DocumentCode :
3513599
Title :
Data Management of Aero Engine Turbine Design Integration System
Author :
Li, H.Y. ; Ma, M.X. ; Cui, D.L.
Author_Institution :
Key Lab. for Process Ind. Autom., Northeastern Univ., Shenyang
fYear :
2007
fDate :
21-25 Sept. 2007
Firstpage :
6166
Lastpage :
6169
Abstract :
According to the features of more computational efforts and high memory in the complicated design process of aero-engine turbine, a data management solution based on C/S network structure is presented. The version management of design data is completed by four components. COM technology is adopted in the functional implementation of each component. Incremental data storage is used in every design module, which minimizes data redundancy and maximizes data connectivity. In the scheme data management, three-layered version identification is designed and version combination based on restraint is presented. Large amount of data produced in the design process is managed effectively. Data reusability is enhanced and quality of design is improved.
Keywords :
CAD; aerospace engines; client-server systems; configuration management; distributed object management; mechanical engineering computing; software reusability; turbines; C-S network structure; COM technology; aero-engine turbine design integration system; data reusability; design data version management; incremental data storage; three-layered version identification; Computer network management; Data analysis; Data engineering; Databases; Design engineering; Engineering management; Engines; Process design; Technology management; Turbines;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Wireless Communications, Networking and Mobile Computing, 2007. WiCom 2007. International Conference on
Conference_Location :
Shanghai
Print_ISBN :
978-1-4244-1311-9
Type :
conf
DOI :
10.1109/WICOM.2007.1512
Filename :
4341287
Link To Document :
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