DocumentCode
3446899
Title
Functional-features-based framework method for the rapid design of aircraft assembly fixture board
Author
Jie, Zhang ; Xu Zhi-jia ; Li Yuan
Author_Institution
Key Lab. of Contemporary Design & Integrated Manuf. Technol., Northwestern Polytech. Univ., Xi´´an, China
Volume
3
fYear
2010
fDate
29-31 Oct. 2010
Firstpage
443
Lastpage
448
Abstract
In order to enhance the fixture board design efficiency and support fixture board original design, a framework method based on functional features was proposed. In this method, Functional Requirements (FRs) for the fixture board structures were analyzed. Through incorporating FR and Design Knowledge (DK) into the fixture board´s Structure Features (SFs), the Functional Features (FFs) of fixture board were defined and grouped using the object-oriented technology. In order to design the SFs in FFs, a mapping mechanism from Functional Requirements Domain (FRD) to Structure Features Domain (SFD) was established based on the DK, as well as a combination mechanism to organize SFs to generate a Integrated Structure of Fixture Board (ISFB), and the two mechanisms were both explicitly expressed as optimization models. Finally, an example was introduced, and the result demonstrated the feasibility of the framework method.
Keywords
CAD; aircraft manufacture; assembling; object-oriented methods; production engineering computing; aircraft assembly fixture board; board functional feature; board structure feature; combination mechanism; design knowledge; fixture board design; functional requirements; mapping mechanism; object-oriented technology; Aircraft; Assembly; Variable speed drives; combination mechanism; functional feature; mapping mechanism from FRD to SFD; rapid design of fixture board;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Computing and Intelligent Systems (ICIS), 2010 IEEE International Conference on
Conference_Location
Xiamen
Print_ISBN
978-1-4244-6582-8
Type
conf
DOI
10.1109/ICICISYS.2010.5658663
Filename
5658663
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