CN104865921A - Airplane clear water vehicle intelligent management system - Google Patents
Airplane clear water vehicle intelligent management system Download PDFInfo
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- CN104865921A CN104865921A CN201510124910.5A CN201510124910A CN104865921A CN 104865921 A CN104865921 A CN 104865921A CN 201510124910 A CN201510124910 A CN 201510124910A CN 104865921 A CN104865921 A CN 104865921A
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/418—Total factory control, i.e. centrally controlling a plurality of machines, e.g. direct or distributed numerical control [DNC], flexible manufacturing systems [FMS], integrated manufacturing systems [IMS], computer integrated manufacturing [CIM]
- G05B19/4188—Total factory control, i.e. centrally controlling a plurality of machines, e.g. direct or distributed numerical control [DNC], flexible manufacturing systems [FMS], integrated manufacturing systems [IMS], computer integrated manufacturing [CIM] characterised by CIM planning or realisation
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02P—CLIMATE CHANGE MITIGATION TECHNOLOGIES IN THE PRODUCTION OR PROCESSING OF GOODS
- Y02P90/00—Enabling technologies with a potential contribution to greenhouse gas [GHG] emissions mitigation
- Y02P90/02—Total factory control, e.g. smart factories, flexible manufacturing systems [FMS] or integrated manufacturing systems [IMS]
Abstract
The invention relates to an airplane clear water vehicle intelligent management system. The airplane clear water vehicle intelligent management system includes a data acquisition terminal, a wired/wireless transmission network, a data receiving terminal and a monitoring center, wherein the data acquisition terminal and the data receiving terminal are connected with each other through the wired/wireless transmission network, and the data receiving terminal and the monitoring center are connected with each other through the wired/wireless transmission network. With the airplane clear water vehicle intelligent management system provided by the invention adopted, airplane clear water vehicles can be effectively scheduled, and therefore, manpower and material resources can be saved, and monitoring on the working states of the airplane clear water vehicles can be realized, and the intensity of monitoring and management on the airplane clear water vehicles by an airport can be strengthened, and the operating time of the vehicles can be accurately calculated and recorded, and thus, the overall operating efficiency of the airport can be improved.
Description
Technical field
The invention belongs to special vehicle administrative skill field, airport, particularly relate to and a kind ofly add up for aircraft clear water car scheduling, job state monitoring and carry out the device of charging according to the activity duration with the activity duration.
Background technology
Along with the development of domestic air mail cause, the quantity of aircarrier aircraft continues to increase, and inside, airport is that the special vehicle of serving aircraft is also on the increase, and therefore the demand of passenger plane to ground safeguard and service is also more and more higher.How airport special vehicle is monitored and intelligent management in real time, ensure these vehicle safeties, run efficiently, become the problem that airliner place is concerned about.Correspondingly, the aircraft clear water car of airport ground operation also progressively increases, therefore also increasing to the scheduling of aircraft clear water car, monitoring and management difficulty.
Present stage, aircraft clear water car activity duration information also needs acquisition of manually signing a bill, and this method greatly reduces the efficiency of Airport Operation management.At present, airport does not also have aircraft clear water car job state data acquisition equipment, therefore can not Real-time Collection job state data automatic acquisition activity duration.Therefore design a aircraft clear water car intelligent management apapratus to be extremely necessary.
Summary of the invention
In order to solve the problem, the object of the present invention is to provide a kind of aircraft clear water car intelligent management system.
In order to achieve the above object, aircraft clear water car intelligent management system provided by the invention comprises: data collection station, wire/wireless transmission network, data receiving terminal, Surveillance center; Wherein: be connected by wire/wireless transmission network between data collection station with data receiving terminal; Data receiving terminal is connected by wire/radio network with Surveillance center;
Data collection station is the data collector be arranged on aircraft clear water car, and data receiving terminal is the communication interface being arranged on air traffic control centre, and Surveillance center is the supervisory computer system being arranged on air traffic control centre.
Described data collection station comprises: microprocessor, sensor assembly, wireless transport module, locating module, identification module, OBD module; Wherein: sensor assembly, wireless transport module, locating module, identification module, OBD module are all connected by serial bus or cpu bus with microprocessor;
Microprocessor is the core controller of data collection station, for controlling sensor assembly, wireless transport module, locating module, OBD module realize data acquisition, data transfer operation;
Wireless transport module is provided with radio transmission antenna, transfers data to wire/wireless transmission network by radio transmission antenna;
Locating module is provided with positioning antenna, and it uses GPS (Global Position System) to gather longitude, latitude, height above sea level, the translational speed information of aircraft clear water car;
Identification module comprises fingerprint identification module, card reader module, infrared scan module, facial recognition modules or bar code scanner module, and the identity information collected is transferred to Surveillance center by wireless transport module by it;
OBD module is aircraft clear water car data collector, and it is connected with the ODB interface of aircraft clear water car, and the operation conditions of monitor engines in real time also gathers aircraft clear water car engine speed, amount of fuel information data by CAN;
Sensor assembly is for monitoring the job state of aircraft clear water car, and according to the signal record aircraft clear water car job state that various types of sensor collects, it comprises: signal picker, clear water pipe reseting sensor, clear water pipe adapter and aircraft water transport port status sensors, high water tank sensor, pump working state sensor; Wherein: signal picker is connected with microprocessor, and be connected with aircraft water transport port status sensors, high water tank sensor and pump working state sensor with clear water pipe reseting sensor, clear water pipe adapter respectively.
Described clear water pipe reseting sensor, clear water pipe adapter and aircraft water transport port status sensors, high water tank sensor and pump working state sensor are connected by the analog acquisition interface of signal wire and signal picker or frequency signal acquisition interface, and signal picker is connected with microprocessor by serial bus or cpu bus.
Described clear water pipe reseting sensor is arranged on operating platform clear water pipe replacement and fixation position, whether reset after judging the operation of clear water pipe, adopt resistance strain gage pressure transducer, semiconductor gauge pressure transducer, piezoresistive pressure sensor, inductance pressure transducer, capacitance pressure transducer, resonance type pressure sensor or capacitance acceleration transducer.
Described clear water pipe adapter and aircraft water transport port status sensors are arranged on clear water pipe adapter place, and whether firm for judging that clear water pipe adapter is connected with aircraft water-supply-pipe, it adopts the pressure transducer of all kinds of maturation.
Described high water tank sensor is arranged on aircraft clear water car tank inner wall, for showing the height of the water surface in water tank, it adopts single flange static pressure/bis-flange differential pressure liquid level transmitter, float ball type level transducer, magnetic level transmitter, throw-in type liquid transmitter, electronic inner float ball fluid level transmitter, electric float level transmitter, capacitive liquid level transmitter, magnetostrictive liquid level transducer, wait upon and take fluid level transmitter, supersonic level sensor or radar level transmitter.
Described pump working state sensor is arranged on aircraft clear water car and drives on the transmission shaft of water pump or drive on hydraulic electric motor axle, for judging the duty whether water pump is in water transport and turns, it adopts Hall voltage sensor, Hall current sensor, proximity Hall switch or Hall magnetic field sensor.
Described data receiving terminal comprises: microprocessor, wireless transport module and wired network interface; Wherein: wireless transport module is connected with microprocessor by serial bus or cpu bus with wired network interface; Wherein microprocessor is the core controller of data receiving terminal, for controlling wireless transport module and wired network interface realizes exchanges data;
Wireless transport module is connected with antenna, and obtain data by antenna from wire/wireless transmission network, and transfer data to microprocessor, data are transferred to Surveillance center by wired network interface by microprocessor.
Described Surveillance center comprises: server, database, display device, wired network interface, Airport Operation management database; Special vehicle activity duration management system is installed in server, database, display device, wired network interface, Airport Operation management database are connected by bus with server, server is communicated with data receiving terminal by wired network interface, and the aircraft clear water car job state collected and activity duration are stored to database, and shown the data collected by display device; Server reads flight, seat in the plane information from Airport Operation management database, and managerial personnel dispatch aircraft clear water vehicle according to the flight read, seat in the plane information.
The effect of aircraft clear water car intelligent management system provided by the invention is: by making rational management to aircraft clear water car, save manpower and materials; To the monitoring of aircraft clear water car job state, strengthen the monitoring of airport to aircraft clear water car, the dynamics of management, to the also accurately charging of activity duration statistics, thus improve the operational efficiency of airport entirety.
Accompanying drawing explanation
Fig. 1 is aircraft clear water car intelligent management system structural drawing provided by the invention;
Fig. 2 is the data collection station structural representation shown in Fig. 1;
Fig. 3 is the data receiving terminal structural representation shown in Fig. 1;
Fig. 4 is sensor module structure schematic diagram in aircraft clear water car intelligent management system provided by the invention;
Fig. 5 is Surveillance center's structural drawing in aircraft clear water car intelligent management system provided by the invention.
Embodiment
Below in conjunction with the drawings and specific embodiments, aircraft clear water car intelligent management apapratus provided by the invention is described in detail:
As shown in Figure 1, aircraft clear water car intelligent management system provided by the invention comprises: data collection station 1, wire/wireless transmission network 2, data receiving terminal 3, Surveillance center 4; Wherein: be connected by wire/wireless transmission network 2 between data collection station 1 with data receiving terminal 3; Data receiving terminal 3 is connected by wired (wireless) network with Surveillance center 4.
Data collection station 1 is for being arranged on the data collector on aircraft clear water car, and data receiving terminal 3 is for being arranged on the communication interface of air traffic control centre, and Surveillance center 4 is for being arranged on the supervisory computer system of air traffic control centre.
Described data collection station 1 is as follows with the connected mode of data receiving terminal 3: the data collected are transferred to data receiving terminal 3 by wire/wireless transmission network 2 by data acquisition monitor terminal 1.
Wire/wireless transmission network 2 is combined by cable network and wireless network and uses, form a hybrid network, wherein the kind of cable network has: LAN (Local Area Network) (LAN), Metropolitan Area Network (MAN) (MAN), fieldbus networks, optical fiber ring network, ethernet ring network etc.; The kind of wireless network has: WLAN (wireless local area network) (WLAN), wireless sense network (WSN), digital trunk network, simulation cluster net, global system for mobile communications (GSM) network, G mobile communication (3G) network and forth generation mobile communication technology (4G) network etc.
As shown in Figure 2, described data collection station 1 comprises: microprocessor 11, sensor assembly 12, wireless transport module 13, locating module 14, identification module 17, OBD (onboard diagnostic system) module 18; Wherein: sensor assembly 12, wireless transport module 13, locating module 14, identification module 17, OBD module 18 are all connected by serial bus or cpu bus (comprising RS-232 bus, RS-485 bus, I2C bus, spi bus, usb bus etc.) with microprocessor 11.
Microprocessor 11 is the core controller of data collection station 1, for controlling sensor assembly 12, wireless transport module 13, locating module 14, OBD module 18 realize the operation such as data acquisition, data transmission; Sensor assembly 12 sends the data preparation collected to microprocessor 11, and then data are transferred to wireless transport module 13 by serial ports or cpu i/f by microprocessor 11 again; Location information data is sent to microprocessor 11 by locating module 14, and data are transferred to wireless transport module 13 by serial ports or cpu i/f by microprocessor 11 again; Identity information data is sent to microprocessor 11, OBD module 18 (onboard diagnostic system) and the vehicle running state information data such as the amount of fuel of vehicle, engine speed is sent to microprocessor 11 by identification module 17; Data are transferred to wireless transport module 13 by serial ports or cpu i/f by microprocessor 11 again.
Wireless transport module 13 is provided with radio transmission antenna 16, transfer data to wire/wireless transmission network 2 by radio transmission antenna 16, it comprises: WLAN (wireless local area network) (WLAN) module, wireless sense network (WSN) module, digital trunk network module, simulation cluster net module, global system for mobile communications (GSM) mixed-media network modules mixed-media, G mobile communication (3G) mixed-media network modules mixed-media and forth generation mobile communication technology (4G) mixed-media network modules mixed-media etc.
Locating module 14 is provided with positioning antenna 15, it uses GPS (Global Position System) (gps satellite navigational system, Beidou satellite navigation system, GLONASS satellite navigation system, GALILEO satellite navigation system etc.) to gather the information such as longitude, latitude, height above sea level, translational speed of aircraft clear water car.Microprocessor 11 initiatively gathers the positional information of aircraft clear water car every the several seconds (such as 1 second to 5 seconds) to locating module 14.
Identification module 17 comprises fingerprint identification module, card reader module, infrared scan module, facial recognition modules or bar code scanner module, and the identity information collected is transferred to Surveillance center 4 by wireless transport module 13 by it.The identity information of identification for detecting the identity of aircraft clear water car operating personnel, and is passed back to Surveillance center by identification module 17, and operating personnel only has and first carries out identification by identification module 17, and the clear water car that just can drive an airplane carries out operation.Wherein, corresponding some the operating personnels of aircraft clear water car.
OBD module 18 is aircraft clear water car vehicle-mounted diagnosis device, and it is connected with the ODB interface of aircraft clear water car, and the operation conditions of monitor engines in real time also gathers the information datas such as aircraft clear water car engine speed, amount of fuel by CAN; OBD module 18 passes by wire/wireless transmission network 2 the travel condition of vehicle data collected back Surveillance center 4; By these data, Surveillance center 4 judges that whether vehicle operating is normal, meanwhile, also can carry out tracking statistics to the life cycle of this vehicle (repair and maintenance and servicing time as vehicle), judge whether this vehicle can complete this flight task with this.
As shown in Figure 4, described sensor assembly 12 is for monitoring the job state of aircraft clear water car, and according to the signal record aircraft clear water car job state that various types of sensor collects, it comprises: signal picker 121, clear water pipe reseting sensor 122, clear water pipe adapter and aircraft water transport port status sensors 123, high water tank sensor 124, pump working state sensor 125; Wherein: signal picker 121 is connected with aircraft water transport port status sensors 123, high water tank sensor 124 and pump working state sensor 125 with microprocessor 11, clear water pipe reseting sensor 122, clear water pipe adapter.
Clear water pipe reseting sensor 122, clear water pipe adapter and aircraft water transport port status sensors 123, high water tank sensor 124 and pump working state sensor 125 are connected by the analog acquisition interface of signal wire and signal picker 121 or frequency signal acquisition interface, and signal picker 121 is connected with microprocessor 11 by serial bus or cpu bus.
Signal picker 121 is signal acquisition controller, gathered the work state information of aircraft clear water car by clear water pipe reseting sensor 122, clear water pipe adapter and aircraft water transport port status sensors 123, high water tank sensor 124 and pump working state sensor 125, and be uploaded to microprocessor 11.
Clear water pipe reseting sensor 122 adopts resistance strain gage pressure transducer, semiconductor gauge pressure transducer, piezoresistive pressure sensor, inductance pressure transducer, capacitance pressure transducer, resonance type pressure sensor or capacitance acceleration transducer, for judging whether clear water pipe resets.
Clear water pipe adapter and aircraft water transport port status sensors 123 adopt the pressure transducer of all kinds of maturation, for the information of the clear water pipe adapter and aircraft water transport port connection status that gather return pipe, guarantee to be connected firmly.
High water tank sensor 124 adopts single flange static pressure/bis-flange differential pressure liquid level transmitter, float ball type level transducer, magnetic level transmitter, throw-in type liquid transmitter, electronic inner float ball fluid level transmitter, electric float level transmitter, capacitive liquid level transmitter, magnetostrictive liquid level transducer, wait upon and take fluid level transmitter, supersonic level sensor or radar level transmitter, for showing the height of water level in aircraft clear water car water tank.
Pump working state sensor 125 adopts Hall voltage sensor, Hall current sensor, proximity Hall switch or Hall magnetic field sensor, for gathering the work state information of water pump, and then judges that whether water pump operates having under regimen condition.
Whether clear water pipe reseting sensor 122 is arranged on operating platform clear water pipe and resets on (off-position) fixed position, reset after judging the operation of clear water pipe; Whether clear water pipe adapter and aircraft water transport port status sensors 123 are arranged on clear water pipe adapter place, firm for judging that clear water pipe adapter is connected with aircraft water-supply-pipe; High water tank sensor 124 is arranged on aircraft clear water car tank inner wall, for showing the height of the water surface in water tank; Pump working state sensor 125 is arranged on aircraft clear water car and drives on the transmission shaft of water pump or drive on hydraulic electric motor axle, for judging the duty whether water pump is in water transport and turns.
As shown in Figure 3, described data receiving terminal 3 comprises: microprocessor 31, wireless transport module 32 and wired network interface 33; Wherein: wireless transport module 32 is connected with microprocessor 31 by serial bus or cpu bus with wired network interface 33.Wherein microprocessor 31 is the core controller of data receiving terminal 3, for controlling wireless transport module 32 and wired network interface 33 realizes exchanges data.
Wireless transport module 32 is connected with antenna 34, obtains data by antenna 34 from wire/wireless transmission network 2, and transfers data to microprocessor 31, and data are transferred to Surveillance center 4 by wired network interface 33 by microprocessor 31.According to system requirements, wired network interface 33 comprises LAN interface usually, industrial field bus interface, optical fiber ring network interface, ethernet ring network interface, field-bus interface etc.
Surveillance center 4 in Fig. 1 is as shown in Figure 5, comprising: server 41, database 42, display device 43, wired network interface 44, Airport Operation management database 45; Special vehicle activity duration management system is installed in server 41, database 42, display device 43, wired network interface 44, Airport Operation management database 45 are connected by bus with server 41, server 41 is communicated with data receiving terminal 3 by wired network interface 44, the aircraft clear water car job state collected and activity duration are stored to database 42, and are shown the data collected by display device 43.Server 41 reads flight, seat in the plane information from Airport Operation management database 45, and managerial personnel dispatch aircraft clear water vehicle according to the flight read, seat in the plane information.
Server 41 in Surveillance center 4 obtains Flight Information and passenger information from Airport Operation management database automatically, then managerial personnel are according to the distribution of flight support mission system, by job task information distribution to the aircraft clear water car operating personnel specified, after as operating personnel, according to serviced aircraft position automatic acquisition, it travels optimal path, drive an airplane clear water car to assignment position, use locating module 14 in real time its transport condition and positional information to be transferred to data receiving terminal 3 by wire/wireless transmission network 2 simultaneously, positional information to be transferred in Surveillance center 4 by wire/wireless transmission network and to show by data receiving terminal 3, the positional information received and Flight Information are checked by managerial personnel, when aircraft clear water car starts operation, data collection station 1 obtains time data at that time, data receiving terminal 3 is transferred to by wire/wireless transmission network 2, data are finally transferred to Surveillance center 4 by wired (wireless) network by data receiving terminal 3, display time data on the display device 43 of Surveillance center 4, and time data is stored into database 42.
Whole workflows of native system are as follows: Surveillance center 4 by server 41 from Airport Operation management database read flight number, type, seat in the plane, aircraft clear water license number information, make and ensure job task scheme, aircraft clear water car and operating personnel are dispatched, first, the aircraft clear water car operating personnel receiving task carries out identification by the identification module 17 on data collection station 1, start aircraft clear water car after identification is errorless to await orders, then Surveillance center 4 is by the running state information of the OBD module 18 Real-time Obtaining aircraft clear water car on data collection station 1, and by being arranged on height of water level information in the liquid level sensor 124 Real-time Obtaining water tank on aircraft clear water car water tank inwall, judge that can this aircraft clear water car complete this subtask, if this subtask can not be completed, then other vehicles of scheduling, if this subtask can be completed, Surveillance center 4 starts to carry out this job instruction to the transmission of this aircraft clear water car by wire/radio network 2, afterwards operating personnel drive an airplane clear water car drive towards specify seat in the plane, in the process of moving, data collection station 1 at regular intervals by the positional information collected (for determine service seat in the plane with service flight) be back to Surveillance center 4, after arriving assigned address, start to carry out operation, the temporal information of this timing node is transferred to Surveillance center 4 by data collection station 1, stores and is presented in Surveillance center 4, at the end of operation, the temporal information of this timing node is transferred to Surveillance center 4, final storage is also presented in Surveillance center 4, carry out charging according to these aircraft clear water car activity duration information according to certain standard afterwards, thus realize the comprehension management to aircraft clear water car scheduling, monitoring, metering, charge.
In the whole workflow of aircraft clear water car, each sensor is respectively at different phase collection signal, idiographic flow is as follows: aircraft clear water car keeps certain speed near aircraft, staff climbs up vehicle operation ladder, operating platform is raised to corresponding height, operating personnel extract clear water pipe from non-job position, by being arranged on the clear water pipe reseting sensor 122 Real-time Collection signal that operating platform clear water pipe resets on (off-position) fixed position, the signal collected is transferred to signal picker 121 by the analog acquisition interface on sensor assembly 12 or frequency signal acquisition interface, open aircraft filler hatchcover, the water pipe head of aircraft clear water car is received the water-supply-pipe of aircraft by operating personnel, now by clear water pipe adapter and aircraft water transport port status sensors 123 Real-time Collection signal, the signal collected is transferred to signal picker 121 by the analog acquisition interface on sensor assembly 12 or frequency signal acquisition interface, press water delivery switch subsequently, now drive by being arranged on aircraft clear water car on the transmission shaft of water pump or drive the working state signal of the pump working state sensor 125 Real-time Collection water pump on hydraulic electric motor axle, the signal collected is transferred to signal picker 121 by the analog acquisition interface on sensor assembly 12 or frequency signal acquisition interface.
Only have when clear water pipe adapter and aircraft water transport port status sensors 123, pump working state sensor 125 is in normal operating conditions simultaneously, and clear water pipe reseting sensor 122 is when being in off working state, two working state signals and an off working state signal are just passed to microprocessor 11 by bus interface by signal picker 121, microprocessor 11 judges, record now timing node, and the starting point using this timing node as the aircraft clear water car activity duration, and transfer data to data receiving terminal 3 by wire/wireless transmission network 2, data receiving terminal 3 is upload the data in Surveillance center 4 by wired (wireless) network.
After aircraft clear water car operation completes, close water delivery switch, operating personnel close filler hatchcover, regain clear water pipe, now by being arranged on clear water pipe adapter and the aircraft water transport port status sensors 123 Real-time Collection signal at clear water pipe adapter place, the signal collected is transferred to signal picker 121 by the analog acquisition interface on sensor assembly 12 or frequency signal acquisition interface, clear water pipe is reset to non-operation fixed position, now by being arranged on the clear water pipe reseting sensor 122 Real-time Collection signal that operating platform clear water pipe resets on (off-position) fixed position, and the off working state signal of collection is transferred to signal picker 121 by the analog acquisition interface on sensor assembly 12 or frequency signal acquisition interface, then operating platform is resetted, operating personnel prepares to sail out of, and aircraft clear water car withdraws working site.
Only have clear water pipe adapter and aircraft water transport port status sensors 123, pump working state sensor 125 is in off working state simultaneously, and clear water pipe reseting sensor 122 in running order time, two off working state signals and a working state signal are just passed to microprocessor 11 by bus interface by signal picker 121, microprocessor 11 judges, record now timing node, and the terminal using this timing node as the aircraft clear water car activity duration, and by wired wireless-transmission network 2 transfer data to data receiving terminal 3, data receiving terminal 3 is upload the data in Surveillance center 4 by wired (wireless) network.
The major function of aircraft clear water car intelligent management system provided by the invention: Surveillance center 4 is read out by the information of server 41 by the flight number in Airport Operation database, type, seat in the plane, aircraft clear water license number, then formulate and ensure job task scheme, aircraft clear water car is dispatched, real-time monitoring aircraft clear water car duty also adds up the aircraft clear water car activity duration, and data are reached Surveillance center 4 by wire/wireless transmission network 2, finally Storage & Display in Surveillance center 4, achieves intelligentized management and scheduling.
Claims (9)
1. an aircraft clear water car intelligent management system, is characterized in that: it comprises: data collection station (1), wire/wireless transmission network (2), data receiving terminal (3), Surveillance center (4); Wherein: be connected by wire/wireless transmission network (2) between data collection station (1) with data receiving terminal (3); Data receiving terminal (3) is connected by wire/radio network with Surveillance center (4);
Data collection station (1) is for being arranged on the data collector on aircraft clear water car, data receiving terminal (3) is for being arranged on the communication interface of air traffic control centre, and Surveillance center (4) is for being arranged on the supervisory computer system of air traffic control centre.
2. aircraft clear water car intelligent management system according to claim 1, is characterized in that: described data collection station (1) comprising: microprocessor (11), sensor assembly (12), wireless transport module (13), locating module (14), identification module (17), OBD module (18); Wherein: sensor assembly (12), wireless transport module (13), locating module (14), identification module (17), OBD module (18) are all connected by serial bus or cpu bus with microprocessor (11);
The core controller that microprocessor (11) is data collection station 1, for controlling sensor assembly (12), wireless transport module (13), locating module (14), OBD module (18) realize data acquisition, data transfer operation;
Wireless transport module (13) is provided with radio transmission antenna (16), transfers data to wire/wireless transmission network (2) by radio transmission antenna (16);
Locating module (14) is provided with positioning antenna (15), it uses GPS (Global Position System) to gather longitude, latitude, height above sea level, the translational speed information of aircraft clear water car;
Identification module (17) comprises fingerprint identification module, card reader module, infrared scan module, facial recognition modules or bar code scanner module, and the identity information collected is transferred to Surveillance center (4) by wireless transport module (13) by it;
OBD module (18) is aircraft clear water car data collector, and it is connected with the ODB interface of aircraft clear water car, and the operation conditions of monitor engines in real time also gathers aircraft clear water car engine speed, amount of fuel information data by CAN;
Sensor assembly (12) is for monitoring the job state of aircraft clear water car, and according to the signal record aircraft clear water car job state that various types of sensor collects, it comprises: signal picker (121), clear water pipe reseting sensor (122), clear water pipe adapter and aircraft water transport port status sensors (123), high water tank sensor (124), pump working state sensor (125); Wherein: signal picker (121) is connected with microprocessor (11), and be connected with aircraft water transport port status sensors (123), high water tank sensor (124) and pump working state sensor (125) with clear water pipe reseting sensor (122), clear water pipe adapter respectively.
3. aircraft clear water car intelligent management system according to claim 2, it is characterized in that: described clear water pipe reseting sensor (122), clear water pipe adapter and aircraft water transport port status sensors (123), high water tank sensor (124) and pump working state sensor (125) are connected by the analog acquisition interface of signal wire and signal picker (121) or frequency signal acquisition interface, and signal picker (121) is connected with microprocessor (11) by serial bus or cpu bus.
4. aircraft clear water car intelligent management system according to claim 2, it is characterized in that: described clear water pipe reseting sensor (122) is arranged on operating platform clear water pipe replacement and fixation position, whether reset after judging the operation of clear water pipe, adopt resistance strain gage pressure transducer, semiconductor gauge pressure transducer, piezoresistive pressure sensor, inductance pressure transducer, capacitance pressure transducer, resonance type pressure sensor or capacitance acceleration transducer.
5. aircraft clear water car intelligent management system according to claim 2, it is characterized in that: described clear water pipe adapter and aircraft water transport port status sensors (123) are arranged on clear water pipe adapter place, whether firm for judging that clear water pipe adapter is connected with aircraft water-supply-pipe, it adopts pressure transducer.
6. aircraft clear water car intelligent management system according to claim 2, it is characterized in that: described high water tank sensor (124) is arranged on aircraft clear water car tank inner wall, for showing the height of the water surface in water tank, it adopts single flange static pressure/bis-flange differential pressure liquid level transmitter, float ball type level transducer, magnetic level transmitter, throw-in type liquid transmitter, electronic inner float ball fluid level transmitter, electric float level transmitter, capacitive liquid level transmitter, magnetostrictive liquid level transducer, wait upon and take fluid level transmitter, supersonic level sensor or radar level transmitter.
7. aircraft clear water car intelligent management system according to claim 2, it is characterized in that: described pump working state sensor (125) is arranged on aircraft clear water car and drives on the transmission shaft of water pump or drive on hydraulic electric motor axle, for judging the duty whether water pump is in water transport and turns, it adopts Hall voltage sensor, Hall current sensor, proximity Hall switch or Hall magnetic field sensor.
8. aircraft clear water car intelligent management system according to claim 1, is characterized in that: described data receiving terminal (3) comprising: microprocessor (31), wireless transport module (32) and wired network interface (33); Wherein: wireless transport module (32) is connected with microprocessor (31) by serial bus or cpu bus with wired network interface (33); Wherein microprocessor (31) core controller that is data receiving terminal (3), for controlling wireless transport module (32) and wired network interface (33) realizes exchanges data;
Wireless transport module (32) is connected with antenna (34), data are obtained from wire/wireless transmission network (2) by antenna (34), and transferring data to microprocessor (31), data are transferred to Surveillance center (4) by wired network interface (33) by microprocessor (31).
9. aircraft clear water car intelligent management system according to claim 1, is characterized in that: described Surveillance center (4) comprising: server (41), database (42), display device (43), wired network interface (44), Airport Operation management database (45); Server is provided with special vehicle activity duration management system in (41), database (42), display device (43), wired network interface (44), Airport Operation management database (45) are connected by bus with server (41), server (41) is communicated with data receiving terminal (3) by wired network interface (44), and the aircraft clear water car job state collected and activity duration are stored to database (42), and show by display device (43) data collected; Server (41) reads flight, seat in the plane information from Airport Operation management database (45), and managerial personnel dispatch aircraft clear water vehicle according to the flight read, seat in the plane information.
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN110514249A (en) * | 2019-09-25 | 2019-11-29 | 东方航空技术有限公司 | A kind of aero-engine washing data collection system |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202815538U (en) * | 2012-08-18 | 2013-03-20 | 四川欧润特软件科技有限公司 | Airport monitoring system with holder control |
| CN103983303A (en) * | 2014-05-06 | 2014-08-13 | 中国民航大学 | System for monitoring environmental pollution of parking apron in airport |
| CN104071351A (en) * | 2014-06-20 | 2014-10-01 | 中国民航大学 | Monitoring system for taking off and landing of plane on airport runway |
| JP2014191933A (en) * | 2013-03-26 | 2014-10-06 | Toshiba Lighting & Technology Corp | Marker lamp device |
| CN104268685A (en) * | 2014-09-23 | 2015-01-07 | 中国民航大学 | Airport ground vehicle tracking management system |
-
2015
- 2015-03-23 CN CN201510124910.5A patent/CN104865921A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN202815538U (en) * | 2012-08-18 | 2013-03-20 | 四川欧润特软件科技有限公司 | Airport monitoring system with holder control |
| JP2014191933A (en) * | 2013-03-26 | 2014-10-06 | Toshiba Lighting & Technology Corp | Marker lamp device |
| CN103983303A (en) * | 2014-05-06 | 2014-08-13 | 中国民航大学 | System for monitoring environmental pollution of parking apron in airport |
| CN104071351A (en) * | 2014-06-20 | 2014-10-01 | 中国民航大学 | Monitoring system for taking off and landing of plane on airport runway |
| CN104268685A (en) * | 2014-09-23 | 2015-01-07 | 中国民航大学 | Airport ground vehicle tracking management system |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110514249A (en) * | 2019-09-25 | 2019-11-29 | 东方航空技术有限公司 | A kind of aero-engine washing data collection system |
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