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체용론(體用論)으로 살펴 본 "동의수세보원(東醫壽世保元) "의 의미
전준영,박성식,Jeon, Jun-Young,Park, Seong-Sik 사상체질의학회 2005 사상체질의학회지 Vol.17 No.2
1. Objectives The pesent study purposed to examine Dongmu Lee Je-Ma's Sasang philosophy from the viewpoint of Che-Yong relation and to understand the effect of Che-Yong relation on Dongmu philosophy. 2. Methods First, we briefly compared the concept of Che-Yong relation in Jeongju philosophy, which has a dualistic philosophical structure, with the concept of Han Suk-Ji's harmonious Che-Yong relation, which has a monistic philosophical struaure and, based on rhe result, analyzed the characteristics of rhe concept of Che-Yong in Dongmu philosophy focused on Seongmyeong rheory, Sadan rheory and Hwakchung theory in ${\ulcorner}$Dongyi Suse Bowon${\lrcorner}$. 3 Results and Conclusions Jeongju philosophy is different from Dongmu philosophy in irs philosophical struaure characterized by Che-Yong relation, and the concept of Che-Yong in Dongmu philosophy forms the characteristics of Han Suk-ji's monistic harmonious Ole- Y ong relation. This produces results as follows. (1) Form a universal view of human beings centering of man's autonomous will and possibility. (2) Have a philosophical structure understood nor as a partial thought but as a total thought. (3) Assert that man has a good nature fundamentally and is obliged to practice goodness. (4) Assume that all human beings are equal. (5) It is assumed that the structural characteristics of harmonious Che-Yong relation in Dongmu philosophy can be the ground of definition of Silhak (practical science) in Oriental philosophy. It can be said that the realities of the universe and human beings can be discussed in philosophical structure with the logic of harmonious Che-Yong relation based on the unity of time and space. The philosophical logic based on the tealities can be defined as Silhak.
능동센서 배열을 이용한 저온 반복하중 환경 항공기 날개 구조물의 손상 탐지
전준영(Jun Young Jeon),정휘권(Hwee kwon Jung),박규해(Gyuhae Park),하재석(Jaeseok Ha),박찬익(Chan-Yik Park) 한국비파괴검사학회 2016 한국비파괴검사학회지 Vol.36 No.5
높은 고도에서 운행되는 항공기는 -50℃이하의 극저온 피로환경에 노출된다. 이때 반복하중을 통해 발생되는 크랙과 같은 미세결함은 항공기 구조물의 물성변화를 야기하고 구조물 파단과 같은 심각한 구조적 결함을 야기한다. 따라서 효율적인 구조물의 유지보수 및 수명 예측을 위해 구조물의 지속적인 상태진단이 필요하다. 본 연구에서는 실제 항공기 운행조건과 유사한 극저온 피로환경에서 항공기 날개의 구조 건전성 모니터링을 수행하였다. 초기 결함 탐지를 위해 사각배열 압전구동기 및 센서를 구조물 하단에 부착한 뒤, 유도초음파 기반 능동센싱 기법을 통해 손상에 의한 산란 및 반사파를 측정하였다. 이후 통계학적 모델 분석과 위상배열기법을 통해 손상 발생 시점을 파악 및 손상 위치 탐지를 실시하였다. 또한, 극저온 환경에서의 센서의 생존성 파악과 구조 건전성 모니터링 결과의 신뢰성 향상을 위해 센서자가진단을 실시하였다. 실험결과, 제안된 기법을 통해 극한환경에서 운행되는 구조물의 초기 손상 탐지 및 손상 위치 탐지가 높은 정확도로 가능함을 확인하였다. As aircrafts are being operated at high altitude, wing structures experience various fatigue loadings under cryogenic environments. As a result, fatigue damage such as a crack could be develop that could eventually lead to a catastrophic failure. For this reason, fatigue damage monitoring is an important process to ensure efficient maintenance and safety of structures. To implement damage detection in real-world flight environments, a special cooling chamber was built. Inside the chamber, the temperature was maintained at the cryogenic temperature, and harmonic fatigue loading was given to a wing structure. In this study, piezoelectric active-sensing based guided waves were used to detect the fatigue damage. In particular, a beamforming technique was applied to efficiently measure the scattering wave caused by the fatigue damage. The system was used for detection, growth monitoring, and localization of a fatigue crack. In addition, a sensor diagnostic process was also applied to ensure the proper operation of piezoelectric sensors. Several experiments were implemented and the results of the experiments demonstrated that this process could efficiently detect damage in such an extreme environment.
Cast Stainless Steel (CF8M) 재료의 시험결과 분산을 고려한 유한요소 손상해석
전준영(Jun-Young Jeon),김낙현(Nak-Hyun Kim),김윤재(Yun-Jae Kim) 대한기계학회 2012 大韓機械學會論文集A Vol.36 No.7
본 논문의 유한요소 손상해석기법은 재료 인장물성과 파괴기준을 필요로 한다. 기존에 연구된 재료들은 노치인장 시험결과로부터 하나의 인장물성과 파괴기준을 구할 수 있었다. 그러나 본 논문에서 사용된 cast stainless steel(CF8M)의 경우, 동일한 조건의 노치인장 시험결과들에 분산이 존재하여 해석자에 따라 다른 인장물성과 파괴기준이 구해질 수 있다. 따라서 해석자에 관계없이 일관된 인장물성 및 파괴기준을 구할 수 있는 적절한 절차가 필요하다. 본 논문에서는 노치반경 16mm 의 인장시편 시험결과로부터 평균 인장물성을 구하였고, 이를 유한요소 해석에 적용하여 3 개의 파괴기준을 구하였다. 구해진 인장물성과 파괴기준을 적용하여 J-R 파괴인성 시험에 대한 손상해석을 수행하였고, 시험결과와 비교함을 통해 제시된 절차의 타당성을 검증하였다. The damage analysis method in this paper needs a material property and failure criteria. The material properties and the failure criteria could be easily obtained from the results of notched bar tensile tests carried out on other materials studied previously. However, for the cast stainless steel (CF8M) material in this paper, because of the variance in the results from notched bar tensile tests under the same conditions, the material property and the failure criteria could be obtained differently, depending on the analyzer. Therefore, a proper procedure that can confirm the material property and failure criteria are needed. In this work, the averaged material property was obtained from the notched bar with a 16-mm notch radius, and three failure criteria for CF8M material by finite element analysis were obtained. Applying the material property and the failure criteria, FE damage analysis for the J-R fracture toughness test was conducted. For validation, the simulated results were compared with the experimental results.