• Journal of Advanced Marine Engineering and Technology
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• 제25권3호
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• pp.617-622
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• 2001

The purpose of this study is to design and the analyze the stress of composited shaft which is wound by filament winding method. The composites shaft has high strength and reduction in weight compared to metal shaft. The classical laminate plate theory(CLT) was used fro analysis the stress, and for structure design. In order to replace metal shaft by composites shaft, the diameter of shaft was determined to $\phi$ 40. The ration of diameter was determined to 0.4 for torsional moment with CLT. In this result of analyzing the stress, composites shaft was safe $30^{\circ}~60^{\circ}$C of winding angle, and was fractured on $90^{\circ}$.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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• pp.193-196
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• 2001

The purpose of this study is the design of composite shaft which is wound by Filament Winding method. Classical laminated plate theory was used for analyzing the stress, and for structure design. The diameter and thickness of composite shaft were calculated by this theory. The result that if tensile stress was zero, torsion stress was a certain value below 0.4(diameter rate) and torsion strength was the highest value on $45^{\circ}C$(winding angle). In case of $90^{\circ}C$(winding angle), we have to consider the torsional monent when the composites shaft was load.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2001년도 춘계학술대회 논문집
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• pp.140-145
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• 2001

The purpose of this study is the design of composite shaft which is wound by Filament Winding method. Classical laminated plate theory was used for analyzing the stress, and for structure design. The diameter and thickness of composite shaft were calculated by this theory. The result that if tensile stress was zero, torsion stress was a certain value below 0.4(diameter rate) and torsion strength was the highest value on 45$^{\circ}$(winding angle). In case of 90$^{\circ}$(winding angle), we have to consider the torsional moment when the composites shaft was load.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 춘계학술발표대회 논문집
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• pp.149-153
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• 2000

Substituting composite structures for conventional metallic structures has many advantages because of higher specific stiffness and specific strength of composite materials. In this work, one-piece propeller shafts composed of carbonfepoxy and glass/epoxy composites were designed and manufactured for a rear wheel drive automobile satisfying three design specifications, such as static torque transmission capability, torsional buckling and the fundamental natural bending frequency. Single lap adhesively bonded joint was employed to join the composite shaft and the aluminum yoke. For the optimal adhesive joining of the composite propeller shaft to the aluminum yoke, the torque transmission capability of the adhesively bonded composite shaft was calculated with respect to bonding length and yoke thickness by finite element method and compared with the experimental result. Then an optimal design method was proposed based on the failure model which incorporated the nonlinear mechanical behavior of aluminum yoke and epoxy adhesive. From the experiments and FEM analyses, it was found that the static torque transmission capability of composite propeller shaft was maximum at the critical yoke thickness, and it saturated beyond the critical length. Also, it was found that the one-piece composite propeller shaft had 40% weight saving effect compared with a two-piece steel propeller shaft.

• 한국해양공학회지
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• 제12권1호
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• pp.23-31
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• 1998

Kind 1 propeller shaft in ships is the shaft which is provided with effective measures against corrosion by sea water, or the shaft which is made of approved corrosion resistance materials. The propeller shaft other than specified above is Kind 2. Thus, this study is mainly concerned with the resistance to fatigue damage in sea water against stress concentrations due to the notches. The results obtained can be summarized as follows; (1) The stress increases with curing time, however, when the curing time reaches at 96 hours the stress becomes a constant value. The elongation decreases with curing time, however, when the curing time reaches at 48 hours the elongation becomes a constant value. Thus, in case of FRP coating on propeller shaft, it is necessary to cure for 48 hours at least. (2) The relation of $\sigma$$_n$-K$_t$ is to be classified into two parts, which is a part where fracture nominal stress, $\sigma$$_n$, decreases with increasing $K_t$, and a part where $\sigma$$_n$ is nearly constant independent of $K_t$. (3) According to a linear notch mechanics, the measure of severity controlling the fracture in notched FRP body is the notch root radius, $\rho$. The notched static strength of an arbitrary specimen will be estimated from $\sigma$$_{max}$ -1/$\rho$ curve. (4) Through the observation of cross section after fatigue test, the part of interface was kept good condition irrespective of loading conditions.

• Composites Research
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• 제34권6호
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• pp.380-386
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• 2021

본 연구에서는 탄소섬유 강화 복합재료를 적용하여 PTO 샤프트의 임계 속도를 향상시키는 연구를 진행하였다. 탄소섬유 강화 복합재료의 경우 전단 강도가 낮은 단점이 있어, 이를 보완하기 위해 티타늄-탄소섬유 강화 복합재료 하이브리드 구조로 설계하는 것을 제안하였다. PTO 샤프트에서 요구하는 최대 허용 토크, 임계 속도, 비틀림 고유진동수 기준을 충족시키는 최적의 구조를 설계하고 제작하였다. 제작한 PTO 샤프트의 성능 평가를 위해 진동 시험, 정적 비틀림 시험, 비틀림 내구성 시험이 수행되었고, 진동 시험에서 PTO 샤프트의 임계 속도는 20570 rpm로 티타늄 샤프트 대비하여 7.5% 향상된 것을 확인하였다. 또한 정적 비틀림 시험을 통해 PTO 샤프트의 최대 허용 토크가 2300 N·m로 해당 기준을 충족시키는 것을 확인하였다. 최종적으로 11.3~113 N·m 범위의 하중을 반복하는 비틀림 내구성 시험에서도 10⁶ 사이클 동안 피로파괴가 발생하지 않는 것으로 평가되었다.

• Composites Research
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• 제14권2호
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• pp.13-21
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• 2001

비강성, 비강도가 우수한 복합재료의 특성상, 기존의 금속 구조물을 복합재료 구조물로 대체 하는 것은 많은 이득을 가져온다. 이 논문에서는 탄소섬유/에폭시 복합재료와 유리섬유/에폭시 복합재료를 이용하여 정적 토크전달 능력, 비틀림 좌굴 하중. 굽힘 1차 고유진동수의 설계 기준을 만족하는 후륜구동 자동차용 일체형 동력전달축이 설계 및 제조되었다. 복합재료 중공축과 알루미늄 요크와의 결합을 위하여 단일 겹치기 접착조인트가 사용되었으며, 접착조인트의 정적 토크전달 능력은 접착길이와 요크두게에 따라 유한요소 해석을 이용하여 계산되었고, 실제 실험결과와 비교되었다. 복합재료 중공축의 정적 토크전달 능력은 Tasi-Wu 파괴지수와 아루미늄 요크와 에폭시 접착제의 비선형 물성을 적용하여 계산되었다. 실험과 해석결과로부터 복합재료 동력전달축의 정적 토크전달 능력은 임계 요크 두께에서 가장 높았으며, 임계 접착길이 이상에서는 포화되었다. 또한 일체형 복합재료 동력전달축은 기존의 2단 분리형 강철 동력전달축과 비교하여 40%의 무게 감소효과를 가져왔다.

• Composites Research
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• 제14권1호
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• pp.47-56
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• 2001

공기정압 주축 시스템의 동적 안정성을 향상시키기 위해 섬유강화 복합재료 주축 자성 분말이 함침된 에폭시 복합재료 회전자 및 알루미늄 재질의 공구 연결부로 구성된 주축 시스템을 설계 및 제작하였다. 복합재료 공기정압 주축 시스템의 최적 설계를 위해 구조의 공진 주파수와 변형량 등을 고려하여 복합재료 주축의 적층 각도와 두께를 결정하였다 해석결과 설계된 복합재료 주축 시스템은 기존의 금속 주축 시스템에 비해 36% 더 높은 공진 주파수를 가지는 것을 알 수 있었다. 계산 및 실험 결과를 통해서 섬유강화 복합재료 주축과 자성 분말이 함침된 에폭시 복합재료 회전자로 구성된 복합재료 주축-회전자 시스템은 높은 비 강성으로 인해 기존 주축 시스템의 동적특성을 향상시킬 수 있음을 확인하였다.

• Composites Research
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• 제20권1호
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• pp.1-7
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• 2007

본 논문에서는 골프클럽샤프트의 정적특성의 최적화 방법론을 제시하였다. 복합재료를 사용한 샤프트의 최적성능향상을 위한 쉬트 프리프레그의 적층순서를 구하였다. 클럽샤프트의 굽힘 강성과 비틀림 강성의 동시 최적화를 위하여 새로운 최적화 목적함수를 제시하였다. 샤프트의 정적특성 분석을 위하여 고전적층 이론을 적용하였으며 최적화 방법으로서 적층순서를 설계변수로 정의하는 유전알고리즘을 사용하였다. 또한 얻어진 최적적층순서를 바탕으로 한 샤프트의 동적특성을 분석하였다.

• 대한기계학회논문집A
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• 제26권2호
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• pp.308-313
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• 2002

It is known that the composite material shafts using on small boats have various advantages comparing to forged steel shafts, fur examples, specific strength, fatigue strength, corrosion, etc. The analysis of the stresses and strains in the composite material shafts made by filament winding method is presented in this paper. The classical laminated plate theory is applied on the patch cut from the composite material hollow shafts. It is verified that the composite material hollow shafts of diameter 40 mm is the most optimum when the ratio of the inner diameter to the outer is 0.4 and winding angle is 45$^{\circ}$. It is also proven that the shear strain does not change seriously between 30$^{\circ}$and 60$^{\circ}$of winding angles. It is dangerous when the winding angle is over 75$^{\circ}$because the values of shear strain and stress produced on the shaft are too high so it must be avoided to wind the filament by the angle over 75$^{\circ}$.