CN108945511A - The anti-collision control system and method for airfield vehicle - Google Patents
The anti-collision control system and method for airfield vehicle Download PDFInfo
- Publication number
- CN108945511A CN108945511A CN201811061043.5A CN201811061043A CN108945511A CN 108945511 A CN108945511 A CN 108945511A CN 201811061043 A CN201811061043 A CN 201811061043A CN 108945511 A CN108945511 A CN 108945511A
- Authority
- CN
- China
- Prior art keywords
- loading
- unloading platform
- aircraft
- controller
- platform
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 title claims abstract description 45
- 230000005693 optoelectronics Effects 0.000 claims abstract description 27
- 238000009434 installation Methods 0.000 claims abstract description 19
- 239000000523 sample Substances 0.000 claims abstract description 18
- 230000003028 elevating effect Effects 0.000 claims abstract description 11
- 230000006698 induction Effects 0.000 claims description 20
- 230000000630 rising effect Effects 0.000 claims description 15
- 238000006243 chemical reaction Methods 0.000 claims description 11
- 230000001681 protective effect Effects 0.000 claims description 5
- 238000003032 molecular docking Methods 0.000 abstract description 2
- 238000005516 engineering process Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000005622 photoelectricity Effects 0.000 description 2
- 230000000644 propagated effect Effects 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- 239000004411 aluminium Substances 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 238000004891 communication Methods 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 230000001939 inductive effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 230000000750 progressive effect Effects 0.000 description 1
- 230000003252 repetitive effect Effects 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 238000013519 translation Methods 0.000 description 1
Classifications
-
- 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
- B64F1/32—Ground or aircraft-carrier-deck installations for handling freight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60R—VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT OTHERWISE PROVIDED FOR
- B60R16/00—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for
- B60R16/02—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements
- B60R16/023—Electric or fluid circuits specially adapted for vehicles and not otherwise provided for; Arrangement of elements of electric or fluid circuits specially adapted for vehicles and not otherwise provided for electric constitutive elements for transmission of signals between vehicle parts or subsystems
- B60R16/0231—Circuits relating to the driving or the functioning of the vehicle
- B60R16/0232—Circuits relating to the driving or the functioning of the vehicle for measuring vehicle parameters and indicating critical, abnormal or dangerous conditions
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Traffic Control Systems (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
The present invention provides the anti-collision control system and method for a kind of airfield vehicle, and wherein system includes limit switch, optoelectronic switch, ultrasonic sensor, radar installations and controller；Limit switch incudes aircraft in uphill process for loading/unloading platform to control the elevating movement of loading/unloading platform；Optoelectronic switch incudes aircraft during extension for loading/unloading platform to control the stretching motion of loading/unloading platform；Ultrasonic sensor is for incuding aircraft hatch door to control the side-to-side movement of loading/unloading platform；Radar installations includes multiple probes, and aircraft is incuded in uphill process in reversing and lifting compartment for airfield vehicle, to control the reversing of airfield vehicle and go up and down the elevating movement in compartment.The present invention can be comprehensive prevent airfield vehicle and aircraft from colliding, and can be realized the accurate docking of the loading/unloading platform and aircraft hatch door of airfield vehicle.
Description
Technical field
Embodiment of the present invention is related to anti-collision control system and the side in anticollision field more particularly to a kind of airfield vehicle
Method.
Background technique
With the continuous development of China's economy Civil Aviation Industry is grown rapidly, airport quantity also increases therewith.Airport tool
It takes up a large area, the features such as airfield vehicle mobility is strong.When aircraft is parked in boarding gate or other service locations, it is possible to
It can be by the collision of airfield vehicle, such as fuel truck, Surface power drive cart, trolley train, cargo loading machine, kitchen service
All there is the risk of collision with aircraft in vehicle and mobile exit ramp, especially need the vehicle cooperated with aircraft loading/unloading platform
, it is easy to collision is in contact with aircraft.In practice, even the damage of slight impact, maintenance cost is all very high
It is expensive, but also may cause departure time delay etc., to bring massive losses to airline.Therefore, airfield vehicle and boat
The anti-collision safety protection of pocket becomes more and more important.
Main estimated by operator of the anti-collision safety of airfield vehicle and aircraft protection at present is completed, for example, by using
It is placed in vehicle platform forefront close to switch or mechanical touching limit switch, before control platform stops when close to aircraft
It stretches.
But in implementing the present invention, it may, inventor has found the prior art, at least there are the following problems:
Under the scene of part, goods transport vehicle in a manner of falling back close to loading/unloading platform, since reversing is there are obstacle and blind area,
Therefore it is easy so that goods transport vehicle collides loading/unloading platform, especially when loading/unloading platform is the large scale equipments such as aircraft, cargo transport
Vehicle load and unload position move left and right, rise and fall and when reversing at the top of carriage body tail end aspect do not accomplish it is enough anti-
Shield, is easy to collide aircraft and other loading/unloading platforms.
It should be noted that the above description of the technical background be intended merely to it is convenient to technical solution of the present invention carry out it is clear,
Complete explanation, and facilitate the understanding of those skilled in the art and illustrate.Cannot merely because these schemes of the invention
Background technology part is expounded and thinks that above-mentioned technical proposal is known to those skilled in the art.
Summary of the invention
In view of the above-mentioned problems, a kind of anti-collision control system for being designed to provide airfield vehicle of embodiment of the present invention and
Method, can be comprehensive prevent airfield vehicle and aircraft from colliding, and can be realized the loading/unloading platform of airfield vehicle
With the accurate docking of aircraft hatch door.
To achieve the above object, embodiment of the present invention provides a kind of airport vehicle anticollision control system, the airport vehicle
It include that headstock, car body, lifting compartment and loading/unloading platform, the lifting compartment are installed on car body, the loading/unloading platform is installed
In lifting compartment close to one end of headstock；The anti-collision control system include: limit switch, optoelectronic switch, ultrasonic sensor,
Radar installations and controller, the limit switch, optoelectronic switch, ultrasonic sensor, radar installations are logical with controller respectively
Letter connection；The limit switch, optoelectronic switch and ultrasonic sensor are located on loading/unloading platform, wherein the limit switch is used for
Loading/unloading platform incudes aircraft in uphill process, to control the elevating movement of loading/unloading platform by the controller；It is described
Optoelectronic switch incudes aircraft during extension for loading/unloading platform, to control stretching for loading/unloading platform by the controller
Contracting movement；The ultrasonic sensor is for incuding aircraft hatch door, to control a left side for loading/unloading platform by the controller
Right movement；The radar installations includes multiple probes, is located at hull back and lifting compartment tail portion top, is used for airport vehicle
Move backward and go up and down compartment aircraft is incuded in uphill process, thus by the controller control airfield vehicle reversing
And the elevating movement in lifting compartment.
To achieve the above object, embodiment of the present invention also provides a kind of airport vehicle anticollision control method, is applied to such as
In the anti-collision control system of the upper airfield vehicle, comprising: in airfield vehicle reversing process, positioned at the radar of hull back
Probe induction aircraft, the reversing of airfield vehicle is controlled by controller；After airfield vehicle comes to a complete stop, in lifting compartment uphill process
In, aircraft is incuded according to the radar probe for being located at lifting compartment tail portion top, while according to the limit being located on loading/unloading platform
Inductive switching aircraft and according to be located at loading/unloading platform on ultrasonic sensor incude aircraft hatch door, pass through controller control
The elevating movement of loading/unloading platform processed；During the extension after loading/unloading platform stops rising, opened according to the photoelectricity on loading/unloading platform
Induction aircraft is closed, the stretching motion of loading/unloading platform is controlled by controller；After loading/unloading platform stops extension, loaded and unloaded according to being located at
Ultrasonic sensor on platform incudes aircraft hatch door, and the side-to-side movement of loading/unloading platform is controlled by the controller, makes to fill
Unload platform alignment aircraft hatch door.
Therefore embodiment of the present invention provide airport vehicle anticollision control system and method, by limit switch,
Optoelectronic switch, ultrasonic sensor, radar installations, can realize respectively airfield vehicle reversing when and aircraft induction, lifting
Compartment tail portion top and aircraft induction and loading/unloading platform and aircraft positioned at car bottom forward position in compartment uphill process
Induction and loading/unloading platform and aircraft hatch door induction, realizing comprehensive prevents airfield vehicle and aircraft from touching
It hits.And by the distance of induction loading/unloading platform and aircraft hatch door, realize that loading/unloading platform is directed at aircraft hatch door.
Detailed description of the invention
It, below will be to embodiment in order to illustrate more clearly of embodiment of the present invention or technical solution in the prior art
Or attached drawing needed to be used in the description of the prior art is simply introduced one by one, it should be apparent that, the accompanying drawings in the following description is
Some embodiments of the present invention, for those of ordinary skill in the art, without creative efforts, also
Other drawings may be obtained according to these drawings without any creative labor.
Fig. 1 is the schematic diagram of the anti-collision control system for the airfield vehicle that embodiment of the present invention provides；
Fig. 2 is that limit switch, optoelectronic switch and the ultrasonic sensor that embodiment of the present invention provides are located at protection cylinder
Position view；
Fig. 3 is the position view that the anti-collision control system that embodiment of the present invention provides is located at airfield vehicle；
Fig. 4 is the flow diagram of the anticollision control method for the airfield vehicle that embodiment of the present invention provides.
Specific embodiment
To keep the purposes, technical schemes and advantages of embodiment of the present invention clearer, implement below in conjunction with the present invention
The technical solution in embodiment of the present invention is clearly and completely described in attached drawing in mode, it is clear that described reality
The mode of applying is some embodiments of the invention, rather than whole embodiments.Based on the embodiment in the present invention, ability
Domain those of ordinary skill every other embodiment obtained without creative efforts, belongs to the present invention
The range of protection.
Embodiment of the present invention provides a kind of anti-collision control system of airfield vehicle, the airfield vehicle include headstock, car body,
Lifting compartment and loading/unloading platform, the lifting compartment are installed on car body, which is installed on lifting compartment close to headstock
One end.
As shown in Figure 1, anti-collision control system include limit switch, optoelectronic switch, ultrasonic sensor, radar installations and
Controller.
As shown in Fig. 2, limit switch, optoelectronic switch and ultrasonic sensor are located on protection cylinder；As shown in connection with fig. 3, should
Protection cylinder is installed on the loading/unloading platform forward position of airfield vehicle, the resilient cushion including protective shell and package protective shell.The present invention is real
It applies in example, which is preferably hollow cylindrical column, which uses Rubber shock-absorbing pad, and certain protective shell can also have it
His shape and resilient cushion can also also have the selection of other materials, herein and without limitation.
Limit switch is mounted on protection cylinder forward position both ends, and contact is arranged obliquely, is rising for incuding loading/unloading platform
Object in the process.Limit switch is to control electricity using realization connection or disjunction when its contact collides object during stroke
Road.In embodiments of the present invention, contact is arranged obliquely with first angle, which is 30~60 degree, preferably 45 degree.Work as dress
When unloading platform rising, if limit switch touches aircraft, signal is sent to controller, controller controls loading/unloading platform
Stop rising.
Optoelectronic switch is mounted on protection cylinder forward position, for incuding object of the loading/unloading platform in telescopic process.Optoelectronic switch
The variation of electric current is converted by the strong and weak variation of light between transmitting terminal and receiving end to achieve the purpose that detection.Of the invention real
It applies in example, sets the distance of reaction of optoelectronic switch as 50~100mm, preferably 100mm, the i.e. process when loading/unloading platform extension
In, if optoelectronic switch senses aircraft, the distance between loading/unloading platform and object are equal to less than 100mm, optoelectronic switch
Signal is sent to controller, controller controls loading/unloading platform and stops extension.
Ultrasonic sensor is installed on the both ends of protection cylinder, for incuding aircraft hatch door, especially incudes aircraft cabin
The side of door is following.Ultrasonic wave refers to the above mechanical wave of frequency 20kHz, is a kind of special sound wave, with sound deflection, instead
The Basic Physical Properties such as penetrate, interfere.By emitter, ultrasonic wave letter is launched in some direction to ultrasonic sensor to the outside
Number, start to carry out timing while emitting the ultrasonic wave moment, ultrasonic wave is propagated by air, and propagation encounters obstacle on the way
Object (such as aircraft hatch door side or following) will return immediately penetrate be propagated back to come, ultrasonic receiver receive back wave when
Quarter just stops timing immediately.The spread speed of ultrasonic wave is 340m/s in air, and timer passes through record time t, so that it may
The distance between calculate from launch point to barrier length (s), it may be assumed that s=340t/2.In loading/unloading platform operational process, surpass
Sonic sensor incudes the distance of loading/unloading platform and aircraft hatch door, and sends signal to controller, makes controller control handling
Platform is directed at aircraft hatch door.Specifically, the ultrasonic sensor positioned at protection cylinder both ends is respectively induced left with aircraft hatch door
The distance at right both ends, controller is according to the side-to-side movement of the distance controlling loading/unloading platform of induction, and in the center line of loading/unloading platform
When being directed at the center of aircraft hatch door, control loading/unloading platform stopping is moved left and right.
Radar installations includes multiple probes, is separately mounted to hull back and the lifting compartment tail portion top of airfield vehicle
Object of the compartment in uphill process is being moved backward and gone up and down in end for detecting airfield vehicle, and radar installations is with automatic IP addressing
Function is obtained that is, in the presence of no Dynamic Host Configuration Protocol server or other IT address assignment agencies by equipment automatically
Legitimate ip address is taken, using this technology, radar installations can be concentrated from reserved IP address and choose an IP address immediately, to
Local network issues inquiry, determines whether the address is being used by other clients, the continuous repetitive addressing of radar installations and school
The step of testing, until discovery, one does not have occupied address.In embodiments of the present invention, the probe of radar installations is walked according to cable
To automatically determining orientation and distribute internal ID.Compartment is being moved backward and gone up and down to radar installations in uphill process to prevent airfield vehicle,
Car body top encounters the components such as wing and causes damages.
Controller is arranged in the headstock of airfield vehicle, ultrasonic sensor, optoelectronic switch, limit switch and radar installations
The signal input part that signal output end connects controller realizes communication connection, and the signal output end of controller passes through signal adapter
The car running computer of airfield vehicle is connected, and is powered by vehicle power supply.When ultrasonic sensor, optoelectronic switch, limit switch sense
Controller is answered or sends a signal to when contacting, controller stops according to the fortune of the signal controlling machine field vehicle received, goes up and down compartment
Lifting and the flexible of loading/unloading platform, translation and lifting.In addition, controller uses aluminium profiles shell, inside uses connectionless line
Design, to have higher seismic behavior, to reach anti-collision effect.
Embodiment of the present invention also provides a kind of anticollision control method of airfield vehicle, comprising:
In airfield vehicle reversing process, the radar probe positioned at hull back incudes aircraft, is controlled by controller
The reversing of airfield vehicle；
After airfield vehicle comes to a complete stop, in lifting compartment uphill process, visited according to the radar for being located at lifting compartment tail portion top
Head induction aircraft, while according to the limit switch induction aircraft being located on loading/unloading platform and according on loading/unloading platform
Ultrasonic sensor incude aircraft hatch door, pass through controller control loading/unloading platform elevating movement；
During the extension after loading/unloading platform stops rising, aircraft is incuded according to the optoelectronic switch on loading/unloading platform,
The stretching motion of loading/unloading platform is controlled by controller；
After loading/unloading platform stops extension, aircraft hatch door is incuded according to the ultrasonic sensor being located on loading/unloading platform, is led to
The side-to-side movement for crossing the controller control loading/unloading platform, makes loading/unloading platform be directed at aircraft hatch door.
The wherein elevating movement that loading/unloading platform is controlled by controller, specifically: in lifting compartment uphill process,
If the contact of limit switch touches aircraft, signal is sent to controller, the controller control loading/unloading platform stops
Rise；And/or if ultrasonic sensor senses aircraft hatch door bottom edge, signal, the controller are sent to controller
Loading/unloading platform is controlled to stop rising；And/or if the probe for being located at lifting compartment tail portion top incudes in third distance of reaction
To aircraft, then signal is sent to controller, the controller control loading/unloading platform stops rising.
The wherein stretching motion by controller control loading/unloading platform, specifically: if the optoelectronic switch is the
Aircraft is sensed in one distance of reaction, then sends signal to controller, and the controller control loading/unloading platform stops extension.
The wherein side-to-side movement that loading/unloading platform is controlled by the controller, specifically: ultrasonic sensor difference
Induction at a distance from aircraft hatch door left and right ends, controller according to the side-to-side movement of the distance controlling loading/unloading platform of induction, and
At the center of the center line alignment aircraft hatch door of loading/unloading platform, control loading/unloading platform stopping is moved left and right.
By with reference to for Fig. 4, in airfield vehicle reversing process, if be located at the radar probe of hull back setting away from
From interior induction aircraft, controller issues alarm by alarm system to control the reversing of airfield vehicle.After airfield vehicle comes to a complete stop,
Start compartment to rise, in lifting compartment uphill process, judges whether the contact of limit switch senses aircraft；If limit
The contact of switch touches aircraft, then controls loading/unloading platform by controller and stop rising, start under compartment as needed, then
Airfield vehicle position is readjusted, compartment rising is restarted in position after adjusting；If the no contact of limit switch touches
Aircraft, incudes aircraft hatch door according to ultrasonic sensor, stops compartment when keeping platform concordant with hatch door and rises；Start platform
Extension is stretched, judges whether optoelectronic switch senses aircraft, such as senses that platform is automatically stopped extension；Start platform or so to move
Dynamic, two ultrasonic sensors are respectively induced the right and left of aircraft hatch door, and are directed at aviation in the center line of loading/unloading platform
When the center of device hatch door, control loading/unloading platform stopping is moved left and right；Hatch door can not be all directed at by such as moving left and right, then contracting is closed flat
Platform, truck position will be readjusted, then accent starts to operate again under compartment by restarting.
The above-mentioned airport vehicle anticollision control method particular technique details being related to and airport vehicle anticollision control system
In it is similar, therefore no longer specifically repeat.
Therefore the anti-collision control system and method for airfield vehicle provided by the invention, it is opened by limit switch, photoelectricity
Pass, ultrasonic sensor, radar installations, can realize respectively airfield vehicle reversing when and aircraft induction, go up and down compartment on
Compartment tail portion top and aircraft induction and the induction of loading/unloading platform and aircraft positioned at car bottom forward position during rising,
And the induction of loading/unloading platform and aircraft hatch door, realizing comprehensive prevents airfield vehicle and aircraft from colliding.And
By incuding the distance of loading/unloading platform and aircraft hatch door, realize that loading/unloading platform is directed at aircraft hatch door.
Each embodiment in this specification is described in a progressive manner, same and similar between each embodiment
Part may refer to each other, what each embodiment stressed is the difference with other embodiments.
Finally, it should be noted that being supplied to ability to the description of various embodiments of the invention above with the purpose described
Field technique personnel.It is that it is not intended to exhaustion or be not intended to and limit the invention to single disclosed embodiment.Institute as above
It states, various substitutions of the invention and variation will be apparent for above-mentioned technology one of ordinary skill in the art.Therefore,
Although having specifically discussed some alternative embodiments, other embodiment will be apparent or ability
Field technique personnel relatively easily obtain.The present invention is intended to include herein by discussion cross all substitutions of the invention, modification and
Variation, and fall in the other embodiment in the spirit and scope of above-mentioned application.
Claims (10)
1. a kind of anti-collision control system of airfield vehicle, the airfield vehicle includes that headstock, car body, lifting compartment and handling are flat
Platform, the lifting compartment are installed on car body, and the loading/unloading platform is installed on lifting compartment close to one end of headstock, and feature exists
In the anti-collision control system includes: limit switch, optoelectronic switch, ultrasonic sensor, radar installations and controller, institute
Limit switch, optoelectronic switch, ultrasonic sensor, radar installations is stated to communicate to connect with controller respectively；
The limit switch, optoelectronic switch and ultrasonic sensor are located on loading/unloading platform, wherein the limit switch is for filling
It unloads platform and incudes aircraft in uphill process, to control the elevating movement of loading/unloading platform by the controller；The light
Electric switch incudes aircraft during extension for loading/unloading platform, to control the flexible of loading/unloading platform by the controller
Movement；The ultrasonic sensor is for incuding aircraft hatch door, to control the left and right of loading/unloading platform by the controller
Movement；
The radar installations includes multiple probes, is located at hull back and lifting compartment tail portion top, is used for airfield vehicle
Move backward and go up and down compartment aircraft is incuded in uphill process, thus by the controller control airfield vehicle reversing and
Go up and down the elevating movement in compartment.
2. the anti-collision control system of airfield vehicle according to claim 1, which is characterized in that the anti-collision control system is also
Including protecting cylinder, the protection cylinder is installed on the loading/unloading platform forward position, the resilient cushion including protective shell and package protective shell.
3. the anti-collision control system of airfield vehicle according to claim 2, which is characterized in that the limit switch is mounted on
Cylinder forward position both ends are protected, and contact is arranged obliquely with first angle；In loading/unloading platform operational process, if the limit is opened
The contact of pass touches aircraft, then sends signal to controller, and the controller control loading/unloading platform stops rising；
The optoelectronic switch is mounted on protection cylinder forward position；In loading/unloading platform operational process, if the optoelectronic switch is first
Aircraft is sensed in distance of reaction, then sends signal to controller, and the controller control loading/unloading platform stops extension；
The ultrasonic sensor is installed on the both ends of protection cylinder；In loading/unloading platform operational process, loading/unloading platform and boat are incuded
The distance of pocket hatch door, and signal is sent to controller, the controller control loading/unloading platform is directed at aircraft hatch door.
4. the anti-collision control system of airfield vehicle according to claim 3, which is characterized in that described to be located at protection cylinder both ends
Ultrasonic sensor be respectively induced at a distance from aircraft hatch door left and right ends, controller according to the distance controlling of induction load and unload
The side-to-side movement of platform, and at the center of the center line of loading/unloading platform alignment aircraft hatch door, control loading/unloading platform stops
Only move left and right.
5. the anti-collision control system of airfield vehicle according to claim 4, which is characterized in that the radar installations it is multiple
Probe automatically determines probe location and distributes internal ID according to cable louding by automatic IP addressing function；
Detectable signal is sent to controller respectively by multiple probes；
If the probe for being located at hull back senses that aircraft, the controller pass through alarm system in the second distance of reaction
System issues alarm；If the probe for being located at lifting compartment tail portion top senses aircraft in third distance of reaction, described
Controller goes up and down compartment and rises.
6. the anti-collision control system of airfield vehicle according to claim 5, which is characterized in that the first angle is oblique
Upper 30~60 degree；
First distance of reaction, the second distance of reaction and third distance of reaction are respectively 50~100mm.
7. a kind of anticollision control method of airfield vehicle, the anticollision applied to the airfield vehicle as described in any one of 1~6 is controlled
In system characterized by comprising
In airfield vehicle reversing process, the radar probe positioned at hull back incudes aircraft, controls airport by controller
The reversing of vehicle；
After airfield vehicle comes to a complete stop, in lifting compartment uphill process, according to the radar probe sense for being located at lifting compartment tail portion top
Aircraft is answered, while according to the limit switch induction aircraft being located on loading/unloading platform and according to super on loading/unloading platform
Sonic sensor incudes aircraft hatch door, and the elevating movement of loading/unloading platform is controlled by controller；
During the extension after loading/unloading platform stops rising, aircraft is incuded according to the optoelectronic switch on loading/unloading platform, is passed through
The stretching motion of controller control loading/unloading platform；
After loading/unloading platform stops extension, aircraft hatch door is incuded according to the ultrasonic sensor being located on loading/unloading platform, passes through institute
The side-to-side movement for stating controller control loading/unloading platform, makes loading/unloading platform be directed at aircraft hatch door.
8. the anticollision control method of airfield vehicle according to claim 7, which is characterized in that described to be controlled by controller
The elevating movement of loading/unloading platform, specifically:
In lifting compartment uphill process, if the contact of limit switch touches aircraft, signal, institute are sent to controller
Controller control loading/unloading platform is stated to stop rising；And/or
If ultrasonic sensor senses aircraft hatch door bottom edge, signal, the controller control dress are sent to controller
Platform is unloaded to stop rising；And/or
If the probe for being located at lifting compartment tail portion top senses aircraft in third distance of reaction, sent to controller
Signal, the controller control loading/unloading platform stop rising.
9. the anticollision control method of airfield vehicle according to claim 7, which is characterized in that described to be controlled by controller
The stretching motion of loading/unloading platform, specifically:
If the optoelectronic switch senses aircraft in the first distance of reaction, signal, the control are sent to controller
Device controls loading/unloading platform and stops extension.
10. the anticollision control method of airfield vehicle according to claim 7, which is characterized in that described to pass through the control
Device controls the side-to-side movement of loading/unloading platform, specifically:
Ultrasonic sensor is respectively induced at a distance from aircraft hatch door left and right ends, and controller is filled according to the distance controlling of induction
The side-to-side movement of platform is unloaded, and at the center of the center line of loading/unloading platform alignment aircraft hatch door, controls loading/unloading platform
Stopping moves left and right.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811061043.5A CN108945511B (en) | 2018-09-12 | 2018-09-12 | Collision avoidance control system and method for airport vehicles |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811061043.5A CN108945511B (en) | 2018-09-12 | 2018-09-12 | Collision avoidance control system and method for airport vehicles |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN108945511A true CN108945511A (en) | 2018-12-07 |
| CN108945511B CN108945511B (en) | 2024-03-01 |
Family
ID=64476655
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811061043.5A Active CN108945511B (en) | 2018-09-12 | 2018-09-12 | Collision avoidance control system and method for airport vehicles |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108945511B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109532659A (en) * | 2018-11-03 | 2019-03-29 | 江苏天机场专用设备股份有限公司 | A kind of device and method that control airport vehicle anticollision machine system releases |
| CN109703432A (en) * | 2019-01-09 | 2019-05-03 | 中铁第四勘察设计院集团有限公司 | A kind of city check-in baggage container loading-unloading vehicle system and handling method |
| CN110116889A (en) * | 2019-05-31 | 2019-08-13 | 中铁第四勘察设计院集团有限公司 | A kind of high-speed rail logistics rail mounted automatic sensing platform automatic assembling and disassembling system |
| CN110381173A (en) * | 2019-06-26 | 2019-10-25 | 惠州市德赛西威智能交通技术研究院有限公司 | A kind of method of trailer-mounted radar dynamic IP address allocation |
| CN111319997A (en) * | 2020-03-19 | 2020-06-23 | 扬州雷鸟机器人科技有限公司 | Device is dodged with high efficiency to intelligence loading and unloading |
Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0734411A (en) * | 1993-07-20 | 1995-02-03 | Toyo Umpanki Co Ltd | Work vehicle |
| CN2463313Y (en) * | 2001-01-05 | 2001-12-05 | 师万清 | Passenger ferry lifting push for use in airport |
| FR2836468A1 (en) * | 2002-02-28 | 2003-08-29 | Pinguely Haulotte | Lift cage for working at height has radar or ultrasound detectors to measure distance from obstacles and linked to controls and/or alarm |
| JP2006036481A (en) * | 2004-07-28 | 2006-02-09 | Shinko Electric Co Ltd | Container pallet loader and freight conveyance system by container pallet loader |
| CN101966833A (en) * | 2010-10-27 | 2011-02-09 | 中国民航大学 | Airplane deicing vehicle with vehicle chassis adopting wire control technology |
| CN103171971A (en) * | 2013-03-19 | 2013-06-26 | 河南省矿山起重机有限公司 | Hanging over rail of crane and automatic centering system of hanging over rail |
| CN105383708A (en) * | 2015-12-16 | 2016-03-09 | 中国人民解放军军事交通学院 | Lift loading and unloading ferrying device for airport |
| KR20160072542A (en) * | 2014-12-15 | 2016-06-23 | 한국공항공사 | Passenger Boarding Bridges collision avoidance system |
| CN206624013U (en) * | 2017-03-13 | 2017-11-10 | 东风汽车股份有限公司 | Pure electric motor field boarding vehicle |
| CN107450080A (en) * | 2017-09-27 | 2017-12-08 | 北京特种机械研究所 | View-based access control model positions and two car automatic butt methods of laser ranging |
| CN107521716A (en) * | 2017-09-01 | 2017-12-29 | 上海晟骓汽车科技有限责任公司 | A kind of passenger plane intelligent elevator vehicle and its application |
| CN107878779A (en) * | 2016-09-30 | 2018-04-06 | 中国国际海运集装箱(集团)股份有限公司 | Pick platform and the lift truck with the platform that picks |
| CN208760919U (en) * | 2018-09-12 | 2019-04-19 | 东方航空食品投资有限公司 | The anti-collision control system of airfield vehicle |
-
2018
- 2018-09-12 CN CN201811061043.5A patent/CN108945511B/en active Active
Patent Citations (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH0734411A (en) * | 1993-07-20 | 1995-02-03 | Toyo Umpanki Co Ltd | Work vehicle |
| CN2463313Y (en) * | 2001-01-05 | 2001-12-05 | 师万清 | Passenger ferry lifting push for use in airport |
| FR2836468A1 (en) * | 2002-02-28 | 2003-08-29 | Pinguely Haulotte | Lift cage for working at height has radar or ultrasound detectors to measure distance from obstacles and linked to controls and/or alarm |
| JP2006036481A (en) * | 2004-07-28 | 2006-02-09 | Shinko Electric Co Ltd | Container pallet loader and freight conveyance system by container pallet loader |
| CN101966833A (en) * | 2010-10-27 | 2011-02-09 | 中国民航大学 | Airplane deicing vehicle with vehicle chassis adopting wire control technology |
| CN103171971A (en) * | 2013-03-19 | 2013-06-26 | 河南省矿山起重机有限公司 | Hanging over rail of crane and automatic centering system of hanging over rail |
| KR20160072542A (en) * | 2014-12-15 | 2016-06-23 | 한국공항공사 | Passenger Boarding Bridges collision avoidance system |
| CN105383708A (en) * | 2015-12-16 | 2016-03-09 | 中国人民解放军军事交通学院 | Lift loading and unloading ferrying device for airport |
| CN107878779A (en) * | 2016-09-30 | 2018-04-06 | 中国国际海运集装箱(集团)股份有限公司 | Pick platform and the lift truck with the platform that picks |
| CN206624013U (en) * | 2017-03-13 | 2017-11-10 | 东风汽车股份有限公司 | Pure electric motor field boarding vehicle |
| CN107521716A (en) * | 2017-09-01 | 2017-12-29 | 上海晟骓汽车科技有限责任公司 | A kind of passenger plane intelligent elevator vehicle and its application |
| CN107450080A (en) * | 2017-09-27 | 2017-12-08 | 北京特种机械研究所 | View-based access control model positions and two car automatic butt methods of laser ranging |
| CN208760919U (en) * | 2018-09-12 | 2019-04-19 | 东方航空食品投资有限公司 | The anti-collision control system of airfield vehicle |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109532659A (en) * | 2018-11-03 | 2019-03-29 | 江苏天机场专用设备股份有限公司 | A kind of device and method that control airport vehicle anticollision machine system releases |
| CN109703432A (en) * | 2019-01-09 | 2019-05-03 | 中铁第四勘察设计院集团有限公司 | A kind of city check-in baggage container loading-unloading vehicle system and handling method |
| CN110116889A (en) * | 2019-05-31 | 2019-08-13 | 中铁第四勘察设计院集团有限公司 | A kind of high-speed rail logistics rail mounted automatic sensing platform automatic assembling and disassembling system |
| CN110381173A (en) * | 2019-06-26 | 2019-10-25 | 惠州市德赛西威智能交通技术研究院有限公司 | A kind of method of trailer-mounted radar dynamic IP address allocation |
| CN111319997A (en) * | 2020-03-19 | 2020-06-23 | 扬州雷鸟机器人科技有限公司 | Device is dodged with high efficiency to intelligence loading and unloading |
Also Published As
| Publication number | Publication date |
|---|---|
| CN108945511B (en) | 2024-03-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN108945511A (en) | The anti-collision control system and method for airfield vehicle | |
| US10556760B2 (en) | Automatic tire loader/unloader for stacking/unstacking tires in a trailer | |
| US10343855B2 (en) | System and method for automated truck loading | |
| US10519614B2 (en) | System and method for automated deployment of a passenger boarding bridge | |
| CN110116889A (en) | A kind of high-speed rail logistics rail mounted automatic sensing platform automatic assembling and disassembling system | |
| US6420846B1 (en) | Power drive unit with stall sensor | |
| US9676567B2 (en) | Cargo compartment and method for loading a cargo compartment | |
| EP1253079B1 (en) | Air cargo transport system | |
| EP2206664A1 (en) | Method for docking of a vehicle, such as a truck, at a loading and unloading platform, and buffer | |
| CN103392157A (en) | Object tracking and steer maneuvers for materials handling vehicles | |
| JP6513544B2 (en) | Collision prevention device for cargo handling crane | |
| CN208760919U (en) | The anti-collision control system of airfield vehicle | |
| WO2012078257A1 (en) | X-ray inspection tool moving on tracks fixed to an aircraft by use of suction cups | |
| US9676493B2 (en) | System and method for damage tracking and monitoring during ground handling of aircraft | |
| WO2019141850A1 (en) | Autonomous self propelled ground support equipment | |
| US20200140088A1 (en) | Method for verifying latch engagement for cargo handling systems | |
| CN108025755B (en) | Method and transport device for transporting containers or pallets with air cargo | |
| US20180016126A1 (en) | Floor Conveyor | |
| CN113086542A (en) | Movable conveying platform | |
| CN207225509U (en) | Body frame structure for automotive and the unmanned carrying implement of anticollision | |
| CN208776218U (en) | A kind of driving | |
| CN220371411U (en) | Omnidirectional anti-collision aerial work platform | |
| CN102874612A (en) | Coupler alignment device for car dumper and car dumper | |
| KR101685015B1 (en) | Car assembling line to be able to control the speed of a assembly truck | |
| CN201952122U (en) | Landing leg anti-collision device and gantry crane comprising same |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |