• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2014.11a
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• pp.202-203
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• 2014

금형 내부의 마모를 줄이기 위한 경질 박막의 안정성 향상과 표면에 인가된 압축 잔류 응력이 고주기 피로 특성에 미치는 영향을 연구하기 위해 정밀 플라스틱 사출 금형강에 주로 사용되는 Fe-3.0%Ni-0.7%Cr-1.4%Mn-X강에 스크린 질화처리와 DLC 코팅을 시간과 단일, 복합처리의 변수를 두어 코팅하였다. PAPVD법으로 DLC($3{\mu}m$), 스크린 질화(3h, $50{\mu}m$)/DLC($3{\mu}m$) 코팅 후 고주기 피로 시험을 행하여 고주기 피로 특성을 평가하였다. 스크래치 시험, 마모 시험, 잔류응력 측정을 통해 질화 처리 여부에 따른 코팅의 안정성을 평가하였다. DLC, 스크린질화/DLC 코팅한 경우 압축 잔류 응력의 영향으로 모두 피로 수명이 향상되었고 스크린질화/DLC 코팅한 경우 그 향상폭은 더 컸다. 질화 처리 후 DLC 코팅한 경우 질화층은 버퍼레이어로 작용하여 코팅의 박리를 억제함을 확인하였다.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.142.2-142.2
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• 2005

• Journal of the KSME
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• v.55 no.2
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• pp.45-49
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• 2015

해석 및 측정 기술의 발전과 고내구성 소재 개발 등으로 인해 그동안 무한 수명으로 여겨져 왔던 천만 회의 피로수명을 넘어 운용되는 구조물들이 많아졌다. 이 글에서는 초고주기 피로현상과 이에 기초한 내구 설계의 개념 변화 및 시험법 등에 대해 소개하고자 한다.

• Korean Journal of Materials Research
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• v.11 no.4
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• pp.300-304
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• 2001

Effect of Cd addition on the fatigue properties of Al-Cu-Mn cast alloy was investigated by low and high cycle fatigue tests. With increasing Cd content, fatigue life and tensile strength were increased. It was found that the fatigue strength was 115MPa and the fatigue ratio was 0.31. Metallographic observation revealed that the fatigue crack initiated at the surface and propagated along the grain boundary. This propagation path was attributed to the presence of PFZ along the grain boundary. The tensile strength increased from 330MPa in the Cd-free Al-Cu- Mn cast alloy to 401MPa in the 0.15%Cd-containing alloy.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2004.05a
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• pp.117-117
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• 2004

일반적으로 접촉 피로 마멸은 구름 또는 미끄럼 접촉시 작용하는 반복 응력에 의해 표면과 표면 아래에 균열이 형성되고 성장 및 합체의 과정을 거쳐 표면의 일부가 떨어져 나가는 손상으로 기어나 캠-롤러, 구름 베어링과 같이 구름-미끄럼 접촉상태로 운전하는 기계요소에서 가장 중요하게 고려되어야 할 파손 메커니즘이다. 특히 기어나 구름 베어링 같이 고주기 접촉 피로 특성을 지니는 기계요소의 수명은 피로수명 실험과 통계적 기법을 이용한 Weibull 이론을 기초로 한 수명식을 대부분 사용하고 있다.(중략)

• Proceedings of the Materials Research Society of Korea Conference
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• 2001.11a
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• pp.30-30
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• 2001

• Journal of the Korean Society for Nondestructive Testing
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• v.30 no.4
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• pp.345-351
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• 2010

The oblique incidence technique for ultrasonic nonlinear characterization was studied in stainless steel 316L alloy subjected to high cycle fatigue. A dog-bone plate specimen was prepared to make different faitgue-driven deformation at each position where the stress concentration could occur in the middle of specimen. In addition to the normal transmission technique, the oblique incidence technique which is newly suggested in this study, was used to measure ultrasonic nonlinear parameter. The fatigued specimen shows higher ultrasonic nonlinear parameter than the virgin specimen for both techniques. Ultrasonic nonlinear parameter highly increases in the middle of test specimen where the stress concentration existes. Relative nonlinear parameter has strong correlation with fatigue damage. Consequently, the oblique incidence technique with longitudinal wave can be potential to characterize high cycle fatigue damage.

• Journal of the Korean Society of Propulsion Engineers
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• v.4 no.1
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• pp.93-101
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• 2000

In a gas-turbine engine, fan blades in flow path are confronted with many kinds of loading. The study of the excited force by the wake of struts has proposed and the possibility of fatigue failure about rotating fan blades by the excited force at the steady state is evaluated. Equations of the excited force of wakes has been derived at the steady state and the maximum pressure distributions measured at the transient state are proposed. Dynamic characteristics and the fatigue strength of fan blades by experimental test were obtained. To evaluate HCF(High Cycle Fatigue) damage of fan blades, FEM analysis was performed with a steady state harmonic response, which was followed by high cycle fatigue damage factor from goodman diagram.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.40 no.8
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• pp.759-765
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• 2016

The PTO (Power Take-Off) shaft for aircraft, with welded construction using multiple thin membranes, was developed in the 1950s to improve the elasticity of the part. As it is lightweight, stable at high speeds, and has good flexibility, it is used in most of the fighter aircraft. It connects the AMAD (aircraft mounted accessory drive) gearbox with the EMAD (engine mounted accessory drive) gearbox and transmits the rotational power between them. It operates in the high speed range of 10,000-18,000 rpm. In this study, the safety of the PTO shaft made of Ti alloy was investigated using finite element analysis, and the ability to transmit power was demonstrated through a high-cycle fatigue test conducted in a laboratory. Further, the life of the ball joints of the aircraft under high-cycle fatigue test conditions was predicted, and the wear characteristics were analyzed.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.240-244
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• 2017

Experimental verification in the rig test stage for component development is a vital link between the aeromechanical design and structural integrity validation process. Based on this premise, Non-Intrusive Stress Measuring System was adopted on the axial compressor test rig to measure the static and dynamic tip deflection of all blades by using tip-timing sensors. Through analyzing vibration characteristics, we evaluated the vibratory stresses seen on the blades fatigue critical location; detected synchronous resonances which are the source of High Cycle Fatigue (HCF) in blades; presented non-synchronous vibration response by aerodynamic excitation and individual blade mis-tuning patterns.