• 동력기계공학회지
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• 제13권5호
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• pp.52-58
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• 2009

A gas turbine consists of an upstream compressor and a downstream turbine with a combustion chamber, and also the compressor and the turbine are generally coupled using a single shaft. Many casing bolts are used to assemble two horizontally separated casings, the gas turbine casing and the compressor casing, in both of axial and vertical directions. Because drilled holes for casing bolts in vertical direction are often too close to drilled holes for casing bolts in axial direction, one can observe cracks in the area frequently during operations of a gas turbine. In this study of the root cause analysis for the cracking initiating from the drilled holes of the casings of a gas turbine, the finite element analysis(FEA) was applied to evaluate the thermal and mechanical characteristics of the casings. By applying the field operation data recorded from combined cycle power plants for FEA, thermal and thermo-mechanical characteristics of a gas turbine are analyzed. The crack is initiated at the geometrical weak point, but it is found that the maximum stress is relieved when the same type of cracks is introduced on purpose during FEA. So, it is verified that the local fracture could be delayed by machining the same type of defects near the hole for casing flange bolts of the gas turbine, where the crack is initiated.

• 한국추진공학회지
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• 제17권1호
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• pp.103-115
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• 2013

액체로켓 연소기에 사용되는 열차폐코팅(TBC)의 내구성 시험 기술동향을 조사하였다. 표면 접합력 측정을 위한 기계적 시험, 레이저나 가열로, 버너나 플라즈마 등을 이용한 열피로 시험, 분사기를 이용한 소형 연소시험, 열적 기계적 피로시험 등의 많은 내구성 시험들이 있었다. 연소기에 사용하기 위해 이러한 시편 수준의 시험을 통해 내구성이 확보된 TBC를 결정할 수 있으며, 실제 연소시험을 통해 내구성을 검증할 수 있다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.603-615
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• 2012

액체로켓 연소기에 사용되는 열차폐코팅(TBC)의 내구성 시험 기술동향을 조사하였다. 표면 접합력 측정을 위한 기계적 시험, 레이저나 가열로, 버너나 플라즈마 등을 이용한 열피로 시험, 분사기를 이용한 소형 연소시험, 열적 기계적 피로시험 등의 많은 내구성 시험들이 있었다. 연소기에 사용하기 위해 이러한 시편 수준의 시험을 통해 내구성이 확보된 TBC를 결정할 수 있으며, 실제 연소시험을 통해 내구성을 검증할 수 있다.

• 한국마이크로전자및패키징학회:학술대회논문집
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• 한국마이크로전자및패키징학회 2003년도 International Symposium
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• pp.147-163
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• 2003

European Union bans the usage of Pb in electronics from July 1 st, 2006. The Near-eutectic Sn-Ag-Cu alloys are the leading candidate Pb-free solders (for SMT card assembly). .The microstructure of Sn-Ag-Cu alloys is discussed in terms of solidification, composition and cooling rate. Methods of controlling Ag3Sn plates are discussed. .Thermo-mechanical fatigue behaviors of Sn-Ag-Cu solder joints are reviewed. Tin pest, whisker growth, electromigration of Pb-free solders are discussed.

• 대한기계학회논문집A
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• 제28권4호
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• pp.394-401
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• 2004

In this study the mechanical behaviors of fiber metal laminates(FMLs) such as ARALL, GLARE and CARE which are recently developed as new structural materials and known to have excellent fatigue resistant characteristics while with relatively low densities compared to the conventional aluminum materials, are considered through the classical lamination theory. The mechanical properties such as elastic moduli, thermal expansion coefficients and hygro-thermally induced residual stresses in the fiber metal laminates are obtained and compared each other. Also, carpet plots of effective elastic moduli, Poisson's ratio and the thermal expansion coefficient for GLARE FML are plotted.

• 대한조선학회논문집
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• 제38권3호
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• pp.93-106
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• 2001

선체 구조에서 피로 손상을 받기 쉬운 용접 부위인 T형 이음부(T-joint) 및 호퍼 너클 이음부(hopper knuckle joint) 모델의 피로실험 및 선형탄성 파괴역학을 이용한 피로균열 진전해석을 수행하였다. 집중 응력(hot spot stress)을 적용하여 정의된 균열 개시수명(균열 깊이 1mm)을 기준으로 하는 통합된 S-N선도를 작성하였으며, 잔류응력을 고려한 피로균열 진전해석을 통하여 피로균열 진전수명을 정확히 예측할 수 있었다. 또한, 임의의 형상을 가지는 용접 이음부(weld joint)의 피로균열 진전수명에 대한 정량화의 가능성을 확인하였다.

• 열처리공학회지
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• 제8권1호
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• pp.75-83
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• 1995

The purpose of this study is to investigate the effect of heat treatments on the martensite transformation and tensile deformation behavior in Ti-Ni-B alloys with various boron concentration. Three types of heat treatment are given to the specimens; i) solution treatment ii) aging iii) thermo-mechanical treatment. In solution treated specimens. R-phase transition which is related to abnormal increase of electrical resistance prior to martensitic transformation has been formed at a boron content of 0.2at % and the $M_s$ temperature has been decreased with the increasing of boron content. However. It has not been affected by aging, while that of thermo-mechanically treated specimens has been remarkably increased in the vicinity of recrystallization temperature. The thermo-mechanically treated specimen has showed a good thermal fatigue characteristics, shape memory effect and superelasticity in comparison with the solution treated specimen.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 춘계학술대회논문집A
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• pp.7-12
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• 2000

The automatic turbine startup system provides turbine control based on thermal stress. During the startup, control system monitors and evaluates main components of turbine using damage mechanism and life assessment. In case of valve chest, the temperature of inner/outer wall is measured by thermo-couples and the safety of these values are evaluated by using allowable ${\Delta}T$ limit curve during the startup. Because allowable ${\Delta}T$ limit curve includes life assessment, it is possible to apply this curve to turbine control system. In this paper, low cycle fatigue damage and combined rupture and low cycle fatigue damage criterion proposed for yielding the allowable ${\Delta}T$ limit curve of CV(control valve) chest. To calculate low cycle fatigue damage, the stress analysis of valve chest has peformed using FEM. Automatic turbine startup to assure service life of CV was achieved using allowable ${\Delta}T$ limit curve.

• 대한기계학회논문집A
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• 제39권4호
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• pp.447-451
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• 2015

본 연구의 목적은 유한요소 해석을 이용하여 항공기 엔진에 장착된 미세 튜브형 열교환기의 작동하중에 대한 특성을 파악하고 구조안전성을 평가하는 것이다. 작동 하중은 열-기계하중이 고려되었다. 항공기 엔진 부품의 특수성으로 인하여 구조적 강성확보뿐만 아니라 고효율, 저중량, 최소체적을 만족하는 형상 설계가 요구 된다. 브레이징한 미세튜브의 기계적물성치 확보를 위해 고온 인장 실험을 수행하였다. Ansys 12.1의 자체 모델러를 이용하여 형상을 모델링하고 유한요소해석을 수행하였다. 열-구조 연성해석을 통하여 튜브를 제외한 모듈형(modular type) 열교환기에 대한 설계방법을 제시하고 구조적 건전성을 평가하였다.

• 한국재료학회:학술대회논문집
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• 한국재료학회 2011년도 춘계학술발표대회
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• pp.48.1-48.1
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• 2011

In this presentation, We monitored weather data, such as global irradiance, ambient temperature, temperature of PV module, relative humidity and windspeed for 2 years, for determining accelerated test condition. then, we determined the temperature limit of accelerated test through weather data and FEM analysis. Detailed procedures will be summarized in this work. After analysing outdoor stress such as thermal stress, we decided main failure modes and mechanisms of PV module, especially solder joint of ribbon wire. we carried out the measurement of material properties such as thermal expansion coefficient for planning of accelerated test. we designed accelerated test based on FEM analysis results. we carried out thermal cycling test with 1 cell mini module for 3 months. We monitored the change of electrical performance every 1 week such as Voc, Isc, Pmax, etc. and then, we analized the ribbon wire/electrode intefaces. Detailed results will be summarized in this work.