CN113719215B - Method and device for operating cabin door - Google Patents
Method and device for operating cabin door Download PDFInfo
- Publication number
- CN113719215B CN113719215B CN202111066642.8A CN202111066642A CN113719215B CN 113719215 B CN113719215 B CN 113719215B CN 202111066642 A CN202111066642 A CN 202111066642A CN 113719215 B CN113719215 B CN 113719215B
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- actuator
- signal
- lock
- cabin door
- sensor
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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
- E05F15/70—Power-operated mechanisms for wings with automatic actuation
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B17/00—Accessories in connection with locks
- E05B17/22—Means for operating or controlling lock or fastening device accessories, i.e. other than the fastening members, e.g. switches, indicators
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
- E05B47/0001—Operating or controlling locks or other fastening devices by electric or magnetic means with electric actuators; Constructional features thereof
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B65/00—Locks or fastenings for special use
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
- E05B2047/0048—Circuits, feeding, monitoring
- E05B2047/0067—Monitoring
- E05B2047/0069—Monitoring bolt position
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
- E05Y2900/502—Application of doors, windows, wings or fittings thereof for vehicles for aircraft
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- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05Y—INDEXING SCHEME RELATING TO HINGES OR OTHER SUSPENSION DEVICES FOR DOORS, WINDOWS OR WINGS AND DEVICES FOR MOVING WINGS INTO OPEN OR CLOSED POSITION, CHECKS FOR WINGS AND WING FITTINGS NOT OTHERWISE PROVIDED FOR, CONCERNED WITH THE FUNCTIONING OF THE WING
- E05Y2900/00—Application of doors, windows, wings or fittings thereof
- E05Y2900/50—Application of doors, windows, wings or fittings thereof for vehicles
- E05Y2900/53—Application of doors, windows, wings or fittings thereof for vehicles characterised by the type of wing
- E05Y2900/531—Doors
Abstract
The application discloses a method and a device for operating a cabin door, and belongs to the technical field of cabin doors. The method comprises the steps that when a display operation unit is detected to receive a door opening signal and a cabin door locking signal is received, a first control instruction is sent to a latch actuator; when a leaving signal sent by a lock sensor is received, a cabin door unlocking signal is sent to a display operation unit; when a leaving signal sent by a pressurization prevention door sensor is received, whether an unlocking in-place signal sent by a lock sensor is received or not is detected; when receiving the unlocking in-place signal, sending a cabin door unlocking in-place signal to the display operation unit; when receiving an unlatching signal sent by the latch sensor, sending a cabin door unlatching signal to the display operation unit; and when receiving a lifting-in-place signal sent by the lifting-in-place sensor, sending a third control instruction to the opening actuator, and sending a cabin door opening signal to the display operation unit. The monitoring and centralized management of the state of the airplane cabin door are realized.
Description
Technical Field
The invention belongs to the technical field of cabin doors, and particularly relates to a method and a device for operating a cabin door.
Background
At present, a cabin door actuating system of a civil airplane is mainly an electric actuating system, partial actions are completed by manually operating a handle, a switch is triggered at certain positions by the handle in an electric driving part to drive an actuator to actuate, the mechanical operation is more, and full-automatic driving is not realized.
With the development of large civil airliners, the number and the types of cabin doors are increased, the weight and the size are increased, and if a control technology with more mechanical operations is still adopted, the control technology is labor-consuming, low in efficiency, low in safety and low in reliability.
Disclosure of Invention
In order to solve the problems of labor waste, low efficiency, low safety and low reliability caused by the adoption of a control technology with more mechanical operations in the related art, the application provides a method and a device for operating a cabin door, and the technical scheme is as follows:
in a first aspect, there is provided a device for operating a door, comprising: a controller unit, a display operation unit, a latch actuator, an opening actuator, a lock shaft, a lock sensor, a pressure-increasing preventive door sensor, a latch sensor, and a lift-in-place sensor,
the controller unit is electrically connected with the display operation unit, the latch actuator, the opening actuator, the lock sensor, the pressure-increasing preventive door sensor, the latch sensor, and the lift-to-position sensor, respectively, each sensor being provided at a position in which the corresponding mechanism is in place, the controller unit being configured to:
when the display operation unit is detected to receive a door opening signal, detecting whether a cabin door locking signal sent by the lock sensor is received;
when the cabin door locking signal is received, the latching actuator is electrified, and a first control command is sent to the latching actuator, wherein the first control command is used for indicating the latching actuator to rotate forwards and driving the lock shaft to rotate;
when a leaving signal sent by the lock sensor is received, a cabin door unlocking signal is sent to the display operation unit, and the cabin door unlocking signal is used for indicating the display operation unit to control a cabin door unlocking indicator lamp to flicker;
when a leaving signal sent by the pressurization prevention door sensor is received, whether an unlocking in-place signal sent by the lock sensor is received or not is detected, and the unlocking in-place signal is used for indicating that the lock shaft rotates to a preset unlocking position;
when the unlocking in-place signal is received, a cabin door unlocking in-place signal is sent to the display operation unit, and the cabin door unlocking in-place signal is used for indicating the display operation unit to control a cabin door unlocking indicator lamp to be on;
when an unlocking signal sent by a latch sensor is received, sending a cabin door unlocking signal to the display operation unit, wherein the cabin door unlocking signal is used for indicating the display operation unit to control a cabin door latching indicator lamp to be turned off, and the unlocking signal is used for indicating the lock shaft to rotate and driving the latch shaft to move;
when receiving a lifting in-place signal sent by a lifting in-place sensor, the opening actuator is electrified, a second control instruction is sent to the opening actuator, a cabin door opening signal is sent to the display operation unit until the cabin door is opened to the maximum position, the second control instruction is used for indicating the opening actuator to rotate positively, the lifting in-place signal is used for indicating the lock shaft to rotate and driving the cabin door to execute lifting operation, and the cabin door opening operation is completed.
Optionally, the apparatus further comprises: gust wind lock sensor and gust wind lock actuator, the controller unit respectively with gust wind lock sensor and gust wind lock actuator electricity are connected, the controller unit still is used for:
when the display operation unit is detected to receive a door closing signal, the gust lock sensor is powered on, and whether a gust lock locking signal sent by the gust lock sensor is received or not is detected;
when the locking signal of the wind array lock is received, electrifying the wind array lock actuator, and sending a third control instruction to the wind array lock actuator, wherein the third control instruction is used for indicating the wind array lock actuator to control the unlocking of the wind array lock;
when a gust lock unlocking in-place signal sent by the gust lock sensor is received, the gust lock actuator is powered off, the opening actuator is powered on, and a fourth control instruction is sent to the opening actuator and used for indicating the opening actuator to rotate reversely and controlling the cabin door to be closed;
when a cabin door in-position lifting signal sent by the in-position lifting sensor is received, the opening actuator is powered off, the latching actuator is powered on, and a fifth control instruction is sent to the latching actuator, wherein the fifth control instruction is used for indicating the latching actuator to reversely rotate and controlling the cabin door to sink;
when a cabin door latching-in-place signal sent by the latch sensor and a pressurization prevention door closing signal sent by the pressurization prevention door sensor are received, whether a latching-in-place signal sent by the lock sensor is received or not is detected;
and when receiving a locking in-place signal sent by the lock sensor, stopping supplying power to the latch actuator and sending a cabin door locking signal to the display operation unit, wherein the cabin door locking signal is used for indicating the display operation unit to control a cabin door locking and closing indicator lamp to be turned on.
Optionally, the apparatus further comprises: flight lock actuator, pre-positioning actuator and pre-positioning sensor, the controller unit respectively with flight lock actuator, pre-positioning actuator and pre-positioning sensor electricity are connected, the controller unit still is used for:
when the speed of the airplane is detected to be lower than the preset speed and a wheel load signal is received, powering off the flight lock actuator and sending a sixth control command to the flight lock actuator, wherein the sixth control command is used for indicating the flight lock actuator to control a flight lock to be disengaged from the lock shaft;
when the landing airspeed of the airplane is detected to be 0, the wheel load signal is effective, and the display operation unit does not receive the emergency signal, whether the display operation unit receives the preposition releasing signal is detected;
when the display operation unit is detected to receive the pre-positioning releasing signal, electrifying the pre-positioning actuator, and sending a seventh control instruction to the pre-positioning actuator, wherein the seventh control instruction is used for instructing the pre-positioning actuator to perform reverse operation so as to enable the pre-positioning mechanism to move towards a first preset position;
the detection is in advance the position actuator receives when the signal that targets in place that the position sensor sent gives the position actuator outage in advance, and to the position actuator sends eighth control command in advance, the signal that targets in place is used for instructing the position mechanism reachs in advance first preset position, eighth control command is used for instructing the position actuator stops to carry out the reversal operation in advance.
In a second aspect, there is provided a method of operating a door for a device for operating a door according to the first aspect, the method comprising:
when the display operation unit is detected to receive the door opening signal, detecting whether a cabin door locking signal sent by a locking sensor is received;
when the cabin door locking signal is received, energizing a latch actuator, and sending a first control instruction to the latch actuator, wherein the first control instruction is used for indicating the latch actuator to rotate forwards and driving the lock shaft to rotate;
when a leaving signal sent by a lock sensor is received, a cabin door unlocking signal is sent to the display operation unit, and the cabin door unlocking signal is used for indicating the display operation unit to control a cabin door unlocking indicator lamp to flicker;
when a leaving signal sent by a pressurization prevention door sensor is received, whether an unlocking in-place signal sent by a lock sensor is received or not is detected, and the unlocking in-place signal is used for indicating that the lock shaft rotates to a preset unlocking position;
when the unlocking in-place signal is received, a cabin door unlocking in-place signal is sent to the display operation unit, and the cabin door unlocking in-place signal is used for indicating the display operation unit to control a cabin door unlocking indicator lamp to be on;
when an unlatching signal sent by a latch sensor is received, sending a cabin door unlatching signal to the display operation unit, wherein the cabin door unlatching signal is used for indicating the display operation unit to control a cabin door latching indicator lamp to be turned off, and the unlatching signal is used for indicating the lock shaft to rotate and driving the latch shaft to move;
when receiving a lifting in-place signal sent by a lifting in-place sensor, the opening actuator is electrified, a second control instruction is sent to the opening actuator, a cabin door opening signal is sent to the display operation unit until the cabin door is opened to the maximum position, the second control instruction is used for indicating the opening actuator to rotate positively, the lifting in-place signal is used for indicating the lock shaft to rotate and drive the cabin door to execute lifting operation, and the cabin door opening operation is completed.
Optionally, the method further comprises:
when the display operation unit is detected to receive a door closing signal, the gust lock sensor is electrified, and whether a gust lock locking signal sent by the gust lock sensor is received or not is detected;
when the locking signal of the wind array lock is received, electrifying the wind array lock actuator, and sending a third control instruction to the wind array lock actuator, wherein the third control instruction is used for indicating the wind array lock actuator to control the unlocking of the wind array lock;
when a gust lock unlocking in-place signal sent by the gust lock sensor is received, the gust lock actuator is powered off, the opening actuator is powered on, and a fourth control instruction is sent to the opening actuator, wherein the fourth control instruction is used for indicating the opening actuator to reversely rotate and controlling the cabin door to be closed;
when a cabin door in-position lifting signal sent by the in-position lifting sensor is received, the opening actuator is powered off, the latching actuator is powered on, and a fifth control instruction is sent to the latching actuator, wherein the fifth control instruction is used for indicating the latching actuator to rotate reversely and controlling the cabin door to sink;
when a cabin door latching in-place signal sent by the latch sensor and a pressurization prevention door closing signal sent by the pressurization prevention door sensor are received, detecting whether a latching in-place signal sent by a lock sensor is received;
and when receiving a locking in-place signal sent by the lock sensor, stopping supplying power to the latch actuator and sending a cabin door locking signal to the display operation unit, wherein the cabin door locking signal is used for indicating the display operation unit to control a cabin door locking and closing indicator lamp to be turned on.
Optionally, the method further comprises:
when the speed of the airplane is detected to be lower than the preset speed and a wheel load signal is received, powering off a flight lock actuator, and sending a sixth control instruction to the flight lock actuator, wherein the sixth control instruction is used for indicating the flight lock actuator to control a flight lock to be disengaged from a lock shaft;
when the landing airspeed of the airplane is detected to be 0, the wheel load signal is effective, and the display operation unit does not receive the emergency signal, whether the display operation unit receives a pre-positioning releasing signal or not is detected;
when the display operation unit is detected to receive the pre-positioning release signal, electrifying a pre-positioning actuator, and sending a seventh control instruction to the pre-positioning actuator, wherein the seventh control instruction is used for instructing the pre-positioning actuator to perform reverse operation so as to enable the pre-positioning mechanism to move towards a first preset position;
when detecting the pilot actuator receives the signal that targets in place that the sensor sent in advance, give the pilot actuator outage, and to pilot actuator sends eighth control command, the signal that targets in place is used for instructing the pilot mechanism reachs first preset position, eighth control command is used for instructing the pilot actuator stops to carry out the reversal operation.
Optionally, the method further comprises:
when the display operation unit is detected to receive the pre-positioning signal, the pre-positioning actuator is electrified, a ninth control instruction is sent to the pre-positioning actuator, and the ninth control instruction is used for indicating the pre-positioning actuator to push the pre-positioning mechanism into the floor clamp for locking.
Optionally, the method further comprises:
and when detecting whether the speed of the airplane reaches the preset speed or not, electrifying the flight lock actuator, and sending a tenth control instruction to the flight lock actuator, wherein the tenth control instruction is used for indicating the flight lock actuator to control the flight lock to be locked.
Optionally, the method further comprises:
when the display operation unit is detected to receive an emergency signal, detecting whether the display operation unit receives a door opening signal;
when the display operation unit is detected to receive a door opening signal, executing the cabin door opening operation;
sending an eleventh control instruction to the opening actuator, wherein the eleventh control instruction is used for instructing the opening actuator to start an emergency actuating device so as to open and lock the cabin door to the maximum position;
when a first complete opening signal sent by the gust lock sensor is received, the opening actuator is stopped to be powered on, and a second complete opening signal is sent to the display operation unit, wherein the first complete opening signal is used for indicating the cabin door to be opened and locked to the maximum position, and the second complete opening signal is used for indicating the display operation unit to control a complete opening signal lamp to be turned on.
The method and the device for operating the cabin door can realize automatic operation of the boarding door, can effectively reduce physical strength paid by operators for unlocking and lifting the boarding door in the face of heavier and heavier boarding doors of large-scale wide passenger planes, reduce the risk of taking people out of an airplane when the cabin door is opened, have a simple and clear operation interface, have clear cabin door state indication, effectively realize mechanism blanking, and merge a cabin door monitoring and actuation signal detection unit to better realize state monitoring and centralized management of the cabin door of the airplane.
Drawings
Fig. 1 is a schematic structural diagram of an apparatus for operating a door according to the present application.
Detailed Description
The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the flowchart of the method of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.
In the related art, the cabin door actuating system is partially electrically actuated, full-automatic driving cannot be realized, partial actions are completed by manually operating a handle, and a switch is triggered at certain positions by the handle in the electric driving part to drive an actuator to actuate. Some methods do not integrate the actuation control unit and the cabin door control unit, and occupy the corresponding space. For the above reasons, there is a need for improvements in the prior art to facilitate more convenient operation, to provide a higher degree of integration, to reduce mechanical operations, and to reduce personnel burden.
Fig. 1 shows an apparatus for operating a door according to an embodiment of the present invention, including: a controller unit 3, a display operation unit 4, a latch actuator 2, an opening actuator 11, a lock shaft 12, a lock sensor 100, a pressure-increasing preventive door sensor 200, a latch sensor 300, and a lift-to-position sensor 400,
the controller unit 3 is electrically connected with the display operation unit 4, the latch actuator 2, the opening actuator 11, the lock sensor 100, the pressure-increasing preventive door sensor 200, the latch sensor 300, and the lift-to-place sensor 400, respectively, the controller unit and the display operation unit are disposed in the total control area, each sensor is disposed at the in-place position of the corresponding mechanism, and the controller unit 3 is used for:
when detecting that the display operation unit 4 receives the door opening signal, detecting whether a door locking signal sent by the lock sensor 100 is received; the display operation unit has a display function and an operation function and is a man-machine interaction interface, the controller unit sends corresponding signals to the panel for display after judging through sensor signals, and the operation interface is used for manually inputting instructions;
when a cabin door locking signal is received, the latching actuator 2 is powered on, and a first control instruction is sent to the latching actuator 2, wherein the first control instruction is used for indicating the latching actuator 2 to rotate forwards and driving the lock shaft 12 to rotate;
when a leaving signal sent by the lock sensor 100 is received, a cabin door unlocking signal is sent to the display operation unit 4, and the cabin door unlocking signal is used for indicating the display operation unit 4 to control the cabin door unlocking indicator lamp to flash; the cabin door unlocking operation is completed;
when a leaving signal sent by the pressurization prevention door sensor 200 is received, whether an unlocking in-place signal sent by the lock sensor 100 is received or not is detected, and the unlocking in-place signal is used for indicating that the lock shaft 12 rotates to a preset unlocking position;
when the unlocking in-place signal is received, a cabin door unlocking in-place signal is sent to the display operation unit 4, and the cabin door unlocking in-place signal is used for indicating the display operation unit 4 to control a cabin door unlocking indicator lamp to be on;
when receiving an unlatching signal sent by the latch sensor 300, sending a cabin door unlatching signal to the display operation unit 4, wherein the cabin door unlatching signal is used for indicating the display operation unit 4 to control a cabin door latching indicator lamp to be turned off, and the unlatching signal is used for indicating the lock shaft 12 to rotate and driving the latch shaft 13 to move;
when receiving the in-place lifting signal sent by the in-place lifting sensor 400, the opening actuator 11 is powered on, a second control instruction is sent to the opening actuator 11, and a cabin door opening signal is sent to the display operation unit 4 until the cabin door 8 is opened to the maximum position, the lock hook on the cabin door hinge arm 9 can enter the gust lock hook, and the cabin door is locked at the maximum position. The second control instruction is used for indicating the opening actuator to rotate positively, and the lifting in-place signal is used for indicating the lock shaft to rotate and driving the cabin door to execute lifting operation, so that the cabin door opening operation is completed.
The application provides a pair of device of operation hatch door, can realize automatic hatch door opening operation, in the face of the increasingly heavy gate of boarding of large-scale wide body passenger plane, the device can effectively alleviate operating personnel unblock, promote the physical power that the gate of boarding paid out, reduce the risk of taking the people out of the aircraft when opening the hatch door, operation interface is simple, it is clear, the hatch door state instruction is clear and definite, effectively realized the mechanism and blank, with the hatch door control with actuate the signal detection unit and merge, realize the state control and the centralized management to the aircraft hatch door better.
As shown in fig. 1, the apparatus further comprises: gust lock sensor 500 and gust lock actuator 10 realize that the hatch door locks the shutdown function, and wherein, controller unit 3 is connected with gust lock sensor 500 and gust lock actuator 10 electricity respectively, and controller unit 3 still is used for:
when detecting that the display operation unit 4 receives a door closing signal, powering on the gust lock sensor 500 to detect whether a gust lock locking signal sent by the gust lock sensor 500 is received;
when a locking signal of the gust lock is received, electrifying the gust lock actuator 10, and sending a third control instruction to the gust lock actuator 10, wherein the third control instruction is used for instructing the gust lock actuator 10 to control the gust lock to unlock;
when a gust lock unlocking in-place signal sent by the gust lock sensor 500 is received, the power of the gust lock actuator 10 is cut off, the power of the opening actuator 11 is supplied, and a fourth control instruction is sent to the opening actuator 11 and used for indicating the opening actuator 11 to rotate reversely and controlling the cabin door 8 to be closed;
when a cabin door in-place lifting signal sent by the in-place lifting sensor 400 is received, the opening actuator 11 is powered off, the latching actuator 2 is powered on, and a fifth control instruction is sent to the latching actuator 2, wherein the fifth control instruction is used for indicating the latching actuator 2 to reversely rotate and controlling the cabin door to sink;
detecting whether the door locking in-place signal transmitted by the lock sensor 100 is received or not when the door locking in-place signal transmitted by the latch sensor 300 and the door closing signal transmitted by the door pressurization prevention sensor 200 are received;
when receiving the lock in-place signal sent by the lock sensor 100, the power supply to the latch actuator 2 is stopped, and a door lock signal is sent to the display operation unit 4, where the door lock signal is used to instruct the display operation unit 4 to control the door lock close indicator light to be on.
Further, the apparatus further comprises: flight lock actuator 5, the actuator of position 6 and the sensor 700 of position in advance, controller unit 3 is connected with flight lock actuator 5, the actuator of position 6 and the sensor 700 electricity in advance respectively, and controller unit 3 still is used for:
when the speed of the airplane is detected to be lower than the preset speed and the wheel load signal is received, the power is cut off for the flight lock actuator 5, and a sixth control instruction is sent to the flight lock actuator 5 and used for instructing the flight lock actuator 5 to control the flight lock to be separated from the lock shaft 12; the state of the flight lock sensor 600 is switched, and the handle can move freely; typically, the preset speed is 60 knots.
When the landing airspeed of the airplane is detected to be 0, the wheel load signal is effective, and the display operation unit 4 does not receive the emergency signal, whether the display operation unit 4 receives the disalignment signal is detected, wherein it needs to be stated that three conditions that the landing airspeed of the airplane is 0, the wheel load signal is effective, and the display operation unit 4 does not receive the emergency signal are simultaneously met;
when the display operation unit 4 is detected to receive the pre-positioning releasing signal, the pre-positioning actuator 6 is electrified, and a seventh control instruction is sent to the pre-positioning actuator 6, wherein the seventh control instruction is used for instructing the pre-positioning actuator 6 to perform reverse rotation operation so as to enable the pre-positioning mechanism to move towards the first preset position;
when the in-place signal sent by the pre-position sensor 700 is received by the pre-position actuator 6, the power of the pre-position actuator 6 is cut off, an eighth control instruction is sent to the pre-position actuator 6, the in-place signal is used for indicating the pre-position mechanism to reach a first preset position, and the eighth control instruction is used for indicating the pre-position actuator 6 to stop executing the reverse rotation operation, so that the function of removing the pre-position operation is realized. Fig. 1 shows a door frame 7.
The application provides a pair of device of operation hatch door, can realize the automatic operation gate of boarding, in the face of the increasingly heavy gate of boarding of large-scale wide body passenger plane, the device can effectively alleviate operating personnel unblock, promote the physical power that the gate of boarding paid out, reduce the risk of taking the people out of the aircraft when opening the hatch door, operation interface is simple, it is clear, the hatch door state instruction is clear and definite, effectively realized the mechanism and blank, with the hatch door control with actuate the signal detection unit and merge, realize the state control and the centralized management to the aircraft hatch door better.
The present application also provides a method of operating a door for an apparatus for operating a door as shown in figure 1, the method comprising:
when the display operation unit is detected to receive the door opening signal, detecting whether a cabin door locking signal sent by a locking sensor is received;
when a cabin door locking signal is received, the latch actuator is electrified, and a first control instruction is sent to the latch actuator, wherein the first control instruction is used for indicating the latch actuator to rotate positively and driving the lock shaft to rotate;
when a leaving signal sent by a lock sensor is received, a cabin door unlocking signal is sent to a display operation unit, and the cabin door unlocking signal is used for indicating the display operation unit to control a cabin door unlocking indicator lamp to flicker; completing the automatic unlocking operation of the cabin door;
when a leaving signal sent by a pressurization prevention door sensor is received, whether an unlocking in-place signal sent by a lock sensor is received or not is detected, and the unlocking in-place signal is used for indicating that a lock shaft rotates to a preset unlocking position;
when the unlocking in-place signal is received, a cabin door unlocking in-place signal is sent to the display operation unit, and the cabin door unlocking in-place signal is used for indicating the display operation unit to control the cabin door unlocking indicator lamp to be on; the cabin door is unlocked in place;
when an unlatching signal sent by a latch sensor is received, a cabin door unlatching signal is sent to a display operation unit, the cabin door unlatching signal is used for indicating the display operation unit to control a latch indicator lamp on a cabin door to be turned off, and the unlatching signal is used for indicating a lock shaft to rotate and driving the latch shaft to move;
when a lifting in-place signal sent by a lifting in-place sensor is received, the opening actuator is electrified, a second control instruction is sent to the opening actuator, and a cabin door opening signal is sent to the display operation unit until the cabin door is opened to the maximum position, the lock hook on the hinge arm of the cabin door can enter the gust lock hook, and the cabin door is locked at the maximum position. The second control instruction is used for indicating the opening actuator to rotate forwards, and the lifting in-place signal is used for indicating the lock shaft to rotate and driving the cabin door to execute lifting operation to complete cabin door opening operation.
In order to realize the automatic closing function of the cabin door, the method further comprises the following steps:
when the fact that the display operation unit receives a door closing signal is detected, the gust lock sensor is powered on, and whether a gust lock locking signal sent by the gust lock sensor is received or not is detected;
when a locking signal of the gust lock is received, electrifying the gust lock actuator and sending a third control instruction to the gust lock actuator, wherein the third control instruction is used for instructing the gust lock actuator to control unlocking of the gust lock;
when a gust lock unlocking in-place signal sent by a gust lock sensor is received, the gust lock actuator is powered off, the opening actuator is powered on, and a fourth control instruction is sent to the opening actuator and used for indicating the opening actuator to rotate reversely and controlling the cabin door to be closed;
when a cabin door in-place lifting signal sent by a in-place lifting sensor is received, the opening actuator is powered off, the latching actuator is powered on, and a fifth control instruction is sent to the latching actuator and used for indicating the latching actuator to rotate reversely and controlling the cabin door to sink;
when a cabin door latching in-place signal sent by a latching sensor and a pressurization prevention door closing signal sent by a pressurization prevention door sensor are received, whether a latching in-place signal sent by a locking sensor is received or not is detected;
when the locking in-place signal sent by the lock sensor is received, the power supply for the latch actuator is stopped, and a cabin door locking signal is sent to the display operation unit and used for indicating the display operation unit to control the cabin door locking and closing indicator lamp to be turned on.
In order to realize the automatic pre-positioning releasing function before the cabin door is opened, the method further comprises the following steps:
when the speed of the airplane is detected to be lower than the preset speed and the wheel load signal is received, powering off the flight lock actuator, and sending a sixth control instruction to the flight lock actuator, wherein the sixth control instruction is used for indicating the flight lock actuator to control the flight lock to be disengaged from the lock shaft;
when the landing airspeed of the airplane is detected to be 0, the wheel load signal is effective, and the display operation unit does not receive the emergency signal, whether the display operation unit receives a pre-positioning releasing signal or not is detected;
when the display operation unit is detected to receive the pre-positioning releasing signal, electrifying the pre-positioning actuator and sending a seventh control instruction to the pre-positioning actuator, wherein the seventh control instruction is used for indicating the pre-positioning actuator to perform reverse operation so as to enable the pre-positioning mechanism to move towards the first preset position;
when the fact that the positioning actuator receives a positioning signal sent by the positioning sensor is detected, the positioning actuator is powered off, an eighth control instruction is sent to the positioning actuator, the positioning signal is used for indicating the positioning mechanism to reach a first preset position, and the eighth control instruction is used for indicating the positioning actuator to stop executing reverse rotation operation. The disarming operation is completed.
In order to realize the automatic pre-positioning function after the cabin door is closed, the method further comprises the following steps:
when the display operation unit is detected to receive the pre-positioning signal, the pre-positioning actuator is electrified, a ninth control instruction is sent to the pre-positioning actuator, and the ninth control instruction is used for indicating the pre-positioning actuator to push the pre-positioning mechanism into the floor clamp for locking, so that pre-positioning operation is completed.
In order to prevent the cabin door lock shaft from moving, and further prevent the cabin door from being accidentally opened in the air, the safety of the accidental opening of the cabin door is improved. The method further comprises the following steps:
and when detecting whether the speed of the airplane reaches the preset speed or not, electrifying the flight lock actuator, and sending a tenth control instruction to the flight lock actuator, wherein the tenth control instruction is used for indicating the flight lock actuator to control the flight lock to be locked.
In order to ensure the safety of the flight in an emergency situation, the method further comprises:
when detecting that the display operation unit receives the emergency signal, detecting whether the display operation unit receives a door opening signal;
when detecting that the display operation unit receives a door opening signal, executing the opening operation of the cabin door;
sending an eleventh control instruction to the opening actuator, wherein the eleventh control instruction is used for indicating the opening actuator to start the emergency actuating device so as to open and lock the cabin door to the maximum position;
when a first complete opening signal sent by a gust lock sensor is received, the power supply for the opening actuator is stopped, a second complete opening signal is sent to the display operation unit, the first complete opening signal is used for indicating the cabin door to be opened and locked to the maximum position, and the second complete opening signal is used for indicating the display operation unit to control the complete opening signal lamp to be on.
The method for operating the cabin door combines the control panel instruction to electrify different actuators, drives the actuators to move, and enables the cabin door to finish unlocking of the flight lock, unlocking of the pre-positioning, unlocking, lifting, opening, locking and opening of the gust lock and reverse door closing actions.
The method for operating the cabin door can realize automatic operation of the boarding door, and in the face of the increasingly heavy boarding door of a large-sized wide-body passenger plane, the device can effectively reduce physical strength paid by operators for unlocking and lifting the boarding door, reduces risk of bringing people out of the airplane when the cabin door is opened, is simple and clear in operation interface, clear in cabin door state indication, and capable of effectively realizing mechanism blanking, merging cabin door monitoring and actuation signal detection units, and better realizes state monitoring and centralized management of the cabin door of the airplane.
The foregoing is merely a detailed description of the embodiments of the present invention, and some of the conventional techniques are not detailed. The scope of the present invention is not limited thereto, and any changes or substitutions that can be easily made by those skilled in the art within the technical scope of the present invention will be covered by the scope of the present invention. The protection scope of the present invention shall be subject to the protection scope of the claims.
Claims (9)
1. A device for operating a door, comprising: a controller unit (3), a display operation unit (4), a latch actuator (2), an opening actuator (11), a lock shaft (12), a lock sensor (100), a pressure-increasing preventive door sensor (200), a latch sensor (300), and a lift-to-position sensor (400),
the controller unit (3) is electrically connected with the display operation unit (4), the latch actuator (2), the opening actuator (11), the lock sensor (100), the pressure-increasing preventive door sensor (200), the latch sensor (300), and the lift-to-position sensor (400), respectively, each sensor being provided at a position at which the corresponding mechanism is in place, the controller unit (3) being configured to:
when the display operation unit (4) is detected to receive a door opening signal, whether a cabin door locking signal sent by the lock sensor (100) is received or not is detected;
when the cabin door locking signal is received, electrifying the latch actuator (2), and sending a first control instruction to the latch actuator (2), wherein the first control instruction is used for indicating the latch actuator (2) to rotate positively and driving the lock shaft (12) to rotate;
when a leaving signal sent by the lock sensor (100) is received, a cabin door unlocking signal is sent to the display operation unit (4), and the cabin door unlocking signal is used for indicating the display operation unit (4) to control a cabin door unlocking indicator lamp to flicker;
when a leaving signal sent by the pressurization preventive door sensor (200) is received, whether an unlocking in-place signal sent by the lock sensor (100) is received or not is detected, and the unlocking in-place signal is used for indicating that the lock shaft (12) rotates to a preset unlocking position;
when the unlocking in-place signal is received, a cabin door unlocking in-place signal is sent to the display operation unit (4), and the cabin door unlocking in-place signal is used for indicating the display operation unit (4) to control a cabin door unlocking indicator lamp to be on;
when receiving an unlocking signal sent by a bolt sensor (300), sending a cabin door unlocking signal to the display operation unit (4), wherein the cabin door unlocking signal is used for indicating the display operation unit (4) to control a cabin door bolt indicator lamp to be turned off, and the unlocking signal is used for indicating the lock shaft (12) to rotate and driving the bolt shaft (13) to move;
when receiving a lifting in-place signal sent by a lifting in-place sensor (400), the opening actuator (11) is powered on, a second control instruction is sent to the opening actuator (11), and a cabin door opening signal is sent to the display operation unit (4) until the cabin door (8) is opened to the maximum position, the second control instruction is used for indicating the opening actuator to rotate positively, and the lifting in-place signal is used for indicating the lock shaft to rotate and driving the cabin door to perform lifting operation, so that the cabin door opening operation is completed.
2. The apparatus of claim 1, further comprising: gust wind lock sensor (500) and gust wind lock actuator (10), controller unit (3) respectively with gust wind lock sensor (500) and gust wind lock actuator (10) electricity are connected, controller unit (3) still are used for:
when the display operation unit (4) is detected to receive a door closing signal, the gust lock sensor (500) is powered on, and whether a gust lock locking signal sent by the gust lock sensor (500) is received or not is detected;
when the locking signal of the wind array lock is received, electrifying the wind array lock actuator (10) and sending a third control instruction to the wind array lock actuator (10), wherein the third control instruction is used for indicating the wind array lock actuator (10) to control the unlocking of the wind array lock;
when a gust lock unlocking in-place signal sent by the gust lock sensor (500) is received, the gust lock actuator (10) is powered off, the opening actuator (11) is powered on, and a fourth control instruction is sent to the opening actuator (11), wherein the fourth control instruction is used for indicating the opening actuator (11) to reversely rotate and controlling the cabin door (8) to be closed;
when a cabin door in-position lifting signal sent by the in-position lifting sensor (400) is received, the opening actuator (11) is powered off, the latching actuator (2) is powered on, and a fifth control instruction is sent to the latching actuator (2), wherein the fifth control instruction is used for indicating the latching actuator (2) to reversely rotate and controlling the cabin door to sink;
detecting whether an upper lock in-place signal transmitted by the lock sensor (100) is received or not when a door lock in-place signal transmitted by the latch sensor (300) and a door closing signal transmitted by the door pressurization prevention sensor (200) are received;
when a locking in-place signal sent by the lock sensor (100) is received, power supply to the latch actuator (2) is stopped, and a cabin door locking signal is sent to the display operation unit (4), wherein the cabin door locking signal is used for indicating the display operation unit (4) to control a cabin door locking and closing indicator lamp to be turned on.
3. The apparatus of claim 1, further comprising: flight lock actuator (5), pilot actuator (6) and pilot sensor (700), controller unit (3) respectively with flight lock actuator (5), pilot actuator (6) and pilot sensor (700) electricity are connected, controller unit (3) still are used for:
when the speed of the airplane is detected to be lower than the preset speed and a wheel load signal is received, powering off the flight lock actuator (5), and sending a sixth control command to the flight lock actuator (5), wherein the sixth control command is used for indicating the flight lock actuator (5) to control the flight lock to be disengaged from the lock shaft (12);
when the landing airspeed of the airplane is detected to be 0, the wheel load signal is effective, and the display operation unit (4) does not receive the emergency signal, whether the display operation unit (4) receives a pilot release signal or not is detected;
when the display operation unit (4) is detected to receive the pre-positioning releasing signal, electrifying the pre-positioning actuator (6), and sending a seventh control instruction to the pre-positioning actuator (6), wherein the seventh control instruction is used for instructing the pre-positioning actuator (6) to perform reverse operation so as to enable the pre-positioning mechanism to move towards a first preset position;
when detecting pilot actuator (6) receives the signal that targets in place that pilot sensor (700) sent, give pilot actuator (6) outage, and to pilot actuator (6) send ninth control command, the signal that targets in place is used for instructing pilot mechanism reachs first default position, ninth control command is used for instructing pilot actuator (6) stop to carry out the reversal operation.
4. A method of operating a door for a vehicle according to any of claims 1 to 3, the method comprising:
when the display operation unit is detected to receive the door opening signal, detecting whether a cabin door locking signal sent by a locking sensor is received;
when the cabin door locking signal is received, powering on a latching actuator, and sending a first control instruction to the latching actuator, wherein the first control instruction is used for indicating the latching actuator to rotate forwards and driving a lock shaft to rotate;
when a leaving signal sent by a lock sensor is received, a cabin door unlocking signal is sent to the display operation unit, and the cabin door unlocking signal is used for indicating the display operation unit to control a cabin door unlocking indicator lamp to flicker;
when a leaving signal sent by a pressurization prevention door sensor is received, whether an unlocking in-place signal sent by a lock sensor is received or not is detected, and the unlocking in-place signal is used for indicating that the lock shaft rotates to a preset unlocking position;
when the unlocking in-place signal is received, a cabin door unlocking in-place signal is sent to the display operation unit, and the cabin door unlocking in-place signal is used for indicating the display operation unit to control a cabin door unlocking indicator lamp to be on;
when an unlocking signal sent by a latch sensor is received, a cabin door unlocking signal is sent to the display operation unit, the cabin door unlocking signal is used for indicating the display operation unit to control a cabin door latching indicator lamp to be turned off, and the unlocking signal is used for indicating the lock shaft to rotate and driving the latch shaft to move;
when receiving a lifting in-place signal sent by a lifting in-place sensor, the opening actuator is electrified, a second control instruction is sent to the opening actuator, a cabin door opening signal is sent to the display operation unit until the cabin door is opened to the maximum position, the second control instruction is used for indicating the opening actuator to rotate positively, the lifting in-place signal is used for indicating the lock shaft to rotate and drive the cabin door to execute lifting operation, and the cabin door opening operation is completed.
5. The method of claim 4, further comprising:
when the fact that the display operation unit receives a door closing signal is detected, a gust lock sensor is powered on, and whether a gust lock locking signal sent by the gust lock sensor is received or not is detected;
when the locking signal of the wind gust lock is received, electrifying the wind gust lock actuator and sending a third control instruction to the wind gust lock actuator, wherein the third control instruction is used for indicating the wind gust lock actuator to control the unlocking of the wind gust lock;
when a gust lock unlocking in-place signal sent by the gust lock sensor is received, the gust lock actuator is powered off, the opening actuator is powered on, and a fourth control instruction is sent to the opening actuator and used for indicating the opening actuator to rotate reversely and controlling the cabin door to be closed;
when a cabin door in-position lifting signal sent by the in-position lifting sensor is received, the opening actuator is powered off, the latching actuator is powered on, and a fifth control instruction is sent to the latching actuator, wherein the fifth control instruction is used for indicating the latching actuator to reversely rotate and controlling the cabin door to sink;
when a cabin door latching in-place signal sent by the latch sensor and a pressurization prevention door closing signal sent by the pressurization prevention door sensor are received, detecting whether a latching in-place signal sent by a lock sensor is received;
and when receiving a locking in-place signal sent by the lock sensor, stopping supplying power to the latch actuator and sending a cabin door locking signal to the display operation unit, wherein the cabin door locking signal is used for indicating the display operation unit to control a cabin door locking and closing indicator lamp to be turned on.
6. The method of claim 4, further comprising:
when the speed of the airplane is detected to be lower than the preset speed and a wheel load signal is received, powering off a flight lock actuator, and sending a sixth control instruction to the flight lock actuator, wherein the sixth control instruction is used for indicating the flight lock actuator to control a flight lock to be disengaged from a lock shaft;
when the landing airspeed of the airplane is detected to be 0, the wheel load signal is effective, and the display operation unit does not receive the emergency signal, whether the display operation unit receives a pre-positioning releasing signal or not is detected;
when the display operation unit is detected to receive the pre-positioning release signal, electrifying a pre-positioning actuator, and sending a seventh control instruction to the pre-positioning actuator, wherein the seventh control instruction is used for instructing the pre-positioning actuator to perform reverse operation so as to enable the pre-positioning mechanism to move towards a first preset position;
when detecting the pilot actuator receives the signal that targets in place that the sensor sent in advance, give the pilot actuator outage, and to the pilot actuator sends eighth control command, the signal that targets in place is used for instructing the pilot mechanism reachs first preset position, eighth control command is used for instructing the pilot actuator stops to carry out the reversal operation.
7. The method of claim 4, further comprising:
when the display operation unit is detected to receive the pre-positioning signal, the pre-positioning actuator is electrified, a ninth control instruction is sent to the pre-positioning actuator, and the ninth control instruction is used for indicating the pre-positioning actuator to push the pre-positioning mechanism into the floor clamp for locking.
8. The method of claim 4, further comprising:
and when detecting whether the speed of the airplane reaches the preset speed or not, electrifying the flight lock actuator, and sending a tenth control instruction to the flight lock actuator, wherein the tenth control instruction is used for indicating the flight lock actuator to control the flight lock to be locked.
9. The method of claim 4, further comprising:
when detecting that the display operation unit receives an emergency signal, detecting whether the display operation unit receives a door opening signal;
when the display operation unit is detected to receive a door opening signal, executing the cabin door opening operation;
sending an eleventh control instruction to the opening actuator, wherein the eleventh control instruction is used for instructing the opening actuator to start an emergency actuating device so as to open and lock the cabin door to the maximum position;
when a first complete opening signal sent by a gust lock sensor is received, the opening actuator is stopped to be powered on, and a second complete opening signal is sent to the display operation unit, wherein the first complete opening signal is used for indicating the cabin door to be opened and locked to the maximum position, and the second complete opening signal is used for indicating the display operation unit to control a complete opening signal lamp to be turned on.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111066642.8A CN113719215B (en) | 2021-09-10 | 2021-09-10 | Method and device for operating cabin door |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202111066642.8A CN113719215B (en) | 2021-09-10 | 2021-09-10 | Method and device for operating cabin door |
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| CN113719215A CN113719215A (en) | 2021-11-30 |
| CN113719215B true CN113719215B (en) | 2022-10-11 |
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| CN114482753B (en) * | 2022-02-15 | 2024-03-08 | 中国商用飞机有限责任公司 | Cabin door control device, aircraft and cabin door control method |
| CN115522815A (en) * | 2022-10-25 | 2022-12-27 | 中国商用飞机有限责任公司 | Method for releasing stress of actuator of cargo door and cargo door operating device |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN103879545B (en) * | 2014-03-20 | 2017-06-09 | 中国商用飞机有限责任公司 | For the hatch door flight lock system of aircraft |
| CN103967373B (en) * | 2014-05-05 | 2017-01-04 | 中国商用飞机有限责任公司 | Aircraft electronic hatch door safety control system and control method thereof |
| WO2018194728A1 (en) * | 2017-04-21 | 2018-10-25 | Curry James M | Aircraft plug door with in-plane load transfer capacity and methods of use |
| CN111232180B (en) * | 2020-02-26 | 2021-10-19 | 中国商用飞机有限责任公司 | Aircraft cabin door gust wind lock device |
| CN212243777U (en) * | 2020-04-30 | 2020-12-29 | 庆安集团有限公司 | Cabin door alarm device |
| CN112327686B (en) * | 2020-10-27 | 2022-05-24 | 西北工业大学 | Advanced airplane cabin door centralized management system |
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