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
- 학술대회자료
- 저자정보
- 발행연도
- 2002.5
- 수록면
- 468 - 474 (7page)
이용수
초록· 키워드
오류제보하기
The driving torque and damping cbaracteristic of a SEH(Strain Energy Hinge) used in a satellite deployment mechanism depend on the geometrical shape and material property of the. thin plate spring used in the SEH. To obtain the desired motion of a deployment system, the SEH must be designed carefully. The design factors of a SEH include curvature, length and fixing method of the thin plate spring. Design factors are analyzed using experiments but a computational method must be developed to design the SEH effectively.
The buckling load of the SEH is the most important characteristic. to select the design factors. So in this paper: a computational method for the buckling analysis of a thin plate spring is presented. First, a nonlinear analysis method for the buckling load of a thin plate spring is presented. Next, finite element analysis of a presented method is applied to the SEH. Finally, the analysis result is compared with the testing result to show the effectiveness of the presented method.
The buckling load of the SEH is the most important characteristic. to select the design factors. So in this paper: a computational method for the buckling analysis of a thin plate spring is presented. First, a nonlinear analysis method for the buckling load of a thin plate spring is presented. Next, finite element analysis of a presented method is applied to the SEH. Finally, the analysis result is compared with the testing result to show the effectiveness of the presented method.
목차
Abstract
1. 서론
2. 이론
3. 예제
4. 결론
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UCI(KEPA) : I410-ECN-0101-2009-550-014199297