CN106570243A - Missile design and simulation integrated platform - Google Patents

Missile design and simulation integrated platform Download PDF

Info

Publication number
CN106570243A
CN106570243A CN201610941034.XA CN201610941034A CN106570243A CN 106570243 A CN106570243 A CN 106570243A CN 201610941034 A CN201610941034 A CN 201610941034A CN 106570243 A CN106570243 A CN 106570243A
Authority
CN
China
Prior art keywords
design
missile
simulation
platform
professional
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.)
Pending
Application number
CN201610941034.XA
Other languages
Chinese (zh)
Inventor
刘广
杨积东
许斌
庄国平
张志军
苗晓婷
刘小波
李晓东
司马珂
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Shanghai Institute of Electromechanical Engineering
Original Assignee
Shanghai Institute of Electromechanical Engineering
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Shanghai Institute of Electromechanical Engineering filed Critical Shanghai Institute of Electromechanical Engineering
Priority to CN201610941034.XA priority Critical patent/CN106570243A/en
Publication of CN106570243A publication Critical patent/CN106570243A/en
Pending legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B17/00Systems involving the use of models or simulators of said systems
    • G05B17/02Systems involving the use of models or simulators of said systems electric
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F2111/00Details relating to CAD techniques
    • G06F2111/02CAD in a network environment, e.g. collaborative CAD or distributed simulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • Geometry (AREA)
  • General Engineering & Computer Science (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

The invention discloses a missile design and simulation integrated platform comprising a platform portal layer serving as a portal for united work of missile design engineers and missile simulation engineers of each specialty; a design application layer applied to rapid design of overall missile, guidance control system, structure and pneumatic specialties; a simulation application layer used for performing simulation analysis on the overall missile, guidance control system, structure and pneumatic specialties; a platform service layer used for performing effective configuration management on existing missile knowledge data, professional models, analysis processes, professional tools and IT tools of enterprises; and a basic resource layer used for performing effective share management on product design experiences, software analysis tools and hardware computation equipment formed by accumulating, summarizing and concluding during missile research and development processes. According to the platform provided by the invention, digital design simulation of an overall missile scheme and accumulation and reuse of design knowledge are achieved, and a professional design, simulation analysis and data management tool is provided for overall missile designers.

Description

The emulation integrated platform of Missile Design
Technical field
The present invention relates to application of the digital prototype technology in Integrated Missile Design field, specifically refers to a kind of new leading Design and simulation unified platform is played, belongs to the technical field of Missile Preliminary Design of digital.
Background technology
Hypersonic missile master-plan under complex environment has integrated level height, complex structure, construction cycle length, tests into The features such as this is huge, digital prototype technology provides means to solve these problems, also obtains during Missile Design Numerous applications, but under traditional research and development pattern, digital simulation technique does not also become core technology means and develops the mark of flow process Lead ring section.Digitizing technique has accelerated Missile Design process, but guided missile R&D experience, the mould of the personal accumulation of many designers Type, data are not yet effectively managed, and effective way is not also found in the succession of design knowledge.Digital simulation technique is one multiple Miscellaneous technical activity, needs to do strict process management just in links such as simulation modeling, simulation model validation, evaluation of simulation result High-quality simulation result can be obtained, product design is supported.
The content of the invention
It is an object of the invention to provide a kind of emulation integrated platform of new Missile Design, breaches digital simulation technique In the difficulty of the aspect such as technology and resource guarantee, Integrated Missile Design ability is improved, Missile Design knowledge accumulation is realized and is answered With.
The present invention is realized by scheme in detail below:
The emulation integrated platform of Missile Design, including
Platform portal layer, for each Specialty Design engineer of guided missile, Simulation Engineering's teacher uniform operational;
Design application layer, for the quick design of each specialty such as Missile Preliminary, guidance control system, structure, pneumatic;
Simulation Application layer, for each professional simulation analysis such as Missile Preliminary, guidance control system, structure, pneumatic;
Platform services layer, for the existing guided missile knowledge data of enterprise, Professional Model, analysis process, professional tool, IT Instrument etc. carries out effective configuration management;The management method of system engineering thought is effectively implemented by IT technical capabilities, in data Integrated management, Tool integration and the information processing capability aspect such as process automation, systematic collaboration emulation and Robust Optimization excessively pass through Data interaction efficiency and quality, computation efficiency and data-handling capacity, abundant decision making approach and its science are greatly improved, Finally realize work efficiency raising, the purpose that the R&D cycle shortens, designing quality is lifted of designer;
Basic resource layer, for will accumulation in guided missile R&D process, summarize, conclude formed product design experience, soft Part analytical tool, hardware computing device etc. carry out effective Sharing Management;It is favourable by classification storage, accumulation product design data In the meeting of design information is total, the refinement of design knowledge and design the real-time support of help, by share software and hardware technology resource and By integrated with resource management and scheduling system, high-performance calculation resource can be provided for all designers, improve design effect Rate and reliability, improve the benefit of investment.
Further, described each Specialty Design teacher of platform portal layer is stepped on Simulation Engineering teacher by unified portal interface Record, completes complete from the guided missile needed for each business such as beforehand research demonstration, conceptual design to engineering design in unified platform network environment Lead time Design of digital simulation work.
Further, described design application layer is made up of the professional quick design system of each capacity unit;Capacity unit Professional quick design system at least includes overall specialty quick design system, guidance control system specialty quick design system, knot Structure specialty quick design system, Pneumatic Professional quick design system.Professional quick design system is according to model job requirements, profit With single pro digital design system of operation process organization.Customized by interface, form design data stream;Use standard procedure shape Formula encapsulates all kinds of analysis softwares (business software, self-compiling program), forms technical support ability;By calculating process, automatization reduces Personnel amount demand, man-machine interaction replenishment system Intelligent treatment level, the driving research and development pattern of Forming ability.
Further, described Simulation Application layer is made up of the analogue system of each capacity unit, the analogue system of capacity unit At least include total simulation system, guidance control system analogue system, structure simulation system, aerodynamics simu1ation system.Each energy The analogue system of power unit be used for by standard, high degree of automation, the simulation flow that has precision guarantee addition interface Into design cycle, issue is used for type design teacher;Using standard, have the simulation flow of certain technology maturity as analysis mould Version is issued, used for professional Simulation Engineering teacher;Emulation tool, empirical parameter, Professional Model, the analysis masterplate work that enterprise is shared Issue for technical resource and use, create job analysis flow process for the specialty research teacher on platform.
Further, including system client, system client includes the man-machine interactive interface of each capacity unit, ability The man-machine interactive interface of unit at least includes overall man-machine interactive interface, guidance control system man-machine interactive operation circle Face, structure man-machine interactive interface, pneumatic man-machine interactive interface
Compared with prior art, the invention has the advantages that:
The emulation of Missile Preliminary scheme Design of digital, the accumulation of design knowledge and multiplexing are realized, is Integrated Missile Design Personnel provide specialized design, simulation analysis and data organizing tool;Improve the operation energy of engineering knowledge in guided missile development process Power and scientific level, allow high efficiency, high-quality, high reliability, the Digital Simulation of low cost to incorporate guided missile processes of research & development, with setting The emulation integrated raising designed capacity of meter, product competitiveness.Its characteristic is mainly reflected in by Missile Design operation flow, specialty The architecture collocation method of simulation flow promotes Missile Design with professional artificial service depth integration, formation Product Digitalization Design Pattern, realizes the Various types of data unified management during Missile Design;Digitized mine is defined by specification and realizes guided missile development Effective accumulation of engineering knowledge, flow instanceization operation are realized the multiplexing of engineering knowledge and are shared;By to digital simulation flow Centralized management plan as a whole the resources supplIes such as tool software, computing capability, the network storage of enterprise, promote pro digital ability to build If.
Description of the drawings
By reading the detailed description made to non-limiting example made with reference to the following drawings, other of the invention Feature, objects and advantages will become more apparent upon:
Fig. 1 is the structure principle chart of the emulation integrated design platform of embodiment of the present invention Missile Design.
Specific embodiment
With reference to specific embodiment, the present invention is described in detail.Following examples will be helpful to the technology of this area Personnel further understand the present invention, but the invention is not limited in any way.It should be pointed out that the ordinary skill to this area For personnel, without departing from the inventive concept of the premise, some deformations and improvement can also be made.These belong to the present invention Protection domain.
As shown in figure 1, embodiments providing a kind of emulation integrated platform of Missile Design, it is total that it is applied to guided missile Body Design of digital, specifically includes:Platform portal layer, it is used for each Specialty Design engineer of guided missile, Simulation Engineering Shi Tongyi work The door of work;Design application layer, it is used for the quick design of each specialty such as Missile Preliminary, guidance control system, structure, pneumatic;It is imitative True application layer, it is used for each professional simulation analysis such as Missile Preliminary, guidance control system, structure, pneumatic;Platform services layer, its For effectively being matched somebody with somebody to the existing guided missile knowledge data of enterprise, Professional Model, analysis process, professional tool, IT instruments etc. Put management;Basic resource layer, its be used for will accumulation in guided missile R&D process, summarize, conclude formed product design experience, soft Part analytical tool, hardware computing device etc. carry out effective Sharing Management.
As shown in figure 1, each Specialty Design teacher can be by unified portal interface with Simulation Engineering teacher in platform portal layer Log in, complete complete from the guided missile needed for the business such as beforehand research demonstration, conceptual design to engineering design in unified platform network environment Lead time Design of digital simulation work.Specifically, according to Project R&D present situation, needed for being realized by customized development mode Integration of user interaction functionality, platform portal layer provide IE styles, plug-in unit support under meet different design stage, different designs personnel Human-computer interaction interface.System client includes design and the simulation capacity unit such as totality, guidance control system, structure, pneumatic Man-machine interactive interface.
As shown in figure 1, design application layer is mainly by the specialty of the capacity unit such as totality, guidance control system, structure, pneumatic Quick design system is constituted.Designed capacity unit is the small-scale multi-specialized collaboration that flow process work requirements tissue is developed according to guided missile Design environment;Professional quick design system is set according to model job requirements, the single pro digital organized using work flow Meter systems, specialty Gneral analysis flow process be Specialty Design experience accumulation, extractions, decompositions, standardization, combine configure concatenate out Somewhat complex design process, data, instrument, process, personnel are separate.Customized by interface, form design data stream;Use standard mistake Journey form encapsulates all kinds of analysis softwares (business software, self-compiling program), forms technical support ability;By calculating process automatization Reduce personnel amount demand, man-machine interaction replenishment system Intelligent treatment level, the driving research and development pattern of Forming ability.Specifically Say, according to Project R&D present situation, each professional collaborative design system completed by customized development, and carry out with platform portal layer it is right Connect, design engineer on the human-computer interaction interface of platform portal layer just can with complete design data input, check design result Output, Feedback Design decision-making, acquisition design help are supported.
As shown in figure 1, Simulation Application layer is mainly by the emulation of the capacity unit such as totality, guidance control system, structure, pneumatic System is constituted, groundwork:By standard, high degree of automation, the simulation flow that has precision guarantee add interface into Design cycle, issue is used for type design teacher;Using standard, have the simulation flow of certain technology maturity as analysis masterplate Issue, use for professional Simulation Engineering teacher;Using enterprise share emulation tool, empirical parameter, Professional Model, analysis masterplate as Technical resource is issued and uses, creates job analysis flow process for the specialty research teacher on platform;Simulation Application layer is used as ability culture Unit, with interactions such as emulation project management, Professional knowledge management, IT technical supports, artificial service examination & verification, the emulation communal spaces Working interface.Specifically, present situation and career development level of ability are accumulated according to enterprise technology, each specialty is customized by secondary development Analogue system, and docked with design application layer and platform portal layer, Simulation Engineering teacher can just access imitative in platform portal layer The digitalized artificial environment met needed for research and development of products that true application layer is set up.
As shown in figure 1, platform services layer will be realized to the existing knowledge data of enterprise, Professional Model, analysis process, specialty Instrument, IT instruments etc. carry out effective configuration management, and by IT technical capabilities the management method of system engineering thought is effectively implemented, In data integration management, Tool integration and cross process automation, systematic collaboration emulation and the information processing capability side such as Robust Optimization Face by greatly improve data interaction efficiency and quality, computation efficiency and data-handling capacity, abundant decision making approach and its Science, finally realizes that the work efficiency of designer is improved, the purpose that the R&D cycle shortens, designing quality is lifted.Platform takes Business layer is the key foundation condition that Digital Simulation management platform is built, and needs the design and simulation management platform Framework of specialty Support.Platform services layer is docked with design application layer, Simulation Application layer and basic resource layer, and platform services layer should to design Effectively managed with the job content of layer, Simulation Application layer, the resource of basic resource layer is effectively dispatched.
As shown in figure 1, basic resource layer will accumulation in research and development of products, summarize, conclude formed product design experience, soft Part analytical tool, hardware computing device etc. carry out effective Sharing Management;It is favourable by classification storage, accumulation product design data In the meeting of design information is total, the refinement of design knowledge and design the real-time support of help, by share software and hardware technology resource and By integrated with resource management and scheduling system, high-performance calculation resource can be provided for all designers, improve design effect Rate and reliability, improve the benefit of investment.Skill element in basic resource layer needs the resources such as specialized database system to support, Receive scheduling, the management of platform services layer.
The specific embodiment of the present invention is described above.It is to be appreciated that the invention is not limited in above-mentioned Particular implementation, those skilled in the art can within the scope of the claims make various modifications or modification, this not shadow Ring the flesh and blood of the present invention.

Claims (5)

1. the emulation integrated platform of Missile Design, it is characterised in that include
Platform portal layer, for each Specialty Design engineer of guided missile, Simulation Engineering's teacher uniform operational;
Design application layer, for the quick design of each specialty;
Simulation Application layer, for each professional simulation analysis;
Platform services layer, for the existing guided missile knowledge data of enterprise, Professional Model, analysis process, professional tool, IT instruments Carry out effective configuration management;
Basic resource layer, for the formed product design experience of accumulation, summary, conclusion in guided missile R&D process, software to be divided Analysis instrument, hardware computing device carry out effective Sharing Management;Be conducive to design by classification storage, accumulation product design data The meeting of information is total, the refinement of design knowledge and design the real-time support of help, by share software and hardware technology resource and by with Resource management and scheduling system it is integrated, can provide high-performance calculation resource for all designers, improve design efficiency with can By property, the benefit of investment is improved.
2. the emulation integrated platform of Missile Design as claimed in claim 1, it is characterised in that described platform portal layer is each specially Industry designer is logged in Simulation Engineering teacher by unified portal interface, needed for each business is completed in unified platform network environment The full lead time Design of digital simulation work of guided missile.
3. the emulation integrated platform of Missile Design as claimed in claim 1, it is characterised in that described design application layer is by each The professional quick design system composition of capacity unit;The professional quick design system of capacity unit at least includes that overall specialty is quick Design system, guidance control system specialty quick design system, structure discipline quick design system, the quick design department of Pneumatic Professional System.
4. the emulation integrated platform of Missile Design as claimed in claim 1, it is characterised in that described Simulation Application layer is by each The analogue system composition of capacity unit, the analogue system of capacity unit at least includes that total simulation system, guidance control system are imitated True system, structure simulation system, aerodynamics simu1ation system.
5. the emulation integrated platform of Missile Design as claimed in claim 1, it is characterised in that including system client, system Client includes the man-machine interactive interface of each capacity unit, and the man-machine interactive interface of capacity unit is at least included totally Man-machine interactive interface, guidance control system man-machine interactive interface, structure man-machine interactive interface, pneumatic man-machine friendship Interoperability interface.
CN201610941034.XA 2016-10-25 2016-10-25 Missile design and simulation integrated platform Pending CN106570243A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610941034.XA CN106570243A (en) 2016-10-25 2016-10-25 Missile design and simulation integrated platform

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610941034.XA CN106570243A (en) 2016-10-25 2016-10-25 Missile design and simulation integrated platform

Publications (1)

Publication Number Publication Date
CN106570243A true CN106570243A (en) 2017-04-19

Family

ID=58536332

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610941034.XA Pending CN106570243A (en) 2016-10-25 2016-10-25 Missile design and simulation integrated platform

Country Status (1)

Country Link
CN (1) CN106570243A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107967518A (en) * 2017-11-21 2018-04-27 中国运载火箭技术研究院 A kind of knowledge auto-associating system and method based on product design
CN109407552A (en) * 2018-12-17 2019-03-01 上海机电工程研究所 A kind of most matter simulating system synergy emulation methods
CN109905490A (en) * 2019-04-03 2019-06-18 深圳市岸线资本投资管理有限公司 Virtual Simulative Experiment shared platform framework
CN110334441A (en) * 2019-07-04 2019-10-15 成都安世亚太科技有限公司 A kind of novel rocket projectile quickly designs and simulating analysis
CN112560264A (en) * 2020-12-15 2021-03-26 北京动力机械研究所 Aerospace dynamic design simulation system architecture and method based on two-library four-layer architecture
CN112580809A (en) * 2020-12-15 2021-03-30 北京动力机械研究所 Engine knowledge and expert management device based on distributed service
CN113449444A (en) * 2021-09-02 2021-09-28 湖南高至科技有限公司 Simulation method, computer device and storage medium for domain engineering
US11599373B2 (en) 2020-02-17 2023-03-07 Raytheon Company Virtualized hardware and methods for leveraging virtualized hardware with munition support software

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101609479A (en) * 2009-06-23 2009-12-23 北京理工大学 A kind of optimal design method for trajectory robust
CN103455647A (en) * 2012-06-04 2013-12-18 黄晓冬 Reflective-type object-oriented simulation engine
CN104166764A (en) * 2014-08-17 2014-11-26 西北工业大学 Method for guided missile overall multi-disciplinary design oriented to multi-level performance
CN105677446A (en) * 2016-01-28 2016-06-15 中国电子科技集团公司第十研究所 Visual modeling method for distributed simulation platform

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101609479A (en) * 2009-06-23 2009-12-23 北京理工大学 A kind of optimal design method for trajectory robust
CN103455647A (en) * 2012-06-04 2013-12-18 黄晓冬 Reflective-type object-oriented simulation engine
CN104166764A (en) * 2014-08-17 2014-11-26 西北工业大学 Method for guided missile overall multi-disciplinary design oriented to multi-level performance
CN105677446A (en) * 2016-01-28 2016-06-15 中国电子科技集团公司第十研究所 Visual modeling method for distributed simulation platform

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107967518A (en) * 2017-11-21 2018-04-27 中国运载火箭技术研究院 A kind of knowledge auto-associating system and method based on product design
CN109407552A (en) * 2018-12-17 2019-03-01 上海机电工程研究所 A kind of most matter simulating system synergy emulation methods
CN109905490A (en) * 2019-04-03 2019-06-18 深圳市岸线资本投资管理有限公司 Virtual Simulative Experiment shared platform framework
CN109905490B (en) * 2019-04-03 2022-03-04 厦门潭宏信息科技有限公司 Virtual simulation experiment sharing platform architecture
CN110334441A (en) * 2019-07-04 2019-10-15 成都安世亚太科技有限公司 A kind of novel rocket projectile quickly designs and simulating analysis
CN110334441B (en) * 2019-07-04 2021-10-29 成都安世亚太科技有限公司 Novel rocket projectile rapid design and simulation analysis method
US11599373B2 (en) 2020-02-17 2023-03-07 Raytheon Company Virtualized hardware and methods for leveraging virtualized hardware with munition support software
CN112560264B (en) * 2020-12-15 2024-05-28 北京动力机械研究所 Space-sky power design simulation system architecture and method based on two-library four-layer architecture
CN112560264A (en) * 2020-12-15 2021-03-26 北京动力机械研究所 Aerospace dynamic design simulation system architecture and method based on two-library four-layer architecture
CN112580809A (en) * 2020-12-15 2021-03-30 北京动力机械研究所 Engine knowledge and expert management device based on distributed service
CN112580809B (en) * 2020-12-15 2024-05-31 北京动力机械研究所 Engine knowledge and expert management device based on distributed service
CN113449444A (en) * 2021-09-02 2021-09-28 湖南高至科技有限公司 Simulation method, computer device and storage medium for domain engineering
CN113449444B (en) * 2021-09-02 2022-04-22 湖南高至科技有限公司 Simulation method, computer device and storage medium for domain engineering

Similar Documents

Publication Publication Date Title
CN106570243A (en) Missile design and simulation integrated platform
Lee et al. Understanding digital transformation in advanced manufacturing and engineering: A bibliometric analysis, topic modeling and research trend discovery
Wijayakumar et al. Automation of BIM quantity take-off to suit QS’s requirements
CN1713192A (en) Method and device for processing logic mode establishment and carrying out
Gembarski et al. KBE-modeling techniques in standard CAD-systems: Case study—Autodesk inventor professional
CN103049620A (en) Ship simulating system and ship simulating method used during shipbuilding
CN103646154A (en) Three-dimensional digitization final assembly technology collaborative design system
JP2006164219A (en) Interface for analyzing finite-element, computer-readable storage medium which records program of interface for analyzing finite-element, method for analyzing finite-element using high value-added communication network, parallel processing computer for analyzing finite-element, and computer for analyzing finite-element
CN103678815A (en) Mechanical product collaborative simulation platform system and simulation method thereof
Kim et al. An integrative user-level customized modeling and simulation environment for smart manufacturing
Wu et al. BIM facilitated web service for LEED automation
CN114896677B (en) BIM (building information modeling) -based construction simulation method and system
Vasilecas et al. Business process modelling and simulation: hybrid method for concurrency aspect modelling
Nowakowski et al. An Enterprise Architecture Planning Process for Industry 4.0 Transformations.
Kuzmanovska et al. DfMA in building design and construction: Uses and abuses
Ascheri et al. Feasibility of an assembly line layout automatic configuration based on a KBE approach
CN103853862A (en) Templated design method for cannon parts
CN108205564A (en) Knowledge hierarchy construction method and system
Cheutet et al. Consistency management of simulation information in Digital Factory
Novello et al. Which drawing to deliver more information?
Zhang et al. Concurrent design approach and its collaborative environment for integrated complex product development
Figliola Post-industrial robotics: esplorazione di architetture informate nell'era post-digitale
Esposito et al. BIM e Pratiche Collaborative. Abilità e Competenze per l'Ambiente Digitale-BIM and Collaborative Practices. Expertise and Skills for the Digital Environment
Li et al. A system for 3D digital assembly process planning and simulation in airplane manufacturing enterprises
Jun et al. Development of NPP Collaborative Design Management Platform

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication

Application publication date: 20170419

RJ01 Rejection of invention patent application after publication