CN111756983A - Three-dimensional space mobile monitoring equipment - Google Patents
Three-dimensional space mobile monitoring equipment Download PDFInfo
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- CN111756983A CN111756983A CN202010744083.0A CN202010744083A CN111756983A CN 111756983 A CN111756983 A CN 111756983A CN 202010744083 A CN202010744083 A CN 202010744083A CN 111756983 A CN111756983 A CN 111756983A
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- 238000012544 monitoring process Methods 0.000 title claims abstract description 193
- 238000012806 monitoring device Methods 0.000 claims abstract description 37
- 238000004891 communication Methods 0.000 claims description 25
- 230000007246 mechanism Effects 0.000 claims description 9
- 230000006870 function Effects 0.000 claims description 7
- 238000000889 atomisation Methods 0.000 claims description 4
- 230000000694 effects Effects 0.000 claims description 4
- 230000007613 environmental effect Effects 0.000 claims description 4
- 238000012545 processing Methods 0.000 claims description 4
- 239000007787 solid Substances 0.000 claims description 2
- 238000000034 method Methods 0.000 abstract description 11
- 230000008569 process Effects 0.000 abstract description 8
- 238000010586 diagram Methods 0.000 description 11
- 230000008447 perception Effects 0.000 description 8
- 238000013461 design Methods 0.000 description 3
- 238000010276 construction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000001788 irregular Effects 0.000 description 1
- 238000010030 laminating Methods 0.000 description 1
- 230000000149 penetrating effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- 230000000087 stabilizing effect Effects 0.000 description 1
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/30—Parts of fuselage relatively movable to reduce overall dimensions of aircraft
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
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- 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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N23/00—Cameras or camera modules comprising electronic image sensors; Control thereof
- H04N23/50—Constructional details
- H04N23/51—Housings
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- 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
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Studio Devices (AREA)
Abstract
The invention relates to a three-dimensional space mobile monitoring device, which comprises a mobile monitoring device and a monitoring fixed base, wherein the monitoring device is movably arranged on the fixed base, and the three-dimensional space mobile monitoring device comprises: the monitoring equipment comprises a monitoring shell, a foldable support arm positioned on the monitoring shell, a support arm folding structure, a flight power module, a detachable monitoring video system, an air outlet, an equipment cabin, a battery cabin and a locking and charging interface; the fixed base comprises a fixed structure, a monitoring base, a rotating shaft and a locking structure, wherein the rotating shaft and the locking structure are connected between the fixed structure and the monitoring base. The invention adopts the arrangement mode of mutually combining the monitoring equipment and the fixed base, realizes movable and fixed monitoring in a specific area, has high automation degree, does not occupy larger space in the using process, and has stronger practicability and functionality, thereby being widely applied to the technical field of the monitoring equipment.
Description
Technical Field
The invention relates to the technical field of monitoring equipment, in particular to a three-dimensional space mobile monitoring device.
Background
Monitoring cameras are often used as devices for inputting and acquiring information through videos, and are widely applied to the fields of security monitoring, traffic and the like in cities and among cities in the past. The installation site also covers various infrastructure such as streets, cells, hospitals, banks, public buildings, construction sites, intercity highways, transportation hubs and the like. In recent years, with the development of social urbanization, high-rise buildings in cities are gradually increased, and the traditional urban street camera often covers the ground area and is difficult to acquire complete urban monitoring information such as the high-rise buildings, roofs and the like; on the other hand, under the trend of the internet of things and smart cities, more information such as urban environments, facilities and traffic needs to be acquired, and the future needs cannot be met only by a video data acquisition mode.
Chinese patent CN106915461A, "aircraft", provides an aircraft design scheme that can recover the arms and the legs when not in use, further save the space occupied by the aircraft, and facilitate the storage of the aircraft. The Chinese patent CN109515731A discloses vehicle-mounted automatic airport landing equipment of an unmanned aerial vehicle and a control method thereof, in particular to the vehicle-mounted automatic airport landing equipment of the unmanned aerial vehicle, which comprises a GPS positioning system, a horizontally arranged lifting platform, a centering module, a clamping module, an active stabilizing module, a supporting platform, a fixed bottom plate, a battery replacing module, a shell and a landing beacon; the control method comprises the steps of position identification, position keeping, road condition judgment, active stabilization, accurate synchronization, landing, centering and fixing. CN102710892A Mobile monitoring System, CN107087139A Mobile monitoring device, CN208707815U Mobile monitoring terminal, and CN107067489A Mobile monitoring System, wherein the camera device or video monitoring System is arranged on a mobile platform or a robot running on the ground, so that the monitoring System can move flexibly on the ground or in a room.
Under the trend in wisdom city, unmanned aerial vehicle plays more and more effect in fields such as city security protection, city inspection as miniaturized portable supervisory equipment. However, the unmanned aerial vehicle in the prior art has the following problems: firstly, the unmanned aerial vehicle is often required to be manually carried to the position near an operation place, and then data are acquired through the control of personnel; secondly, the battery replacement, charging and other parts of the unmanned aerial vehicle need to be manually assisted; thirdly, there is huge appearance difference in conventional unmanned aerial vehicle appearance and current control, occupies great space, size also is not pleasing to the eye.
In order to solve these problems, the prior art provides an automatic airport system for unmanned aerial vehicles, in which an unmanned aerial vehicle can automatically take off and land at the airport, and a charging system for automatically replacing batteries and replacing the batteries is provided in the airport, so that the remote mobile monitoring becomes more convenient. On the one hand, however, such airports often have aircraft completely enclosed therein, which is of a large external size; meanwhile, more complex mechanical structures such as cabin doors and unmanned aerial vehicle lifting structures are arranged, so that the weight of the system is very large, and the set of automatic airport is usually hundreds of kilograms. Thus, such airport deployments are extremely inflexible. In addition, the other solution is to adopt a mobile monitoring device design scheme, and design the monitoring on a platform such as a movable trolley, so that the monitoring can be moved on the ground, the flexibility of a monitoring area is increased, however, the problem of monitoring and checking a high-rise area is still solved, and the capability of collecting city data of different positions in space is not provided.
Disclosure of Invention
In order to solve the technical problems, the technical scheme provided by the invention is as follows:
the utility model provides a cubical space removes supervisory equipment, includes portable supervisory equipment and control unable adjustment base, the supervisory equipment activity sets up on unable adjustment base, wherein:
the monitoring equipment comprises a monitoring shell, a multi-color LED lamp, a foldable support arm positioned on the monitoring shell, a support arm folding mechanism, a flight power module, a detachable monitoring video system, an air outlet, an equipment cabin, a battery cabin and a locking and charging interface, wherein the flight power module is used for providing power for the monitoring equipment for flight, and the locking and charging interface is used for locking the monitoring equipment and the fixed base mutually and charging;
the fixed base comprises a fixed structure, a monitoring base, and a rotating shaft and a locking structure which are connected between the fixed structure and the monitoring base, wherein the fixed structure is used for installing the monitoring base on a surface to be installed; the monitoring base is used for clamping the monitoring equipment.
Further, the monitoring shell is set to be one of an ellipsoid shape, a cylinder shape or a round corner cuboid shape; the support arm is rotatably connected to the monitoring shell through a rotating shaft and is driven to expand or retract, and the mounting surface of a support arm motor changes by not less than 90 degrees in the two states of expansion and retraction of the support arm;
the flight power module is positioned on the support arm and comprises an electronic speed regulator, an LED indicator light, a contra-level reset type brushless motor, a propeller and a blade fixing structure, wherein the brushless motor and the propeller are arranged on the inner side of the support arm, the LED indicator light is arranged at one end of the support arm far away from the rotating shaft, and the blade fixing structure is used for fixedly connecting the propeller with a rotor of the brushless motor; the stator and the rotor of the brushless motor are provided with a reset magnetic pole mechanism, so that when the brushless motor stops being electrified, the rotor is positioned at two alignment positions of 0 degree or 180 degrees, and the propeller and the support arm are kept horizontal;
the reset magnetic pole structure comprises at least 1 fan-shaped stator magnetic pole and at least 1 fan-shaped rotor magnetic pole, wherein the included angle between the two ends of the stator magnetic pole or the two ends of the rotor magnetic pole and the circle center of the fan shape is not less than 90 degrees, and the stator magnetic pole and the rotor magnetic pole are homopolar or heteropolar;
the support arms are arranged in four, are circumferentially arranged at the outer position of the monitoring shell at equal intervals, and are arranged at one end, far away from the monitoring video system, of the rotating shaft.
Further, the support arm folding mechanism comprises a worm direct current motor and a motor control module, the worm direct current motor is used for driving forward and reverse constant-speed rotation, the motor control module is used for feeding back electric control, and when the support arm is unfolded to the limit position, the motor control module automatically stops controlling the rotation of the worm direct current motor; when the motor control module is given a signal to drive the worm direct current motor again, the motor control module controls the worm direct current motor to rotate reversely.
Furthermore, a mobile control system, a power supply and interface management module, a risk sensing and calculating module, a communication antenna and an environmental sensor module are arranged in the equipment cabin; a replaceable power battery is arranged in the battery compartment; the monitoring video system comprises an image acquisition system and a holder system, wherein the image acquisition system comprises a lens, a sensor and an image processing module; the holder system is not less than two-axis control and has two axial controls of pitching and course; and an internet of things communication module and a gain antenna are also arranged in the equipment cabin.
Furthermore, the equipment cabin and the battery cabin are both located inside the monitoring shell, the monitoring video system is located on the lower portion of the monitoring shell, and the monitoring video system is externally coated with a detachable transparent shell.
Furthermore, the risk perception and calculation module comprises a risk perception module and a calculation module, the risk perception module is exposed outside the monitoring shell, the number of the risk perception modules is not less than 1, and the risk in not less than 1 direction is monitored; the charging interface structure is located on the outer side wall surface of the monitoring shell.
Further, the control base is including the casing that is used for joint supervisory equipment and locate control guide structure, control laminating structure, communication equipment cabin, the only code identification area on the casing, wherein:
the shell comprises a base and fan-shaped baffles which are circumferentially arranged on the base at intervals, when the monitoring shell is clamped on the monitoring base, the inner sides of the baffles are attached to the outer wall surface of the bottom of the monitoring shell, and the outer sides of the baffles are attached to the outer wall surface of the shell;
the monitoring guide structures are arranged on the upper part of the baffle and are mutually meshed with the lower part of the monitoring equipment, the monitoring guide structures are in a wave shape or a gear shape distributed in a sine function and have guiding functions in two directions of direction and vertical direction, and at least 3 monitoring guide structures are arranged;
the communication equipment cabin is arranged in the baffle and comprises a detachable equipment cabin door, and an Internet of things communication module is arranged in the communication equipment cabin and is used for communicating with the mobile equipment, the nearby Internet connection equipment and the Internet server; an anti-atomization module is further arranged in the communication equipment cabin, and comprises an anti-atomization air outlet arranged at the lower end of the monitoring base;
and an infrared LED lamp array and a polygonal color block are arranged in the unique code identification area.
Furthermore, the rotating shaft and the locking structure comprise a cantilever connected between the fixed structure and the monitoring base, the cantilever is movably connected with the fixed structure, and the cantilever is fixedly connected with the monitoring base; a charging equipment cabin is arranged in the cantilever, a charging control module, a first sensor module and a first locking and charging structure are arranged in the charging equipment cabin, and the first sensor module comprises a temperature and humidity sensor;
the first locking and charging structure is driven by a steering engine or a worm direct current motor, so that the locking structure and a charging interface structure of the monitoring shell form locking and unlocking through radial movement or circumferential movement along a rotating shaft.
Furthermore, the lower part of the fixed structure is provided with a mounting hole, a power supply and a network interface; the fixing structure is in a plane plate shape or a bayonet shape and is used for meeting the requirement of installing a solid body in a plane or a column shape.
Furthermore, the cantilever is of a hollow rod-shaped structure, and the section of the cantilever is of a round-corner rectangle or an oval shape; one end of the cantilever is connected to the fixing structure through the locking piece, and the other end of the cantilever is integrally connected with the monitoring base.
After adopting the structure, the invention has the following advantages:
the invention adopts the arrangement mode of mutually combining the monitoring equipment and the fixed base, realizes the movable type and fixed type monitoring in a specific area, has high automation degree, does not occupy larger space in the using process, and has stronger practicability and functionality.
Drawings
FIG. 1 is a schematic structural diagram of an embodiment of the present invention;
FIG. 2 is a structural diagram of an embodiment of the present invention in a flying state;
FIG. 3 is a diagram of a monitoring base connection configuration according to an embodiment of the present invention;
FIG. 4 is a diagram of an expanded state of a monitoring housing of an embodiment of the present invention when the monitoring housing is spherical;
FIG. 5 is a first state diagram of a monitoring enclosure according to an embodiment of the present invention;
FIG. 6 is a first view of a monitor housing connection configuration according to an embodiment of the present invention;
FIG. 7 is a second block diagram of a monitoring housing in accordance with an embodiment of the present invention;
FIG. 8 is a second view of a connection configuration of a monitoring housing according to an embodiment of the present invention;
FIG. 9 is a block diagram of a third embodiment of a monitoring housing of the present invention;
FIG. 10 is a block diagram of a monitoring enclosure according to an embodiment of the present invention;
FIG. 11 is a fifth block diagram of a monitoring housing in accordance with an embodiment of the present invention;
FIG. 12 is a block diagram of a monitoring housing of an embodiment of the present invention;
FIG. 13 is a third view of the connection structure of the monitoring housing according to the embodiment of the present invention;
FIG. 14 is a fourth view of the connection configuration of the monitoring housing of the embodiment of the present invention;
FIG. 15 is a bottom view of the coupling structure of the monitor housing according to the embodiment of the present invention;
fig. 16 is a partial structural schematic diagram of an embodiment of the present invention.
Detailed Description
The present invention will be described in further detail with reference to the accompanying drawings.
With reference to fig. 1-16, a three-dimensional space mobile monitoring device includes a mobile monitoring device 1 and a monitoring fixed base 2, the monitoring device 1 is movably disposed on the fixed base 2, wherein:
the monitoring device 1 comprises a monitoring shell 3, a multi-color LED lamp, a foldable support arm 4 positioned on the monitoring shell 3, a support arm folding structure, a flight power module 5, a detachable monitoring video system 6, an air outlet 61, a device cabin 7, a battery cabin 8 and a locking and charging interface 9, wherein the flight power module 5 is used for providing flight power for the monitoring device 1, and the locking and charging interface 9 is used for locking the monitoring device 1 and the fixed base 2 with each other and charging;
the fixed base 2 comprises a fixed structure 10, a monitoring base 11 and a rotating shaft and locking structure 12 connected between the fixed structure 10 and the monitoring base 11, wherein the fixed structure 10 is used for installing the fixed base 2 on a surface to be installed, and the rotating shaft and locking structure 12 is used for adjusting an included angle between the fixed base 2 and the surface to be installed and realizing mutual locking with the fixed structure 10 after adjustment; the monitoring base 11 is used for clamping the monitoring device 1.
The invention is optimized in appearance and structure, and has two modes, namely a conventional monitoring mode and a mobile monitoring mode, when in work, the invention comprises the following steps: the monitoring device 1 is arranged on the fixed base 2 for monitoring, the monitoring device 1 and the fixed base 2 are in a locking state, and the support arm 4 and the support arm folding structure of the monitoring device 1 are folded inwards and accommodated at the same time, so that the sealing performance of the power assembly in a conventional state can be ensured, the dustproof and waterproof effects are achieved, the appearance is similar to that of conventional monitoring, and the monitoring function in different directions when the monitoring device 1 is in a fixed position can be realized; in mobile monitoring mode: at the moment, the fixed base 2 is unlocked from the monitoring device 1, the support arm 4 on the monitoring device 1 is opened outwards to the limit position, the flight power module 5 is arranged in an external space, the flight power module 5 on the monitoring device 1 can be started to operate, so that the monitoring device 1 is enabled to vertically and upwards leave the fixed base 2, the three-dimensional space automatically moves according to a set mode or a task, and when the task is executed or a return voltage is reached, the monitoring device 1 can automatically return to the position above the fixed base 2 and finally descends to the fixed base 2, and is locked and enters a conventional monitoring mode again. The invention of the device can solve the limitation of arranging conventional fixed cameras inside and outside cities on monitoring areas, so that the monitoring has wider three-dimensional monitoring coverage range and meets more outdoor monitoring scenes.
The monitoring shell 3 is set to be one of an ellipsoid shape, a cylinder shape or a round corner cuboid shape; the support arm 4 is rotatably connected to the monitoring shell 3 through a rotating shaft and is driven to be unfolded or retracted;
the flight power module 5 is positioned on the support arm 4 and comprises an electronic speed regulator, an LED indicator light, a contra-level reset type brushless motor, a propeller 51 and a blade fixing structure, wherein the brushless motor and the propeller 51 are arranged on the inner side of the support arm 4, the LED indicator light is arranged at one end of the support arm 4 far away from the rotating shaft, and the blade fixing structure is used for fixedly connecting the propeller 51 with a rotor of the brushless motor; a reset magnetic pole mechanism is arranged between a stator and a rotor of the brushless motor, so that when the brushless motor stops being electrified, the rotor can be positioned at two alignment positions of 0 degree or 180 degrees, and the support arm 4 is kept horizontal;
the reset magnetic pole structure comprises at least 1 fan-shaped stator magnetic pole and at least 1 fan-shaped rotor magnetic pole, wherein the included angle between the two ends of the stator magnetic pole or the two ends of the rotor magnetic pole and the circle center of the fan shape is not less than 90 degrees, and the stator magnetic pole and the rotor magnetic pole are homopolar or heteropolar;
the number of the support arms 4 is four, the support arms are circumferentially arranged at the outer position of the monitoring shell 3 at equal intervals, and the rotating shaft is arranged at one end far away from the monitoring video system 6.
In order to realize that support arm 4 can realize its 0 degrees and the motion of two extreme position of 180 degrees relatively monitoring shell 3, set up flight power module 5, wherein, to the level reset formula brushless motor adopt among the prior art through the modified motor can, specifically do: in the existing motor, the stator and the rotor are fixed by bonding and other fixing modes, and the fixation is realized by utilizing the characteristics of like-pole repulsion and opposite-pole attraction between magnets. For the rotation of the support arm 4 at two extreme positions by using the rotating shaft, the rotation of the support arm 4 can be realized by a motor and a gear which are connected through a shaft, specifically, the motor is connected with the gear through an output shaft of the motor, and the gear is connected with the support arm 4, so that the support arm 4 is driven to expand or contract in the rotation process of the gear. The blade fixing structure can adopt a coupler to realize the connection between the brushless motor and the propeller 51, and ensure that the propeller 51 rotates under the driving of the brushless motor.
When the invention is used for monitoring in a conventional form, the monitoring equipment 1 is locked on the fixed base 2 at the moment, and a specific area is monitored directly through the monitoring video system 6 on the monitoring equipment 1; when monitoring is carried out on three-dimensional space positions in different areas, the monitoring equipment 1 is unlocked from the fixed base 2 at the moment, the battery compartment 8 is electrically connected with the flight power module 5 and supplies power to the flight power module, the support arm 4 is opened from the monitoring shell 3, and at the moment, the brushless motor drives the propeller 51 to move, so that the monitoring equipment 1 starts to move and carries out monitoring processes of different areas in the three-dimensional space; when the monitoring device 1 completes the monitoring task and returns, the propeller 51 is driven by the blade fixing mechanism to retract, and finally moves to the monitoring housing 3 and is accommodated on the outer wall surface of the monitoring housing 3. Wherein a notch is provided in the monitoring housing 3 for receiving the arm 3, and when the arm 3 is retracted into the notch, the monitoring device 1 returns to an ellipsoidal, cylindrical or rectangular state and other regular or irregular geometric shapes.
The support arm folding mechanism comprises a worm direct current motor and a motor control module, the worm direct current motor is used for driving forward and reverse constant-speed rotation, the motor control module is used for feeding back electric control, and when the support arm 4 is unfolded to be in a horizontal state, the motor control module automatically stops controlling the rotation of the worm direct current motor; when the motor control module is given a signal to drive the worm direct current motor again, the motor control module controls the worm direct current motor to rotate reversely. The worm direct current motor drives a gear connected with the worm direct current motor through a shaft, and the gear drives the support arm 4 through a rotating shaft, so that the support arm 4 is unfolded or retracted.
In the process of realizing the unfolding or the storage of the support arm 4, the driving device is a motor control module and a worm direct current motor which are connected by electric signals, and when the worm direct current motor rotates forwards, the support arm 4 is driven to unfold and finally unfold to the limit position, and then the motor control module stops controlling the worm direct current motor to rotate forwards; then, when the support arm 4 is required to be retracted, the motor control module can control the worm direct current motor to rotate reversely through an electric signal, so that the support arm 4 is driven to be retracted and finally accommodated on the monitoring shell 3. A mobile control system, a power supply and interface management module, a risk sensing and calculating module 91, a communication module, a communication antenna and an environmental sensor module are arranged in the equipment cabin 7; a replaceable power battery is arranged in the battery cabin 8; the monitoring video system 6 comprises an image acquisition system and a holder system, wherein the image acquisition system comprises a lens, a sensor and an image processing module; the holder system is not less than two-axis control and has two axial controls of pitching and course; an internet of things communication module and a gain antenna are further arranged in the equipment cabin 7.
In order to achieve the purpose of supplying power to the equipment cabin 7 and the monitoring video system 6, the equipment cabin 7 and the monitoring video system are electrically connected with a power battery in a battery cabin 8, and the power battery and the monitoring video system can be connected in parallel; then, in the equipment compartment 7, a power supply and interface management module, a risk sensing and calculating module 91, a communication module and a communication antenna, and an environmental sensor module are respectively connected in parallel with the mobile control system; in the monitoring video system 6, an image acquisition system is in signal connection with a holder system, and a lens, a sensor and an image processing module in the image acquisition system are electrically connected. In addition, in the specific working process of the equipment cabin 7 and the battery cabin 8, signal connection between the equipment cabin and the battery cabin is realized through the internet of things communication module and the gain antenna.
The equipment cabin 7 and the battery cabin 8 are both positioned inside the monitoring shell 3, and the monitoring video system 6 is positioned at the lower part of the monitoring shell 3; the number of the support arms 4 is four, the support arms are circumferentially arranged at the outer position of the monitoring shell 3 at intervals, and the support arms 4 are arranged at one end far away from the monitoring video system 6; the monitoring video system is externally covered with a detachable transparent shell.
In order to ensure that the monitoring shell 3 is stressed in a balanced manner in the flying process, an even number of pairs of support arms 4 are arranged, and in order to ensure that the support arms 4 can be flexibly unfolded or retracted, the support arms 4 and the monitoring shell 3 are arranged in a rotatable connection mode, specifically, can be connected through a rotating shaft; then, the arm 4 is provided in an arc-shaped configuration, and after connecting one end thereof to the monitor housing 3, the propeller 51 is provided at the other end of the arm 4. When the monitoring device 1 is in flight, it can sense the external environment through the risk sensing and calculating module 91 located outside it, and send a signal to the mobile control system. Inside the monitoring housing 3, the equipment compartment 7 is located at an upper position of the battery compartment 8; the video monitoring system 6 is located at the bottom position of the monitoring shell 3 and is used for collecting video signals. The mobile control system can specifically adopt a single chip microcomputer to realize the electrical signal connection between signals and each component.
The risk perception and calculation module 91 includes a risk perception module and a calculation module, the risk perception module is exposed outside the monitoring shell 3, wherein the risk perception module is not less than 1 group, and the risk of not less than 1 direction is monitored.
The monitoring base 11 includes a housing 13 for clamping the monitoring device 1, and a monitoring guide structure 14, a monitoring attaching structure 15, a communication device cabin 17 and a unique coding identification area which are arranged on the housing 13, wherein:
the shell 13 comprises a base 131 and fan-shaped baffles 132 circumferentially and at intervals arranged on the base 131, when the monitoring shell 3 is clamped on the monitoring base 11, the inner side of the baffle 132 is attached to the outer wall surface of the bottom of the monitoring shell 3, and the outer side of the baffle 132 is attached to the outer wall surface of the monitoring shell 3;
the monitoring guide structures 14 are arranged on the upper part of the baffle 132 and are mutually meshed with the lower part of the monitoring device 1, the monitoring guide structures 14 are in a wave shape or a gear shape distributed in a sine function, have guiding functions in two directions of direction and vertical, and are at least 3;
the communication equipment cabin 17 is arranged inside the baffle 132 and comprises a detachable equipment cabin door, and an internet of things communication module is arranged in the communication equipment cabin 17 and is used for communicating with the mobile equipment, the nearby internet connection equipment and the internet server; still be equipped with in the communication equipment cabin 17 and prevent atomizing module, prevent atomizing module including locating the antifog air outlet 61 of control base 11 lower extreme.
An infrared LED lamp array and a polygonal color block are arranged in the unique code identification area, and the locking and charging interface 9 is positioned on the outer side wall surface of the monitoring shell 3.
The upper end of the baffle 132 is also provided with a first LED lamp 133.
In the monitoring base 11, the base 131 and the baffle 132 together form a side closed space, which is used for returning and falling into the closed space after the monitoring device 1 performs the monitoring task, so as to lock the monitoring device 1 and the fixed base 2, specifically, the inner side of the baffle 132 is provided with a locking and charging structure 9, which is used for locking and charging. In the present invention, the distance between each two baffles 132 is equal to the width of the arm 4, so that when the monitoring device 1 returns and falls onto the housing 13, the monitoring housing 3 and the housing 13 are just clamped to each other.
The rotating shaft and locking structure 12 comprises a cantilever 18 connected between the fixed structure 10 and the monitoring base 11, wherein the cantilever 18 is movably connected with the fixed structure 10, and the cantilever 18 is fixedly connected with the monitoring base 11; a charging equipment cabin 20 is arranged on the cantilever 18, a charging control module, a first sensor module and a first locking and charging structure are arranged in the charging equipment cabin 20, and the first sensor module comprises a temperature and humidity sensor;
the first locking and charging structure is driven by a steering engine or a worm direct current motor, so that the locking structure and the charging interface structure of the monitoring shell 3 form locking and unlocking through radial movement or axial movement along a rotating shaft, and the first locking and charging structure can be of a columnar structure.
A gear guide groove 201, and a motor and a gear 202 which are positioned in the gear guide groove 201 and are coupled to each other are also provided in the charging equipment compartment 20.
In the process of fixedly connecting the cantilever 18 with the fixed structure 10 and the monitoring base 11 respectively, the cantilever can be connected with the fixed structure 11 through a movable rotating shaft or connected with a hinge element, so that the aim of movable connection is fulfilled; the cantilever 18 and the monitoring base 11 can be fixedly connected by plugging.
The lower portion of the fixing structure 10 is further provided with a mounting hole 101 and a power supply and network cable interface 102, and the fixing structure 10 is formed in a plate shape.
The cantilever 18 is a hollow rod-shaped structure, and the section of the cantilever is a round-corner rectangle or an ellipse; one end of the cantilever is connected to the fixed structure 10 through a locking piece or a movable rotating shaft, and the other end of the cantilever is integrally connected with the monitoring base 11.
The fixing structure 10 is provided with a plurality of mounting holes 101 for mounting the device on a to-be-mounted surface (a roof, a vertical mounting surface of a rod body, a wall surface and the like), specifically, a mode of penetrating the mounting holes 101 and the to-be-mounted surface through screws. The power supply interface 102 is an external power-taking 220V interface. In the present device, one end of the cantilever 18 is movably connected to the fixed structure 10, when the user installs the device, the angle between the monitoring base 11 and the vertical plane can be adjusted by 180 degrees until the angle is satisfied, and then the cantilever 18 is locked by the locking structure, which can be a locking member 181 connected between the fixed structure 10 and the cantilever 18.
In the invention, by arranging the movable connection between the monitoring equipment 1 and the fixed base 2, the movable monitoring of a specific space and three-dimensional spaces at different positions is realized, and the functionality is strong. The method specifically comprises the following steps: when monitoring in a specific space, the monitoring equipment 1 is fixed on the fixed base 2, and the video monitoring system 6 collects images and processes the images to achieve the purpose of monitoring; when a specific task is executed to carry out mobile monitoring, the monitoring device 1 is separated from the fixed base 2, the monitoring device 1 flies under the driving of the flying power module 5, and monitoring shooting on a task route is carried out according to a set route.
Claims (10)
1. The utility model provides a cubical space removes supervisory equipment, its characterized in that, includes portable supervisory equipment and control unable adjustment base, the supervisory equipment activity sets up on unable adjustment base, wherein:
the monitoring equipment comprises a monitoring shell, a multi-color LED lamp, a foldable support arm positioned on the monitoring shell, a support arm folding mechanism, a flight power module, a detachable monitoring video system, an air outlet, an equipment cabin, a battery cabin and a locking and charging interface, wherein the flight power module is used for providing power for the monitoring equipment for flight, and the locking and charging interface is used for locking the monitoring equipment and the fixed base mutually and charging;
the fixed base comprises a fixed structure, a monitoring base, and a rotating shaft and a locking structure which are connected between the fixed structure and the monitoring base, wherein the fixed structure is used for installing the monitoring base on a surface to be installed; the monitoring base is used for clamping the monitoring equipment.
2. The device according to claim 1, wherein the monitoring housing is one of an ellipsoid shape, a cylinder shape or a rounded rectangle shape; the support arm is rotatably connected to the monitoring shell through a rotating shaft and is driven to expand or retract, and the mounting surface of a support arm motor changes by not less than 90 degrees in the two states of expansion and retraction of the support arm;
the flight power module is positioned on the support arm and comprises an electronic speed regulator, an LED indicator light, a contra-level reset type brushless motor, a propeller and a blade fixing structure, wherein the brushless motor and the propeller are arranged on the inner side of the support arm, the LED indicator light is arranged at one end of the support arm far away from the rotating shaft, and the blade fixing structure is used for fixedly connecting the propeller with a rotor of the brushless motor; the stator and the rotor of the brushless motor are provided with a reset magnetic pole mechanism, so that when the brushless motor stops being electrified, the rotor is positioned at two alignment positions of 0 degree or 180 degrees, and the propeller and the support arm are kept horizontal;
the reset magnetic pole structure comprises at least 1 fan-shaped stator magnetic pole and at least 1 fan-shaped rotor magnetic pole, wherein the included angle between the two ends of the stator magnetic pole or the two ends of the rotor magnetic pole and the circle center of the fan shape is not less than 90 degrees, and the stator magnetic pole and the rotor magnetic pole are homopolar or heteropolar;
the support arms are arranged in four, are circumferentially arranged at the outer position of the monitoring shell at equal intervals, and are arranged at one end, far away from the monitoring video system, of the rotating shaft.
3. The monitor device according to claim 1, wherein the arm folding mechanism comprises a worm dc motor and a motor control module, the worm dc motor is used for driving forward and reverse constant speed rotation, the motor control module is used for feeding back electric control, and when the arm is unfolded to the limit position, the motor control module automatically stops controlling the rotation of the worm dc motor; when the motor control module is given a signal to drive the worm direct current motor again, the motor control module controls the worm direct current motor to rotate reversely.
4. The three-dimensional space mobile monitoring device according to claim 1, wherein a mobile control system, a power supply and interface management module, a risk sensing and calculating module, a communication antenna and an environmental sensor module are arranged in the device cabin; a replaceable power battery is arranged in the battery compartment; the monitoring video system comprises an image acquisition system and a holder system, wherein the image acquisition system comprises a lens, a sensor and an image processing module; the holder system is not less than two-axis control and has two axial controls of pitching and course; and an internet of things communication module and a gain antenna are also arranged in the equipment cabin.
5. The three-dimensional space mobile monitoring device according to claim 4, wherein the device compartment and the battery compartment are both located inside the monitoring housing, the monitoring video system is located at the lower part of the monitoring housing, and the monitoring video system is externally covered by a detachable transparent housing.
6. The device according to claim 4, wherein the risk sensing and calculating module comprises a risk sensing module and a calculating module, the risk sensing module is exposed outside the monitoring housing, the risk sensing module is not less than 1 group, and the risk sensing module monitors the risk in not less than 1 direction; the charging interface structure is located on the outer side wall surface of the monitoring shell.
7. The three-dimensional space mobile monitoring device according to claim 1, wherein the monitoring base comprises a housing for clamping the monitoring device, and a monitoring guide structure, a monitoring fitting structure, a communication device cabin and a unique coding identification area which are arranged on the housing, wherein:
the shell comprises a base and fan-shaped baffles which are circumferentially arranged on the base at intervals, when the monitoring shell is clamped on the monitoring base, the inner sides of the baffles are attached to the outer wall surface of the bottom of the monitoring shell, and the outer sides of the baffles are attached to the outer wall surface of the shell;
the monitoring guide structures are arranged on the upper part of the baffle and are mutually meshed with the lower part of the monitoring equipment, the monitoring guide structures are in a wave shape or a gear shape distributed in a sine function and have guiding functions in two directions of direction and vertical direction, and at least 3 monitoring guide structures are arranged;
the communication equipment cabin is arranged in the baffle and comprises a detachable equipment cabin door, and an Internet of things communication module is arranged in the communication equipment cabin and is used for communicating with the mobile equipment, the nearby Internet connection equipment and the Internet server; an anti-atomization module is further arranged in the communication equipment cabin, and comprises an anti-atomization air outlet arranged at the lower end of the monitoring base;
and an infrared LED lamp array and a polygonal color block are arranged in the unique code identification area.
8. The device according to claim 1, wherein the rotation shaft and the locking structure comprise a cantilever connected between the fixed structure and the monitoring base, the cantilever is movably connected with the fixed structure, and the cantilever is fixedly connected with the monitoring base; a charging equipment cabin is arranged in the cantilever, a charging control module, a first sensor module and a first locking and charging structure are arranged in the charging equipment cabin, and the first sensor module comprises a temperature and humidity sensor;
the first locking and charging structure is driven by a steering engine or a worm direct current motor, so that the locking structure and a charging interface structure of the monitoring shell form locking and unlocking through radial movement or circumferential movement along a rotating shaft.
9. The device according to claim 8, wherein the lower portion of the fixing structure is provided with a mounting hole, a power supply and a network interface; the fixing structure is in a plane plate shape or a bayonet shape and is used for meeting the requirement of installing a solid body in a plane or a column shape.
10. The device according to claim 8, wherein the cantilever is a hollow rod-shaped structure with a rectangular or elliptical cross-section; one end of the cantilever is connected to the fixing structure through the locking piece, and the other end of the cantilever is integrally connected with the monitoring base.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010744083.0A CN111756983A (en) | 2020-07-29 | 2020-07-29 | Three-dimensional space mobile monitoring equipment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202010744083.0A CN111756983A (en) | 2020-07-29 | 2020-07-29 | Three-dimensional space mobile monitoring equipment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN111756983A true CN111756983A (en) | 2020-10-09 |
Family
ID=72712374
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202010744083.0A Withdrawn CN111756983A (en) | 2020-07-29 | 2020-07-29 | Three-dimensional space mobile monitoring equipment |
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| CN (1) | CN111756983A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112224411A (en) * | 2020-10-30 | 2021-01-15 | 北京特种机械研究所 | Microminiature unmanned aerial vehicle |
-
2020
- 2020-07-29 CN CN202010744083.0A patent/CN111756983A/en not_active Withdrawn
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112224411A (en) * | 2020-10-30 | 2021-01-15 | 北京特种机械研究所 | Microminiature unmanned aerial vehicle |
| CN112224411B (en) * | 2020-10-30 | 2021-10-22 | 北京特种机械研究所 | Microminiature unmanned aerial vehicle |
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Application publication date: 20201009 |