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.15 Number.1
- 발행연도
- 2014.3
- 수록면
- 32 - 43 (12page)
이용수
초록· 키워드
오류제보하기
Automatic fiber placement (AFP) has become a popular processing technique for composites in the aerospace industry, due to its ability to place prepregs or tapes precisely in the exact position when complex parts are being manufactured. This paper presents the design, analysis, and manufacture of an AFP mandrel for composite aircraft fuselage skin fabrication. According to the design requirements, an AFP mandrel was developed and a numerical study was performed through the finite element method. Linear static load analyses were performed considering the mandrel structure self-weight and a 2940 N load from the AFP machine head. Modal analysis was also performed to determine the mandrel’s natural frequencies. These analyses confirmed that the proposed mandrel meets the design requirements. A prototype mandrel was then manufactured and used to fabricate a composite fuselage skin. Material load tests were conducted on the AFP fuselage skin curved laminates, equivalent flat AFP, and hand layup laminates. The flat AFP and hand layup laminates showed almost identical strength results in tension and compression. Compared to hand layup, the flat AFP laminate modulus was 5.2% higher in tension and 12.6% lower in compression. The AFP curved laminates had an ultimate compressive strength of 1.6% to 8.7% higher than flat laminates. The FEM simulation predicted strengths were 4% higher in tension and 11% higher in compression than the flat laminate test results.
목차
Abstract
1. Introduction
2. Mandrel design
3. Finite element model
4. Finite element results and discussion
5. Composite fuselage skin development
6. Fuselage skin mechanical property test
7. Mechanical property test results and discussion
8. Conclusion
References
참고문헌 (24)
참고문헌 신청
1. [학술지(정기간행물)] - Hinrichsen, J. / 2001 / The challenge of Reducing both Airframe Weight and Manufacturing Cost / Air & Space Europe 3 (3-4) : 119 ~ 121
2. [학술지(정기간행물)] - Croft, K. / 2011 / Experimental Study of the Automated Fiber Placement Induced Defects on Performance of Composite Laminates / Composites Part A 42 (5) : 484 ~ 491
3. [보고서] - Russel, D. / / High-Speed Fiber Placement on Large Complex Structures
4. [단행본] - John, M. / / Applying Automation to the Fabrication of Composite based Aerospace Parts and Developing a Machine Specification / Accudyne Systems Inc
5. [기타자료] - Clarke, R. R. / 2005 / Unidirectional, Multi- head Fiber Placement / United States patent 7048024 B2
2. [학술지(정기간행물)] - Croft, K. / 2011 / Experimental Study of the Automated Fiber Placement Induced Defects on Performance of Composite Laminates / Composites Part A 42 (5) : 484 ~ 491
3. [보고서] - Russel, D. / / High-Speed Fiber Placement on Large Complex Structures
4. [단행본] - John, M. / / Applying Automation to the Fabrication of Composite based Aerospace Parts and Developing a Machine Specification / Accudyne Systems Inc
5. [기타자료] - Clarke, R. R. / 2005 / Unidirectional, Multi- head Fiber Placement / United States patent 7048024 B2
이 논문의 저자 정보
이 논문과 함께 이용한 논문
Study on the Influence of Clearance Ratio between Mandrel and Workpiece on the Spinning Stability of Cylindrical Workpiece with Extra Diameter-Thick Ratio
Xinhe Li
,
Yuesheng Yan
,
Rui Deng
기타자료
2011
.08
이음매 없는 관 인발에서 맨드렐과 금형 형상의 영향
이용신
,
윤상헌
,
윤덕재
소성·가공
2011
.12
맨드렐 관입길이에 따른 연약지반 스미어 존의 특성에 관한 연구
박영목
,
서정유
,
김재석
외 1명
대한토목학회 학술대회
2007
.10
실내모형시험을 이용한 Mandrels의 교란특성 비교
황성원
,
김종렬
,
정상국
외 1명
대한토목학회 학술대회
2006
.10
형상봉의 모양이 홀확장 잔류응력 분포에 미치는 영향에 대한 유한요소해석
장재순
,
조명래
,
양원호
Journal of the Korean Society for Precision Engineering
2006
.09
최근 본 자료
댓글(0)
0
UCI(KEPA) : I410-ECN-0101-2015-550-001318152