CN110243535A - A kind of pressure monitoring system and monitoring method of movable type movie theatre - Google Patents
A kind of pressure monitoring system and monitoring method of movable type movie theatre Download PDFInfo
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- CN110243535A CN110243535A CN201910619267.1A CN201910619267A CN110243535A CN 110243535 A CN110243535 A CN 110243535A CN 201910619267 A CN201910619267 A CN 201910619267A CN 110243535 A CN110243535 A CN 110243535A
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L19/00—Details of, or accessories for, apparatus for measuring steady or quasi-steady pressure of a fluent medium insofar as such details or accessories are not special to particular types of pressure gauges
- G01L19/08—Means for indicating or recording, e.g. for remote indication
- G01L19/12—Alarms or signals
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Abstract
The present invention proposes the pressure monitoring system and monitoring method of a kind of mobile movie theatre, which includes: link block, connects at least one cockpit system, at least one described cockpit system includes multiple cockpits；Induction module, for monitoring the air pressure change in the cockpit system；Collection module for collecting the fault message of the link block and induction module, and carries out Macro or mass analysis；Alarm module provides corresponding information warning based on the analysis results and records current warning message.The pressure monitoring system design of movable type movie theatre proposed by the present invention is rationally, easy to operate.
Description
Technical field
The invention belongs to movie theatre technical fields, and in particular to it is a kind of movable type movie theatre pressure monitoring system and monitoring side
Method.
Background technique
The movie theatre that circles in the air is a kind of emerging special efficacy amusement film, and spectators take the lifting seat controlled by big machinery system
In the air to movie theatre center, picture is projected huge hemisphere screen by extraordinary fish eye lens by high-definition digital projector, from
The visibility region of the spectators crown to underfooting is all surrounded by grand mute completely, in the abundant extremely powerful ball curtain of impression
While movie and television contents, can also undergo the excitement that vacantly flies by.In addition to can achieve 4D movie theatre, huge curtain vault curtain shadow
The telegraphy interactive device such as simulated flight mechanism can be also added in the effect of institute on this basis, allow spectators' body under the environment of safety
Test circle in the air, interactive recreation and other effects.
The movie theatre that circles in the air is broadly divided into screen system and cockpit system, and the safety of cockpit system is the entire movie theatre that circles in the air of design
Key, the secure system operations of the existing movie theatre that circles in the air are complex, and structure is also complex, and cost of manufacture is high.
Summary of the invention
In view of the defect of the above-mentioned prior art, the present invention proposes pressure monitoring system and the monitoring side of a kind of mobile movie theatre
Method improves the safety of mobile movie theatre, guarantees the viewing experience sense of spectators to simplify the security system of mobile movie theatre.
To achieve the above object and other purposes, the present invention propose a kind of pressure monitoring system of mobile movie theatre, comprising:
Link block connects an at least cockpit system, and an at least cockpit system includes multiple cockpits；
Induction module, connects the link block, and the air pressure that the induction module is used to monitor in the cockpit system becomes
Change；
Collection module connects the link block and induction module, and the collection module is for collecting the link block
And the fault message of induction module, and carry out Macro or mass analysis；
Alarm module, connects the collection module, and the alarm module provides corresponding warning according to the fault message
Information simultaneously records current warning message.
In one embodiment, the link block includes:
Transmitting unit, the transmitting unit are used to emit signal to an at least cockpit system；
Receiving unit connects the transmitting unit, and the transmitting unit is for receiving the signal.
In one embodiment, the induction module includes:
Sensing unit, the pressure change in cockpit system described in real-time monitoring；
Alarm unit connects the sensing unit, when the pressure change in the cockpit system is more than or less than threshold value,
The alarm unit provides alarm signal.
In one embodiment, the collection module includes:
Collector unit collects the fault message of the link block and induction module；
Diagnosis unit, connects the collector unit, and the fault message is carried out Macro or mass analysis by the diagnosis unit.
In one embodiment, the alarm module includes:
Processing unit, for handling the fault message, to obtain corresponding fault code
Alarm unit, connects the processing unit, and the alarm unit provides corresponding warning according to the fault code
Information and solution, and record current warning message.
In one embodiment, the pressure monitoring system further includes motion module, and the motion module includes:
Transmission unit, Xiang Suoshu cockpit system send instruction, and the cockpit system opens or closes master according to described instruction
Door or secondary door；
Linear motion unit controls the cockpit system and moves linearly；
Multifreedom motion unit controls the cockpit system and carries out multifreedom motion.
In one embodiment, the pressure monitoring system further includes protective module, and the protective module includes:
Monitoring unit, the working condition for protective device in cockpit system described in real-time monitoring；
Alarm unit, when the protective device is not in working condition, the alarm unit provides alarm signal.
The present invention also proposes a kind of Pressure monitoring method of mobile movie theatre, comprising:
At least cockpit system of connection, an at least cockpit system includes multiple cockpits；
Monitor the pressure change in the cockpit system；
The phylogenetic fault message of the cockpit is collected, and carries out Macro or mass analysis；
Corresponding information warning is provided according to the fault message, and records current warning message.
In one embodiment, a connection at least cockpit system, an at least cockpit system includes multiple cockpit packets
It includes:
Signal is sent to an at least cockpit system by transmitting unit；
The signal is received by receiving unit, connects an at least cockpit system.
In one embodiment, the pressure change in the monitoring cockpit system includes:
Pass through the pressure change in cockpit system described in sensing unit real-time monitoring；
Alarm signal is provided by alarm unit.
In one embodiment, described to collect the phylogenetic fault message of cockpit, and carry out Macro or mass analysis and include:
The fault message of the cockpit system is collected by collector unit；
The fault message is subjected to Macro or mass analysis by diagnosis unit.
In one embodiment, described that corresponding information warning is provided according to the fault message, and record current alarm
Information includes:
The fault message is handled, through the processing unit to form fault code；
According to the fault code, corresponding information warning and solution are provided by alarm unit, and record current
Warning message.
The present invention proposes the pressure monitoring system and monitoring method of a kind of mobile movie theatre, passes through the pressure monitoring system energy
The air pressure change for enough real-time monitoring mobile movie theatre improves the safety of mobile movie theatre, ensure that the viewing body of spectators
Sense is tested, while the pressure monitoring system of mobile movie theatre proposed by the present invention is easy to operate.
Detailed description of the invention
Fig. 1: the mobile cinema system that the present embodiment proposes.
Fig. 2: the simplified diagram of cockpit system.
Fig. 3: the pressure monitoring system connection schematic diagram for the mobile movie theatre that the present embodiment proposes.
Fig. 4: the connection schematic diagram of link block.
Fig. 5: the connection schematic diagram of motion module.
Fig. 6: the connection schematic diagram of induction module.
Fig. 7: the connection schematic diagram of protective module.
Fig. 8: the connection schematic diagram of collection module.
Fig. 9: the connection schematic diagram of alarm module.
Figure 10: the Pressure monitoring method flow schematic diagram for the mobile movie theatre that the present embodiment proposes.
Figure 11: the outline flowchart of step S1.
Figure 12: the outline flowchart of step S2.
Figure 13: the outline flowchart of step S3.
Figure 14: the outline flowchart of step S4.
Figure 15: the outline flowchart of step S5.
Figure 16: the outline flowchart of step S6.
Specific embodiment
Illustrate embodiments of the present invention below by way of specific specific example, those skilled in the art can be by this specification
Other advantages and efficacy of the present invention can be easily understood for disclosed content.The present invention can also pass through in addition different specific realities
The mode of applying is embodied or practiced, the various details in this specification can also based on different viewpoints and application, without departing from
Various modifications or alterations are carried out under spirit of the invention.
Please refer to Fig. 1-16, it should be noted that diagram provided in the present embodiment only illustrates this hair in a schematic way
Bright basic conception, only shown in schema then with related component in the present invention rather than component count when according to actual implementation,
Shape and size are drawn, when actual implementation kenel, quantity and the ratio of each component can arbitrarily change for one kind, and its component
Being laid out kenel may also be increasingly complex.
Referring to Fig. 1, the present embodiment proposes a kind of mobile cinema system 10, including ball curtain system 11, cockpit system 12
And control centre 13.
It please be referring to Fig. 1, in the present embodiment, the movable type cinema system 10 includes a ball curtain system 11, the ball
Curtain system 11 includes a spherical screen and ball curtain frame, and the spherical screen stated is mounted on the ball curtain frame, the ball
Curtain system 11 is used to show a film or other demonstration events.
Referring to FIG. 1-2, in the present embodiment, the cockpit system 12 includes pedestal 121, support construction 122, pivoting point
123, pivot structure 124, platform 125 and cockpit 126.In the present embodiment, one end of the support construction 122 is fixed on pedestal
On 121, the support construction 122 is for example bolted on the pedestal 121, and the pedestal 121, which can be fixed on, to circle in the air
On the floor of movie theatre, the pivot structure 124 is connected on the other end of the support construction 122, the pivot structure 124 with
The support construction 122 meets at pivoting point 123, and the pivot structure 124 can be rotated around the pivoting point 123.In this reality
Apply in example, the platform 125 is slidably connected on the pivot structure 124, such as the platform 125 by guiding elements by
It is mounted on the pivot structure 124, the guiding elements is used to promote the sliding of the platform 125.In the present embodiment, institute
It states cockpit 126 to be fixed on the platform 125, the cockpit 126 is provided with safety on the cockpit 126 for carrying spectators
Protective device, for protecting spectators.
In the present embodiment, the frame of the pedestal 121, support construction 122, pivot structure 124, platform 125 can be by gold
Category is made, for example, steel or aluminium, in other embodiments, the floor that fibre reinforced plastics can be used on the platform 125.At it
In his embodiment, metal or timber can be used for such floor.In one embodiment, the cockpit 126 can be made of metal.?
In other embodiments, plastics or fiber reinforcement plastic material frame can be used for the cockpit 126.
In the present embodiment, when performance, film or performance start, the platform 124 is in a horizontal position, and spectators pass through
Walk-in type platform enters on the platform 124, subsequently into the cockpit 126.The platform 124 can be at two kinds of operative positions
It sets, i.e. horizontal position and vertical position.When the platform 124 is in a horizontal position, spectators can from the platform 124 and
Under, when the platform 124 is in a vertical position, spectators are sitting on the cockpit 126, and when the platform 124 is in perpendicular
When straight position, the ball curtain system 11 can be performed, film or performance.At the end of performance, the platform 124 and cockpit
126 return to horizontal position, and spectators can leave movie theatre by walk-in type platform.
Referring to Fig. 1, including multiple control units (control system), institute in the control centre 13 in the present embodiment
It states control unit and is moved for showing a film and controlling the cockpit system 12.
In one embodiment, the control centre 13 can also be used in the phase for showing the cockpit system 12 and ball curtain system 11
Close information, such as detailed status screen, emergency stop conditions screen, network state screen, starting screen, warning screen, warning
History screen, Riding Accommodation mode, the state of cockpit system 11, time and date.
In other embodiments, the control centre 13 may also display alert message, and the alert message may include following
Field: time and date, warning ID (that is, unique alphanumeric code of each warning), device id are (that is, each equipment is only
One alphanumeric code), component ID (for example, indication sensor, motor, valve, brake etc. and identify which component be warning
The code in source), result (for example, emergent stopping, dispatch, forbid, Riding Accommodation stops etc.), diagnostic message or recovery process.
In one embodiment, maintenance mode is provided, maintenance mode is only for the mode of maintenance personal and it is permitted
Permitted to manually control the cinema system 10 that circles in the air.The equipment must be manually operated in the sight of control position.It is all urgent
Stop button will be operable under maintenance mode.During on the upper and lower cockpit 126 of spectators, up/down mode can be used.For
Into up/down mode, the platform 124 will be in a horizontal position to allow up/down mode.Under in this mode, all power supplys with
Cockpit system 12 is safely isolated, to prevent any movement during up/down process.
In some embodiments, the mobile cinema system 10 further includes an emergency stop button, the emergent stopping
Button can be used for ensuring that cockpit system 12 can in case of emergency stop.In one embodiment, the emergency stop button is fixed
Position is on all consoles for the cinema system 10 that entirely circles in the air and at strategic location.In one embodiment, the emergent stopping
Button respectively has there are two contact and goes here and there coupling line to form double-strand Cat4/SIL-3 safety circuit.Emergency stop circuit is appointed
What is interrupted the safety stop of cause to circle in the air cinema system 10 and all isolated from power.In other embodiments, emergent stopping
It can be reset at primary operator control station, and after emergent stopping, the platform 125 programmed can return to horizontal position
It sets, to allow spectators to leave cockpit 126.
In some embodiments, the cockpit 126 in the normal operation period, can be placed in by the mobile cinema system 10
Automatic mode, all movements in automatic mode are according to Riding Accommodation control system institute implementation and supervision.It is automatic to enter
Mode, the platform 125 may be at horizontal position, and safety device is locked and is confirmed, and there is no multiply
Sit apparatus control system failure.During automatic mode, cockpit system 12 can only operate together with the performance in ball curtain system 11.
All emergency stop buttons are operable in automatic mode.In some embodiments, the Riding Accommodation control system control
Device processed can be Allen-Bradley GuardLogix safety governor.GuardLogix controller is included in 1oo2 system knot
The ControlLogix processor and redundant safety of the standard to work together in structure form a partnership processor.GuardLogix system branch
Hold 4 security application of SIL3 and classification.The safe mould of control hardwired security protocol can also be used in the Riding Accommodation control system
Block.In one embodiment, the Riding Accommodation control system uses facility network (DeviceNet) safe I/O module and equipment
Net secure network is for hard-wired interface to carry out safety-related output and input.In other embodiments, the seating dress
Setting control system may include the database for storing failure message.In other embodiments, database server is also provided with useful
In the tape backup ability of all diagnostic messages, hardware and software is recorded including required tape backup.
In some embodiments, the cockpit system 12 can be placed in evacuation mode.In case of the prevention cockpit 126
The unit failure being automatically brought into operation, the evacuation mode is for making the platform 125 back to horizontal position, to allow up/down
Position.The evacuation mode may include that the automatic sequence of operator is assisted with evacuation procedures.All emergency stop buttons are being dredged
It is operable for dissipating under mode.
Referring to Fig. 3, the present embodiment proposes a kind of pressure monitoring system 100 of mobile movie theatre, including link block
130, motion module 140, induction module 150, protective module 160, collection module 170 and alarm module 180.
Fig. 3-4 is please referred to, in the present embodiment, the link block 130 connects the cockpit system 110, the cockpit
System 110 includes multiple cockpits, so that the pressure monitoring system 100 can control the cockpit, the link block 130 includes
Transmitting unit 121 and receiving unit 122.The transmitting unit 121 emits signal to the cockpit system 110, when the cockpit
After system 110 receives the signal that the transmitting unit 121 is sent, and when the signal is sent to the receiving unit 122, table
Show that the link block 130 is successfully connected the cockpit system 110, the receiving unit 122 can for example pass through WI-FI wireless network
Transmitting unit 121 described in network, 3G wireless network or 4G wireless network connection.
Referring to Fig. 3, in the present embodiment, the motion module 140 connects the link block 130, the movement mould
Block 140 makes corresponding movement for controlling the cockpit system 110.
Referring to Fig. 5, in the present embodiment, the motion module 140 includes transmission unit 141, linear motion unit 142
And rotary motion unit 143.In the present embodiment, the transmission unit 141 is used to send to the cockpit system 110 and instruct,
Control the cockpit system 110 and main door or secondary door opened or closed according to described instruction, when the cockpit system 110 receive it is described
After instruction, the cockpit system 110 makes corresponding movement according to described instruction, such as opens or closes main door or secondary door.Institute
Stating transmission unit 141 can be for example by WI-FI wireless network, 3G wireless network or 4G wireless network to the cockpit system
110 send instruction.
Referring to Fig. 5, in the present embodiment, when the cockpit system 110 receives the signal that the transmission unit 141 is sent
Afterwards, and by the signal it is sent to the linear motion unit 142, the linear motion unit 142 is to the cockpit system 110
Instruction is sent, and controls the cockpit and moves along a straight line.When the cockpit system 110 receives the linear motion unit 142
After the instruction of transmission, the cockpit system 110 controls the cockpit according to described instruction and is moved forward or back, such as works as entrance
When the viewing stage, the linear motion unit 142 controls the cockpit and advances, at the end of viewing, the linear motion
Unit 142 controls the cockpit and is retreated.
Referring to Fig. 5, in the present embodiment, when the cockpit system 110 receives the signal that the transmission unit 141 is sent
Afterwards, and by the signal it is sent to the multifreedom motion unit 143, the multifreedom motion unit 143 is to the seat
Cabin system 110 sends instruction, and controls the cockpit system and carry out multifreedom motion.When the cockpit system 110 receives institute
After the instruction for stating the transmission of multifreedom motion unit 143, the cockpit system 110 controls the cockpit system according to described instruction
Multifreedom motion is carried out, such as when entering the viewing stage, according to performance or substance film, the multifreedom motion unit
Cockpit platform in the 143 control cockpit systems 110 moves to any attitude.At the end of viewing, the multiple degrees of freedom fortune
The cockpit platform that moving cell 143 controls in the cockpit system 110 moves to origin position, and spectators is facilitated to leave the theatre.In this implementation
In example, the multifreedom motion unit 143 is, for example, three-degree-of-freedom motion unit, in other embodiments, described mostly free
Spending for example, three-degree-of-freedom motion unit of moving cell 143 is, for example, six-freedom motion unit, for example, six-freedom motion
Axis servomotor.
Referring to Fig. 3, the induction module 150 connects the link block 130, the induction module 150 is for real-time
Monitor the pressure change in the cockpit system 110.
Referring to Fig. 6, the induction module 150 includes sensing unit 151 and alarm unit 152, the sensing unit 151
Connect the alarm unit 152.The sensing unit 151 is used to incude the pressure change in the cockpit system 110, institute in real time
State sensing unit 151 can cockpit system 110 described in real-time monitoring pressure value, and the pressure value can be stored.The sense
Answer the threshold range that pressure is provided in unit 151, the pressure value and the threshold range phase that the sensing unit 151 monitors
Than when the pressure change in the cockpit system is not in predetermined threshold range, the alarm unit 152 provides warning letter
Number.If the pressure value is less than the lower limit value of the threshold range, the alarm unit 152 provides under-voltage warning, if institute
The upper limit value that pressure value is greater than the threshold range is stated, the alarm unit 152 provides over-voltage warning.
In other embodiments, the baroceptor is contacted with tested gas circuit, the pressure of the gas of the tested gas circuit
It acts directly on the baroceptor, the baroceptor will collect the atmospheric pressure value of gas circuit, the air pressure sensing
The atmospheric pressure value of device output can be a resistance signal, and collected atmospheric pressure value is transferred to air pressure by the baroceptor
Level shifting circuit, after the air pressure level shifting circuit receives the atmospheric pressure value of baroceptor transmission, by the air pressure
Value is converted to baroswitch amount.
Wherein, the atmospheric pressure value received is converted to baroswitch amount, including following mistake by the air pressure level shifting circuit
Journey:
After the air pressure level shifting circuit receives the atmospheric pressure value of the baroceptor transmission, if the atmospheric pressure value
In the preset threshold range of air pressure level shifting circuit, then the atmospheric pressure value is converted into baroswitch amount 1, if the atmospheric pressure value
Not in the preset threshold range, then the atmospheric pressure value is converted into hydraulic pressure switch amount 0, alternatively, if the atmospheric pressure value is in air pressure electricity
In the preset threshold range of flat conversion circuit, then the atmospheric pressure value is converted into baroswitch amount 0, if the atmospheric pressure value is not pre- at this
If in threshold range, then the atmospheric pressure value is converted to baroswitch amount 1, and the baroswitch amount being converted to is transferred to described
Alarm unit 152, the alarm unit 152 stores the corresponding diagnostic message of baroswitch amount 1 and baroswitch amount 0 is corresponding
Diagnostic message；And alarm signal is provided according to the diagnostic message.
In the present embodiment, the induction module 150 may also include torque sensing unit, electric current sensing unit and voltage sense
Unit is answered, by the torque sensing unit, electric current sensing unit and voltage induced unit can real-time monitoring torque, electric current and electricity
The situation of change of pressure can then pass through report if the torque value monitored, current value and voltage value are more than the range of the threshold value of setting
Alert unit 152 provides information warning, and in the present embodiment, the induction module 150 monitors torque, the step of electric current and voltage change
Suddenly the step of monitoring pressure change with the induction module 150 is consistent, and the present embodiment be not illustrated.
Referring to Fig. 7, in the present embodiment, the movable type movie theatre pressure monitoring system 100 further includes a protective module
160, safety of the spectators in viewing can be improved in the protective module 160, and in the present embodiment, the protective module 160 is wrapped
Monitoring unit 161 and alarm unit 152 are included, the monitoring unit 161 is used to monitor the safety device in the cockpit system 110
Whether in running order, the safety device is, for example, safety belt, if the monitoring unit 161 monitors the cockpit system
Safety device in system 110 is not in working condition, then the alarm unit 152 provides alarm signal, remind staff into
Row maintenance.When the protective module 160 breaks down, fault message is sent to the collection mould by the protective module 160
Block 170.
Referring to Fig. 8, in the present embodiment, the collection module 170 includes collector unit 171 and diagnosis unit 172, institute
Collector unit 171 is stated for collecting the link block 120, motion module 140, the event of induction module 150 and protective module 160
Hinder information, the collector unit 171 is sent to the diagnosis unit 172 after summarizing the fault message.In the present embodiment,
The diagnosis unit 172 analyzes the fault message, and the link block 130 is stored in the diagnosis unit 172, moves mould
Block 140, the Failure Diagnostic Code of induction module 150 and protective module 160 diagnose the prison according to the various monitoring data received
The corresponding fault message of measured data, each control module (130,140,150,160) that the diagnosis unit 172 can will receive
Monitoring data diagnosed using its Failure Diagnostic Code, can thus learn the component to break down, fault type, lead
The reason of causing the failure etc..The Failure Diagnostic Code, which can be, carries out event to each control module (130,140,150,160)
The monitoring data and a variety of different monitoring data corresponding fault message of required reference when barrier diagnosis.The generation event
The reason of location information of barrier includes the component to break down, and the fault message to break down includes fault type, breaks down
Etc. information.In the present embodiment, the fault message includes servo overheat, and servo overload, servo position deviation is excessive, and servo is same
Step missing, the servo forward direction excess of stroke, the reversed excess of stroke of servo, servo main circuit over-voltage, servo main circuit is under-voltage or servo main circuit lacks
Equal fault message.
Referring to Fig. 3, the alarm module 180 connects the collection module 170, the collection module 170 believes failure
Breath is sent to the alarm module 180, and the alarm module 180 provides information warning and solution party according to the fault message
Case, while recording current alarm condition.
Referring to Fig. 9, the alarm module 180 includes processing unit 181 and alarm unit 182, the processing unit 181
For receiving the fault message and the fault message being converted into fault code, stores and turn in the processing unit 181
Rule is changed, the fault code is sent to the alarm unit 182,182 basis of alarm unit by the processing unit 181
The fault code provides corresponding information warning and solution, and the alarm unit 182 can for example propose to repair, maintenance
It is recommended that the alarm unit 182 also can record current alarm condition.
In the present embodiment, the text that the processing unit 181 can identify abstract computer language translation adult
Language, for example, indicating that the data bit " 0 " of the link block 130 indicates normal, " 1 " indicates abnormal, indicates the protective module
140 data bit " 0 " indicates normal, and " 1 " indicates abnormal etc..The alarm unit 182 is believed according to the corresponding warning of fault code
Breath and solution, and record current alarm condition.
Referring to Fig. 10, the present embodiment proposes a kind of Pressure monitoring method of mobile movie theatre, applied to above-mentioned movement
The pressure monitoring system of formula movie theatre, which comprises
S1: a connection at least cockpit system, an at least cockpit system includes multiple cockpits；
S2: being instructed by sending to the cockpit system, and the cockpit system makes corresponding movement according to described instruction；
S3: incude the pressure change in the cockpit system；
S4: the working condition of safety device in the cockpit system is monitored；
S5: the phylogenetic fault message of the cockpit is collected, and carries out Macro or mass analysis；
S6: corresponding information warning and solution are provided based on the analysis results.
Figure 11 is please referred to, in S1, a connection at least cockpit system, an at least cockpit system includes multiple seats
Cabin includes:
S11: Xiang Suoshu cockpit system sends signal；
S12: judge whether to receive the signal sent from cockpit system, if receiving the signal, the side of continuation
Method step, if being not received by the signal, it is determined that connecting fault occur.
Figure 12 is please referred to, in S2, described to instruct by sending to the cockpit system, the cockpit system is according to
Corresponding movement is made in instruction
S21: Xiang Suoshu cockpit system sends instruction, and the cockpit system is acted accordingly according to described instruction；
S22: whether the movement for judging that the cockpit system is made is correct, if the movement made of the cockpit system is not just
Really, it is determined that the movement of the cockpit system is broken down；
S23: if the movement that the cockpit system is made is correct, linear motion unit controls the cockpit system and carries out
Linear movement, if the cockpit system, without linear movement, the linear motion unit connects the collection module, and
The fault message of the linear motion unit is sent to the collection module；
S24: if the movement that the cockpit system is made is correct, multifreedom motion unit controls the cockpit system
Multifreedom motion is carried out, if the cockpit system, without multifreedom motion, the multifreedom motion unit connects
The collection module is connect, and the fault message of the multifreedom motion unit is sent to the collection module；
In step s 2, step S23 and S24 can be carried out simultaneously, only when step S23 and S24 is correct simultaneously, Cai Kejin
Row step S3.In step s 2, by step S23 and S24, spectators can be in the abundant extremely powerful ball curtain movie and television contents of impression
While, can also undergo the excitement that vacantly flies by.
Figure 13 is please referred to, in S3, the pressure change in the induction cockpit system includes:
S31: the pressure change in cockpit system described in real-time monitoring；
S32: the pressure value monitored is judged whether in the threshold range of setting, when the pressure in the cockpit system does not have
When having in predetermined threshold range, it is determined that the pressure in the cockpit system breaks down.
Figure 14 is please referred to, in S4, the working condition of safety device includes: in the monitoring cockpit system
S41: the working condition of safety device in cockpit system described in real-time monitoring；
S42: judging whether the safety device is in running order, if the safety device is not in working condition,
Then determine that safety device breaks down in the cockpit system.
Figure 15 is please referred to, it is described to collect the phylogenetic fault message of cockpit in S5, and carry out Macro or mass analysis packet
It includes:
S41: fault message is collected；
S42: Macro or mass analysis is carried out to appearance of being out of order to the fault message according to the diagnostic rule of fault message
Reason.
Figure 16 is please referred to, it is described according to the fault message in S6, provide corresponding information warning and solution packet
It includes:
S61: the fault message is converted into fault code；
S62: corresponding information warning and solution are provided according to the fault code.It stores in the alarm unit
Corresponding warning rule, the alarm unit can record current warning message.
In conclusion the present invention proposes a kind of mobile movie theatre pressure monitoring system and monitoring method, supervised by the air pressure
Examining system can real-time monitoring air pressure change, simplify operating process, improve the safety of mobile movie theatre, ensure that spectators
Viewing experience sense, pressure monitoring system proposed by the present invention can also record the fault message occurred in monitoring process in real time, letter
Maintenance process is changed.
Above description is only the preferred embodiment of the application and the explanation to institute's application technology principle, those skilled in the art
Member is it should be appreciated that invention scope involved in the application, however it is not limited to technology made of the specific combination of above-mentioned technical characteristic
Scheme, while should also cover in the case where not departing from the inventive concept, it is carried out by above-mentioned technical characteristic or its equivalent feature
Any combination and the other technical solutions formed, such as features described above have similar function with (but being not limited to) disclosed herein
Can technical characteristic replaced mutually and the technical solution that is formed.
Except for the technical features described in the specification, remaining technical characteristic is the known technology of those skilled in the art, is prominent
Innovative characteristics of the invention out, details are not described herein for remaining technical characteristic.
Claims (10)
1. a kind of pressure monitoring system of movable type movie theatre characterized by comprising
Link block connects at least one cockpit system, at least one described cockpit system includes multiple cockpits；
Induction module, for monitoring the air pressure change in the cockpit system；
Collection module for collecting the fault message of the link block and induction module, and carries out Macro or mass analysis；
Alarm module provides corresponding information warning based on the analysis results and records current warning message.
2. pressure monitoring system according to claim 1, which is characterized in that the link block includes:
Transmitting unit, for emitting signal at least one described cockpit system；
Receiving unit receives the signal from least one described cockpit system.
3. pressure monitoring system according to claim 1, which is characterized in that the induction module includes:
Sensing unit, the pressure change in cockpit system described in real-time monitoring；
Alarm unit, when the pressure in the cockpit system is not in predetermined threshold range, the alarm unit is to responding
Show signal.
4. pressure monitoring system according to claim 1, which is characterized in that the collection module includes:
Collector unit collects the fault message of the link block and induction module；
Diagnosis unit carries out Macro or mass analysis to appearance of being out of order to the fault message according to the diagnostic rule of fault message
Reason.
5. pressure monitoring system according to claim 1, which is characterized in that the alarm module includes:
The fault message is converted into fault code by processing unit；
Alarm unit provides corresponding information warning and solution according to the fault code, and records current alarm signal
Breath.
6. pressure monitoring system according to claim 1, which is characterized in that it further include motion module, the motion module
Include:
Transmission unit, Xiang Suoshu cockpit system send instruction, the cockpit system according to described instruction open or close main door or
Secondary door；
Linear motion unit controls the cockpit system and moves linearly；
Multifreedom motion unit controls the cockpit system and carries out multifreedom motion.
7. pressure monitoring system according to claim 1, which is characterized in that it further include protective module, the protective module
Include:
Monitoring unit, the working condition for protective device in cockpit system described in real-time monitoring；
Alarm unit, when the protective device is not in working condition, the alarm unit provides alarm signal.
8. a kind of Pressure monitoring method of movable type movie theatre characterized by comprising
At least cockpit system of connection, an at least cockpit system includes multiple cockpits；
Monitor the pressure change in the cockpit system；
The phylogenetic fault message of the cockpit is collected, and carries out Macro or mass analysis；
Corresponding information warning is provided according to the fault message, and records current warning message.
9. Pressure monitoring method according to claim 6, which is characterized in that the pressure in the monitoring cockpit system
Variation includes:
Pass through the pressure change in cockpit system described in sensing unit real-time monitoring；
Alarm signal is provided by alarm unit.
10. Pressure monitoring method according to claim 6, which is characterized in that the collection cockpit is phylogenetic
Fault message, and carry out Macro or mass analysis and include:
The fault message of the cockpit system is collected by collector unit；
The fault message is subjected to Macro or mass analysis by diagnosis unit.
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| CN201910619267.1A CN110243535A (en) | 2019-07-10 | 2019-07-10 | A kind of pressure monitoring system and monitoring method of movable type movie theatre |
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| CN201910619267.1A CN110243535A (en) | 2019-07-10 | 2019-07-10 | A kind of pressure monitoring system and monitoring method of movable type movie theatre |
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| CN110243535A true CN110243535A (en) | 2019-09-17 |
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| JP2014084686A (en) * | 2012-10-26 | 2014-05-12 | Ohira Giken:Kk | Temporary theater dome |
| CN203689131U (en) * | 2014-01-23 | 2014-07-02 | 中国电影器材有限责任公司 | Control system for dynamic seats in movie theater |
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