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노발리스를 이용한 방사선 수술시 치료테이블을 투과하는 광자선의 감쇠율에 따른 선량 보정방법
김성준,신현수,고승영,박혜리,김자영,이보미,예지원,김성규,Kim, Sung-Joon,Shin, Hyun-Soo,Ko, Seung-Young,Park, Hye-Li,Kim, Ja-Young,Lee, Bo-Mi,Yea, Ji-Woon,Kim, Sung-Kyu 한국의학물리학회 2011 의학물리 Vol.22 No.1
본 연구는 노발리스용 치료테이블(couch top)을 투과하는 광자선의 감쇠율(attenuation rate)을 기하학적 모델을 통해 계산하고 보정함으로써, 치료부위에 정확한 선량이 전달되게 하는데 그 목적이 있다. 실험은 치료테이블을 투과하는 광자선의 투과율과 감쇠율을 기하학적인 모델에 의해 예측하고 이를 바탕으로 실험적으로 측정된 것을 비교 및 분석하였다. 그 결과 기하학적 모델에 의해 예측된 값과 실험값이 매우 잘 일치하는 것으로 나타났다. 또 실제 임상적용의 가능여부를 판단하기 위하여, 척추 방사선수술(spine radiosurgery)환자의 치료계획에 모델링화한 감쇠율을 보정한 뒤 측정한 중심점 선량과 그렇지 않은 것을 비교하였더니, 전자가 치료계획된 것과의 오차율이 감소함을 보였다. 본 논문에서는 치료테이블을 투과하는 광자선의 기하학적 모델을 통해 투과율과 감쇠율을 계산하고 이를 실험적으로 증명하였다. 이 방법은 노발리스를 이용한 방사선 수술뿐만 아니라 일반적인 방사선 치료에 있어서도 매우 유용할 것으로 판단된다. This study has its own goal to deliver the accurate dose on the target volume by calculating and modifying the attenuation rate of photon beam transmitting the couch top with geometric model. The experiment was that the transmission rate and attenuation rate of photon beam transmitting the couch top was predicted by the geometric model, then compared and analyzed with what was measured experimentally based on that. The result showed that the predicted value by the geometric model accorded closely with the experimental value. In addition, in order to judge whether the practical clinical application is available, the point dose, measured after modifying the attenuation rate modelinged according to the treatment plan of a patient of spine radiosurgery, was compared with the one done nothing. The result was that the former showed decreased error range with treatment planned one than the latter. This papers calculated the transmission and attenuation rate with the geometric model transmitting the couch top and verified it experimentally. This method is expected to be very useful in not only the radiosurgery using Novalis but also the general radiation therapy.
김성준,이승규,김태욱,Kim, Sung-Joon,Lee, Seung-gyu,Kim, Tae-Uk 한국항공운항학회 2017 한국항공운항학회지 Vol.25 No.2
Manned aircraft structural design is based on structural safety factor of 1.5, and this safety factor is equivalent to a probability of failure of between 10-2 and 10-3. The target failure probability of FARs is between 10-6 and 10-9 per flight according to aircraft type. NATO released STANAG 4703 to established the airworthiness requirements for small UAV which is less than 150kg. STANAG 4703 requires the Target Level of Safety according to MTOW. The requirements of failure probability for small UAV is between 10-4 and 10-5. In this paper, requirements of airworthiness certification for small UAV were investigated and the relationship of safety factors to the probability of structural failure is analyzed to reduce measure of safety factor and structural weight of unmanned aircraft.
보수시기를 고려한 염해에 노출된 콘크리트 교각의 탄소량 평가
김성준,김영준,권성준,Kim, Seong-Jun,Kim, Young-Joon,Kwon, Seung-Jun 한국건설순환자원학회 2014 한국건설순환자원학회 논문집 Vol.2 No.1
본 연구에서는 탄소배출 평가기법을 이용한 자재생산단계, 운송단계, 시공단계 뿐 아니라 보수시기 및 보수단위 탄소량을 고려하여 콘크리트 교각의 탄소배출량을 평가하였다. 혼화재료를 포함한 4가지 배합이 고려되었고 Life 365를 이용하여 염화물 침투를 평가하였으며, 이에 따른 보수횟수 및 보수시기를 설정하였다. 또한 목표내구수명동안 구조물의 피복두께를 걷어내어 재타설한 경우와 재타설 후 잔존염화물량을 제거하기 위한 전기화학적 공정의 사용유무에 따른 탄소배출량을 평가하였다. 평가결과 높은 물-결합재비를 가진 배합은 초기 시공단계에서의 탄소량은 상대적으로 적지만 보수횟수의 증가에 따라 탄소량이 증가하였으며, 탈염공법이 적용되는 경우 보수시의 단위 탄소량에 따라 전과정 탄소량이 크게 증가하였다. 보수횟수에 따라 탄소량의 증가가 발생하는데, W/B37-OPC의 경우 9번, W/B50-OPC에서는 18번, W/B40-SG에서는 4번, W/B74-SG는 7번으로 평가되었다. 더 긴 보수 불필요 기간을 가진 RC 구조물이 탄소량 감소에 유리함을 알 수 있다. In this paper, $CO_2$ amount is evaluated considering repairing timing and unit $CO_2$ amount per repair method including various stage of material manufacturing, moving, and construction. Four mix proportions with mineral admixture are considered and repairing timing/numbers are simulated based on the results from Life 365 which can handle chloride penetration. Furthermore two repair methods (simple cover concrete replacement and replacement with electro-chemical method for removing chloride content) are considered and the related $CO_2$ emissions are evaluated. From the study, the case with high W/B (water to binder ratio) ratio shows smaller $CO_2$ emission in construction stage but it increases more rapidly with increasing number of repair. $CO_2$ emission considering electro-chemical method greatly increases with the increasing unit $CO_2$ for the repairing method. The numbers of jumping step (repairing number) are evaluated to be 9 for WB37-OPC, 18 for WB50-OPC, 4 for WB40-SG, and 7 for WB47-SG respectively. RC structures with the longer maintenance free period are evaluated to be advantageous for saving $CO_2$ emission.
유무인 겸용 개인항공기(OPPAV) 개념설계를 위한 구조물 사이징
김성준,이승규,Kim, Sung Joon,Lee, Seung-gyu 한국항공운항학회 2020 한국항공운항학회지 Vol.28 No.1
Personal air vehicle (PAV) is considered by aviation engineers as a solution to provide fast urban mobility. The purpose of designing a optionally piloted PAV (OPPAV) is to provide an individual air vehicle. The airframe structure is designed with high strength carbon fiber composite to reduce the aircraft weight. This paper presents an overview of sizing process for OPPAV at the conceptual design level. It consists of load analysis, structural sizing and development of efficient design allowable values for composite material. The weight is estimated based on sizing process, including strength and stiffness requirements. The objective of this study is to present a overview of structural sizing procedure and fast tool for preliminary design phases.