CN103927109B - System for the task guidance of operational administrative in aircraft cockpit - Google Patents
System for the task guidance of operational administrative in aircraft cockpit Download PDFInfo
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- CN103927109B CN103927109B CN201410006690.1A CN201410006690A CN103927109B CN 103927109 B CN103927109 B CN 103927109B CN 201410006690 A CN201410006690 A CN 201410006690A CN 103927109 B CN103927109 B CN 103927109B
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Abstract
This application discloses the systems and computer-readable medium for the task guidance of operational administrative in aircraft cockpit.This theme includes for providing the system and computer-readable medium of task guidance, for managing flight operation during the abnormal conditions caused by normal operating procedure or anomalous event.In certain aspects, the system for providing task guidance may include processor, memory and the flight supplementary module for being configured to receive data from multiple servers.Supplementary module can show the possible aircraft flight stage while indicating mission phase.Supplementary module can also be shown for mission phase operation to be performed, and movement corresponding with these operations.
Description
Cross reference to related applications
This application claims the priority for No. 1350247 french patent application submitted on January 11st, 2013 and 2013 5
The priority of No. 13/905914 U.S. Patent application of No. 30 submissions of the moon, entire contents are incorporated herein by reference.
Technical field
Theme described herein relate generally to it is a kind of for assisting in flying device operation during motion guiding system.More
Specifically, subject matter disclosed herein is related to the system of the management of the aircraft operation for being realized by aircraft operator.
Background technique
During the general operation of aircraft, system management function allows operator's interaction in the case where normal management
With the state of monitoring aerocraft system, and during flight operation, in the case where abnormal case, warning and program are provided.
During flight operation under normal operation, operator can be according to S.O.P. and definition standard operation
Verifying inventory.In order to realize these standard operations, crew is filled using the control being arranged in entire aircraft cockpit
It sets, the movement for constituting these programs is executed by regulation sequence.These control devices are not exclusively located in the control above crew
On panel on central control board on panel, and between crew or in instrument face plate.
Under the emergency or abnormal conditions of such as system failure, other control systems are absorbed in winged under those circumstances
The management of row device system.These control devices include display device, and that display device is presented is being executed by crew, given
The required movement of aircraft ongoing operation under abnormal conditions.
Currently, not for assist will by operator execute movement guidance system, thus standard and extremely
Program and control be concentrated in a system.Currently, these control systems are arranged in such a way flies throughout entire
On row instruments and meters panel: for normal or abnormal flight progress, for auxiliary crew member execute to control device must
The central system to be acted.
Therefore, it for convenience of crew's operation, needs to make standard and abnormal program and control to be centrally located at one to be
System in system.For convenience of crew's operation, it is also necessary to which control device is arranged into the position of a center system.
Summary of the invention
Theme described herein includes being for what the task of operational administrative guided for providing during aircraft flight
System and computer-readable medium.In certain aspects, theme described herein includes for during normal procedure or in exception
During event and/or in the event of failure that there is potential impact to flight management, the task guidance for operational administrative is provided
System and computer-readable medium.
It is a kind of for assisting what is executed by the operator of aircraft to be used for aircraft system according to that on one side, can provide
The system of the guidance of the movement of the management of system.The auxiliary system may include display unit, memory cell and processor, place
Reason device is configured to execute supplementary module with the motion guiding of the management for aerocraft system.
Theme described herein can be implemented in the software for combining hardware and/or firmware.For example, theme described herein
It can implement in the software that processor (such as hardware based processor) executes.In an exemplary implementation, it can make
Implement theme described herein with non-transitory computer-readable medium, is stored with computer in the non-transitory computer-readable medium
Executable instruction controls computer when computer executable instructions are executed by the processor of computer to carry out step.It is suitble to
Computer readable media for implementing theme described herein includes non-transient device, such as disc memory device, core
Piece storage device, programmable logic device such as field programmable gate array and specific integrated circuit.In addition, implementing to retouch herein
The computer-readable medium for the theme stated can be located in single device or computing platform, or can be distributed in multiple devices or meter
It calculates on platform.
As used herein, term " function ", " application program " and/or " module " refers to software and hardware and/or firmware
In conjunction with for implementing features described herein.In some embodiments, module may include field programmable gate array, it is dedicated
Integrated circuit or processor.
Detailed description of the invention
More specifically elaborate in the remainder of the description for those of ordinary skill in the art include its most
The complete and disclosure that can be realized of this theme of good mode, including referring to attached drawing, in which:
Fig. 1 is shown according to the dynamic for assisting being executed by aircraft operator of the various aspects that theme is described herein
The block diagram of the exemplary system of the guidance of work；
Fig. 2 schematically shows during the display normal operating according to various aspects that theme is described herein in aircraft
The display device of motion guiding during the current flight stage；And
Fig. 3 is schematically shown during the display abnormal operation according to various aspects that theme is described herein in aircraft
The display device of motion guiding during the different current flight stages.
Specific embodiment
According to description herein and illustrative relevant drawings, the aircraft for being executed by aircraft operator is disclosed
The new system of the management of operating system.In one aspect shown in Fig. 1, for example, this theme provides and is generally indicated at 1 and is
System, system 1 may be mounted on aircraft, especially on transporter.System 1 may include display unit 2, and display unit 2 can
To be arranged in aircraft cockpit.The display unit 2 may be configured to allow at least one aircraft operator (such as to fly
Office staff) and the standard guidance system of aircraft between dialogue.
In certain aspects, system 1 can also include memory cell 4 and hardware based processor 8.Memory cell
4 may include for by processor 8 execute it is one or more based on software or based on the module of firmware.For example, storage
Device unit 4 may include supplementary module 6, and supplementary module 6 may be configured to show that at least one is possible on the display unit
The aircraft flight stage indicates the current flight stage simultaneously, to be executed for the current flight stage at least one operation and with
Operate at least one corresponding movement.
In another aspect, supplementary module 6 can guide system to be communicated with aircraft, and may be configured to refer to
It leads aircraft guidance system and carries out movement associated with the current flight stage.For example, supplementary module 6 may be configured to
The carry-on system that engine start is carried out before skidding off the stage is communicated, and allows operator from by link and auxiliary
The display unit 2 that module 6 is communicated controls engine start function.Supplementary module 6 may be configured to according to another aspect,
It is communicated at least one operating database 9, operating database 9 includes and is used for standard operation, abnormal operation and additional behaviour
The related operation of the program of work and movement.
In certain aspects, display unit 2 may be configured to display at least first part 10, as shown in Figure 2, wherein
Possible mission phase can be indicated as graphical indicators 12.In certain aspects, mission phase can be expressed as connecting in succession
A series of rectangular graph indicator 12 of elongations together.In certain aspects, the explanation of mission phase can write on each
In mission phase graphical indicators 12.This series of stage may include for example, at least with the next stage: before taking off, engine rise
It is dynamic, sliding run or skid off, take off, climbing, cruising, declining, marching into the arena, landing, ground roll-out or slide-in, berth and fly after.
In order to distinguish the current flight stage, display unit 2 may be configured to protrude relative to other indicators current
Mission phase graphical indicators 13.The protrusion can be for example including or by with the illumination bigger than other stage graphical indicators 12
It illuminates graphical indicators 13 or changes the color composition of graphical indicators 13 relative to other graphical indicators 12.In some sides
In face, interacted by operator with the label 14 being arranged in first part 10, first part 10 may be configured to show
Show any mission phase graphical indicators 12 other than current flight stage graphical indicators 13.These labels 14 can be manipulated
It may sightless graphical indicators 12 in current-configuration to be shown in first part 10.In another aspect, supplementary module 6
It may be configured to the mission phase shown in the first part 10 for allowing operator to select display unit 2.Mission phase figure
Indicator 12 may be configured to through operator's use example if any the tactic movement for touching screen function come directly interaction.The touching
Feel that selection can permit operator and select any mission phase and viewing operation associated with the moment and movement.Display
The first part 10 of unit 2 also may be configured to show basic operation data, carry out more particularly, to aircraft exterior
The data of communication or about take off or close to runway data.First part 10 also may be configured to display time flight number
According to, for example scheduled take off or landing times.
In certain aspects, display unit 2 may be configured to display second part 20, wherein with the current flight stage
The current flight stage corresponding operating list that graphical indicators 13 indicate can be shown as shown in Figures 2 and 3.In another party
In face, at least one operation can be typically shown on display unit 2 by rectangular operation graphical indicators 22.Some
In aspect, operation graphical indicators 12 may include the explanation of the relevant operation write in graphical indicators.
In certain aspects, the operation of operation graphical indicators 12 instruction can be compulsory, as related mission phase
A part.Such imperative operation can be drawn with the normal flight operations of origin from S.O.P. (SOP) or ancillary technique
It leads to determine, usually the operation sequence remembered of unit operation personnel.It is strong that at least one imperative operation may be configured to display
System operation graphical indicators 24, give imperative operation graphical indicators 24 using particular color or more high radiance as to operator
Instruction: during the current flight stage, it is necessary to execute the relevant operation.For example, as shown in Fig. 2, for the current flight stage
The imperative operation of " engine start " by be " engine start " that graphical indicators 24 indicate operation.
Such as using the haptic device that can be obtained with touch screen device, and it is associated with desired operation by selecting
Operation graphical indicators 22, supplementary module 6 may be configured to allow operator select display unit 2 second part 20 in
The operation of display.In the case where having selected operation using operation graphical indicators 22, current operation can be become and can
To be indicated by current operation graphical indicators 26, after operator's selection, current operation graphical indicators 26 can be moved to
The center of second part 20, and may be configured to prominent relative to other operation graphical indicators 22.The protrusion can wrap
Include or by with than other operate the bigger illumination of graphical indicators 22 illuminate graphical indicators 26 or relative to other figures indicate
Device 22 changes the color composition of graphical indicators 26.
In addition, in certain aspects, supplementary module 6 may be configured to 22 He of operation graphical indicators that will currently show
The mission phase indicator 12 currently shown links, so that operator can be with shadow to the selection of mission phase graphical indicators 12
Ring the change of the operation graphical indicators 22 shown in the second part 20 of display unit 2.
In certain aspects, the second part 20 of display unit 2, which may be configured to instruction, has the operation figure completed
At least one of indicator 27 completes operation, and the operation graphical indicators 27 of completion can be disposed in the second of display unit 2
On the left side of part 20.The operation graphical indicators 27 of completion may be configured to prominent relative to other operation graphical indicators 22
Out.The protrusion may include or by illuminating graphical indicators 27 or opposite with operating the bigger illumination of graphical indicators 22 than other
Change the color composition of graphical indicators 27 in other graphical indicators 22.The graphical indicators 27 of completion also may be configured to
Including some labels for indicating its completion status.As shown in Figures 2 and 3, these labels may include check mark.
In certain aspects, the second part 20 of display unit 2 may be configured to selectively actuatable graphical indicators
25 instructions at least one selectively actuatable corresponding with the current flight stage.It can be as follows to operator including selectively actuatable
It is convenient: during aircraft operation, operator's memory being relied on the risk of mitigation obscured with imperative operation or stopping recalling
All possible available action becomes necessary operation preparing to be potentially based on position or background.
In certain aspects, display unit 2 also may be configured to display Part III 40, wherein can show at least
One movement corresponding with current operation and current flight stage.Rectangle movement figure instruction can be used at least one movement
Device 30 is shown, during normal flight operations, rectangle movement graphical indicators 30 can be arranged to true by S.O.P.
The list of fixed priority ranking or the inventory that the program for abnormal operation is described in detail.The priority ranking of movement can permit
Perhaps operator follows correct program in a manner of seeing and do, this will not depend on operator and remember whole group program and according to memory
Execute them.The presentation of the movement by orderly fashion, which has, allows operator to manage aerocraft system in the best way in addition
The advantages of.
Supplementary module 6 may be configured to the haptic methods that available touch screen device acquisition is preferably used or device simultaneously
And by selecting movement graphical indicators 30 associated with expectation movement, operator is allowed to select the third portion of display unit 2
Divide the movement shown in 40.In certain aspects, operator can influence and the movement selection of movement graphical indicators 30
Associated aerocraft system reconfigures.For example, as shown in Fig. 2, movement associated with movement " preparing A/C for deicing "
The selection of graphical indicators 33 can influence the closing of outflow valve door before and after aircraft so that aircraft waterproof and be used for deicing behaviour
Make.
In certain aspects, supplementary module 6 may be configured to execute induction movement, such as including that can make to control on machine
System determines the movement of those of sensor of completion status of movement.For example, " preparing A/ with movement graphical indicators 33 for deicing
C " it is associated movement be after performing movement, can based on the sensory feedback from carry-on outflow valve door and by
It is shown as the induction completed movement.
Supplementary module 6 also may be configured to execute non-inductive movement, for example not include that control system on machine can be made true
Determine the movement of those of their sensor of completion status.For example, associated with movement graphical indicators 34 " request is sprayed "
Movement is that the movement of audio or textcommunication must be carried out between aircraft operator and deicing personnel, in this way without corresponding
Sensor determines the completion of movement.Alternatively, the completion of the movement can be determining by operator and be indicated through display unit 2
To supplementary module 6.In some embodiments, the movement graphical indicators 34 acted for non-inductive may be configured to
Box or other geometries, wherein can when operator further selects cloth set symbol to indicate execution.
In certain aspects, movement can require operator from the selection of multiple options.Movement may be selected at least one can
It is indicated on the Part III 40 of display unit 2 so that movement graphical indicators 36 may be selected by least one, movement may be selected
The circle or other geometries that is arranged in and may be selected on movement graphical indicators 36 can be used in graphical indicators 36, wherein
Can when operator further selects cloth set symbol to indicate determining option.For example, as shown in Fig. 2, in the anti-ice operation phase
Between, there is the selection of several deicing liquids that can be used.Operator can be associated with specific type liquid optional by selecting
Movement graphical indicators 36 are selected to select the option of liquid.In addition, the centralization of the movement can be provided with best and efficient
Mode manages the advantages of system of aircraft from high functional level to low-function level.
In certain aspects, three parts of display unit 2 can be linked, so that the selection on a picture influences to appoint
Available options and option state what on his picture.For example, by selecting any mission phase graphical indicators 12, operator
Operation associated with the mission phase can be watched, because operation is illustrated by associated operation graphical indicators 22.In addition,
Operator can choose the associated any available action graphical indicators 22 of mission phase with selection, then can watch with
The associated movement of operation illustrated by corresponding actions graphical indicators 30.The function can permit operator and predict following appoint
Business, or look back having executed for task.The link between three parts of picture, which overcomes, not to be lost movement and is operating it
Between relationship risk in the case where the length with multiple movements that is difficult to carry out of pilot operation the problem of.The link is to concentrate
Mode provides between complex operations and associated movement clear and management connection, possible is obscured and mistake with reducing.
It is associated with the operation of selection that current operation graphical indicators 26 indicate that supplementary module 6 may be configured so that
At least one movement can be performed automatically.It is each and each that this has the advantages that permission operator she or he is not concerned with initiation
A movement is further simplified their responsibility, reduces amount of work, and improve the optimization and efficiency of flight operation.
In one aspect shown in Fig. 2, the Part III 40 of display unit 2 also may be configured to include that summary is shown
32, summary shows that 32 can be schematically illustrated aerocraft system associated with the operation graphical indicators 26 currently selected.
If the action request aerocraft system configuration that operator executes during the operation sequence that movement graphical indicators 30 are described in detail
Change and have the sensing data for indicating those system modes, then system mode can be indicated on summary and show on 32.Example
Such as, as shown in Fig. 2, outflow valve door is displayed on summary shows in 32, summary shows that 32 show the aircraft view being seen from above.
The state of outflow valve door shows in summary and can be indicated as opening or closing on 32, by closing outflow valve door during deicing program
Relevant action graphical indicators 30 state determine.Indicated by not homologous ray as shown in Figure 3, summary shows that 32 can be matched
It is set to any amount of aerocraft system of display.
In addition, summary shows that 32 may be configured to appear in summary by directly selecting and show corresponding system in 32,
To control the execution of movement associated there.It is the basis during flight operation that the characteristic is provided an additional advantage in that operator
The increased control possibility of his or her preference.
System disclosed herein has the advantages that the standardization program and abnormal flight thing during normal flight in operation
The abnormal program to come into force during part concentrates in individual system, and is shown on single display unit 2.Display unit 2 specifically may be used
To show the list for the movement to execute for standard operation and abnormal operation, and it is relevant to given aircraft specification additional
Operation.For this purpose, above-mentioned database 9 may include operation related with standardization program, abnormal program and any appendage and move
Make.Standard operation is operations that all flights execute during being up, and during misoperation, in problem, failure
In the case of, or when the system of aircraft is defective, use abnormal operation.
In certain aspects, auxiliary system may include linking for the monitoring server 7 external with auxiliary system itself,
Transmit information relevant to the monitoring of aerocraft system.Permission fault detection is linked with this of monitoring server, to assist mould
Block 6 can provide the operation guide for the abnormal program for being related to being executed.
Fig. 3 shows under the abnormal operating condition as caused by trouble or failure, especially on machine fuel leakage exception
In the case of display unit 2 embodiment.Monitoring server 7 can detecte the leakage of the fuel on machine in system, and via logical
The link crossed between server and module transmits this information to supplementary module 6.The information of the transmission can automatically lead to trigger
With the corresponding sequence of operations of exception program and associated movement caused by failure.Therefore, once detecting problem, auxiliary
System 1 can propose that aircraft to solve the problems, such as, is otherwise placed in by a series of movements to be carried out and the operation to be taken immediately
Flight optimization condition.The processing of the automatic proposition movement can produce the operation figure instruction of completion associated with troubleshooting
Device 27, and the current operation graphical indicators 26 by updating protrude and new effective operation of instruction, the current operation of update
The operation graphical indicators 27 that graphical indicators 26 are completed before being linked to.Summary shows that 32 can also dynamically update to show
Failure system is illustrated in figure 3 fuel system on machine.In certain aspects, summary show 32 can provide it is current about system
The information of state, the details including failure.As an example, Fig. 3 shows in system fuel between remaining fuel, fuel tank
Imbalance, fuel flow rate and engine condition.Fig. 3 is also shown in embodiments, current action graphical indicators 33
It may be configured to just carrying out in movement or show state instruction when unfinished.Specifically, Fig. 3 is shown " carries out with state
In (maximum 30 minimum) " movement " L/R loss is compared " and small sign indicators 42 to show the property of the movement just carried out.
Although herein by reference to specific aspect, feature and illustrative embodiments, describe aircraft guiding assistance system and
Computer-readable medium, but it is to be understood that the use of theme is not limited thereby, and is extended into and including many other
Modification, modification and alternative embodiment, are based on disclosure herein, and the those of ordinary skill in the field of this theme will expect these
Other modifications, modification and alternative embodiment.For the technical staff with disclosure knowledge, structure described herein and spy
The various combinations and sub-portfolio of sign are expected and apparent.Any various features disclosed herein and element can with one or
More other disclosed features and element combine, unless the contrary indicated otherwise.Accordingly, claimed theme in claim
It is intended to broadly understand and explain, including all such modifications, modification and the alternative embodiment within the scope of its, and including
The equivalent of claim.
Claims (18)
1. it is a kind of for assist will by the operator of aircraft execute movement guidance system, the system comprises:
Display unit；
Memory cell；And
Processor is configured to execute the supplementary module for motion guiding with the management for aerocraft system；
Wherein, the supplementary module is configured to show that single display picture, the single display picture are same on the display unit
When show at least one of first part possible aircraft flight stage of the single display picture and described single
In at least one current flight stage, the single second part for showing picture in the first part of display picture
For at least one the to be executed operation of at least one described current flight stage and the third portion of the single display picture
At least one movement corresponding at least one described operation in point.
2. the system as claimed in claim 1, wherein the single display picture is shown:
For the display unit of the possible mission phase at least one to be executed operation；And
For the display unit of operation at least one to be executed movement of the possibility mission phase of operator selection.
3. the system as claimed in claim 1, wherein the supplementary module is further configured to display standard operation, abnormal operation
And additional operations.
4. system as claimed in claim 3, wherein the supplementary module further includes at least one database, the database
Include operation related with the program for standard operation, abnormal operation and additional operations and movement.
5. system as claimed in claim 4, wherein the supplementary module is further configured to influence and operator selection
Operate the automatic execution of corresponding movement.
6. the system as claimed in claim 1, wherein what the supplementary module was additionally configured to show on the display unit
The selection of operation.
7. system as claimed in claim 6, wherein the supplementary module is further configured to show at least one access control device
For examining the execution of the movement, and it is configured to indicate the movement executed on the display unit.
8. the system as claimed in claim 1, wherein the supplementary module is further configured to show the operation of selection and by excellent
First grade sequence shows at least one described movement associated with the operation of selection.
9. the system as claimed in claim 1, wherein the supplementary module be further configured to show on the display unit to
A few controller, the controller is associated with the movement to execute for operation and is configured to through the operator
Control the execution of associated movement.
10. system as claimed in claim 2, wherein the display unit is display configured to operation data.
11. system as claimed in claim 10, wherein the display unit is display configured to operation data, the operation
Data include carrying out communicating relevant data to the guidance system of aircraft exterior.
12. system as claimed in claim 2, wherein the display unit be further configured to allow the operator refer to
At least one associated operation of at least one mission phase other than the current flight stage.
13. the system as claimed in claim 1, wherein the supplementary module is further configured to be automatically displayed in defective system
Or at least one abnormal operation to be implemented in the case where unusual condition.
14. system as claimed in claim 13, wherein the supplementary module is further configured to the phase by showing on schematic diagram
The selection of system is answered to help the control of the execution of at least one movement.
15. system as claimed in claim 2, wherein the display unit is further configured to showing for the system of display aircraft
It is intended to, the movement of operation of system and selection of display is corresponding.
16. system as claimed in claim 2, wherein the display unit includes interactive touch screen display unit, described
Interactive touch screen display unit is configured to permit choosing of the operator to operation, movement, mission phase or schematic diagram
It selects.
17. a kind of non-transitory computer-readable medium, including comprising computer executable instructions in computer-readable medium,
When computer executable instructions are executed by the processor of computer, controls the computer and show single show on the display unit
Show that picture, the single display picture are shown simultaneously:
At least one of the first part of the single display picture possible aircraft flight stage；
At least one current flight stage in the first part of the single display picture；
In the second part of the single display picture at least one described current flight stage to be executed at least one
A operation；And
At least one movement corresponding at least one described operation in the Part III of the single display picture.
18. a kind of aircraft, including according to claim 1 to system described in any one in 16.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1350247A FR3001066B1 (en) | 2013-01-11 | 2013-01-11 | SYSTEM FOR GUIDING ACTION ASSISTANCE TO BE CARRIED OUT BY AN OPERATOR ON AN AIRCRAFT. |
| FR1350247 | 2013-01-11 | ||
| US13/905,914 US9174725B2 (en) | 2013-01-11 | 2013-05-30 | Systems for tasks guidance of operations management in an aircraft cockpit |
| US13/905,914 | 2013-05-30 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103927109A CN103927109A (en) | 2014-07-16 |
| CN103927109B true CN103927109B (en) | 2019-04-30 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410006690.1A Active CN103927109B (en) | 2013-01-11 | 2014-01-07 | System for the task guidance of operational administrative in aircraft cockpit |
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| Country | Link |
|---|---|
| CN (1) | CN103927109B (en) |
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| CN104537893B (en) * | 2014-12-11 | 2016-08-31 | 中国民航大学 | A kind of civilian pilot's flight behavior monitoring system and the method for supervision |
| FR3031585B1 (en) * | 2015-01-08 | 2020-01-10 | Airbus Operations | METHOD AND DEVICE FOR AIDING THE PILOTAGE OF AN AIRCRAFT, AT LEAST ONE FLIGHT PHASE HAVING A PLURALITY OF STEPPING STEPS. |
| CN105005601A (en) * | 2015-06-30 | 2015-10-28 | 杨珊珊 | System and method for recommending flight field of unmanned aerial vehicle |
| CN108646785B (en) * | 2018-06-22 | 2020-12-29 | 西安飞机工业（集团）有限责任公司 | Flight guidance system of airplane and improvement method |
| CN112596890B (en) * | 2021-01-08 | 2024-07-23 | 中国商用飞机有限责任公司北京民用飞机技术研究中心 | Flight program operation logic structuring method and system |
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| CN1217076A (en) * | 1996-04-30 | 1999-05-19 | 塞克斯丹航空技术公司 | Method and device for inputting and controlling flight data |
| US6236913B1 (en) * | 1996-04-30 | 2001-05-22 | Sextant Avionique | Method and device for inputting and controlling flight data |
| CN101276521A (en) * | 2007-03-28 | 2008-10-01 | 张坤元 | Caution system for airfield runway |
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| CN103927109A (en) | 2014-07-16 |
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