to determine its technical scope according to right.
Claims (10)
1. a kind of strong flight instruments for finding the personnel that wander away of cruising ability, which is characterized in that including main body (1), shooting
Mechanism, power generation mechanism and several supporting mechanisms, the photographic unit and power generation mechanism are separately positioned on the lower section of main body (1) and upper
Side, the main body (1) is interior to be equipped with PLC, and the supporting mechanism is circumferentially evenly distributed on the periphery of main body (1), the power generation mechanism
Including the first photovoltaic panel (2) and generation block (3), first photovoltaic panel (2) is fixed on the upper of main body (1) by generation block (3)
It is square, it is set from top to down on the generation block (3) there are four recess, the opening of four recesses is located at four of generation block (3)
On side, electrification component is equipped in the recess；
The electrification component includes telescopic unit, slide plate (4), lifting unit, the second photovoltaic panel (5) and two sliding units, institute
The bottom that telescopic unit is arranged in recess is stated, the telescopic unit is sequentially connected with slide plate (4), second photovoltaic panel (5)
Top positioned at slide plate (4), the lifting unit are located between slide plate (4) and the second photovoltaic panel (5), the lifting unit and
Two photovoltaic panels (5) are sequentially connected, and two sliding units are located at the both sides of slide plate (4)；
The supporting mechanism includes side plate (6), flight component and support component, and one end of the side plate (6) is fixed on main body (1)
On, the other end in side plate (6) is arranged in the flight component, and the support component is located at the lower section of main body (1), the support group
Part includes fixed link, support tube (7), slide bar (8), buffer board (9), strut (10) and translation unit, the bottom end of the fixed link
It is fixed on the lower section of main body (1), the bottom end of the fixed link and support tube (7) are hinged, and the top setting of the slide bar (8) is being propped up
In stay tube (7), the bottom end of the slide bar (8) is fixedly connected with buffer board (9), and the translation unit is located at the lower section of side plate (6),
The translation unit and one end of strut (10) are sequentially connected, and the other end and support tube (7) of the strut (10) are hinged；
The translation unit includes first motor (11), the first drive shaft (12) and casing (13), and the first motor (11) is solid
It is scheduled on the lower section of side plate (6), the first motor (11) is electrically connected with PLC, the first motor (11) and the first drive shaft
(12) be sequentially connected, described sleeve pipe (13) is set in the first drive shaft (12), described sleeve pipe (13) with the first drive shaft
(12) junction, which is equipped with, to be hinged with matched first screw thread of the first drive shaft (12), described sleeve pipe (13) with strut (10).
2. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that described
Lifting unit includes the second motor (14) and two adjusting units, and second motor (14) is electrically connected with PLC, and two adjust list
Member is located at the both sides of the second motor (14), and the adjusting unit includes bearing (15), the second drive shaft (16), movable block
(17) and adjusting rod (18), the bearing (15) and the second motor (14) are each attached to the top of slide plate (4), second motor
(14) it is sequentially connected with one end of the second drive shaft (16), the other end of second drive shaft (16) is arranged in bearing (15)
Interior, the movable block (17) is set in the second drive shaft (16), the company with the second drive shaft (16) of the movable block (17)
It meets place and is equipped with and pass through adjusting rod (18) and the second photovoltaic panel with the second drive shaft (16) matched screw thread, the movable block (17)
(5) hinged.
3. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that described
Telescopic unit includes third motor (19), first connecting rod (20) and second connecting rod (21), and the third motor (19) is fixed on recessed
Bottom in mouthful, the third motor (19) are electrically connected with PLC, and the third motor (19) connects with first connecting rod (20) transmission
It connects, the first connecting rod (20) is hinged by second connecting rod (21) and slide plate (4).
4. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that described
Sliding unit includes slideway (22) and sliding block (23), and the slideway (22) is fixed on the inner wall of recess, and the sliding block (23) is solid
It is scheduled on slide plate (4), the sliding block (23) is slidably connected with slideway (22).
5. the strong flight instruments for finding the personnel that wander away of cruising ability as claimed in claim 4, which is characterized in that described
Slideway (22) is dovetail groove.
6. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that described
Translation unit further includes fixed ring (24), and the fixed ring (24) is fixed on the lower section of side plate (6), and the fixed ring (24) is arranged
On casing (13).
7. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that described
Flight component includes the 4th motor (25), the 4th drive shaft (26) and several rotors (27), and the 4th motor (25) is fixed on
On side plate (6), the 4th motor (25) is electrically connected with PLC, and the rotor (27) is circumferentially evenly distributed on the 4th drive shaft
(26) periphery, the 4th motor (25) are sequentially connected by the 4th drive shaft (26) and rotor (27).
8. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that described
The first magnet (28), spring (29) and the second magnet (30) are equipped in support tube (7), first magnet (28) is fixed on support
The top in (7) is managed, first magnet (28) is connect by spring (29) with the second magnet (30), second magnet (30)
It is fixedly connected with slide bar (8).
9. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that described
It is additionally provided with spacing ring (31) in support tube (7), the spacing ring (31) is fixed on the inner wall of support tube (7), the spacing ring
(31) it is set on slide bar (8).
10. the strong flight instruments for finding the personnel that wander away of cruising ability as described in claim 1, which is characterized in that institute
State photographic unit include the 5th motor (32), cross bar (33), the 6th motor (34), buffer stopper (35), the 6th drive shaft (36) and
Camera (37), the 5th motor (32) are fixed on the lower section of main body (1), and the 5th motor (32) is driven with cross bar (33)
Connection, the 6th motor (34) and buffer stopper (35) are separately fixed at the both ends of cross bar (33), the 6th drive shaft (36)
Between the 6th motor (34) and buffer stopper (35), the 6th motor (34) is sequentially connected with the 6th drive shaft (36), institute
It states camera (37) to be fixed in the 6th drive shaft (36), the 5th motor (32), the 6th motor (34) and camera (37)
It is electrically connected with PLC.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810505427.5A CN108583884A (en) | 2018-05-24 | 2018-05-24 | A kind of flight instruments for finding the personnel that wander away that cruising ability is strong |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810505427.5A CN108583884A (en) | 2018-05-24 | 2018-05-24 | A kind of flight instruments for finding the personnel that wander away that cruising ability is strong |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108583884A true CN108583884A (en) | 2018-09-28 |
Family
ID=63629181
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810505427.5A Withdrawn CN108583884A (en) | 2018-05-24 | 2018-05-24 | A kind of flight instruments for finding the personnel that wander away that cruising ability is strong |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108583884A (en) |
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| CN109693792A (en) * | 2019-01-15 | 2019-04-30 | 广州市鹭江远科技有限公司 | A kind of unmanned plane with cleaning function |
| 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 |
| CN111829504A (en) * | 2019-04-16 | 2020-10-27 | 深圳富泰宏精密工业有限公司 | Aircraft and detection method |
| CN112093037A (en) * | 2020-09-02 | 2020-12-18 | 南京航空航天大学 | Rotor unmanned aerial vehicle landing device |
| CN113306707A (en) * | 2021-07-29 | 2021-08-27 | 深圳市青之鸟科技有限公司 | Unmanned aerial vehicle undercarriage and unmanned aerial vehicle |
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| CN109693792A (en) * | 2019-01-15 | 2019-04-30 | 广州市鹭江远科技有限公司 | A kind of unmanned plane with cleaning function |
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| CN113306707B (en) * | 2021-07-29 | 2021-12-07 | 深圳市青之鸟科技有限公司 | Unmanned aerial vehicle undercarriage and unmanned aerial vehicle |
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Application publication date: 20180928 |
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