CN1588376A - Grendle intelligent design system and design method - Google Patents
Grendle intelligent design system and design method Download PDFInfo
- Publication number
- CN1588376A CN1588376A CN 200410050528 CN200410050528A CN1588376A CN 1588376 A CN1588376 A CN 1588376A CN 200410050528 CN200410050528 CN 200410050528 CN 200410050528 A CN200410050528 A CN 200410050528A CN 1588376 A CN1588376 A CN 1588376A
- Authority
- CN
- China
- Prior art keywords
- design
- memory
- knowledge
- scheme
- storer
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Landscapes
- Devices For Executing Special Programs (AREA)
- Management, Administration, Business Operations System, And Electronic Commerce (AREA)
Abstract
The intelligent shrapnel designing system includes integrated design CAX platform, scheme standard memory, structure parameter design memory, engineering drawing memory, scheme compiling memory, document memory, parameter drive unit, design scheme operating unit, and parameter drive constraint condition memory. After the parameter drive unit activates the scheme compiling memory and the design scheme operating unit, the scheme compiling memory realizes the knowledge acquiring and system debugging. The design scheme is then determined in the parameter drive constraint condition memory and fed to the engineering drawing memory to form the 3D model drawing and the 2D engineering drawing, while the design results and the structure drawings are stored in the document memory. The present invention completes the overall design, scheme argumentation, simulation analysis and calculation of shrapnel in computer.
Description
Technical field
The invention belongs to the howitzer designing technique, particularly a kind of howitzer intelligent design system and method for designing.
Background technology
Weaponry development fast is the demand of modern war.Shorten the product development cycle, will accelerate the renewal speed of weaponry and the speed of Fuerzas De Accion Armada, also, development, knowhow have been accumulated simultaneously, for the quality time is striven in the initiative and the triumph of winning the war for the development of new-type weapon and equipment of future generation gains time.Howitzer is most widely used general in the army of land, sea, air, a large amount of consumption and remodeling one of the ammunition faster of regenerating in modern war.Howitzer has wide in variety, becomes in batches and the characteristics of producing in enormous quantities.Abroad, developed countries such as the U.S., ammunition development speed is very fast.For example: in Kosovo War, the U.S. uses " JDAM " JDAM in a large number, can develop different guidance devices and warhead fast according to by the concrete feature of target of attack in week age, and is required to adapt to operation.But the howitzer of China some manufacturers of howitzer development means are backward relatively at present, and design, processing, assembling etc. are main by manually finishing, and the new product development cycle is long, generally needs several years, can't satisfy the modern war needs.
Research and development howitzer intelligent design system utilizes computing machine to finish howitzer overall design, demonstration, simulation simulation analysis and calculating.Thereby realize the simulation design of Simulation and the intelligentized design of product, improve the computational analysis precision, improve design and product quality, significantly reduce the number of occurrence of design, trial-production, shorten the howitzer lead time, to adapt to the demand that the howitzer model is many, become batch and production in enormous quantities and modern war.
The design system technology is an important branch in the AI field, since first design system DENDRAL that China succeeded in developing from nineteen sixty-eight, the design system technical development is rapid and increasingly mature, but most of up to now design system all is the analytic type design system, be mainly used in the task of types such as finishing explanation, diagnosis and debugging, the problem of finding the solution all is a classification problem, its conclusion all is limited among the hypothesis set of predesignating, and does not satisfy the needs that the howitzer intelligent design system is developed.
Summary of the invention
Purpose of the present invention is at the long technical matters that exists that waits of howitzer design cycle, provide a kind of computing machine that utilizes to finish howitzer overall design, demonstration, simulation simulation analysis and calculating, lead time is short, designing quality good, production efficiency is high howitzer intelligent design system and method for designing, with adapt to the howitzer model many, become in batches and requirements of large-scale production.
The present invention includes the scheme standard memory, design system CAX integrated platform, the scheme knowledge memory, the design of Structural Parameters storer, draw and the engineering drawing storer, the scheme compiled memory, the document storage storer, the driving parameter unit, design proposal reasoning arithmetic element, driving parameter constraint condition storer, design system CAX integrated platform is respectively by data bus and scheme standard memory, the scheme knowledge memory, the design of Structural Parameters storer, draw and the engineering drawing storer, the scheme compiled memory, the document storage storer, the driving parameter unit, design proposal reasoning arithmetic element, the mutual swap data of driving parameter constraint condition storer, design system CAX integrated platform is an ES/CAD/CAE/CAPP/CAM integrated system, for distributed, client/server architecture, the data of the CAX of design Storage system integrated platform on the server, be the centre data storer, the data of storage user terminal on the client computer, be local data memory, design system CAX integrated platform carries out unified management to centre data storer and local data memory, is furnished with the integrated application software of a cover on each client computer; The data message of scheme standard memory sends scheme knowledge memory, design of Structural Parameters storer, drawing and engineering drawing storer, document storage storer to successively by the I/O access module, and the scheme standard memory stores typical howitzer product design figure and product three-dimensional model diagram; The scheme knowledge memory stores howitzer design rule and theoretical calculation formula; The design of Structural Parameters storer can be determined howitzer main design parameters and preliminary project; The data message of driving parameter unit sends the scheme compiled memory to by the I/O access module, and sends driving parameter constraint condition storer by the I/O access module to through design proposal reasoning arithmetic element; By driving parameter unit activating scheme compiled memory and design proposal reasoning arithmetic element, the scheme compiled memory is realized obtaining and system integration and test of knowledge, after driving parameter constraint condition storer is determined design proposal, enter again and draw and the engineering drawing storer, form three-dimensional model diagram and two-dimensional engineering graphic ， And design calculation result and structural drawing are deposited in document memory with file layout.
Described design proposal reasoning arithmetic element comprises subscriber unit, knowledge editor, the knowledge compilation device, knowledge memory, the frame inference machine, the rule-based reasoning machine, the method inference machine, interpreter, top control module, context data memory, field design knowledge storer, the data-carrier store interface, figure support programs interface, the data message of subscriber unit sends knowledge editor to successively by the I/O access module, the knowledge compilation device, knowledge memory, the data message of subscriber unit also sends the frame inference machine respectively to by the I/O access module, the rule-based reasoning machine, the method inference machine, interpreter, the frame inference machine, the rule-based reasoning machine, the method inference machine, interpreter is intercoursed data with top control module respectively by data bus again, top control module is by data bus and the mutual data information of context data memory, the data message of data-carrier store interface one output terminal sends context data memory to by the I/O access module, another output terminal sends context data memory by the I/O access module to through figure support programs interface, field design knowledge storer is connected with top control module through knowledge memory by the I/O access module, described knowledge editor is by the information management center, morphology is checked, the knowledge interpolation is formed to guide module, has information management, morphology is checked and interpolation knowledge guide function, wherein all frameworks, information management is all managed by the information management center with maintenance, knowledge edition and modification are convenient in organization of unity.
A kind of workflow of howitzer Intelligentized design method is: (1) subscriber unit is the initial actuating of system; (2) tactics index input, desired tactical and technical norms in the incoming task book; (3) selecting similar bullet, is to make amendment and design according to design knowledge; (4) just decide design proposal, form preliminary project according to driving parameter and drawing function; (5) the architectural feature number calculates, and according to design proposal reasoning arithmetic element, carries out basic calculation, the projectile structure characteristic number of bullet design and calculates; (6) heavy, the initial velocity estimation of bullet is carried out the estimation of bullet quality and muzzle velocity, and is detected the requirement of whether satisfying cannon emission constraint condition and design criteria, if not, then return step (3), if yes, then will carry out step (7); (7) intensity, stability estimation are carried out the intensity and the flight stability of bullet and are checked, if not, then return step (3), if yes, then pass through step (5) and carry out step (8); (8) estimation of bullet projectile form factor is carried out in projectile form factor estimation; (9) range carries out the bullet range and calculates, if defective, then returns step (3), if range satisfies index request, then will carry out step (10) through (5); (10) estimation of bullet explosive strength is carried out in explosive strength estimation, if the bullet power can not satisfy index request, then returns step (3), if can meet the demands, then will carry out step (11) through (5); (11) just decide scheme and tentatively manufacture experimently, manufacture experimently production,, can produce in enormous quantities, then carry out step (12), otherwise return step (3) if manufacturing technique requirent is satisfied in design to just deciding scheme; (12) check in the target range, the bullet pilot sample is carried out range firing check, if qualified, then will carry out step (13), if defective, then returns step (3); (13) the design typification stage, put into production, carry out the bullet design typification test, if qualified, if the conceptual design success defective, is then wanted modification, returns step (3).
The workflow of design proposal reasoning arithmetic element of the present invention is: (1) sets up task according to war skill index, according to the technical indicator that requires in the charter, selects reasoning task; (2) determine the design feature parameter according to technical requirement, provide the primary structure characteristic number of howitzer conceptual design according to howitzer technical requirement reasoning; (3) from knowledge memory, choose tentative programme, provide the primary structure characteristic number by inference, from scheme standard memory and knowledge memory, choose original scheme, and revise the formation tentative programme; (4) reasoning of input driving parameters becomes new departure, and the tentative programme to forming drives according to primary structure characteristic number that provides and bullet design driven constraint condition storer, forms new departure; (5) carry out projectile structure characteristic number accurate Calculation; (6) carry out bullet intensity, stability, trajectory calculating; (7) assessment, various result of calculations are detected assessment,, then enter step (8) if assessment is defective, (8) enter Change In Design, set up new departure, activate the design change package function, the design proposal of making amendment is once more set up new departure, turn back to step (2) again, if qualified, then enter step (9), (9) design finishes, data deposit storer in.
The present invention has the computing machine of utilization and finishes howitzer overall design, demonstration, simulation simulation analysis and calculating, lead time is short, designing quality good, the production efficiency advantages of higher, to adapt to the needs that the howitzer model is many, become batch and production in enormous quantities and modernized war.
Description of drawings
Fig. 1 is the structural representation of howitzer intelligent design system of the present invention;
Fig. 2 is the structural representation of design proposal reasoning arithmetic element of the present invention;
Fig. 3 is the workflow diagram of howitzer Intelligentized design method of the present invention;
Fig. 4 is the workflow diagram of design proposal reasoning arithmetic element of the present invention;
Fig. 1, among Fig. 2: 1 scheme standard memory, 2 scheme knowledge memories, 3 design of Structural Parameters storeies, 4 draw and the engineering drawing storer, 5 scheme compiled memories, 6 design system CAX integrated platforms, 7 document memory, 8 driving parameter unit, 9 design proposal reasoning arithmetic elements, 10 driving parameter constraint condition storeies, 11 subscriber units, 12 knowledge editors, 13 frame inference machines, 14 rule-based reasoning machines, 15 method inference machines, 16 interpreters, 17 knowledge compilation devices, 18 top control modules, 19 knowledge memories, 20 context data memory, 21 field design knowledge storeies, 22 data-carrier store interfaces, 23 figure support programs interfaces.
Embodiment
Further specify the workflow of organization plan of the present invention and method for designing below in conjunction with example.
As shown in Figure 1, a kind of howitzer intelligent design system, comprise scheme standard memory 1, design system CAX integrated platform 6, scheme knowledge memory 2, design of Structural Parameters storer 3, drawing and engineering drawing storer 4, scheme compiled memory 5, document memory 7, driving parameter unit 8, design proposal reasoning arithmetic element 9, driving parameter constraint condition storer 10.Scheme standard memory 1 stores howitzer typical products design drawing and product three-dimensional model diagram.The data message of scheme standard memory 1 sends scheme knowledge memory 2 to by the I/O access module, intercourse data message by data bus and design system CAX integrated platform 6 simultaneously, design system CAX integrated platform 6 is ES/CAD/CAE/CAPP/CAM integrated systems, this system is a distributed system, it is client/server architecture, the data of the CAX of design Storage system integrated platform on the server, be the centre data storer, the data of storage user terminal on the client computer, be local data memory, design system CAX integrated platform carries out unified management to centre data storer and local data memory, is furnished with the integrated application software of a cover on each client computer.Scheme knowledge memory 2 stores howitzer design rule and theoretical calculation formula, scheme knowledge memory 2 is intercoursed data message by data bus and intelligent design system CAX integrated platform 6, flow to design of Structural Parameters storer 3 by the I/O access module simultaneously, design of Structural Parameters storer 3 has reasoning and can determine howitzer main design parameters and preliminary project, it intercourses data message by data bus and design system CAX integrated platform 6, design system CAX integrated platform 6 is intercoursed data message by data bus and driving parameter unit 8 again, activate design proposal reasoning arithmetic element 9 and scheme compiled memory 5 by driving parameter unit 8 then, design proposal reasoning arithmetic element 9 is finished the basic calculation of bullet design, the projectile structure characteristic number is calculated, and realizes obtaining and system integration and test of knowledge by scheme compiled memory 5; Design proposal reasoning arithmetic element 9 is by intercoursing data message with design system CAX integrated platform 6, activation parameter drives constraint condition storer 10, driving parameter constraint condition storer 10 is by intercoursing data message with design system CAX integrated platform 6, enter again after design proposal determined and draw and engineering drawing storer 4, drawing and engineering drawing storer 4 are intercoursed data message by data bus and design system CAX integrated platform 6, through the definite design proposal of reasoning, by drawing and engineering drawing storer 4 forms three-dimensional model diagrams and two-dimensional engineering graphic And deposits design calculation result and structural drawing in document memory 7 with file, document memory 7 is intercoursed data message with design system CAX integrated platform 6, and with the unified file format storage file, to realize calling mutually between each data-carrier store and the system.
As shown in Figure 3, a kind of workflow of howitzer Intelligentized design method is: step 24 is a subscriber unit, is the initial actuating of system; Step 25 is the tactics index input, the leading indicator of desired tactics technology in the incoming task book, and window has the prompting explanation; Step 26 relies on design proposal reasoning arithmetic element for selecting similar bullet, selects similar bullet, makes amendment and design proposal; Step 27 is just to decide design proposal, relies on driving parameter and drawing function to form preliminary project; Step 28 is calculated for the architectural feature number, relies on design proposal reasoning arithmetic element, carries out basic calculation, the projectile structure characteristic number of bullet design and calculates; Step 29 is carried out the estimation of bullet quality and muzzle velocity for bullet is heavy, the initial velocity estimation, and detects the requirement of whether satisfying cannon emission constraint condition and design criteria, if yes, then will carry out step 30; Step 30 is intensity, stability estimation, carries out the intensity and the flight stability of bullet and checks, if not, then return step 26, if then carry out step 31, step 31 is the projectile form factor estimation, carries out the projectile form factor estimation of bullet, enters step 32 then; Step 32 is a range, carries out the calculating of bullet range, if range satisfies index request, then will carry out step 33, if step 26 is then returned in the requirement of the discontented toe of range; Step 33 is carried out the estimation of the explosive strength of bullet for the explosive strength estimation, if 26 steps are then returned in the discontented toe target requirement of the power of bullet, if the power of bullet satisfies the requirement of index, then will carry out 34 steps; Step 34 is tentatively manufactured experimently for just deciding scheme, manufactures experimently production to just deciding scheme, if the requirement of production technology is satisfied in design, can produce in enormous quantities, then will carry out 35 steps; If the requirement of production technology is not satisfied in design, cannot produce in enormous quantities, then return step 26; Step 35 is checked for the target range, will carry out range firing to the pilot sample of bullet and check, if qualified, then will carry out step 36, if defective, then returns step 26; Step 36 is the design typification stage, puts into production, carries out the design typification test of bullet.If qualified, this conceptual design success.If defective, then want modification, return step 26.
As shown in Figure 2, the subscriber unit 11 of design proposal reasoning arithmetic element can guide the user to carry out reasoning work easily, and the input relevant technologies is asked.The data message of subscriber unit 11 flows to knowledge editor 12, frame inference machine 13, rule-based reasoning machine 14, method inference machine 15 and interpreter 16 respectively by the I/O access module.Knowledge editor 12 is added by information management center, morphology inspection, knowledge to be formed to guide module, have information management, morphology inspection and add the knowledge guide function, wherein all frameworks, the management of knowledge are all managed by the information management center with maintenance, knowledge edition and modification are convenient in organization of unity.The user double-clicks the framework that will edit on the view at information management center, can edit this framework on editing view.The data of knowledge editor 12 flow to knowledge compilation device 17 by the I/O access module.Frame inference machine 13 is a kind of data structures, the characteristics of this data structure maximum are can description object and relation between objects, framework is made up of groove, the frame inference machine is mainly finished the evaluate operation to frame slot, and this evaluate operation is that the inherited attribute according to the taxonomical hierarchy structure of frame system and frame slot defines and finishes.The data of frame inference machine 13 are transmitted mutually by data bus and top control module 18.The rule of rule-based reasoning machine 14 is a kind of knowledge representation forms, and its use will be finished by the rule-based reasoning machine.What rule-based reasoning machine 14 used is a kind of forward reasoning method, forward reasoning (also claiming data-driven) is from known argument, utilize and the true rule that is complementary, carry out the new fact of expansion, this process carry out repeatedly until reach to set the goal or rule can be by coupling till.The data of rule-based reasoning machine 14 are transmitted mutually by data bus and top control module 18.Method inference machine 15 is a kind of procedural languages, can the implementation procedure operation, numerical evaluation, reasoning control and message transmission.This process was divided into for two steps: the one, and the search of method and coupling, another is the execution of procedure body.When a piece of news was sent to target framework, the method inference machine must at first extract all method that is had in this framework, then these methods and message is complementary, and obtains the method that is complementary with message, the coupling of method that Here it is.The data of method inference machine 15 are transmitted mutually by data bus and top control module 18.Interpreter 16 is finished the explanatory note of each scheme reasoning process, the purpose of interpreter is to use the process of the clear more understanding decision-making in family, the correctness that judgement is found the solution, enhancing is to gained result's degree of belief, and the data of interpreter 16 are transmitted mutually by data bus and top control module 18.The effect of knowledge compilation device 17 is with text mode knowledge compilation to be become the knowledge organization form of internal system, is stored in knowledge memory 19 with the form of binary file.Domain knowledge storer 21 provides knowwhy, common sense knowledge and experimental knowledge, the data message of domain knowledge storer 21 flows to knowledge memory 19 by the I/O access module, knowledge memory 19 is deposited knowwhy, common sense knowledge and experimental knowledge, knowledge memory 19 is to gather knowledge, put in order, abstract and formalization (title knowledge acquisition), with the receptible form of computing machine (the title representation of knowledge) these knowledge are left in the knowledge memory 19 then, the management of knowledge memory 19 is finished by knowledge editor 17, and the data of knowledge memory 19 flow to top control module 18 by the I/O access module.Top control module 18 is invoked procedures between each inference machine of control, and each inference machine is for the reasoning solicit operation of top control module.Top control module 18 will be finished field data and keep when calling, so that can recover the reentry point of upper level reasoning when end is called in reasoning, continue the reasoning operation of last layer.It is the knowledge system development environment of an opening that data-carrier store interface 22 can make native system, can dock with other data-carrier stores.The data of data-carrier store interface 22 flow to context data memory 20 and figure support programs interface 23 by the I/O access module respectively, figure support programs interface 23 is laid a good foundation for continuing follow-up works such as design, can call various large-scale graphics software bags.The data of figure support programs interface 23 flow to context data memory 20 by the I/O access module.Context data memory 20 is dynamic knowledge, the fact knowledges that produced by system dynamics, it and data-carrier store are similar, reflect dynamically or deposit the raw data and the fact when finding the solution field question, and centre and object information, context data memory 20 is by data bus and top control module 18 mutual swap datas.
As shown in Figure 4, the workflow of howitzer design proposal reasoning arithmetic element is: step 37 is an initial actuating for setting up task according to war skill index, according to the technical indicator that requires in the charter, selects reasoning task.Step 38 is for to determine the design feature parameter according to technical requirement, and according to technical requirement, reasoning provides the primary structure characteristic number of howitzer conceptual design.Step 39 provides the primary structure characteristic number by inference for to choose tentative programme from knowledge memory, chooses original scheme from scheme standard memory and knowledge memory, and revises the formation tentative programme.Step 40 becomes new departure for the reasoning of input driving parameters, and the tentative programme to forming drives according to primary structure characteristic number that provides and bullet design driven constraint condition storer, forms new departure.Step 41 is carried out the calculating of the architectural feature number of bullet for carrying out projectile structure characteristic number accurate Calculation.Step 42 is calculated for carrying out bullet intensity, stability, trajectory, according to equation and formula, intensity, flight stability and the trajectory of bullet is comprehensively calculated.Step 43 is that various result of calculations are detected assessment for assessment, if assessment is defective, then enter in the step 44, step 44 is for entering Change In Design, setting up new departure, according to design change package, and the scheme of making amendment once more, set up new departure, turn back to step 38 again,, then enter step 45 if assessment is qualified, design finishes, data deposit storer in, and then the reasoning design finishes.
Claims (6)
1, a kind of howitzer intelligent design system, it is characterized in that, comprise the scheme standard memory, design system CAX integrated platform, the scheme knowledge memory, the design of Structural Parameters storer, draw and the engineering drawing storer, the scheme compiled memory, the document storage storer, the driving parameter unit, design proposal reasoning arithmetic element, driving parameter constraint condition storer, design system CAX integrated platform is respectively by data bus and scheme standard memory, the scheme knowledge memory, the design of Structural Parameters storer, draw and the engineering drawing storer, the scheme compiled memory, the document storage storer, the driving parameter unit, design proposal reasoning arithmetic element, the mutual swap data of driving parameter constraint condition storer, the data message of scheme standard memory sends the scheme knowledge memory to successively by the I/O access module, the design of Structural Parameters storer, draw and the engineering drawing storer, document storage storer, scheme standard memory store typical howitzer product design figure and product three-dimensional model diagram; The scheme knowledge memory stores howitzer design rule and theoretical calculation formula; The design of Structural Parameters storer can be determined howitzer design parameter and preliminary project; The data message of driving parameter unit sends the scheme compiled memory to by the I/O access module, and sends driving parameter constraint condition storer by the I/O access module to through design proposal reasoning arithmetic element; By driving parameter unit activating scheme compiled memory and design proposal reasoning arithmetic element, the scheme compiled memory is realized obtaining and system integration and test of knowledge, after driving parameter constraint condition storer is determined design proposal, enter again and draw and the engineering drawing storer, form three-dimensional model diagram and two-dimensional engineering graphic ， And design calculation result and structural drawing are deposited in document memory with file layout.
2, howitzer intelligent design system according to claim 1, it is characterized in that described design system CAX integrated platform is an ES/CAD/CAE/CAPP/CAM integrated system, for distributed, client/server architecture, the data of the CAX of design Storage system integrated platform on the server, be the centre data storer, the data of storage user terminal on the client computer, be local data memory, design system CAX integrated platform carries out unified management to centre data storer and local data memory, is furnished with the integrated application software of a cover on each client computer.
3, howitzer intelligent design system according to claim 1, it is characterized in that described design proposal reasoning arithmetic element comprises subscriber unit, knowledge editor, the knowledge compilation device, knowledge memory, the frame inference machine, the rule-based reasoning machine, the method inference machine, interpreter, top control module, context data memory, field design knowledge storer, the data-carrier store interface, figure support programs interface, the data message of subscriber unit sends knowledge editor to successively by the I/O access module, the knowledge compilation device, knowledge memory, and the data message of subscriber unit sends the frame inference machine respectively to by the I/O access module, the rule-based reasoning machine, the method inference machine, interpreter, the frame inference machine, the rule-based reasoning machine, the method inference machine, interpreter is intercoursed data with top control module respectively by data bus again, top control module is by data bus and the mutual data information of context data memory, the data message of data-carrier store interface one output terminal sends context data memory to by the I/O access module, another output terminal sends context data memory by the I/O access module to through figure support programs interface, and the data message of field design knowledge storer sends top control module to by knowledge memory.
4, howitzer intelligent design system according to claim 3 is characterized in that the workflow of described design proposal reasoning arithmetic element is:
(1) sets up task according to war skill index,, select reasoning task according to the technical indicator that requires in the charter;
(2 determine the design feature parameter according to technical requirement, provide the primary structure characteristic number of howitzer conceptual design according to howitzer technical requirement reasoning;
(3) from knowledge memory, choose tentative programme, provide the primary structure characteristic number by inference, from scheme standard memory and knowledge memory, choose original scheme, and revise the formation tentative programme;
(4) reasoning of input driving parameters becomes new departure, and the tentative programme to forming drives according to primary structure characteristic number that provides and bullet design driven constraint condition storer, forms new departure;
(5) carry out projectile structure characteristic number accurate Calculation;
(6) carry out bullet intensity, stability, trajectory calculating;
(7) assessment detects assessment to various result of calculations, if defective, then enters step (8), if qualified, then enters step (9);
(8) enter expert's amending advice, set up new departure, activate the design change package function, the scheme of making amendment is once more set up new departure, turns back to step (2);
(9) design end, data are gone into storer.
5, howitzer intelligent design system according to claim 3, it is characterized in that described knowledge editor is added by information management center, morphology inspection, knowledge forms to guide module, have information management, morphology inspection and add the knowledge guide function, wherein all frameworks, the management of knowledge are all managed by the information management center with maintenance, knowledge edition and modification are convenient in organization of unity.
6, a kind of howitzer Intelligentized design method is characterized in that, the workflow of method for designing is:
(1) subscriber unit is system's initial actuating;
(2) tactics index input, desired tactical and technical norms in the incoming task book;
(3) select similar bullet, make amendment and design according to design knowledge;
(4) just decide design proposal, form preliminary project according to driving parameter and drawing function;
(5) the architectural feature number calculates, and according to design proposal reasoning arithmetic element, carries out basic calculation, the projectile structure characteristic number of bullet design and calculates;
(6) heavy, the initial velocity estimation of bullet is carried out the estimation of bullet quality and muzzle velocity, and is detected the requirement of whether satisfying cannon emission constraint condition and design criteria, if non-, then returns step (3), if yes, then will carry out step (7);
(7) intensity, stability estimation are carried out the intensity and the flight stability of bullet and are checked, if not, then return step (3), if yes, then enter in the step (5), carry out bullet intensity and flight stability and check, if qualified, then will carry out step (8);
(8) estimation of bullet projectile form factor is carried out in projectile form factor estimation;
(9) range carries out the bullet range and calculates, if defective, then returns step (3) if range satisfies the requirement of index, then will carry out step (10);
(10) estimation of bullet explosive strength is carried out in explosive strength estimation, if the bullet power can not satisfy the requirement of index, then returns step (3), if can meet the demands, then will carry out step (11);
(11) just decide scheme and tentatively manufacture experimently, manufacture experimently production,, produce in enormous quantities, then carry out step (12), otherwise return step (3) if manufacturing technique requirent is satisfied in design to just deciding scheme;
(12) check in the target range, the pilot sample of bullet is carried out range firing check, if qualified, then will carry out step (13), if defective, then returns step (3);
(13) the design typification stage, put into production, carry out the design typification test of bullet, if qualified, if the conceptual design success defective, is then wanted modification, returns step (3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100505286A CN1315085C (en) | 2004-09-29 | 2004-09-29 | Grendle intelligent design system and design method |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100505286A CN1315085C (en) | 2004-09-29 | 2004-09-29 | Grendle intelligent design system and design method |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1588376A true CN1588376A (en) | 2005-03-02 |
| CN1315085C CN1315085C (en) | 2007-05-09 |
Family
ID=34602265
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2004100505286A Expired - Fee Related CN1315085C (en) | 2004-09-29 | 2004-09-29 | Grendle intelligent design system and design method |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN1315085C (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100365640C (en) * | 2005-11-23 | 2008-01-30 | 中国航天科技集团公司第一研究院 | File-based digital model integrated design method for complex product |
| CN102067130B (en) * | 2008-04-14 | 2013-12-25 | 西门子产品生命周期管理软件公司 | System and method for modifying geometric relationships in solid model |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2689906B2 (en) * | 1994-06-27 | 1997-12-10 | 日本電気株式会社 | Product development management equipment |
| CN1209223C (en) * | 2002-08-06 | 2005-07-06 | 东华大学 | Method for processing mounting system based on active addressing and position memory |
-
2004
- 2004-09-29 CN CNB2004100505286A patent/CN1315085C/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100365640C (en) * | 2005-11-23 | 2008-01-30 | 中国航天科技集团公司第一研究院 | File-based digital model integrated design method for complex product |
| CN102067130B (en) * | 2008-04-14 | 2013-12-25 | 西门子产品生命周期管理软件公司 | System and method for modifying geometric relationships in solid model |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1315085C (en) | 2007-05-09 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN107590319B (en) | Knowledge modeling method and system for auxiliary design of mechanical product scheme | |
| CN106200575B (en) | A kind of robustness control method of the automated manufacturing system based on Petri network | |
| CN109857395B (en) | Integrated application method of intelligent camshaft grinding process software database system based on open numerical control system | |
| CN105138802B (en) | A kind of gun barrel intelligent design system and design method | |
| Sacks et al. | Automating design review with artificial intelligence and BIM: State of the art and research framework | |
| CN110427006A (en) | A kind of multi-agent cooperative control system and method for process industry | |
| CN102306223B (en) | High level architecture (HLA) technology-based ship gas turbine device integrated simulation platform and implementation method thereof | |
| CN104933265A (en) | Method for designing interior decoration of building based on BIM | |
| CN104915524A (en) | BIM-based interior module group library construction method for building interior design | |
| CN106529028A (en) | Technological procedure automatic generating method | |
| CN112200319A (en) | Rule reasoning method and system for achieving unmanned vehicle navigation obstacle avoidance | |
| Costa et al. | Automatic generation of disassembly sequences and exploded views from solidworks symbolic geometric relationships | |
| CN115494796B (en) | Edge cloud collaborative digital twin system based on STEP-NC | |
| WO2020167316A1 (en) | Machine learning-based generative design for process planning | |
| Lu et al. | Formal modelling of a sheet metal smart manufacturing system by using Petri nets and first-order predicate logic | |
| CN1315085C (en) | Grendle intelligent design system and design method | |
| CN109997123A (en) | For room for improvement-time data management mthods, systems and devices | |
| CN114693036A (en) | Intelligent management method, device and medium for building system based on knowledge graph | |
| CN102760085B (en) | Communication track expanding method and device, communication track drive simulation method and system | |
| CN116822631A (en) | Graph-based interpretable cognitive reasoning penetration robot system | |
| CN104182596B (en) | Wireless data transmission equipment testing data mining system and method based on LabVIEW and Matlab hybrid programming | |
| CN116070922A (en) | Training platform and method for air combat command decision agent | |
| CN105005210A (en) | Mechanical-electrical integration simulation system and use method thereof | |
| CN115358477A (en) | Random generation system for battle scenario and application thereof | |
| Huang et al. | Efficient NC process scheme generation method based on reusable macro and micro process fusion |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |