CN114123464A - Boarding gate control system and control method based on super capacitor - Google Patents
Boarding gate control system and control method based on super capacitor Download PDFInfo
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- CN114123464A CN114123464A CN202111373837.7A CN202111373837A CN114123464A CN 114123464 A CN114123464 A CN 114123464A CN 202111373837 A CN202111373837 A CN 202111373837A CN 114123464 A CN114123464 A CN 114123464A
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- 239000003990 capacitor Substances 0.000 title claims abstract description 29
- 238000000034 method Methods 0.000 title claims abstract description 15
- 238000012544 monitoring process Methods 0.000 claims description 31
- 230000002159 abnormal effect Effects 0.000 claims description 3
- 238000007599 discharging Methods 0.000 claims description 3
- 230000007246 mechanism Effects 0.000 description 6
- 230000006835 compression Effects 0.000 description 2
- 238000007906 compression Methods 0.000 description 2
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- 230000008569 process Effects 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
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- 238000006243 chemical reaction Methods 0.000 description 1
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- 238000011161 development Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
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- 239000007788 liquid Substances 0.000 description 1
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J9/00—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting
- H02J9/04—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source
- H02J9/06—Circuit arrangements for emergency or stand-by power supply, e.g. for emergency lighting in which the distribution system is disconnected from the normal source and connected to a standby source with automatic change-over, e.g. UPS systems
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/30—Ground or aircraft-carrier-deck installations for embarking or disembarking passengers
- B64F1/305—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable
- B64F1/3055—Bridges extending between terminal building and aircraft, e.g. telescopic, vertically adjustable with hinged head interface between aircraft and passenger bridge
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/40—Safety devices, e.g. detection of obstructions or end positions
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05F—DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION; CHECKS FOR WINGS; WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05F15/00—Power-operated mechanisms for wings
- E05F15/40—Safety devices, e.g. detection of obstructions or end positions
- E05F15/42—Detection using safety edges
- E05F15/46—Detection using safety edges responsive to changes in electrical capacitance
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/0047—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries with monitoring or indicating devices or circuits
- H02J7/0048—Detection of remaining charge capacity or state of charge [SOC]
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/007—Regulation of charging or discharging current or voltage
- H02J7/00712—Regulation of charging or discharging current or voltage the cycle being controlled or terminated in response to electric parameters
- H02J7/00714—Regulation of charging or discharging current or voltage the cycle being controlled or terminated in response to electric parameters in response to battery charging or discharging current
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/007—Regulation of charging or discharging current or voltage
- H02J7/00712—Regulation of charging or discharging current or voltage the cycle being controlled or terminated in response to electric parameters
- H02J7/007182—Regulation of charging or discharging current or voltage the cycle being controlled or terminated in response to electric parameters in response to battery voltage
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other DC sources, e.g. providing buffering
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J7/00—Circuit arrangements for charging or depolarising batteries or for supplying loads from batteries
- H02J7/34—Parallel operation in networks using both storage and other DC sources, e.g. providing buffering
- H02J7/345—Parallel operation in networks using both storage and other DC sources, e.g. providing buffering using capacitors as storage or buffering devices
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
- H02J2310/00—The network for supplying or distributing electric power characterised by its spatial reach or by the load
- H02J2310/40—The network being an on-board power network, i.e. within a vehicle
- H02J2310/44—The network being an on-board power network, i.e. within a vehicle for aircrafts
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- Engineering & Computer Science (AREA)
- Power Engineering (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Lock And Its Accessories (AREA)
Abstract
The invention belongs to the field of boarding gate actuation control, and particularly relates to a boarding gate control system and a control method based on a storage battery and a super capacitor. The boarding gate control system comprises a boarding gate actuating control module (1), and a gust lock actuator (8), a flight lock actuator (9), a preposition actuator (10), a latch actuator (13) and an opening actuator (14) which are electrically connected with the boarding gate actuating control module (1). The invention has the advantages of high energy utilization rate, reusable energy and good economical efficiency.
Description
Technical Field
The invention belongs to the field of boarding gate actuation control, and particularly relates to a boarding gate control system and a control method based on a storage battery and a super capacitor.
Background
At present, the emergency opening of a boarding door (simultaneously used as an emergency door) of a medium and large civil airliner at home and abroad is realized by an emergency actuator arranged on the boarding door, and the emergency actuator mostly adopts high-pressure gas and oil-gas mixed liquid as energy to release energy to realize the emergency opening. When the door is normally opened, the door serves as a damper, the speed of the door in the movement process is limited on a boarding door (or an emergency door), accidental injury to crew and passengers is avoided, and the structure of a machine body is prevented from being damaged; when the emergency actuator is opened, the emergency actuator serves as a power source for emergency actuation, the actuator is provided with a high-pressure gas storage tank to release energy, and the cabin door is automatically and quickly opened within a limited time.
In the prior art, a patent with application number EP02079650 proposes that after chemical reaction occurs in chemical substances filled in an actuator, high-pressure gas is generated to push a piston rod to extend out to realize emergency actuation, and after the actuator is used once, the chemical substances need to be continuously filled; the patent with the application number of US14119901 provides a mechanical elastic compression device for realizing emergency actuation, and the elastic compression device needs to be reset after being used once; an application number EP16788220 patent provides an aircraft emergency door opening system and a control method, and normal and emergency opening is realized through mechanical structures and switching of different sliding grooves; in patent applications FR2830564 and EP0741073, pneumatic or hydraulic actuators similar to jacks are used, on which fluid storage containers are mounted to effect emergency actuation. The existing scheme has the problems of complex product structure design, non-renewable energy, repeated inflation, easy leakage, poor economy and the like.
Disclosure of Invention
The purpose of the invention is as follows: the boarding gate control system and the boarding gate control method based on the super capacitor are high in energy utilization rate, reusable in energy and good in economical efficiency.
The technical scheme is as follows: the gate emergency power supply system comprises a gate actuating control module 1, and a gust lock actuator 8, a flight lock actuator 9, a pre-positioning actuator 10, a latch actuator 13 and an opening actuator 14 which are electrically connected with the gate actuating control module 1;
the boarding gate actuation control module 1 responds to a normal opening or closing input instruction of the control panel 11 so as to realize on-off logic of the power supply 2 on the controller to the power supply of the actuator;
the boarding gate actuation control module 1 is electrically connected with a charging module 4, and the charging module 4 is respectively electrically connected with a storage battery pack 3 and a super capacitor unit 6; the storage battery pack 3 and the super capacitor unit 6 are respectively and electrically connected with the boarding gate actuation control module 1 through the discharge module 5;
the storage battery pack 3 is used for switching the boarding gate actuation control module 1 to the storage battery pack 3 for supplying power after the power failure of the onboard power supply 2, and is used for meeting the monitoring function of the boarding gate actuation control module 1 on the position state of the boarding gate;
after the gate actuation control module 1 receives the emergency opening input instruction of the control panel 11, the gate actuation control module 1 controls the power-on logic of the power supply 2 on the controller for the gust lock actuator 8, the flight lock actuator 9, the preposition actuator 10 and the latch actuator 13, and controls the super capacitor unit 6 to instantly release large current to the opening actuator 14, so that the gate is opened in an emergency.
Optionally, the gate actuation control module 1 detects current and voltage states of the storage battery 3 and the super capacitor unit 6; and controlling the charging module 4 to charge the storage battery pack 3 and the super capacitor unit 6 according to preset voltage thresholds of the storage battery pack 3 and the super capacitor unit 6.
Optionally, the supercapacitor unit 6 is connected to a capacitance balancing unit 7 to balance the capacity of the supercapacitor module 6, thereby ensuring the time requirement for emergency opening.
Optionally, the gate control system further comprises a sensor assembly 15 connected to the gate actuation control module 1; the sensor assembly 15 is used to monitor the gate position status.
Optionally, the sensor assembly 15 includes an actuator monitoring sensor group, a gate position monitoring sensor group;
the actuator monitoring sensor group is used for monitoring the position state of the actuator and feeding back the position state to the gate actuation control module 1; the boarding gate actuation control module 1 carries out logic judgment according to the position state information of the actuator, and then controls the actuator to carry out on-off control according to a preset logic sequence;
the gate position monitoring sensor group is used for monitoring the position state of the gate and feeding back the position state to the gate actuation control module 1; the gate actuation control module 1 gives gate status indication and abnormal status alarm according to the position status information of the gate.
Optionally, the gust lock actuator 8 and the flight lock actuator 9 are electromagnetic actuators; the prepositioning actuator 10, the latch actuator 13 and the opening actuator 14 are rotary or linear actuators.
Optionally, the boarding gate control system further includes an inverter module 12; the gate actuation control module 1 is respectively connected with the latch actuator 13 and the opening actuator 14 after passing through the inverter module 12;
the inverter module 12 is used for converting the direct current into the alternating current.
On the other hand, the invention provides a boarding gate control method based on a super capacitor, which is based on the boarding gate control system, and the control method comprises the following steps:
when the power supply on the machine is normally powered, the boarding gate actuation control module 1 responds to a normal opening input instruction of the control panel 11; the boarding gate actuation control module 1 controls the flight lock actuator 9, the preposition actuator 10, the latch actuator 13, the opening actuator 14 and the gust lock actuator 8 to actuate in sequence after comprehensive logic judgment according to the actuation state of the actuator fed back by the actuator monitoring sensor group; after the previous actuator acts in place, the boarding gate actuation control module 1 controls the next actuator to actuate;
when the power supply on the machine is normally powered, the boarding gate actuation control module 1 responds to a normal closing input instruction of the control panel 11; the boarding gate actuation control module 1 controls the gust lock actuator 8, the opening actuator 14, the latch actuator 13, the pre-positioning actuator 10 and the flight lock actuator 9 to actuate in sequence after comprehensive logic judgment according to the actuation state of the actuator fed back by the actuator monitoring sensor group; after the previous actuator acts in place, the boarding gate actuation control module 1 controls the next actuator to actuate;
when the power supply is powered off when the airplane is shut down, the boarding gate actuation control module 1 is switched to the storage battery pack 3 to supply power, the boarding gate actuation control module 1 supplies power to the operation panel 12 and the sensor assembly 15, and the boarding gate position state monitoring of the boarding gate actuation control module 1 is met;
when the power supply on the machine is normally powered, the boarding gate actuation control module 1 responds to an emergency opening input instruction of the control panel 11; the boarding gate actuation control module 1 controls the flight lock actuator 9, the preposition actuator 10 and the latch actuator 13 to actuate in sequence after comprehensive logic judgment according to the actuation state of the actuator fed back by the actuator monitoring sensor group; when the latch actuator 13 is actuated in place, the boarding gate actuation control module 1 controls the super capacitor unit 6 to instantly release large current to the opening actuator 14, so that the quick movement of the opening actuator 14 is realized, and the emergency opening time of the boarding gate is ensured; after the starting actuator 14 is actuated in place, the boarding gate actuation control module 1 controls the gust wind lock actuator 8 to actuate; wherein, the flight lock actuator 9, the pre-positioning actuator 10, the latch actuator 13 and the gust lock actuator 8 are powered by an onboard power supply.
The technical effects are as follows: under the development trend of multi-electric aircrafts, the boarding gate control system and the control method applied to a large civil passenger plane in the future have the advantages of high energy utilization rate, reusable energy, good economy and the like, can efficiently meet the control requirements of at least more than 1 boarding gate or emergency gate of the whole aircraft, and have good reliability, safety and expansibility. Therefore, the boarding gate control system and the control method have great economic application value.
The boarding gate control system and the control method thereof are used on a future full-automatic boarding gate actuating system, and have the advantages of light system weight, less maintenance, high safety and the like.
Drawings
Fig. 1 is a schematic diagram of a gate control system based on a super capacitor.
Detailed Description
In this embodiment, as shown in fig. 1, a gate control system based on a super capacitor is provided, which includes a gate actuating control module 1, an onboard power supply 2, a storage battery 3, a charging module 4, a discharging module 5, a super capacitor unit 6, a capacitance balancing unit 7, a gust lock actuator 8, a flight lock actuator 9, a pre-positioning actuator 10, a control panel 11, an inverting module 12, a latch actuator 13, a start actuator 14, and a sensor assembly 15.
The onboard power supply 2 is connected with the gate actuation control module 1, and the gate actuation control module 1 responds to an input instruction of the operation panel 11 when the onboard power supply 2 supplies electric energy.
Gust wind lock actuator 8, flight lock actuator 9, pre-positioning actuator 10, latch actuator 13 and opening actuator 14 set up respectively on the gate gust wind lock mechanism, flight lock mechanism, pre-positioning mechanism, latch mechanism and the parallel opening mechanism that correspond. The gust lock actuator 8, the flight lock actuator 9, the pre-positioning actuator 10, the latch actuator 11 and the opening actuator 14 are driven by a motor and a power output mechanism of the gust lock to lock/unlock, lock/unlock the flight lock, pre-position/unlock a handle, lock/unlock a latch and open/close a boarding gate.
The gate operating control module 1 is connected with the gust wind lock actuator 8, the flight lock actuator 9, the preposition actuator 10, the latch actuator 11 and the opening actuator 14 through the arranged cables,
the gate boarding actuation control module 1 controls the gust lock actuator 8, the flight lock actuator 9, the preposition actuator 10, the latch actuator 11 and the opening actuator 14 to execute actuation according to a specified logic sequence.
The sensor assembly 15 comprises an actuator monitoring sensor group and a boarding gate position monitoring sensor group; the actuator monitoring sensor group is used for monitoring the position state of the actuator and feeding back the position state to the gate actuation control module 1; the gate actuation control module 1 performs logic judgment according to the position state information of the actuator, and then controls the actuator to perform on-off control according to a preset logic sequence. The gate position monitoring sensor group is used for monitoring the position state of the gate and feeding back the position state to the gate actuation control module 1; the gate actuation control module 1 gives gate status indication and abnormal status alarm according to the position status information of the gate.
The onboard power supply 2 provides electric energy for the boarding gate actuation control module 1, the boarding gate actuation control module 1 charges the storage battery pack 3 and the super capacitor unit 6 through the charging module 4, and when the charging electric quantity of the storage battery pack 3 and the super capacitor unit 6 reaches a preset threshold value, the boarding gate actuation control module 1 stops charging the storage battery pack 3 and the super capacitor unit.
The boarding gate actuation control module 1 is connected with the storage battery pack 3 through a set cable, and after the power failure of the onboard power supply 2, the storage battery pack 3 starts to discharge through the discharge module 5 to provide electric energy for the boarding gate actuation control module 1, so that the boarding gate actuation control module 1 and a system can continuously and normally monitor functions.
The state of the sensors in the sensor assembly 15 determines the logical sequence of actuation control of the gust lock actuator 8, the flight lock actuator 9, the pre-positioning actuator 10, the latch actuator 11 and the opening actuator 14.
When the power supply on the machine is normally powered, the boarding gate actuation control module 1 responds to a normal opening input instruction of the control panel 11; the boarding gate actuation control module 1 controls the flight lock actuator 9, the preposition actuator 10, the latch actuator 13, the opening actuator 14 and the gust lock actuator 8 to actuate in sequence after comprehensive logic judgment according to the actuation state of the actuator fed back by the actuator monitoring sensor group; after the last actuator acts in place, the boarding gate actuation control module 1 controls the next actuator to actuate.
When the power supply on the machine is normally powered, the boarding gate actuation control module 1 responds to a normal closing input instruction of the control panel 11; the boarding gate actuation control module 1 controls the gust lock actuator 8, the opening actuator 14, the latch actuator 13, the pre-positioning actuator 10 and the flight lock actuator 9 to actuate in sequence after comprehensive logic judgment according to the actuation state of the actuator fed back by the actuator monitoring sensor group; after the last actuator acts in place, the boarding gate actuation control module 1 controls the next actuator to actuate.
When the power supply is powered off when the boarding gate is shut down, the boarding gate actuation control module 1 is switched to the storage battery pack 3 to supply power, the boarding gate actuation control module 1 supplies power to the operation panel 11 and the sensor assembly 15, and the boarding gate actuation control module 1 can monitor the position state of the boarding gate.
When the gate actuation control module 1 responds to the emergency opening input command of the control panel 11, the gate actuation control module 1 controls the flight lock actuator 9, the pre-positioning actuator 13 and the latch actuator 14 to execute the actions of unlocking, pre-positioning release and latch release of the flight lock according to a preset logic sequence and by combining the signals of the sensor assembly 15; after the gate actuation control module 1 receives the signal of releasing the latch in place in the sensor assembly 15, the gate actuation control module 1 controls the discharge module 5 through a cable to enable the supercapacitor unit 6 to discharge rapidly and instantly to generate a large current to provide the current required by rapid emergency opening for the opening actuator 14. Meanwhile, the super capacitor unit 6 is connected with the capacitance balancing unit 7 to balance the capacity of the super capacitor module 6, so that the time requirement of emergency opening is ensured.
Furthermore, the capacity of the storage battery pack 3 can be adjusted, when the storage battery pack 3 is powered off from the onboard power supply 2, the electric energy is provided for the boarding gate actuation control module 1 and each actuator through the discharging module 5, and the boarding gate actuation control module 1 and the system can be guaranteed to continuously and normally work. When the onboard power supply 2 fails and is powered down, the gate actuation control module 1 responds to an emergency opening input instruction of the control panel 10 under the condition that the storage battery pack 3 provides electric energy, the gate actuation control module 1 controls the flight lock actuator 9, the preposition actuator 13 and the latch actuator 14 to execute flight lock unlocking, preposition release and latch release actions according to a preset logic sequence and in combination with a signal of the sensor assembly 15, after the gate actuation control module 1 receives an unlocking latch in-place signal in the sensor assembly 15, the gate actuation control module 1 controls the discharge module 5 through a cable to enable the supercapacitor unit 6 to discharge fast to generate a large current instantly, and the gate actuation control module 1 transmits the large current to the opening actuator 14 to enable the gate actuation control module to operate fast, thereby realizing the emergency opening of the gate.
In addition, in the practical application process, according to the number of the gate control systems corresponding to the number of the gates on the practical airplane, the gate control systems normally obtain electric energy through the on-board power supply 2, after the system is powered on to work, the gate actuation control module 1 acquires the state of the sensor in the sensor assembly 15 in real time, and meanwhile, the gate actuation control module 1 receives a normal opening instruction input by the control panel 11 in real time; after receiving the instruction, the boarding gate actuation control module 1 controls the gust lock actuator 8, the flight lock actuator 9, the preposition actuator 10, the latch actuator 13 and the opening actuator 14 to actuate according to a preset logic sequence by combining with the state information of the sensor in the sensor assembly 15, so that the locking/unlocking of the gust lock, the locking/unlocking of the flight lock, the locking/unlocking of the latching/unlocking and the opening/closing of the boarding gate are realized.
In this embodiment, the gust lock actuator 8 and the flight lock actuator 9 are electromagnetic actuators; the prepositioning actuator 10, the latch actuator 13 and the opening actuator 14 are rotary or linear actuators. The type of power supplied to the latch actuator 13 and the opening actuator 14 may be either ac or dc.
Claims (8)
1. A boarding gate control system based on a super capacitor is characterized by comprising a boarding gate actuating control module (1), and a gust lock actuator (8), a flight lock actuator (9), a pre-positioning actuator (10), a latch actuator (13) and an opening actuator (14) which are electrically connected with the boarding gate actuating control module (1);
the boarding gate actuation control module (1) responds to a normal opening or closing input instruction of the control panel (11) so as to realize on-off logic of a power supply (2) on the controller to power supplies of actuators;
the gate actuation control module (1) is electrically connected with the charging module (4), and the charging module (4) is respectively electrically connected with the storage battery pack (3) and the super capacitor unit (6); the storage battery pack (3) and the super capacitor unit (6) are respectively and electrically connected with the boarding gate actuation control module (1) through the discharging module (5);
the storage battery pack (3) is used for switching the boarding gate actuation control module (1) to the storage battery pack (3) for supplying power after the power supply (2) on the boarding gate is powered off and is used for monitoring the position state of the boarding gate by the boarding gate actuation control module (1);
after the boarding gate actuation control module (1) receives an emergency opening input instruction of the control panel (11), the boarding gate actuation control module (1) controls on-off logic of the power supply (2) on the machine to the gust lock actuator (8), the flight lock actuator (9), the pre-positioning actuator (10) and the latch actuator (13), and controls the super capacitor unit (6) to instantly release large current for the opening actuator (14), so that emergency opening of the boarding gate is realized.
2. The gate control system according to claim 1, characterized in that the gate actuation control module (1) detects the current and voltage status of the battery pack (3), the supercapacitor unit (6); and controlling the charging module (4) to charge the storage battery pack (3) and the super capacitor unit (6) according to preset voltage thresholds of the storage battery pack (3) and the super capacitor unit (6).
3. Gate control system according to claim 1, characterized in that a supercapacitor unit (6) is connected to a capacitance balancing unit (7) to balance the capacity of the supercapacitor unit (6) to guarantee the time requirement for emergency gate opening.
4. The gate control system of claim 1, further comprising a sensor assembly (15) coupled to the gate actuation control module (1); the sensor assembly (15) is used for monitoring the position state of the boarding gate.
5. Gate control system according to claim 4, characterized in that the sensor assembly (15) comprises an actuator monitoring sensor group, a gate position monitoring sensor group;
the actuator monitoring sensor group is used for monitoring the position state of the actuator and feeding back the position state to the boarding gate actuation control module (1); the boarding gate actuation control module (1) performs logic judgment according to the position state information of the actuator, and then controls the actuator to perform on-off control according to a preset logic sequence;
the gate position monitoring sensor group is used for monitoring the position state of the gate and feeding back the position state to the gate actuation control module (1); the gate actuation control module (1) gives gate state indication and abnormal state alarm according to the position state information of the gate.
6. The gate control system according to claim 1, characterized in that the gust lock actuator (8) and the flight lock actuator (9) are electromagnetic actuators; the pre-positioning actuator (10), the latching actuator (13) and the opening actuator (14) are rotary or linear actuators.
7. The gate control system of claim 1, further comprising an inverter module (12); the gate actuation control module (1) is electrically connected with the latch actuator (13) and the opening actuator (14) respectively after passing through the inverter module (12);
and the inverter module (12) is used for converting the direct current into the alternating current.
8. A gate control method based on a super capacitor, the gate control system based on any one of claims 1 to 7, the control method comprising:
when the power supply on the machine is normally powered, the boarding gate actuation control module (1) responds to a normal opening input instruction of the control panel (11); the boarding gate actuation control module (1) controls the flight lock actuator (9), the pre-positioning actuator (10), the latch actuator (13), the unlocking actuator (14) and the gust lock actuator (8) to actuate in sequence after comprehensive logic judgment according to the position state of the actuator fed back by the actuator monitoring sensor group; after the previous actuator acts in place, the boarding gate actuation control module (1) controls the next actuator to actuate;
when the power supply on the machine is normally powered, the boarding gate actuation control module (1) responds to a normal closing input instruction of the control panel (11); the boarding gate actuation control module (1) controls the gust wind lock actuator (8), the opening actuator (14), the latch actuator (13), the pre-positioning actuator (10) and the flight lock actuator (9) to actuate in sequence after comprehensive logic judgment according to the position state of the actuator fed back by the actuator monitoring sensor group; after the previous actuator acts in place, the boarding gate actuation control module (1) controls the next actuator to actuate;
when a power supply is powered off when the machine is powered on, the boarding gate actuation control module (1) is switched to the storage battery pack (3) for supplying power, and the boarding gate actuation control module (1) supplies power to the control panel (12) and the sensor assembly (15), so that the monitoring of the boarding gate position state by the boarding gate actuation control module (1) is met;
when the power supply on the machine is normally powered, the boarding gate actuation control module (1) responds to an emergency opening input instruction of the control panel (11); the boarding gate actuation control module (1) controls the flight lock actuator (9), the preposition actuator (10) and the latch actuator (13) to actuate in sequence after comprehensive logic judgment according to the position state of the actuator fed back by the actuator monitoring sensor group; when the latch actuator (13) is actuated in place, the boarding gate actuation control module (1) controls the super capacitor unit (6) to instantly release large current to the opening actuator (14), so that the high-speed movement of the opening actuator (14) is realized, and the emergency opening time of the boarding gate is ensured; after the starting actuator (14) is actuated in place, the boarding gate actuation control module (1) controls the gust wind lock actuator (8) to actuate; wherein, the flight lock actuator (9), the pre-positioning actuator (10), the latch actuator (13) and the gust lock actuator (8) are powered by an onboard power supply.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111373837.7A CN114123464A (en) | 2021-11-18 | 2021-11-18 | Boarding gate control system and control method based on super capacitor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111373837.7A CN114123464A (en) | 2021-11-18 | 2021-11-18 | Boarding gate control system and control method based on super capacitor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN114123464A true CN114123464A (en) | 2022-03-01 |
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Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1942907A (en) * | 2004-02-27 | 2007-04-04 | 克里斯托弗·亚德利 | Improvements in aircraft doors |
| CN102343826A (en) * | 2011-07-18 | 2012-02-08 | 陈昌志 | New energy electric automobile |
| WO2016163201A1 (en) * | 2015-04-07 | 2016-10-13 | 三菱電機株式会社 | Power conversion device |
| US20190263507A1 (en) * | 2018-02-28 | 2019-08-29 | Airbus Operations Limited | System for moving an aircraft door |
| CN111583481A (en) * | 2020-04-21 | 2020-08-25 | 中国商用飞机有限责任公司 | Access control system for cockpit door of aircraft and aircraft |
| CN111593962A (en) * | 2020-06-04 | 2020-08-28 | 中国商用飞机有限责任公司 | Airplane cabin door control device and control method |
| CN212243777U (en) * | 2020-04-30 | 2020-12-29 | 庆安集团有限公司 | Cabin door alarm device |
-
2021
- 2021-11-18 CN CN202111373837.7A patent/CN114123464A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1942907A (en) * | 2004-02-27 | 2007-04-04 | 克里斯托弗·亚德利 | Improvements in aircraft doors |
| CN102343826A (en) * | 2011-07-18 | 2012-02-08 | 陈昌志 | New energy electric automobile |
| WO2016163201A1 (en) * | 2015-04-07 | 2016-10-13 | 三菱電機株式会社 | Power conversion device |
| US20190263507A1 (en) * | 2018-02-28 | 2019-08-29 | Airbus Operations Limited | System for moving an aircraft door |
| CN111583481A (en) * | 2020-04-21 | 2020-08-25 | 中国商用飞机有限责任公司 | Access control system for cockpit door of aircraft and aircraft |
| CN212243777U (en) * | 2020-04-30 | 2020-12-29 | 庆安集团有限公司 | Cabin door alarm device |
| CN111593962A (en) * | 2020-06-04 | 2020-08-28 | 中国商用飞机有限责任公司 | Airplane cabin door control device and control method |
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