CN212556781U - Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft - Google Patents
Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft Download PDFInfo
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- CN212556781U CN212556781U CN202021179849.7U CN202021179849U CN212556781U CN 212556781 U CN212556781 U CN 212556781U CN 202021179849 U CN202021179849 U CN 202021179849U CN 212556781 U CN212556781 U CN 212556781U
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Abstract
The utility model provides a green photoelectric sensing system of integrated application of on-vehicle stereomonitoring aircraft of suspension type, its characteristic: the bottom of the six-axis solar monitoring aircraft is provided with a magnetic type positioning seat, and the lower surface of a positioning magnetic steel sheet of the magnetic type positioning seat is upwards recessed into a plurality of positioning pits; the magnetic type positioning disc is arranged on the rear wall of the tail of the motor vehicle and the top of the motor vehicle, and a plurality of positioning columns extend upwards from the upper surface of a positioning magnetic steel sheet of the magnetic type positioning disc; the magnetic positioning disc positioning magnetic steel sheet is connected with a vehicle-mounted monitoring platform host computer in the motor vehicle; the sensor mounting plate is mounted on a shell of the six-axis solar monitoring aircraft, and the photoelectric sensor is mounted on the sensor mounting plate; the sensor main control board is connected with a vehicle-mounted platform main computer in the motor vehicle in a 5G network wireless signal mode. The utility model discloses make on-vehicle monitoring device combine and implement the vertical take-off with green protection casing organic reliably, realize all-round control and real-time warning.
Description
Technical Field
The utility model relates to an integrated application field of on-vehicle moving platform sensor technique specifically relates to the integrated photoelectric sensing system who uses of on-vehicle stereo monitoring aircraft of suspension type.
Background
With continuous progress of scientific technology and increasingly complex urban traffic, demands of people are increasingly diversified, so that urban public safety is challenged and threatened more severely, demands for monitoring types and quality of data sources are higher and higher, and new demands and challenges are provided for planning and designing public safety monitoring.
The vehicle-mounted monitoring is generally fixed on the vehicle roof, the monitoring data is single, a three-dimensional monitoring function is not realized, the provided data is unscientific and comprehensive, the warning can not be stopped through monitoring when illegal and messy behaviors are met, a great deal of inconvenience is brought to a manager, and the ever-increasing urban public safety requirements can not be met.
SUMMERY OF THE UTILITY MODEL
In order to solve the above-mentioned problem that exists among the prior art, the utility model provides a green photoelectric sensing system of the integrated application of on-vehicle three-dimensional monitoring aircraft of suspension type, its novel purpose of usefulness makes on-vehicle monitoring device combine with green protection casing reliably, implements vertical takeoff to can realize the effective control and the real-time warning of multiple data source.
The technical scheme of the utility model as follows:
green photoelectric sensing system of integrated application of on-vehicle three-dimensional surveillance aircraft of suspension type, its characterized in that:
the six-axis solar monitoring aircraft is provided with six foldable propeller supports, and the end parts of the propeller supports are propellers driven by motors;
an aircraft main control board is installed in the six-axis solar monitoring aircraft, and the aircraft main control board is connected with a vehicle-mounted monitoring platform main computer in a motor vehicle in a 5G wireless mode;
the magnetic type positioning seat is mounted at the bottom of a shell of the six-axis solar monitoring aircraft, a main body of the magnetic type positioning seat is a positioning magnetic steel sheet, and the lower surface of the positioning magnetic steel sheet is upwards recessed into a plurality of oval positioning pits;
the magnetic suction type positioning disc is arranged on the rear wall and the top of the tail of the motor vehicle respectively, the main body of the magnetic suction type positioning disc is a positioning magnetic steel sheet, and a plurality of oval positioning columns extend upwards from the upper surface of the positioning magnetic steel sheet;
the positioning magnetic steel sheet of the magnetic type positioning disc is connected with a vehicle-mounted monitoring platform host computer in the motor vehicle;
the sensor mounting plate is mounted on a shell of the six-axis solar monitoring aircraft, and the photoelectric sensor is mounted on the sensor mounting plate;
a sensor main control board is installed on the sensor installation board and connected with the photoelectric sensor, and the sensor main control board is connected with a vehicle-mounted monitoring platform host computer in the motor vehicle in a 5G network wireless signal mode;
the solar cell panel is arranged on the upper surface of the six-axis solar monitoring aircraft and connected with the battery to charge the battery, and the battery drives and supplies power to the motor of the propeller, the aircraft main control board, the photoelectric sensor and the sensor main control board;
in the parking state:
the six-axis solar monitoring aircraft is matched with the magnetic type positioning disc on the rear wall of the tail of the motor vehicle and is fixedly hung on the rear wall of the tail of the motor vehicle to prevent the protective cover from covering the magnetic type positioning disc on the rear wall of the tail of the motor vehicle and the six-axis solar monitoring aircraft, the protective cover is made of cylindrical waterproof rubber cloth, flexible solar photovoltaic power generation materials are arranged on the protective cover and are connected with the battery through a plug,
the six-axis solar monitoring aircraft is suspended in the middle of the rear wall of the vehicle tail to facilitate safe camouflage and hidden sneak, and closely cooperates with the vehicle-mounted platform to hide forward and maneuver for long-distance travel. When the aircraft is positioned on the magnetic type positioning disk at the tail of the vehicle, the aircraft can be protected and disguised by covering a green protective cover (made of rubber cloth photovoltaic power generation materials), and a spiral power line and a plug are arranged in the protective cover to charge the aircraft; the protective cover has green and environment-friendly positive energy and vehicle-mounted camouflage function, can assist and cooperate with an internal aircraft in the field to implement on-site emergency vertical takeoff at the tail of the vehicle under special conditions,
or the six-axis solar monitoring aircraft is fixed on the top of the motor vehicle by matching with the magnetic-type positioning disc on the top of the motor vehicle,
when the six-axis solar monitoring aircraft is matched with the magnetic type positioning disc, the oval positioning column of the magnetic type positioning disc is inserted into the oval positioning pit of the magnetic type positioning seat, the positioning magnetic steel sheet of the magnetic type positioning disc is electrified to generate magnetic force, and the positioning magnetic steel sheet of the magnetic type positioning disc and the positioning magnetic steel sheet of the magnetic type positioning seat are attracted;
when in a flying state:
the magnetic steel sheet of the magnetic type positioning disc is powered off, and the six-axis solar monitoring aircraft flies away.
Preferably:
the photoelectric sensor is one or more integrated applications of a lightning detection sensor, a human body pyroelectric sensor, a mobile metal detector, an air quality sensor, a full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system, a servo holder network camera and a strong light lamp.
Preferably:
the cross section of the shell of the six-axis solar monitoring aircraft is oval.
Preferably:
a shielding magnetic field copper sheet is arranged between the upper surface of the positioning magnetic steel sheet of the magnetic type positioning seat and the six-axis solar monitoring aircraft, and a rubber pad is arranged on the lower surface of the positioning magnetic steel sheet of the magnetic type positioning seat; be equipped with shielding magnetic field copper sheet between the location magnetic steel sheet lower surface of formula positioning disk and the motor vehicle is inhaled to magnetism, the last surface mounting who inhales the location magnetic steel sheet of formula positioning disk has the screw hole that is used for fixing that runs through.
Preferably:
the cross sections of the positioning pits and the positioning columns are in precise matching ellipses.
Preferably:
when the positioning column of the magnetic type positioning disc is inserted into the positioning pit of the magnetic type positioning seat, a stainless steel bolt installed on the rear wall of the motor vehicle penetrates through the jack on the six-axis solar monitoring aircraft shell and is locked.
Preferably:
the sensor mounting plate is arranged on a shell of the six-axis solar monitoring aircraft to form a closed space with heat dissipation holes; and a signal processor protection device for protecting the sensor signal processor is arranged above the closed space, and the protection device is fixedly connected with the shell.
Preferably:
and a buffer gasket is arranged between the sensor mounting plate and the shell of the six-axis solar aircraft.
Preferably:
the installation position of the photoelectric sensor on the sensor installation plate is as follows: the upper part of the upper surface is provided with a lightning detection sensor, the middle part is provided with an air quality monitoring sensor, the right rear part is provided with a servo pan-tilt network camera with adjustable high-multiple high resolution, the left rear part is provided with a human body pyroelectric sensor, the right front part is provided with a mobile metal detector, the left front part is provided with a full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system, and the middle of the lower surface is provided with a strong light and a high-power horn; the middle part of the magnetic type positioning seat below the highlight lamp is provided with a light through hole.
The utility model has the advantages that:
(1) the six-axis solar flight monitor is integrated with a servo holder network camera, a lightning detection sensor, an air quality monitor, a mobile metal detector, a human body pyroelectric sensor, a full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system and a strong light, so that the six-axis solar flight monitor has the latest monitoring functions of lightning monitoring, air quality monitoring, control cutter monitoring, people flow monitoring, epidemic situation monitoring and the like, and has the functions of warning and stopping illegal and disordered activities by utilizing the strong light and a high-power horn.
(2) The concave-convex steel metal plate which is easy to attract magnetically utilizes the electromagnetic field effect to achieve fixed wall hanging at the tail part of the vehicle, so that the six-axis solar flight monitor can take off freely and be fixed.
(3) Through stainless steel bolt embolus for six solar energy flight watch-dog reliably are fixed in the rear of a vehicle and are protected.
(4) The six propellers can be arranged to freely, conveniently and stereoscopically acquire and monitor data.
(5) The solar cell panel photovoltaic power generation can charge for the inside battery of six solar flight watch-dog, and the battery provides the energy for six solar flight watch-dogs.
Drawings
Fig. 1 is a schematic view of an overall appearance structure of an embodiment of a photoelectric sensing system component for integrated application of a suspension type vehicle-mounted stereo monitoring aircraft according to the present invention;
FIG. 2 is a schematic view of the green photoelectric sensing system component of the suspension type vehicle-mounted stereo surveillance aircraft of the present invention, which is suspended and parked at the rear wall of the tail of the motor vehicle when in a static state;
FIG. 3 is a schematic view of the suspended type vehicle-mounted stereo surveillance aircraft of the present invention, which is parked on the top of the motor vehicle during the dynamic state of the photoelectric sensing system assembly
FIG. 4 is a schematic diagram of a lightning sensor circuit in a photoelectric sensing system component of the suspension type vehicle-mounted three-dimensional monitoring aircraft of the present invention;
FIG. 5 is a schematic view of the internal layout of the components of the photoelectric sensing system of the integrated application of the suspension type vehicle-mounted stereo surveillance aircraft of the present invention;
fig. 6 is a schematic top view of the magnetic positioning plate installed on the motor vehicle according to the present invention;
fig. 7 is a view of the magnetic-type positioning plate a mounted on the motor vehicle of the present invention;
fig. 8 is a schematic bottom view of the magnetic type positioning seat installed on the six-axis solar monitoring aircraft of the present invention;
fig. 9 is a view of the magnetic type positioning seat B installed on the six-axis solar monitoring aircraft of the present invention;
fig. 10 is a bottom view of the green protective cover of the present invention.
Detailed Description
In order to more clearly illustrate the technical solution of the present invention, the drawings used in the description will be briefly introduced, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other embodiments can be obtained according to the drawings without inventive labor. In order to facilitate understanding of the present invention, the present invention will be described in more detail with reference to the accompanying drawings and specific embodiments.
It will be understood that when an element is referred to as being "secured to" another element, it can be directly on the other element or intervening elements may also be present. When an element is referred to as being "connected" to another element, it can be directly connected to the other element or intervening elements may be present. The terms "upper", "lower", "inner", "outer", "bottom", and the like as used herein are used in the description to indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are used only for convenience in describing the present invention and for simplicity in description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.
As shown in fig. 1 and 5:
the utility model discloses an integrated green photoelectric sensing system's of using of on-vehicle stereomonitoring aircraft of suspension type embodiment:
the six-shaft solar monitoring aircraft 3 as a main body is provided with six propeller supports, the end parts of the propeller supports are motor-driven propellers 9, and the propellers 9 are components for assisting free flight.
The cross section of the shell of the six-axis solar monitoring aircraft 3 is oval, and the oval shell can enable the photoelectric sensor to be mounted more conveniently, so that the monitoring range is wider. The shell is provided with heat dissipation holes.
The propeller 9 of the six-axis solar monitoring aircraft 3 is automatically foldable. After folding, the six-axis solar monitoring aircraft 3 is in a portable oval shape.
An aircraft main control board is installed inside the six-axis solar monitoring aircraft 3, state signals of the six-axis solar monitoring aircraft 3 are transmitted to a vehicle-mounted monitoring platform main computer in a motor vehicle in a wireless mode, and control signals transmitted by the vehicle-mounted monitoring platform main computer are used for controlling the six-axis solar monitoring aircraft 3, so that stable free flight control of the six-axis aircraft is achieved.
The upper surface of the six-axis solar monitoring aircraft 3 is provided with a solar cell panel, the solar cell panel is connected with an internal battery, and the internal battery drives a motor of the propeller 9 and an aircraft main control board to supply power for the internal battery.
The propellers 9 and the motors of the six-axis solar monitoring aircraft 3, the aircraft main control board and the control system can be realized by purchasing the prior art. And then, the shell of the six-axis solar monitoring aircraft 3 is refitted and provided with the magnetic type positioning seat 2 and the following photoelectric sensor accessories.
As shown in fig. 1, 8, and 9:
the formula positioning seat 2 is inhaled with the connecting rod connection to install to six solar energy monitoring aircraft 3's casing bottom, and magnetism is inhaled 2 main parts of formula positioning seat and is a location magnetic steel sheet 20, is equipped with shielding magnetic field copper thin slice 23 between the upper surface of location magnetic steel sheet 20 and six solar energy monitoring aircraft 3 in order to protect photoelectric sensor, and the lower surface of location magnetic steel sheet 20 is upwards sunken to form the positioning pit 21 of three oval cross-section, and magnetism is inhaled 2 middle parts of formula positioning seat and is had light through-hole 29.
A rubber pad 22 is disposed on the lower surface of the positioning magnetic steel sheet 20, and the rubber pad 22 protects the roof of the motor vehicle 100 shown in fig. 2 and 3 and the magnetic type positioning plate 2' shown in fig. 6 and 7, and makes the appearance of the vehicle more beautiful.
As shown in fig. 2, 3, 6, and 7:
the main body of the magnetic type positioning disc 2 'is a positioning magnetic steel sheet 20', a magnetic field shielding copper sheet 23 'is arranged between the lower surface of the positioning magnetic steel sheet 20' and the motor vehicle 100 to protect the photoelectric sensor, and three positioning columns 21 'with oval cross sections extend upwards from the upper surface of the positioning magnetic steel sheet 20'.
The magnetic-type positioning plate 2 'is provided with a through screw hole 24' for fixing.
As shown in fig. 2, 3, 6, and 7:
a magnetic type positioning plate 2' for parking the six-axis solar monitoring aircraft 3 is mounted in a middle portion of a rear wall of the vehicle tail of the motor vehicle 100 by screwing.
The positioning magnetic steel sheet 20 'of the magnetic type positioning disc 2' is connected with a vehicle-mounted monitoring platform host computer in the motor vehicle 100.
A magnetically-attracted positioning plate 2' for parking the six-axis solar monitoring aircraft 3 is mounted in a screwed connection in the middle part of the roof of the motor vehicle 100.
The positioning magnetic steel sheet 20 'of the magnetic type positioning disc 2' is connected with a vehicle-mounted monitoring platform host computer in the motor vehicle 100.
As shown in fig. 2, 6, 7, 8, and 9:
when the vehicle went, six solar energy control aircraft 3 and the magnetic type positioning disk 2' cooperation of the back wall of motor vehicle 100 and fixed suspension are on the rear wall of the rear of a vehicle of motor vehicle 100, under the general condition, the motor vehicle is cross country vehicle, six solar energy control aircraft 3 hang and are convenient for safely disguise in the middle of the rear wall of the rear of a vehicle, conceal the sneak, closely cooperate on-vehicle platform to conceal the advance, motor vehicle is far away, accessible green cover protection casing (rubber blanket material, have the raincoat function) to protect and disguise when the aircraft is on the magnetic type positioning disk of the rear of a vehicle, and charge.
Magnetism is inhaled 2 positions of formula positioning seat and is inhaled formula positioning disk 2 ' position and correspond, and magnetism is inhaled reference column 21 ' of formula positioning disk 2 ' and is inserted in magnetism's the locating hole 21 of formula positioning seat 2, and reference column 21 ' and locating hole 21 play the spacing effect of avoiding breaking away from in location.
The vehicle-mounted monitoring platform main computer instructs the positioning magnetic steel sheet 20 'to be electrified to generate magnetic force, the positioning magnetic steel sheet 20' and the positioning magnetic steel sheet 20 are attracted, and the six-axis solar monitoring aircraft 3 is fixedly hung on the rear wall of the tail of the motor vehicle 100.
A stainless steel bolt 3' installed on the rear wall of the motor vehicle 100 penetrates through a jack on the shell of the six-axis solar monitoring aircraft 3 and is locked, so that the safety guarantee effect is achieved.
As shown in fig. 2 and 10:
when six solar energy control aircraft 3 were in on the magnetism of rear of a vehicle wall inhale formula positioning disk 2' the accessible covers green waterproof protection casing 200 (the rubberized fabric material, has the raincoat function) and protects and pretend:
the magnetic type positioning disc 2' for preventing the shield 200 from covering the rear walls of the six-axis solar monitoring aircraft 3 and the motor vehicle 100 is protected and camouflaged, the shield 200 is made of cylindrical waterproof rubber cloth, the flexible solar photovoltaic power generation material is arranged on the shield 200, and a spiral power line 201 and a plug 204 are arranged inside the shield and connected with the battery of the six-axis solar monitoring aircraft 3 to charge the six-axis solar monitoring aircraft 3.
The hood 200 is fixed to the rear wall of the vehicle 100 by a hood fixing bracket 202 and is locked by a hood lock 203 installed on the rear wall of the vehicle.
The six-axis solar monitoring aircraft 3 is suspended in the middle of the rear wall of the vehicle tail to facilitate safe camouflage and hidden sneak, and closely cooperates with the vehicle-mounted platform to hide forward and maneuver for long-distance travel. The protective cover 200 has the functions of environmental protection and vehicle-mounted camouflage, and can assist the internal six-axis solar monitoring aircraft 3 to implement the vehicle tail on-site emergency vertical takeoff under special conditions.
As shown in fig. 3, 6, 7, 8, and 9:
when the vehicle stops and the six-axis solar monitoring aircraft 3 is used, the six-axis solar monitoring aircraft 3 is matched with the magnetic type positioning disc 2' in the middle of the roof of the motor vehicle 100 and is fixed in the middle of the roof of the motor vehicle 100, so that the flying and the recovery are convenient:
magnetism is inhaled 2 positions of formula positioning seat and is inhaled formula positioning disk 2 ' position and correspond, and magnetism is inhaled reference column 21 ' of formula positioning disk 2 ' and is inserted in magnetism's the locating hole 21 of formula positioning seat 2, and reference column 21 ' and locating hole 21 play the spacing effect of avoiding breaking away from in location.
The vehicle-mounted monitoring platform main computer instructs the positioning magnetic steel sheet 20 'to be electrified to generate magnetic force, the positioning magnetic steel sheet 20' and the positioning magnetic steel sheet 20 are attracted, and the six-axis solar monitoring aircraft 3 is fixed in the middle of the roof of the motor vehicle 100.
When in a flying state:
the vehicle-mounted monitoring platform host computer instructs the positioning magnetic steel sheet 20' to power off, and the six-axis solar monitoring aircraft 3 flies away.
When in recovery:
the six-axis solar monitoring aircraft 3 flies back, the positioning column 21 ' is inserted into the positioning pit 21 after being positioned, the vehicle-mounted monitoring platform main computer instructs the positioning magnetic steel sheet 20 ' to be electrified to generate magnetic force, the positioning magnetic steel sheet 20 ' and the positioning magnetic steel sheet 20 are attracted, and the six-axis solar monitoring aircraft 3 is fixed in the middle of the roof of the motor vehicle 100.
As shown in fig. 1 and 5:
the photoelectric sensor as an accessory includes:
thunder and lightning detection sensor 6, human pyroelectric sensor 4, removal metal detector 5, air quality sensor 8, full-automatic AI non-contact infrared temperature measurement thermal imaging monitored control system 7, servo cloud platform network camera 10, strong light 1 and high-power loudspeaker 11 all install on the sensor mounting panel to all pass through screw with the sensor mounting panel and add shake gasket mode fixed connection.
The sensor mounting plate is arranged on a shell of the six-axis solar monitoring aircraft 3 to form a closed space with heat dissipation holes.
And a signal processor protection device for protecting the sensor signal processor is arranged above the closed space, and the protection device is fixedly connected with the shell.
Be equipped with the buffer spacer between the shell of sensor mounting panel and six solar aircraft 3, this buffer spacer plays the connection of stabilizing sensor mounting panel and six solar aircraft 3's shell.
The installation position of the photoelectric sensor on the sensor installation plate is as follows: the upper part of the upper surface of the main body is provided with a lightning detection sensor 6, the middle part of the main body is provided with an air quality sensor 8, the right rear part of the main body is provided with a servo pan-tilt network camera 10 capable of regulating high-multiple high-resolution, the left rear part is provided with a body pyroelectric sensor 4, the right front part is provided with a movable metal detector 5, the left front part is provided with a full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system 7, the middle of the lower surface is provided with a highlight lamp 1, and the left rear part of.
The lightning detection sensor 6 is used for lightning monitoring, and a circuit diagram thereof is shown in fig. 4 and is formed by connecting a lightning detector, a carrier circuit of a DFRobot, a charger, a power supply, a switch, a buzzer and the like.
The air quality sensor 8 monitors the air quality.
The servo tripod head network camera 10 is an adjustable high-multiple high-resolution tripod head servo network camera, and can remotely and freely control the camera at the background to realize free high-definition shooting at long distance and multiple angles.
The human body pyroelectric sensor 4 is used for counting by detecting human body pyroelectric signals so as to monitor the flow of people.
The moving metal detector 5 performs the monitoring of the pipe cutter by detecting a metal signal.
The full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system 7 monitors the epidemic situation of the person who gets the fever by measuring the temperature of the specific person remotely and keeping the distance of the aircraft beyond two meters of the human body.
The powerful light 1 and the powerful horn 11 can emit powerful light and real-time voice to warn the personnel of illegal discipline. Dotted lines in fig. 1 and 5 are light columns emitted by the floodlight 1, the light columns penetrate through the light through holes 29 formed in the middle of the magnetic type positioning seat 2, the irradiation lower part plays a role in warning left and right, and warning two characters in the drawings show the functions of the magnetic type positioning seat.
According to specific needs, one or more of the lightning detection sensor 6, the human body pyroelectric sensor 4, the movable metal detector 5, the air quality sensor 8, the full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system 7, the servo holder network camera 10 and the strong light lamp 1 can be selected, and other types of sensors can be arranged according to actual needs.
The sensor mounting plate is provided with a sensor main control board 32 which is connected with the lightning detection sensor 6, the human body pyroelectric sensor 4, the movable metal detector 5, the air quality sensor 8, the full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system 7, the servo cradle head network camera 10 and the highlight lamp 1, the sensor main control board 32 receives data signals monitored by all the photoelectric sensors and transmits the data signals to a vehicle-mounted monitoring platform main computer in a motor vehicle in a 5G network wireless signal mode, and control signals transmitted by the vehicle-mounted monitoring platform main computer are respectively transmitted to all the sensors to enable the sensors to be started or operated.
The technical contents of the wireless communication of the 5G network and the data processing of the host computer of the vehicle-mounted monitoring platform are mature technologies in the prior art, and are not described herein again.
The solar cell panel is connected with a battery, and the battery is connected with and supplies power to the photoelectric sensors, namely the lightning detection sensor 6, the human body pyroelectric sensor 4, the mobile metal detector 5, the air quality sensor 8, the full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system 7, the servo cradle head network camera 10 and the highlight lamp 1, and is also connected with and supplies power to the sensor main control panel 32.
The specific technical content of supplying power to the battery through the photovoltaic power generation material of the solar cell panel belongs to the mature technology in the prior art, and is not repeated again.
The embodiments in the present description are described in a progressive manner, each embodiment focuses on differences from other embodiments, and the same and similar parts among the embodiments are referred to each other. The previous description of the disclosed embodiments is provided to enable any person skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the generic principles defined herein may be applied to other embodiments without departing from the spirit or scope of the invention. Thus, the present invention is not intended to be limited to the embodiments shown herein but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.
Claims (10)
1. Green photoelectric sensing system of integrated application of on-vehicle three-dimensional surveillance aircraft of suspension type, its characterized in that:
the six-axis solar monitoring aircraft is provided with six propeller supports, and the end parts of the propeller supports are propellers driven by motors;
an aircraft main control board is installed in the six-axis solar monitoring aircraft, and the aircraft main control board is connected with a vehicle-mounted monitoring platform main computer system in a motor vehicle in a 5G wireless communication mode;
the magnetic type positioning seat is mounted at the bottom of a shell of the six-axis solar monitoring aircraft, a main body of the magnetic type positioning seat is a positioning magnetic steel sheet, and the lower surface of the positioning magnetic steel sheet is upwards recessed into a plurality of positioning pits;
the magnetic suction type positioning disc is arranged on the rear wall and the top of the tail of the motor vehicle respectively, the main body of the magnetic suction type positioning disc is a positioning magnetic steel sheet, and a plurality of positioning columns extend upwards from the upper surface of the positioning magnetic steel sheet;
the positioning magnetic steel sheet of the magnetic type positioning disc is connected with a vehicle-mounted monitoring platform host computer in the motor vehicle;
the sensor mounting plate is mounted on a shell of the six-axis solar monitoring aircraft, and the photoelectric sensor is mounted on the sensor mounting plate;
a sensor main control board is installed on the sensor installation board and connected with the photoelectric sensor, and the sensor main control board is connected with a vehicle-mounted monitoring platform host computer in the motor vehicle in a 5G network wireless signal mode;
the upper surface of the six-axis solar monitoring aircraft is provided with a solar cell panel, the solar cell panel is connected with a battery, and the battery drives and supplies power to a motor of the propeller, an aircraft main control board, a photoelectric sensor and a sensor main control board;
in the parking state:
the six-axis solar monitoring aircraft is matched with the magnetic type positioning disc on the rear wall of the tail of the motor vehicle and is fixedly hung on the rear wall of the tail of the motor vehicle, the magnetic type positioning disc on the rear wall of the tail of the motor vehicle and the six-axis solar monitoring aircraft are covered by a green protective cover, the green protective cover is made of cylindrical waterproof rubber cloth, flexible solar photovoltaic power generation materials are arranged on the protective cover and are connected with the aircraft through plugs,
or the six-axis solar monitoring aircraft is fixed on the top of the motor vehicle by matching with the magnetic-type positioning disc on the top of the motor vehicle,
when the six-axis solar monitoring aircraft is matched with the magnetic type positioning disc, the positioning column of the magnetic type positioning disc is inserted into the positioning pit of the magnetic type positioning seat, the positioning magnetic steel sheet of the magnetic type positioning disc is electrified to generate magnetic force, and the positioning magnetic steel sheet of the magnetic type positioning disc and the positioning magnetic steel sheet of the magnetic type positioning seat are attracted;
when in a flying state:
the magnetic steel sheet of the magnetic type positioning disc is powered off, and the six-axis solar monitoring aircraft flies away.
2. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein:
the photoelectric sensor is integrated and applied to one or more of a lightning detection sensor, a human body pyroelectric sensor, a mobile metal detector, an air quality sensor, a full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system, a servo holder network camera, a highlight lamp and a high-power loudspeaker.
3. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein:
the cross section of the shell of the six-axis solar monitoring aircraft is oval.
4. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein:
a shielding magnetic field copper sheet is arranged between the upper surface of the positioning magnetic steel sheet of the magnetic type positioning seat and the six-axis solar monitoring aircraft, and a rubber pad is arranged on the lower surface of the positioning magnetic steel sheet of the magnetic type positioning seat; be equipped with shielding magnetic field copper sheet between the location magnetic steel sheet lower surface of formula positioning disk and the motor vehicle is inhaled to magnetism, the last surface mounting who inhales the location magnetic steel sheet of formula positioning disk has the screw hole that is used for fixing that runs through.
5. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein:
the cross sections of the positioning pits and the positioning columns are elliptical.
6. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein:
when the six-axis solar monitoring aircraft is matched with the magnetic type positioning disc on the rear wall of the tail of the motor vehicle and is fixedly hung on the rear wall of the tail of the motor vehicle, a stainless steel bolt installed on the rear wall of the motor vehicle penetrates through a jack on the shell of the six-axis solar monitoring aircraft and is locked.
7. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein:
the sensor mounting plate is arranged on a shell of the six-axis solar monitoring aircraft to form a closed space with heat dissipation holes; and a signal processor protection device for protecting the sensor signal processor is arranged above the closed space, and the protection device is fixedly connected with the shell.
8. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein:
and a buffer gasket is arranged between the sensor mounting plate and the shell of the six-axis solar aircraft.
9. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 2, wherein:
the photoelectric sensor is arranged on the sensor mounting plate, the upper part of the upper surface of the photoelectric sensor is provided with a lightning detection sensor, the middle part of the photoelectric sensor is provided with an air quality monitoring sensor, the right rear part of the photoelectric sensor is provided with a servo pan-tilt network camera with adjustable high multiple and high resolution, the left rear part of the photoelectric sensor is provided with a human body heat release electric sensor, the right front part of the photoelectric sensor is provided with a mobile metal detector, the left front part of the photoelectric sensor is provided with a full-automatic AI non-contact infrared temperature measurement thermal imaging monitoring system; the middle part of the magnetic type positioning seat below the highlight lamp is provided with a light through hole.
10. The overhead vehicular stereo surveillance aircraft integrated green photosensor system of claim 1, wherein: the rotary wing and the bracket of the aircraft can be folded for use.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021179849.7U CN212556781U (en) | 2020-06-23 | 2020-06-23 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202021179849.7U CN212556781U (en) | 2020-06-23 | 2020-06-23 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft |
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| Publication Number | Publication Date |
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| CN212556781U true CN212556781U (en) | 2021-02-19 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202021179849.7U Withdrawn - After Issue CN212556781U (en) | 2020-06-23 | 2020-06-23 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111806685A (en) * | 2020-06-23 | 2020-10-23 | 亚投中财(北京)科技开发有限公司 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft |
-
2020
- 2020-06-23 CN CN202021179849.7U patent/CN212556781U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111806685A (en) * | 2020-06-23 | 2020-10-23 | 亚投中财(北京)科技开发有限公司 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted three-dimensional monitoring aircraft |
| CN111806685B (en) * | 2020-06-23 | 2024-07-23 | 亚投中财(北京)科技开发有限公司 | Green photoelectric sensing system for integrated application of suspension type vehicle-mounted stereoscopic monitoring aircraft |
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