지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.17 Number.1
- 발행연도
- 2016.3
- 수록면
- 45 - 53 (9page)
이용수
초록· 키워드
오류제보하기
This work is mainly done by too many manual operations in the aircraft structure design process resulting in heavy workload, low efficiency and quality, non-standardized processes and procedures. A top-down associated design method employing the template parametric technology is proposed here in order to improve the quality of design and efficiency of aircraft wing structure at the preliminary design stage. The appropriate parametric tool is chosen and the rapid design system of knowledgedriven aircraft wing structure is developed. First, a skeleton model of aircraft wing structure is rapidly built up through the template encapsulated design knowledge. Associated design is then introduced to realize the association between the typical structural part and skeleton model. Finally, the related elements are referenced from skeleton model, and a typical structural part reflecting an automatic response for design changes of the upstream skeleton model is quickly constructed within the template. The rapid design system proposed and developed in this paper is able to formalize the design standardization of aircraft wing structure and thus the rapid generation of different aircraft wing structure programs and achieve the structural design knowledge reuse as well.
목차
Abstract
1. Introduction
2. Top-down design
3. Rapid design methods and development tool
4. Aircraft wing structure definition
5. Rapid modeling of skeleton model
6. Rapid modeling of typical structural part
7. Conclusion
References
참고문헌 (15)
참고문헌 신청
Haocheng, F. E. N. G., Mingqiang, L. U. O., Hu, L. I. U. and Zhe, W. U., “A Knowledge-based and Extensible Aircraft Conceptual Design Environment”, Chinese Journal of Aeronautics, Vol. 24, No. 6, 2011, pp. 709-719.
Ledermann, C., Ermanni, P. and Kelm, R., “Dynamic CAD objects for structural optimization in preliminary aircraft design”, Aerospace Science and Technology, Vol. 10, No. 7, 2006, pp. 601-610.
Tecklenburg, G. F. K., “Design of automotive body assemblies with distributed tasks under support of parametric associative design”, Hamburg: University of Hertfordshire, 2010.
Jia, H. L., Wang, A. M. and Tang, C. T., “Coordinate design technology based on product structure association mode”, Computer Integrated Manufacturing Systems, Vol. 17, No. 5, 2011, pp. 897-907.
Chen, Y. P., “Study and Application of Helicopter Collaborative Design Based on Digital Mock-Up”, Nanjing University of Aeronautics and Astronautic, 2010.
Ledermann, C., Ermanni, P. and Kelm, R., “Dynamic CAD objects for structural optimization in preliminary aircraft design”, Aerospace Science and Technology, Vol. 10, No. 7, 2006, pp. 601-610.
Tecklenburg, G. F. K., “Design of automotive body assemblies with distributed tasks under support of parametric associative design”, Hamburg: University of Hertfordshire, 2010.
Jia, H. L., Wang, A. M. and Tang, C. T., “Coordinate design technology based on product structure association mode”, Computer Integrated Manufacturing Systems, Vol. 17, No. 5, 2011, pp. 897-907.
Chen, Y. P., “Study and Application of Helicopter Collaborative Design Based on Digital Mock-Up”, Nanjing University of Aeronautics and Astronautic, 2010.
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UCI(KEPA) : I410-ECN-0101-2016-558-002776263