• 한국콘크리트학회:학술대회논문집
• /
• 한국콘크리트학회 2005년도 추계 학술발표회 제17권2호
• /
• pp.255-258
• /
• 2005

The current ACI design code does not take into account the contribution of concrete for the torsional moment of reinforced concrete(RC) beams subjected to pure torsion. This code is not capable of evaluating the inter-effects between concrete and torsional reinforcement on the torsional resistance of the RC beams. In this study, 9 RC beams subjected to pure torsion were tested. The main parameter of the beams was the amount of torsional reinforcement and the angle of twist. Test results indicated that the current ACI code over-estimated the torsional strength of RC beams that had larger amount of torsional reinforcement.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2000년도 춘계학술대회논문집A
• /
• pp.803-808
• /
• 2000

This thesis studied whether friction welding of SPSS, localized torsion bar material could be accomplished or not. And then optimum welding conditions were examined and leaded through tensile, impact, torsion and hardness test after postweld heat treatment of the actual field condition. Obtained results were as follows; Linear relationship was existed between heating time and total upset, and a quadratic equation model could be made between tensile strength and heating time. Optimum welding conditions with fine structure were as follows in case total upset(U)=8.5mm; the number of rotations(n)=2,000 rpm, heating pressure($p_1$)=80MPa, upset pressure($p_2$)=200MPa, heating time($t_1$)=4sec, upset time($t_2$)=3 sec.

• 한국전기전자재료학회:학술대회논문집
• /
• 한국전기전자재료학회 2000년도 추계학술대회 논문집
• /
• pp.85-88
• /
• 2000

FRP has been used very much as high strength core materials for insulators because of its high strength and good insulation properties. In this study cantilever, tension and torsion stress were simulation along to the unidirection glass fiber. In addition, FRP was made by pultrusion method. This paper proposed the procedure of the finite element model updating and pretest using the commercial finite element code MSC. Nastran. To enhance the efficiency of experimental modal analysis, we proposed the process which is the selection of the locations and the number of measurement points for pre-test.

• Coupled systems mechanics
• /
• 제6권1호
• /
• pp.55-74
• /
• 2017

The evaluation of torsional effects on multistory buildings remains an open issue, despite considerable research efforts and numerous publications. In this study, a large number of multiple test structures are considered with normally distributed topological attributes, in order to quantify the statistically derived relationships between the torsional criteria and response parameters. The linear regression analysis results, depict that the center of twist and the ratio of torsion (ROT) index proved numerically to be the most reliable criteria for the prediction of the modal rotation and displacements, however the residuals distribution and R-squared derived for the ductility demands prediction, was not constant and low respectively. Thus, the assessment of the torsional parameters' contribution to the nonlinear structural response was investigated using artificial neural networks. Utilizing the connection weights approach, the Center of Strength, Torsional Stiffness and the Base Shear Torque curves were found to exhibit the highest impact numerically, while all the other torsional indices' contribution was investigated and quantified.

• 항공우주시스템공학회지
• /
• 제12권2호
• /
• pp.30-36
• /
• 2018

본 연구에서는 무인복합형 회전익기 연구의 일환으로 축소형 Tip Jet 로터 시험장치를 개발하였으며, 이를 이용하여 Tip Jet 로터에 대한 성능 및 동특성 연구를 수행하였다. 축소로터는 시험장 여건 및 공압조건 등을 고려하여 2m급이 되도록 하였으며, 압축공기를 이용하여 구동된다. 축소로터의 회전속도는 압축공기의 압력을 이용하여 조절되며, 별도의 하중측정부를 두어 회전 시 발생하는 추력과 각 방향의 하중 데이터를 획득하게 된다. 동특성 시험을 위해 별도의 유압 가진기가 장착되어 있으며, 로터 가진 시 발생하는 블레이드의 flap, lag 및 torsion 방향에 대한 동적 응답을 확인하기 위해, 각 블레이드의 익근부에는 full-bridge strain gage를 부착하였다. 성능 및 동특성 시험은 로터 회전수 및 블레이드 피치각을 변경해가며 실시되었다. 아울러 시험 결과의 유효성을 확인하기 위해 CAMRAD II 해석 결과와 비교하였다.

• 대한금속재료학회지
• /
• 제47권7호
• /
• pp.397-405
• /
• 2009

The high strain rate deformation behavior of ultra-fine grained 5083 aluminum alloys prepared via equal channel angular (ECA) extrusion was investigated in this study. The microstructure of ECA extruded specimens consisted of ultra-fine grains, and contained a considerable amount of second phase particles, which were fragmented and distributed homogeneously in the matrix. According to the dynamic torsion test results, the maximum shear stress and fracture shear strain of the route A (no rotation) specimen were lower than those of route C ($180^{\circ}$ rotation) specimen since that adiabatic shear bands of $100{\mu}m$ in width were formed in the route A specimen. The formation of adiabatic shear bands was addressed by concepts of critical shear strain, deformation energy required for void initiation, and microstructural homogeneity associated with ECA operations.

• 대한조선학회논문집
• /
• 제58권6호
• /
• pp.431-439
• /
• 2021

The Carbon Fiber Reinforced Plastic (CFRP) material is recently widely used in the composite industry with excellent rigidity and lightweight properties. A ship shaft system requires high standards of safety on torsional strength capacity. The purpose of this study is to verify the applicability of a CFRP shaft system to take the place of metal shaft systems for ships from a viewpoint of torsional strength. Selection of materials and manufacturing method are executed then two geometrically scaled CFRP shaft system models were designed and manufactured with three-layer patterns. The models were used for a series of torsion tests under single and repeated torsional loading conditions. Detailed design and manufacturing methods for a CFRP ship shaft system are documented and the torsion test results are listed in this paper. The results of this study could be useful guidelines on the development of CFRP ship shaft systems and a test method.

• 한국산학기술학회논문지
• /
• 제13권11호
• /
• pp.4956-4962
• /
• 2012

자동차의 다양한 부품 중 자동차 시트는 인간과의 직접 접촉 부위로서 승차감을 평가 할 수 있는 가장 기본적인 항목이다. 따라서 자동차 시트는 승차감과 동시에 충분한 강성과 강도를 가져야 할 것이다. 본 연구에서는 자동차 시트에서의 시트 쿠션 프레임과 백 프레임을 3D 모델링하였고, 쿠션 프레임의 비틀림 강도, 수직하중강도 시험, 백 프레임의 강도 시험 3가지 실험에 대해서 시뮬레이션으로 구조해석을 하였다. 해석결과, 쿠션 프레임 비틀림 강도 시험에서는 초기 전변형량의 최대값은 5.8421mm가 나왔고, 영구 전변형량의 최대값은 0.02539mm가 나왔다. 쿠션 프레임 수직하중강도 시험에서는 쿠션 프레임 앞쪽 끝단의 전변형량은 2.1159mm이고, 뒤쪽 끝단은 0.0606mm이다. 하중을 더 증가한 경우는 전변형량의 최대값은 3.1739mm가 나왔다. 3 가지의 백 프레임 강도 시험에서는 최대의 전변형량은 0.18634mm로 나타났다. 본 연구결과는 자동차 시트 쿠션 프레임 및 백프레임의 과도한 변형 및 파괴가 없음으로서 승객의 안전을 보장하는 충분한 강성과 강도를 검증할 수 있었다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2005년도 추계 학술대회논문집(수송기계편)
• /
• pp.41-44
• /
• 2005

This paper described improvement and operation of a 'Tail-Fan' anti-torque performance test system KARI (Korea Aerospace Research Institute) developed a 'Tail-Fan' anti-torque system of a helicopter and a performance test-rig to test the performance of the Tail-Fan. The test-rig was improved for full rotating test in 4300rpm(100%). Machinery and hydraulic parts ware changed to reduce vibration and to increase safety. To find the operation rotating speed for the performance test, vibration test were carried out rising accelerometers on tail gear box. The performance test conditions of the Tail-Fan to avoid a resonance were found from vibration test results. The Tail-Fan operation tests were performed safely frier to carry out performance test.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2004년도 추계학술대회논문집
• /
• pp.508-512
• /
• 2004

This paper described operation and vibration characteristics of 'Tail-Fan' performance test system. KARI(Korea Aerospace Research Institute) developed 'Tail-Fan' system as a kind of helicopter anti-torque system(ATS) and designed ATS performance test-rig for Tail-Fan system performance test. Test-rig consists of driving parts, supporting parts and rotating parts. For Tail-Fan system performance tests, firstly, test-rig operation tests were carried out for verification of design specifications. Secondly, natural frequencies of fan blade and test-rig were measured respectively. Lastly, to find the operation rotating speed for performance tests, vibration tests using accelerometers on tail gear box(TGB) were carried out. Through the fanplot and vibration test results, Tail-Fan performance test conditions to avoid a resonance were found and performance tests were well done safely.