CN107679329A - The integrated approach and device of a variety of host computers in aeroengine control system - Google Patents
The integrated approach and device of a variety of host computers in aeroengine control system Download PDFInfo
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- CN107679329A CN107679329A CN201710936592.1A CN201710936592A CN107679329A CN 107679329 A CN107679329 A CN 107679329A CN 201710936592 A CN201710936592 A CN 201710936592A CN 107679329 A CN107679329 A CN 107679329A
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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
- G06F30/17—Mechanical parametric or variational design
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- G—PHYSICS
- G06—COMPUTING; CALCULATING OR COUNTING
- G06F—ELECTRIC DIGITAL DATA PROCESSING
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Abstract
The invention discloses a kind of integrated approach of a variety of host computers in aeroengine control system, wherein, including：The configuration information of each host computer is obtained, and the configuration information of multiple host computers is formed into configuration file；Judge whether configuration file is empty；When configuration file is not space-time, the installation path of each host computer in configuration file is obtained；Whether the installation path for judging to obtain each host computer in configuration file succeeds；When the installation path success for obtaining each host computer in configuration file, according to the function button of the installation path dynamic generation of each host computer host computer；Create the left button of the function button for the function button of each host computer and click function and right button clicks function.The invention also discloses a kind of integrating device of a variety of host computers in aeroengine control system.The integrated approach of a variety of host computers solves the problems, such as that a variety of host computers use chaotic in aeroengine control system in aeroengine control system provided by the invention.
Description
Technical field
The present invention relates in aeroengine control system technical field, more particularly to a kind of aeroengine control system
The integrating device of a variety of host computers in the integrated approach of a variety of host computers and a kind of aeroengine control system.
Background technology
The normal operation of aeroengine control system needs the support of substantial amounts of auxiliary operation class software, is made according to difference
With the different host computer instrument of situation and different functional developments, with meet the monitoring of the data of aeroengine control system,
Parameter modification, transducer calibration, software burning, historical data such as read at the operation, the installations of so many support programs and renewal
Management is very necessary.
Current aerospace engine control system ground-support device uses relatively more, the different work people of the personnel being related to
When member can not determine the software using which version, it will reinstall and oneself think suitable software, equipment table just occurs
There is the upper computer software of multiple said functions on face, but version is different, and can become more and more, host computer is increasingly
Disorderly, the increasing of manpower maintenance cost is caused indirectly.
Therefore, how to avoid multiple host computers turns into those skilled in the art urgently using the chaotic risk brought
The technical problem of solution.
The content of the invention
It is contemplated that at least solves one of technical problem present in prior art, there is provided a kind of aero-engine control
In system in the integrated approach of a variety of host computers and a kind of aeroengine control system a variety of host computers integrating device., with
Solve the problems of the prior art.
As the first aspect of the invention, there is provided the integrated side of a variety of host computers in a kind of aeroengine control system
Method, wherein, aeroengine control system includes control device and a variety of host computers being connected with the control device, every kind of
Host computer is used to send control instruction to the control device, and the control instruction that a variety of host computers are sent is different, every kind of
Host computer includes configuration information, and the integrated approach includes：
The configuration information of each host computer is obtained, and the configuration information of multiple host computers is formed into configuration file, wherein, Mei Geshang
The installation path of the host computer is stored with the configuration information of position machine；
Judge whether the configuration file is empty；
When the configuration file is not space-time, the installation path of each host computer in the configuration file is obtained；
Whether the installation path for judging to obtain each host computer in the configuration file succeeds；
When the installation path success for obtaining each host computer in the configuration file, according to the installation path of each host computer
The function button of the dynamic generation host computer；
Create the left button of the function button for the function button of each host computer and click function and right button clicks function.
Preferably, the integrated approach includes：
When the configuration file is space-time, the warning information of " configuration file reads failure " is sent.
Preferably, the integrated approach includes：
When the installation path for obtaining each host computer in the configuration file is unsuccessful, the announcement of " configuration format mistake " is sent
Alert information.
Preferably, the configuration information for obtaining each host computer, and the configuration information of multiple host computers is formed into configuration
File includes：The configuration information of multiple host computers is formed into configuration file or automatically by the configuration information shape of multiple host computers manually
Into configuration file.
Preferably, it is described manually to include the configuration information formation configuration file of multiple host computers：
The configuration information of each host computer is set according to agreement form；
The configuration information of the multiple host computers set according to agreement form is formed into configuration file.
Preferably, it is described automatically to include the configuration information formation configuration file of multiple host computers：
Automatically extract the configuration information of each host computer；
According to the form of the configuration information of each host computer of configuration information tissue automatically extracted；
The configuration information for each host computer organized is formed into configuration file.
Preferably, the left button is clicked function and included when clicking the function button by left button, opens the function and presses
Host computer corresponding to button.
Preferably, the right button click function include when clicking the function button by right button, recall the function by
The menu of host computer corresponding to button.
As the second aspect of the invention, there is provided the integrated dress of a variety of host computers in a kind of aeroengine control system
Put, wherein, aeroengine control system includes control device and a variety of host computers being connected with the control device, every kind of
Host computer is used to send control instruction to the control device, and the control instruction that a variety of host computers are sent is different, every kind of
Host computer includes configuration information, and the integrating device includes：
Configuration file forms module, and the configuration file forms the configuration information that module is used to obtain each host computer, and will be more
The configuration information of individual host computer forms configuration file, wherein, it is stored with the host computer in the configuration information of each host computer
Installation path；
First judge module, first judge module are used to judge whether the configuration file is empty；
Acquisition module, the acquisition module obtain each in the configuration file for being not space-time when the configuration file
The installation path of host computer；
Second judge module, second judge module are used to judge the installation for obtaining each host computer in the configuration file
Whether path succeeds；
Function button generation module, the function button generation module are used for when each host computer in the acquisition configuration file
Installation path success when, according to the function button of the installation path dynamic generation of each host computer host computer；
Function creation module, the function creation module are used to create the function button for the function button of each host computer
Left button clicks function and right button clicks function.
Preferably, the integrating device also includes：
First alarm module, first alarm module send " configuration file reading mistake for being space-time when the configuration file
Lose " warning information；
Second alarm module, second alarm module are used for when the installation road for obtaining each host computer in the configuration file
When footpath is unsuccessful, the warning information of " configuration format mistake " is sent.
The integrated approach of a variety of host computers in aeroengine control system provided by the invention, by not being same as above multiple
The configuration information of position machine forms configuration file, and realizes by the configuration file reflecting one by one for the installation path of multiple host computers
To penetrate, it is ensured that the source of the host computer used is one, realizes to integrate a variety of host computers and is managed collectively, therefore,
By the way that a variety of host computers are integrated, solve use of the aeroengine control system to occurring during a variety of host computer uses
Caused by confusion the problem of maintenance cost increase, while avoid the generation controlled risk brought due to misuse.
Brief description of the drawings
Accompanying drawing is for providing a further understanding of the present invention, and a part for constitution instruction, with following tool
Body embodiment is used to explain the present invention together, but is not construed as limiting the invention.In the accompanying drawings：
Fig. 1 is the flow chart of the integrated approach of a variety of host computers in aeroengine control system provided by the invention.
Fig. 2 is that the idiographic flow of the integrated approach of a variety of host computers in aeroengine control system provided by the invention shows
It is intended to.
Fig. 3 is the configuration file in the integrated approach of a variety of host computers in aeroengine control system provided by the invention
With the corresponding relation schematic diagram of a variety of host computers.
Fig. 4 is the structural representation of the integrating device of a variety of host computers in aeroengine control system provided by the invention
Figure.
Embodiment
The embodiment of the present invention is described in detail below in conjunction with accompanying drawing.It should be appreciated that this place is retouched
The embodiment stated is merely to illustrate and explain the present invention, and is not intended to limit the invention.
As the first aspect of the invention, there is provided the integrated side of a variety of host computers in a kind of aeroengine control system
Method, wherein, as shown in figure 1, aeroengine control system includes control device and is connected with the control device a variety of
Host computer, every kind of host computer is used to send control instruction to the control device, and the control instruction that a variety of host computers are sent is mutual
Differ, every kind of host computer includes configuration information, and the integrated approach includes：
S110, the configuration information for obtaining each host computer, and the configuration information of multiple host computers is formed into configuration file, wherein,
The installation path of the host computer is stored with the configuration information of each host computer；
S120, judge whether the configuration file is empty；
S130, when the configuration file is not space-time, obtain the installation path of each host computer in the configuration file；
Whether S140, the installation path for judging to obtain each host computer in the configuration file succeed；
S150, when the installation path success for obtaining each host computer in the configuration file, according to the peace of each host computer
Fill the function button of the path dynamic generation host computer；
The left button that S160, the function button for each host computer create the function button clicks function and right button clicks function.
The integrated approach of a variety of host computers in aeroengine control system provided by the invention, by not being same as above multiple
The configuration information of position machine forms configuration file, and realizes by the configuration file reflecting one by one for the installation path of multiple host computers
To penetrate, it is ensured that the source of the host computer used is one, realizes to integrate a variety of host computers and is managed collectively, therefore,
By the way that a variety of host computers are integrated, solve use of the aeroengine control system to occurring during a variety of host computer uses
Caused by confusion the problem of maintenance cost increase, while avoid the generation controlled risk brought due to misuse.
As a kind of specifically embodiment, when the configuration file be space-time, send " configuration file, which is read, to fail "
Warning information.
It is understood that working as the configuration file for not space-time, illustrate that the configuration information of the host computer forms and match somebody with somebody
File is put, therefore the installation path of the host computer can be got, if the configuration file is sky, sends warning information.
As another specifically embodiment, when the installation path for obtaining each host computer in the configuration file not
During success, the warning information of " configuration format mistake " is sent.
It is understood that when obtaining the installation path of host computer, it is possible to due to the mistake of configuration file format, go out
Unsuccessful situation is now obtained, at this time, it may be necessary to send the warning information of " configuration format mistake ".
Specifically, the configuration information for obtaining each host computer, and the configuration information of multiple host computers is formed into configuration
File includes：The configuration information of multiple host computers is formed into configuration file or automatically by the configuration information shape of multiple host computers manually
Into configuration file.
Further specifically, it is described manually to include the configuration information formation configuration file of multiple host computers：
The configuration information of each host computer is set according to agreement form；
The configuration information of the multiple host computers set according to agreement form is formed into configuration file.
Further specifically, it is described automatically to include the configuration information formation configuration file of multiple host computers：
Automatically extract the configuration information of each host computer；
According to the form of the configuration information of each host computer of configuration information tissue automatically extracted；
The configuration information for each host computer organized is formed into configuration file.
Preferably, the left button is clicked function and included when clicking the function button by left button, opens the function and presses
Host computer corresponding to button.
Preferably, the right button click function include when clicking the function button by right button, recall the function by
The menu of host computer corresponding to button.
On the integrated approach of a variety of host computers in aeroengine control system provided by the invention, its specific work
Flow chart is referred to shown in Fig. 2.
It should be noted that the integrated approach that the present invention provides a variety of host computers in aeroengine control system can lead to
Integration tool is crossed to be managed collectively a variety of host computers.
Specifically, the integration tool uses specific software development environment, creates integration tool framework, sets integration tool
Configuration file, the installation path of each upper computer software described in this configuration file.For convenience of understanding, set in configuration file
Configure the explanation of sample and form.
Then according to the installation path of each upper computer software in configuration file, the dynamic generation pair on integration tool interface
The upper computer software icon answered, wherein each upper computer software icon is set according to the executable file pattern ratio of former upper computer software
Meter, and follow former upper computer software title after each icon closely and annotated, as shown in Figure 3.
Designing after this integration tool is opened has top set hidden function.By the movement of mouse realize the display at interface with it is hidden
Hide, to prevent from forgetting stowed position, using computer display lower right corner small icon pattern, clicking on the wake-up of this small icon, this is integrated
Instrument carries out position display.
It should be noted that user must install corresponding upper computer software before using upper computer software, installing
After complete, write using the fullpath of corresponding host computer executable file on computers as a configuration information to integrated work
Has configuration file, as shown in figure 1, this instrument provides two kinds of collocation methods：1）Manual configuration（Configuration format configures in integration tool
File is arranged with comment）；2）The upper computer software executable file pulled after installing is fast to integration tool interface
Victory configuration（Instrument writes information into the configuration file of integration tool automatically）.
It should also be noted that, calling drag function method, automatic setting configuration information is set in drag function method
Logic, first according to file is pulled using associated data information technology is obtained, get the relevant information for pulling file, and extract
File path, file name in this information etc., the form of configuration information is then organized according to the information of extraction, is then passed through
Read byte stream text techniques and open configuration file, the information organized is write into configuration file, is then shut off configuration file, this
Sample pulls file and realizes that automatically configuring function is achieved that
On the one hand this configuration file facilitates upper computer software attendant to search the information such as the installation path of current upper computer software,
Safeguard the renewal of upper computer software；On the one hand it is newest to ensure each upper computer software current version, avoids attendant's misuse old
Version software causes damage.
Subsequently in use, the renewal of upper computer software, and the flowing of engine maintenance personnel be can be potentially encountered
Property is especially big, and therefore, attendant can find early version host computer address by this work by the configuration information in integration tool
Tool is updated, and the configuration file of such case integration tool can not have to update again.If attendant needs to change mesh
Record is reinstalled, then is reconfigured this time more after the former corresponding host computer configuration information for being currently needed for renewal can be deleted
New upper machine information.
It is as follows on specifically used process of the integration tool during a variety of host computers are managed：Host computer integrates work
After tool starts, read byte stream text techniques and open configuration file, and the information in configuration file is read according to agreement form
Out, put in the buffer, be then shut off data flow, complete the reading of configuration file.According to the configuration information in configuration file
Number, circulation dynamic generation correspond to the button control of number, and automatic setting button control puts in order and position, and by each correspondence
The icon information of position machine software is arranged in the icon attribute of button control, the name information of host computer is arranged on into button control
Text attribute in.Meanwhile integration tool interface carries out the attribute such as equal proportion amplification, same font according to button maximum position
Beautification setting can be carried out.
When mouse is placed on above button, a small rectangle pop-up window can be called, i.e. user's mouse pointer is being controlled
Display information when above part, this tool information are arranged to the destination address of instrument.
When click right, instrument can call the menu of addition to show control, and the pad name that developer is defined is shown
Out, and in the corresponding menu of display function logic is set, searches mesh such as self-defined two common functions of this instrument in a menu
Mark and opening configuration file, when clicking on lookup targets option, instrument corresponds to read in caching according to control matches somebody with somebody confidence
Breath（The routing information of host computer）Launching process resource instruction unpack corresponding folder path is directly invoked, realizes and searches target work(
Energy；When clicking on opening Profile option, the configuration file for starting this instrument of process resource instruction unpack is directly invoked, is used for
Check configuration information or modification configuration information.
When clicking on left button, integration tool can by reading the configuration information in caching, with reference to the control of corresponding generation,
That configuration information path and executable file title corresponding to control are extracted, pass through calling process resource instruction unpack
Corresponding executable file, realization, which is equal to, to be found corresponding host computer and double-clicks the operation of opening
As the second aspect of the invention, there is provided the integrating device of a variety of host computers in a kind of aeroengine control system,
Wherein, aeroengine control system includes control device and a variety of host computers being connected with the control device, Mei Zhongshang
Position machine is used to send control instruction to the control device, and the control instruction that a variety of host computers are sent is different, Mei Zhongshang
Position machine includes configuration information, as shown in figure 4, the integrating device 10 includes：
Configuration file forms module 110, and the configuration file forms the configuration information that module 110 is used to obtain each host computer,
And the configuration information of multiple host computers is formed into configuration file, wherein, it is stored with the configuration information of each host computer on this
The installation path of position machine；
First judge module 120, first judge module 120 are used to judge whether the configuration file is empty；
Acquisition module 130, the acquisition module 130 are obtained in the configuration file for being not space-time when the configuration file
Each host computer installation path；
Second judge module 140, second judge module 140 are used to judge to obtain each host computer in the configuration file
Installation path whether succeed；
Function button generation module 150, the function button generation module 150 are used for each in the configuration file when obtaining
During the installation path success of host computer, according to the function button of the installation path dynamic generation of each host computer host computer；
Function creation module 160, the function creation module 160 are used to create the function for the function button of each host computer
The left button of button clicks function and right button clicks function.
The integrating device of a variety of host computers in aeroengine control system provided by the invention, by not being same as above multiple
The configuration information of position machine forms configuration file, and realizes by the configuration file reflecting one by one for the installation path of multiple host computers
To penetrate, it is ensured that the source of the host computer used is one, realizes to integrate a variety of host computers and is managed collectively, therefore,
By the way that a variety of host computers are integrated, solve use of the aeroengine control system to occurring during a variety of host computer uses
Caused by confusion the problem of maintenance cost increase, while avoid the generation controlled risk brought due to misuse.
Specifically, the integrating device 10 also includes：
First alarm module 170, first alarm module send " configuration file reading for being space-time when the configuration file
Take failure " warning information；
Second alarm module 180, second alarm module are used for when the peace for obtaining each host computer in the configuration file
When dress path is unsuccessful, the warning information of " configuration format mistake " is sent.
It is understood that the principle that embodiment of above is intended to be merely illustrative of the present and the exemplary implementation that uses
Mode, but the invention is not limited in this.For those skilled in the art, the essence of the present invention is not being departed from
In the case of refreshing and essence, various changes and modifications can be made therein, and these variations and modifications are also considered as protection scope of the present invention.
Claims (10)
1. the integrated approach of a variety of host computers in a kind of aeroengine control system, it is characterised in that aero-engine controls
System includes control device and a variety of host computers being connected with the control device, and every kind of host computer is used to fill to the control
Transmission control instruction is put, and the control instruction that a variety of host computers are sent is different, every kind of host computer includes configuration information, institute
Stating integrated approach includes：
The configuration information of each host computer is obtained, and the configuration information of multiple host computers is formed into configuration file, wherein, Mei Geshang
The installation path of the host computer is stored with the configuration information of position machine；
Judge whether the configuration file is empty；
When the configuration file is not space-time, the installation path of each host computer in the configuration file is obtained；
Whether the installation path for judging to obtain each host computer in the configuration file succeeds；
When the installation path success for obtaining each host computer in the configuration file, according to the installation path of each host computer
The function button of the dynamic generation host computer；
Create the left button of the function button for the function button of each host computer and click function and right button clicks function.
2. the integrated approach of a variety of host computers in aeroengine control system according to claim 1, it is characterised in that
The integrated approach includes：
When the configuration file is space-time, the warning information of " configuration file reads failure " is sent.
3. the integrated approach of a variety of host computers in aeroengine control system according to claim 1, it is characterised in that
The integrated approach includes：
When the installation path for obtaining each host computer in the configuration file is unsuccessful, the announcement of " configuration format mistake " is sent
Alert information.
4. the integrated side of a variety of host computers in aeroengine control system as claimed in any of claims 1 to 3
Method, it is characterised in that the configuration information for obtaining each host computer, and the configuration information of multiple host computers is formed into configuration text
Part includes：The configuration information of multiple host computers is formed into configuration file manually or automatically formed the configuration information of multiple host computers
Configuration file.
5. the integrated approach of a variety of host computers in aeroengine control system according to claim 4, it is characterised in that
It is described manually to include the configuration information formation configuration file of multiple host computers：
The configuration information of each host computer is set according to agreement form；
The configuration information of the multiple host computers set according to agreement form is formed into configuration file.
6. the integrated approach of a variety of host computers in aeroengine control system according to claim 4, it is characterised in that
It is described automatically to include the configuration information formation configuration file of multiple host computers：
Automatically extract the configuration information of each host computer；
According to the form of the configuration information of each host computer of configuration information tissue automatically extracted；
The configuration information for each host computer organized is formed into configuration file.
7. the integrated side of a variety of host computers in aeroengine control system as claimed in any of claims 1 to 3
Method, it is characterised in that the left button, which clicks function, to be included when clicking the function button by left button, opens the function button
Corresponding host computer.
8. the integrated side of a variety of host computers in aeroengine control system as claimed in any of claims 1 to 3
Method, it is characterised in that the right button, which clicks function, to be included when clicking the function button by right button, recalls the function button
The menu of corresponding host computer.
9. the integrating device of a variety of host computers in a kind of aeroengine control system, it is characterised in that aero-engine controls
System includes control device and a variety of host computers being connected with the control device, and every kind of host computer is used to fill to the control
Transmission control instruction is put, and the control instruction that a variety of host computers are sent is different, every kind of host computer includes configuration information, institute
Stating integrating device includes：
Configuration file forms module, and the configuration file forms the configuration information that module is used to obtain each host computer, and will be more
The configuration information of individual host computer forms configuration file, wherein, it is stored with the host computer in the configuration information of each host computer
Installation path；
First judge module, first judge module are used to judge whether the configuration file is empty；
Acquisition module, the acquisition module obtain each in the configuration file for being not space-time when the configuration file
The installation path of host computer；
Second judge module, second judge module are used to judge the installation for obtaining each host computer in the configuration file
Whether path succeeds；
Function button generation module, the function button generation module are used for when each host computer in the acquisition configuration file
Installation path success when, according to the function button of the installation path dynamic generation of each host computer host computer；
Function creation module, the function creation module are used to create the function button for the function button of each host computer
Left button clicks function and right button clicks function.
10. the integrating device of a variety of host computers in aeroengine control system according to claim 9, its feature exist
In the integrating device also includes：
First alarm module, first alarm module send " configuration file reading mistake for being space-time when the configuration file
Lose " warning information；
Second alarm module, second alarm module are used for when the installation road for obtaining each host computer in the configuration file
When footpath is unsuccessful, the warning information of " configuration format mistake " is sent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710936592.1A CN107679329B (en) | 2017-10-10 | 2017-10-10 | Method and device for integrating various upper computers in aircraft engine control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201710936592.1A CN107679329B (en) | 2017-10-10 | 2017-10-10 | Method and device for integrating various upper computers in aircraft engine control system |
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| Publication Number | Publication Date |
|---|---|
| CN107679329A true CN107679329A (en) | 2018-02-09 |
| CN107679329B CN107679329B (en) | 2021-09-03 |
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ID=61138838
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201710936592.1A Active CN107679329B (en) | 2017-10-10 | 2017-10-10 | Method and device for integrating various upper computers in aircraft engine control system |
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Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7266807B2 (en) * | 2002-12-20 | 2007-09-04 | Hitachi, Ltd. | Method for integration edition of setting file and setting file integration base |
| CN103455640A (en) * | 2013-09-29 | 2013-12-18 | 宇龙计算机通信科技(深圳)有限公司 | Method and device for displaying file management interfaces |
| CN103995833A (en) * | 2014-04-21 | 2014-08-20 | 深圳天珑无线科技有限公司 | Method and device for sharing configuration information |
| CN105630932A (en) * | 2015-12-22 | 2016-06-01 | 北京奇虎科技有限公司 | Method and device for managing files of intelligent terminals |
| CN106775725A (en) * | 2016-12-19 | 2017-05-31 | 网易（杭州）网络有限公司 | A kind of visual configuration edit methods and device |
-
2017
- 2017-10-10 CN CN201710936592.1A patent/CN107679329B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7266807B2 (en) * | 2002-12-20 | 2007-09-04 | Hitachi, Ltd. | Method for integration edition of setting file and setting file integration base |
| CN103455640A (en) * | 2013-09-29 | 2013-12-18 | 宇龙计算机通信科技(深圳)有限公司 | Method and device for displaying file management interfaces |
| CN103995833A (en) * | 2014-04-21 | 2014-08-20 | 深圳天珑无线科技有限公司 | Method and device for sharing configuration information |
| CN105630932A (en) * | 2015-12-22 | 2016-06-01 | 北京奇虎科技有限公司 | Method and device for managing files of intelligent terminals |
| CN106775725A (en) * | 2016-12-19 | 2017-05-31 | 网易（杭州）网络有限公司 | A kind of visual configuration edit methods and device |
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| Publication number | Publication date |
|---|---|
| CN107679329B (en) | 2021-09-03 |
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