CN109598021A - A kind of information display method, device, equipment and storage medium - Google Patents
A kind of information display method, device, equipment and storage medium Download PDFInfo
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- 238000000034 method Methods 0.000 title claims abstract description 35
- 230000006378 damage Effects 0.000 claims abstract description 158
- 230000006735 deficit Effects 0.000 claims abstract description 28
- 238000004590 computer program Methods 0.000 claims description 12
- 230000000007 visual effect Effects 0.000 claims description 6
- 238000010276 construction Methods 0.000 claims description 4
- 238000010586 diagram Methods 0.000 description 10
- 230000006870 function Effects 0.000 description 6
- 208000027418 Wounds and injury Diseases 0.000 description 5
- 230000006854 communication Effects 0.000 description 4
- 238000004891 communication Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 2
- 208000012880 Finger injury Diseases 0.000 description 1
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- 239000004973 liquid crystal related substance Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000004065 semiconductor Substances 0.000 description 1
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
- G06F30/00—Computer-aided design [CAD]
- G06F30/10—Geometric CAD
- G06F30/15—Vehicle, aircraft or watercraft design
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T17/00—Three dimensional [3D] modelling, e.g. data description of 3D objects
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06T—IMAGE DATA PROCESSING OR GENERATION, IN GENERAL
- G06T19/00—Manipulating 3D models or images for computer graphics
- G06T19/20—Editing of 3D images, e.g. changing shapes or colours, aligning objects or positioning parts
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Abstract
This application discloses a kind of information display method, device, equipment and storage mediums.This method comprises: the threedimensional model of building aircraft；Wherein, the three-dimensional model structure is corresponding with the aircaft configuration；The location information respectively damaged based on the aircraft adds damage score in the corresponding position of the threedimensional model；Damage score in the threedimensional model is mapped to two-dimensional space, generates the damage figure for characterizing the aircraft damage situation.The damage figure that the technical program generates can directly reflect the degree of impairment of aircraft each position, more intuitive compared with the ways of presentation of table.
Description
Technical field
The present disclosure relates generally to airplane information process field more particularly to a kind of information display method, device, equipment and deposit
Storage media.
Background technique
Aircraft in use, operating overload, operating mistake or maintenance it is improper etc. due to, usually will cause aircraft
Damage, such as aircraft systems crack, deform and wound or burn.These damage reduce aircaft configuration intensity and just
Degree, influences the aeroperformance of aircraft.It then becomes necessary to which the degree of impairment to aircraft counts, further to grasp aircraft
Use state.Currently, the degree of impairment of aircraft mainly passes through user's active submission data and shows in a tabular form.However, this
The data of kind mode show not intuitive enough.
Summary of the invention
In view of drawbacks described above in the prior art or deficiency, it is intended to provide a kind of degree of impairment that can directly react aircraft
Scheme.
In a first aspect, the embodiment of the present application provides a kind of information display method, comprising:
Construct the threedimensional model of aircraft；Wherein, the three-dimensional model structure is corresponding with the aircaft configuration；
Based on the damage information of the aircraft, the corresponding damage mark of the damage information is added in the threedimensional model
Note；
Damage score in the threedimensional model is mapped to two-dimensional space, is generated for characterizing the aircraft damage situation
Damage figure.
Optionally, the damage information based on the aircraft, it is corresponding to add the damage information in the threedimensional model
Damage score, comprising:
Based on the position of each damage information, damage score is added on the corresponding position of the threedimensional model.
Optionally, the method also includes:
Based on the attribute of the damage information, the damage score is carried out with corresponding attribute in the threedimensional model
Association.
Optionally, the attribute includes type of impairment；
Damage score in the threedimensional model is mapped to two-dimensional space, is generated for characterizing the aircraft damage situation
Damage figure, comprising:
According to the type of impairment, the damage score in the threedimensional model is mapped to two-dimensional space, generates the damage
Wound figure.
Optionally, the damage score in the threedimensional model is mapped to two-dimensional space, generated for characterizing the aircraft
The damage figure of degree of impairment, comprising:
Based on the threedimensional model, two-dimentional aircraft brake disc corresponding with the threedimensional model is generated；Wherein, the two dimension flies
There are corresponding relationships between the three-dimensional coordinate in two-dimensional coordinate and the threedimensional model in machine image；
According to the corresponding relationship, the damage figure is generated.
Optionally, the damage score in the threedimensional model is mapped to two-dimensional space, generated for characterizing the aircraft
The damage figure of degree of impairment, comprising:
According to the viewing visual angle of setting, the damage score in the threedimensional model is mapped to two-dimensional space, described in generation
Damage figure.
Optionally, the method also includes:
Receive the export instruction of user's input；
It is instructed according to the export, the damage figure is exported and stored.
Second aspect, the embodiment of the present application also provides a kind of information display devices, comprising:
Threedimensional model construction unit, for constructing the threedimensional model of aircraft；Wherein, the three-dimensional model structure flies with described
Machine structure is corresponding；
Damage score adding unit, for the damage information based on the aircraft, in the threedimensional model described in addition
The corresponding damage score of damage information；
Figure generation unit is damaged, for the damage score in the threedimensional model to be mapped to two-dimensional space, generation is used for
Characterize the damage figure of the aircraft damage situation.
The third aspect, the embodiment of the present application also provides a kind of computer equipments, including memory, processor and storage
On a memory and the computer program that can run on a processor, the processor are realized when executing described program such as above-mentioned institute
The display methods for the aircraft damage stated.
Fourth aspect, the embodiment of the present application also provides a kind of computer readable storage mediums, are stored thereon with computer
Program, the computer program are used for:
The computer program realizes the display methods of aircraft damage as described above when being executed by processor.
The displaying scheme of aircraft damage provided by the embodiments of the present application is based on aircraft by constructing the threedimensional model of aircraft
The location information respectively damaged, add damage score in the corresponding position of the threedimensional model of building, and by the damage in threedimensional model
Wound label is mapped to two-dimensional space, generates the damage figure for characterizing aircraft damage situation.The technical program is straight using damage figure
The degree of impairment for reflecting aircraft each position is connect, it is more intuitive compared with the ways of presentation of table.
Detailed description of the invention
By reading a detailed description of non-restrictive embodiments in the light of the attached drawings below, the application's is other
Feature, objects and advantages will become more apparent upon:
Fig. 1 shows a kind of exemplary process diagram of information display method provided by the embodiments of the present application；
Fig. 2 shows a kind of exemplary block diagrams of information display device provided by the embodiments of the present application；
Fig. 3 shows the structural schematic diagram for being suitable for the computer equipment for being used to realize the embodiment of the present application.
Specific embodiment
The application is described in further detail with reference to the accompanying drawings and examples.It is understood that this place is retouched
The specific embodiment stated is used only for explaining related invention, rather than the restriction to the invention.It also should be noted that in order to
Convenient for description, part relevant to invention is illustrated only in attached drawing.
It should be noted that in the absence of conflict, the features in the embodiments and the embodiments of the present application can phase
Mutually combination.The application is described in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
Referring to FIG. 1, Fig. 1 shows the exemplary process diagram of information display method provided by the embodiments of the present application.Wherein,
This method may include:
Step 110, the threedimensional model of aircraft is constructed, three-dimensional model structure is corresponding with aircaft configuration.
Wherein it is possible to then use three-dimensional modeling according to aircraft drawing by using laser scanner scans aircraft configuration
Software building goes out the threedimensional model of aircraft.
Step 120, based on the damage information of aircraft, the corresponding damage score of damage information is added in the three-dimensional model.
Involved damage is generally referred to as the damage on aircaft configuration in the embodiment of the present application.
Specifically, step 120 can be based on the position of damage information, the addition damage mark on the corresponding position of threedimensional model
Note.
Wherein, the specific location that the position of damage information can be occurred with finger injury, including erect-position, waterline, stringer position and vertical
Parabola etc.；Based on the specific location that damage occurs, damage score is added on the corresponding position of threedimensional model.
Further, it is added in the three-dimensional model after the corresponding damage score of damage information, it can also be further
According to the attribute of damage information, damage score is associated with corresponding attribute in the three-dimensional model.
Wherein, the attribute of damage information can be, but not limited to include type of impairment, damage discovery time, damage reason and damage
Wound description etc..
In this way, engineer can check at any time the specific feelings of each damage on terminal device (such as mobile phone or computer)
Condition.
Step 130, the damage score in threedimensional model is mapped to two-dimensional space, generated for characterizing aircraft damage situation
Damage figure.
In the embodiment of the present application, when in the attribute of damage information including type of impairment, it can be generated according to type of impairment
Damage figure corresponding with type of impairment.
Specifically, when generating damage corresponding with type of impairment figure, it can be directly according to type of impairment, it will be in threedimensional model
The damage score of different type of impairment is respectively mapped to two-dimensional space, generates the corresponding damage figure of each type of impairment；It can also root
Corresponding damage figure is generated according to the instruction of user, for example receives the instruction of user's input, and specified damage class is carried in the instruction
The damage score that threedimensional model middle finger determines type of impairment is mapped to two-dimensional space according still further to the instruction received by type, and generating should
Specify the corresponding damage figure of type of impairment.
Engineer, which can be convenient, so efficiently checks the corresponding damage figure of each type of impairment of aircraft.
For example, being then pit by type of impairment in threedimensional model when carrying Notch damage type in the instruction of user's input
The damage score of type of impairment is mapped in two-dimensional space, generates Notch damage figure.
Specifically, the damage score in threedimensional model is mapped in two-dimensional space, can come by two-dimentional aircraft brake disc
It realizes.
The threedimensional model for being first depending on aircraft generates two-dimentional aircraft brake disc, wherein the two-dimensional coordinate in two-dimentional aircraft brake disc
There are corresponding relationships between the three-dimensional coordinate in threedimensional model.
Then, existing corresponding according to the two-dimensional coordinate in two-dimentional aircraft brake disc and between the three-dimensional coordinate in threedimensional model
Relationship generates damage figure.
Above-mentioned two-dimensional coordinate can refer to the pixel coordinate of two-dimentional aircraft brake disc.
Further, the damage score in threedimensional model can also be mapped to two-dimentional sky according to the viewing visual angle of setting
Between, generate damage figure.
Specifically, first threedimensional model can be adjusted to the viewing visual angle of setting, then will be in threedimensional model adjusted
Damage score is mapped to two-dimensional space, generates damage figure.
Engineer can watch the damage figure of generation by different viewing visual angles in this way, so that showing in damage figure
Degree of impairment it is more intuitive, easily facilitate engineer and check.
Furthermore it is also possible to receive the export instruction of user's input, and instructed according to the export, the damage figure of generation is exported
And it stores.
Information display scheme provided by the embodiments of the present application, by constructing the threedimensional model of aircraft, the damage based on aircraft
Information adds the corresponding damage score of damage information in the threedimensional model of building, and the damage score in threedimensional model is reflected
It is mapped to two-dimensional space, generates the damage figure for characterizing aircraft damage situation.The technical program is directly reflected using damage figure
The degree of impairment of aircraft each position, it is more intuitive compared with the ways of presentation of table.
It should be noted that although describing the operation of the method for the present invention in the accompanying drawings with particular order, this is not required that
Or hint must execute these operations in this particular order, or have to carry out operation shown in whole and be just able to achieve the phase
The result of prestige.On the contrary, the step of describing in flow chart can change and execute sequence.Additionally or alternatively, it is convenient to omit certain
Multiple steps are merged into a step and executed, and/or a step is decomposed into execution of multiple steps by step.
With further reference to Fig. 2, it illustrates a kind of examples of the display device of aircraft damage provided by the embodiments of the present application
Property structural block diagram.The device includes:
Threedimensional model construction unit 21, for constructing the threedimensional model of aircraft；Wherein, the three-dimensional model structure with it is described
Aircaft configuration is corresponding；
Damage score adding unit 22 adds institute for the damage information based on the aircraft in the threedimensional model
State the corresponding damage score of damage information；
Figure generation unit 23 is damaged, for the damage score in the threedimensional model to be mapped to two-dimensional space, generates and uses
In the damage figure for characterizing the aircraft damage situation.
Optionally, the damage score adding unit 22, is specifically used for:
Based on the position of each damage information, damage score is added on the corresponding position of the threedimensional model.
Optionally, described device further include:
Attribute Association unit 24, for the attribute based on the damage information, by the damage in the threedimensional model
Label is associated with corresponding attribute.
Optionally, the attribute includes type of impairment；
The damage figure generation unit 23, is specifically used for:
According to the type of impairment, the damage score in the threedimensional model is mapped to two-dimensional space, generates the damage
Wound figure.
Optionally, the damage figure generation unit 23, comprising:
Two-dimentional aircraft brake disc generation module 231 generates corresponding with the threedimensional model for being based on the threedimensional model
Two-dimentional aircraft brake disc；Wherein, between the three-dimensional coordinate in the two-dimensional coordinate and the threedimensional model in the two-dimentional aircraft brake disc
There are corresponding relationships；
Figure generation module 232 is damaged, for generating the damage figure according to the corresponding relationship.
Optionally, the damage figure generation unit 23, is specifically used for:
According to the viewing visual angle of setting, the damage score in the threedimensional model is mapped to two-dimensional space, described in generation
Damage figure.
Optionally, described device further include:
Instruction receiving unit 25 is exported, for receiving the export instruction of user's input；
The damage figure is exported and is stored for being instructed according to the export by lead-out unit 26.
It should be appreciated that all units or module recorded in the device and each step phase in the method with reference to Fig. 1 description
It is corresponding.It is equally applicable to the device and unit wherein included above with respect to the operation and feature of method description as a result, herein not
It repeats again.The device can be realized in advance in the electronic device, can also be loaded into electronic equipment by modes such as downloadings.
Corresponding units in the device can be cooperated with the unit in electronic equipment to realize the scheme of the embodiment of the present application.
Below with reference to Fig. 3, it illustrates the calculating of the terminal device or server that are suitable for being used to realize the embodiment of the present application
The structural schematic diagram of machine system 300.
As shown in figure 3, computer system 300 includes central processing unit (CPU) 301, it can be read-only according to being stored in
Program in memory (ROM) 302 or be loaded into the program in random access storage device (RAM) 303 from storage section 308 and
Execute various movements appropriate and processing.In RAM 303, also it is stored with system 300 and operates required various programs and data.
CPU 301, ROM 302 and RAM 303 are connected with each other by bus 304.Input/output (I/O) interface 305 is also connected to always
Line 304.
I/O interface 305 is connected to lower component: the importation 306 including keyboard, mouse etc.；It is penetrated including such as cathode
The output par, c 307 of spool (CRT), liquid crystal display (LCD) etc. and loudspeaker etc.；Storage section 308 including hard disk etc.；
And the communications portion 309 of the network interface card including LAN card, modem etc..Communications portion 309 via such as because
The network of spy's net executes communication process.Driver 310 is also connected to I/O interface 305 as needed.Detachable media 311, such as
Disk, CD, magneto-optic disk, semiconductor memory etc. are mounted on as needed on driver 310, in order to read from thereon
Computer program be mounted into storage section 308 as needed.
Particularly, in accordance with an embodiment of the present disclosure, it may be implemented as computer software above with reference to the process of Fig. 1 description
Program.For example, embodiment of the disclosure includes a kind of computer program product comprising be tangibly embodied in machine readable media
On computer program, the computer program includes program code for executing the method for Fig. 1.In such embodiment
In, which can be downloaded and installed from network by communications portion 309, and/or from 311 quilt of detachable media
Installation.
Flow chart and block diagram in attached drawing are illustrated according to the system of various embodiments of the invention, method and computer journey
The architecture, function and operation in the cards of sequence product.In this regard, each box in flowchart or block diagram can generation
A part of one module, program segment or code of table, a part of the module, program segment or code include one or more
Executable instruction for implementing the specified logical function.It should also be noted that in some implementations as replacements, institute in box
The function of mark can also occur in a different order than that indicated in the drawings.For example, two boxes succeedingly indicated are practical
On can be basically executed in parallel, they can also be executed in the opposite order sometimes, and this depends on the function involved.Also it wants
It is noted that the combination of each box in block diagram and or flow chart and the box in block diagram and or flow chart, Ke Yiyong
The dedicated hardware based system of defined functions or operations is executed to realize, or can be referred to specialized hardware and computer
The combination of order is realized.
Being described in the embodiment of the present application involved unit or module can be realized by way of software, can also be with
It is realized by way of hardware.Described unit or module also can be set in the processor, for example, can be described as:
A kind of processor includes threedimensional model construction unit, damage score adding unit and damage figure generation unit.Wherein, these lists
The title of member or module does not constitute the restriction to the unit or module itself under certain conditions, for example, threedimensional model constructs
Unit is also described as " unit for threedimensional model building ".
As on the other hand, present invention also provides a kind of computer readable storage medium, the computer-readable storage mediums
Matter can be computer readable storage medium included in device described in above-described embodiment；It is also possible to individualism, not
The computer readable storage medium being fitted into equipment.Computer-readable recording medium storage has one or more than one journey
Sequence, described program are used to execute the formula input method for being described in the application by one or more than one processor.
Above description is only the preferred embodiment of the application and the explanation to institute's application technology principle.Those skilled in the art
Member is it should be appreciated that invention scope involved in the application, however it is not limited to technology made of the specific combination of above-mentioned technical characteristic
Scheme, while should also cover in the case where not departing from the inventive concept, it is carried out by above-mentioned technical characteristic or its equivalent feature
Any combination and the other technical solutions formed.Such as features described above has similar function with (but being not limited to) disclosed herein
Can technical characteristic replaced mutually and the technical solution that is formed.
Claims (10)
1. a kind of information display method, which is characterized in that the described method includes:
Construct the threedimensional model of aircraft；Wherein, the three-dimensional model structure is corresponding with the aircaft configuration；
Based on the damage information of the aircraft, the corresponding damage score of the damage information is added in the threedimensional model；
Damage score in the threedimensional model is mapped to two-dimensional space, generates the damage for characterizing the aircraft damage situation
Wound figure.
2. information display method according to claim 1, which is characterized in that the damage information based on the aircraft, in institute
It states and adds the corresponding damage score of the damage information in threedimensional model, comprising:
Based on the position of the damage information, damage score is added on the corresponding position of the threedimensional model.
3. information display method according to claim 1, which is characterized in that the method also includes:
Based on the attribute of the damage information, the damage score is closed with corresponding attribute in the threedimensional model
Connection.
4. information display method according to claim 3, which is characterized in that the attribute includes type of impairment；
Damage score in the threedimensional model is mapped to two-dimensional space, generates the damage for characterizing the aircraft damage situation
Wound figure, comprising:
According to the type of impairment, the damage score in the threedimensional model is mapped to two-dimensional space, generates the damage figure.
5. information display method according to claim 1, which is characterized in that reflect the damage score in the threedimensional model
It is mapped to two-dimensional space, generates the damage figure for characterizing the aircraft damage situation, comprising:
Based on the threedimensional model, two-dimentional aircraft brake disc corresponding with the threedimensional model is generated；Wherein, the two-dimentional aircraft figure
There are corresponding relationships between the three-dimensional coordinate in two-dimensional coordinate and the threedimensional model as in；
According to the corresponding relationship, the damage figure is generated.
6. information display method according to claim 1, which is characterized in that reflect the damage score in the threedimensional model
It is mapped to two-dimensional space, generates the damage figure for characterizing the aircraft damage situation, comprising:
According to the viewing visual angle of setting, the damage score in the threedimensional model is mapped to two-dimensional space, generates the damage
Figure.
7. information display method according to claim 1, which is characterized in that the method also includes:
Receive the export instruction of user's input；
It is instructed according to the export, the damage figure is exported and stored.
8. a kind of information display device characterized by comprising
Threedimensional model construction unit, for constructing the threedimensional model of aircraft；Wherein, the three-dimensional model structure and the aircraft knot
Structure is corresponding；
Damage score adding unit adds the damage for the damage information based on the aircraft in the threedimensional model
The corresponding damage score of information；
Figure generation unit is damaged, for the damage score in the threedimensional model to be mapped to two-dimensional space, is generated for characterizing
The damage figure of the aircraft damage situation.
9. a kind of computer equipment, can run on a memory and on a processor including memory, processor and storage
Computer program, which is characterized in that the processor realizes the side as described in any in claim 1-7 when executing described program
Method.
10. a kind of computer readable storage medium is stored thereon with computer program, the computer program is used for:
The method as described in any in claim 1-7 is realized when the computer program is executed by processor.
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| Application Number | Priority Date | Filing Date | Title |
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| CN201811285496.6A CN109598021B (en) | 2018-10-31 | 2018-10-31 | Information display method, device, equipment and storage medium |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811285496.6A CN109598021B (en) | 2018-10-31 | 2018-10-31 | Information display method, device, equipment and storage medium |
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| CN109598021A true CN109598021A (en) | 2019-04-09 |
| CN109598021B CN109598021B (en) | 2024-03-26 |
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| CN110648396A (en) * | 2019-09-17 | 2020-01-03 | 西安万像电子科技有限公司 | Image processing method, device and system |
| CN111275812A (en) * | 2020-01-19 | 2020-06-12 | 北京恒华伟业科技股份有限公司 | Data display method and device and electronic equipment |
| CN113076602A (en) * | 2021-04-21 | 2021-07-06 | 中国商用飞机有限责任公司 | Method, system and medium for realizing three-dimension of impact damage information of composite material |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN113076602B (en) * | 2021-04-21 | 2024-04-02 | 中国商用飞机有限责任公司 | Method, system and medium for realizing three-dimensional impact damage information of composite material |
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| Publication number | Publication date |
|---|---|
| CN109598021B (en) | 2024-03-26 |
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