• Journal of the Korea institute for structural maintenance and inspection
• /
• v.24 no.4
• /
• pp.91-99
• /
• 2020

Post-installed anchors were widely used due to its workable benefits. Regarding the resistance performance of anchors, the critical edge distance is presented to minimize the impact of concrete splitting. In the case of actual anchors, however, it is difficult to obtain the ideal edge distance. The purpose of this study is to identify resistance performance and behavior characteristics that contain complex elements such as concrete crack occurring under tensile load. Tensile tests were conducted based on the standard method. Failure shape and the resistance characteristics that do not have the critical edge distance were derived by tensile load. Parametric analysis according to the boundary condition was performed to simulate the actual tensile behavior, through a nonlinear finite element model based on the specimen. Consequently therefore, verifying analysis results the resistance mechanism can be applied through boundary conditions.

• Journal of the Korean Magnetics Society
• /
• v.18 no.2
• /
• pp.54-57
• /
• 2008

Magnetic torquer, which uses torque between magnetic dipole moment and earth magnetic field, has been used to control attitude of satellites. In this work, we developed a magnetic torquer for small scientific satellite and test under environmental conditions of the satellite launching and orbital motion have been carried out. The developed magnetic torquer shows saturation magnetic dipole moment of $15Am^2$, linearity of 0.3 % in the range of ${\pm}12Am^2$, mass of 0.46 kg, and power consumption of 1 Watt at magnetic dipole moment of $10Am^2$.

• Transactions of the Korean Society of Mechanical Engineers A
• /
• v.24 no.6 s.177
• /
• pp.1446-1455
• /
• 2000

Fatigue crack initiation and propagation behavior under cyclic biaxial loading has been investigated using thin-walled tubular specimen with a hole. Two types of biaxial loading system, i.e. cyclic tensile loading with super-imposed static torsional load and cyclic torsional loading with superimposed static tensile load, with various values of the biaxial loading ratio, $\tau$ s/ $\sigma$ max (or $\tau$ max/ $\sigma$s) were employed. Fatigue tests show that fatigue crack near the hole initiates and propagates at 900 and 450 direction to the longitudinal direction of the specimen under cyclic tensile and torsion loading with static biaxial stress, respectively, and the static biaxial stress doesn't have any great influence on fatigue crack initiation and growth direction. Stress analysis near the hole of the specimen shows that the crack around the hole initiates along the plane of maximum tangential stress range. Fatigue crack growth rates were evaluated as functions of equivalent stress intensity factor range, strain energy density factor range and crack tip opening displacement vector, respectively. It is shown that the biaxial mode fatigue crack growth rates can be relatively consistently predicted with these cyclic parameters.

• The Transactions of the Korean Institute of Power Electronics
• /
• v.16 no.5
• /
• pp.503-510
• /
• 2011

This paper presents a method of optimizing the blade pitch and generator torque controllers which have been already designed for an existing wind turbine generator system. Since the highly nonlinear and uncertain characteristics of the wind turbine generator can not be fully considered in the controller design phase, some parameters such as control gains must be tuned during the field implementation phase. In this paper, nonlinear simulation software, which is based high fidelity wind turbine model, and optimization technique are effectively combined and used to tune a set of gains for the blade pitch and the generator torque controllers. Simulation results show that the baseline controllers can be effectively optimized to reduce the errors in wind turbine rotor speed and generator power output controls as well as twisting of the high and low speed shafts.

• Computational Structural Engineering
• /
• v.10 no.3
• /
• pp.133-143
• /
• 1997

In Korea, the construction of the first high-speed railroad on the Seoul-Pusan Corridor has already started 3 years ago, in the paper, an attempt is made to develop reliability-based safety and capacity evaluation models for the computer-aided maintenance of the high-speed railroad bridges. The strength limit state models of PC railroad bridges for reliability analysis encompass both the single failure mode such as bending or shear strength and the combined interaction equations which simultaneously take into account flexures, shear and torsion. Then, the actual load carrying capacity and the realistic safety of bridges are evaluated using the system reliability-based equivalent strength, and the results are compared with those of the element reliability based or conventional methods. It is concluded that the proposed models may be appropriately applied in practice for the realistic assessment of safety and capacity of high-speed railroad bridges.

• Journal of the Society of Cosmetic Scientists of Korea
• /
• v.46 no.3
• /
• pp.243-252
• /
• 2020

Using Fervidobacterium islandicum AW-1, polar low molecular weight keratin peptides were produced and confirmed through factors related to the skin elasticity. As a result of confirming the cytotoxicity and collagen synthesis ability according to the concentration of the polar low molecular weight keratin peptide in human fibroblasts, it was confirmed that the cytotoxicity did not appear and the collagen synthesis in human fibroblasts was increased. A mask pack containing a polar low-molecular weight keratin peptide was used, and a test product was used for 4 weeks in 22 healthy women subjects. As a result, it showed statistically significant effects on skin elasticity, skin torsion elasticity, skin color and moisture improvement. Through this test, it was confirmed that the polar low-molecular keratin peptide can be used as a cosmetic ingredient that helps improve skin elasticity.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.30 no.7
• /
• pp.20-28
• /
• 2002

In this paper, the aerodynamic performance prediction of a 30kW counter-rotating (C/R) wind turbine system has been made by using the momentum theory as well as the two-dimensional quasi-steady strip theory with special care on the wake and the post-stall effects. In order to take into account the wake effects in the performance analysis, the wind tunnel test data obtained for a scaled blade are used. Both the axial and rotational inductions behind the auxiliary rotors are determined through the wake model. In addition, the optimum chord and twist distributions along the blades are obtained from the Glauert's optimum actuator disk model considering the Prandtl's tip loss effect. The performance results of the counter-rotating wind turbine system are compared with those of the conventional single rotor system and demonstrated the effectiveness of the counter-rotating wind turbine system.

• Proceedings of the KWS Conference
• /
• 2009.11a
• /
• pp.114-114
• /
• 2009

최근 국내외에서 자동차 연비와 성능 향상을 위하여 고부가가치 자동변속기의 개발이 적극적으로 추진되고 있다. 특히, 유럽(ZF)과 일본(JATCO, AISIN)을 비롯한 변속기 부품의 기술선진국에서는 전자빔 용접을 적용한 고부가가치 자동변속기 제품이 개발되어 다양한 고급차 모델에 적용되고 있으며 2010년까지 8속 자동변속기를 출시할 예정으로 개발을 추진하고 있다. 이러한 자동변속기를 개발하기 위하여 부품의 성형 및 가공정밀도 관리가 중요하며, 최종 조립되는 부품의 전처리(연질화처리, 탈지, 이물질 제거등)와 용접시 용접변형을 최소화하기 위한 공정조건의 엄격한 관리가 요구되고 있다. 변속기 부품으로 사용되는 소재는 성형성 확보를 위한 연질재(SPCC)와 강도를 확보하기 위한 고강도강(SAPH400, SPFH590)으로 서로 다른 두께의 재질이 조립되어 최종단계에서 용접공정에 의해 제작되고 있다. 특히, 연질재는 복잡한 형상으로 성형한 다음, 가공을 거쳐 경화를 위한 연질화처리가 요구되기 때문에 건전한 용접을 하기 위해서는 용접면에 접한 연질화 처리부는 연질화 처리재가 잔존하지 않도록 완전한 제거할 필요가 있다. 만약 전처리 공정에서 충분한 세척과 가공품의 정도관리가 확보되지 않으면 전자빔 용접시 고온에서 이물질 증발과 잔류, 스패터 발생등에 의한 용접부 결함발생이나 용접변형으로 인하여 제품불량이 발생하게 된다. 따라서 본 연구에서는 최종 조립공정인 용접작업시 발생되는 결함을 방지하고 이 두께 및 이종소재의 전자빔 용접비드 형상(비드 폭, 용입깊이)을 최적화 함으로서 용접부 변형을 최소화하고 충분한 강도를 확보하고자 전자빔 용접전류와 속도에 따른 비드형상을 비교검토 하고자 하였다. 그리고 실차적용시 신뢰성을 확보하기 위하여 전자빔 용접한 자동차 변속기 부품의 비틀림 시험을 실시하였으며 전자빔 용접 전, 후의 변형량을 측정하여 변속기 부품으로서의 적용성을 검증하고자 하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.39 no.5
• /
• pp.442-450
• /
• 2011

A measurement system using stereo pattern recognition (SPR) method was configured to measure the rotor blade deformations and motions. An SPR-based measurement system was prepared using six stereo cameras. Through a series of experiments to evaluate the system measurement uncertainty, it was verified that the SPR system had less than 0.2mm standard uncertainty. The combined standard uncertainties for the lead-lag, flapping, and pitching motions were estimated as 0.296mm, 0.209mm, and $0.238^{\circ}$, respectively. The SPR system was installed at a general small-scaled rotor test system at Korea Aerospace Research Institute. The blade motions and elastic deformation were successfully measured under the conditions with rotating speeds of 360rpm or 589rpm, and collective pitch angles of $0^{\circ}$, $4^{\circ}$, or $6^{\circ}$. The advantages of the SPR system was analyzed in comparison with the measurement system used in Higher Harmonic Control Aeroacoustic Rotor Test -II.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.41 no.12
• /
• pp.931-939
• /
• 2013

In this paper, we try to find the lifting-line method which is applicable to the conceptual design of aircraft wings, and analyze the accuracy and coverage of the method. Two methods that are extended from the lifting-line theory of Prandtl are selected. One of the methods is Weissinger's method which imposes the velocity boundary condition at the control points located at the quarter chord, and the other is Phillips's method which combines the three-dimensional vortex lifting law. Calculations are performed for an elliptic wing, a swept back wing, and a tapered unswept wing with dihedral angle and geometric twist. The aerodynamic data of the potential flow such as spanwise distributions of circulation and downwash, lift and induced drag are obtained through calculations, and these data are compared with theoretical results and wind tunnel test data. As a result, Weissinger's method showed good accuracy and reliability regardless of wing shapes, but Phillips's method revealed inaccurate results for a swept back wing.