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