• Journal of Aerospace System Engineering
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• v.18 no.1
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• pp.64-71
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• 2024

The external fuel tank of an aircraft is a main component that can increase the cruising range of the aircraft. It must be able to be stably separated from the pylon in an emergency situation. At this time, a separation load is applied to the fin and the pivot of the external fuel tank. To stably separate the external fuel tank, the structural soundness of the fin and the pivot must be confirmed. In this study, structural tests were conducted to verify the structural integrity of the external fuel tank pin and pivot when the external fuel tank was separated from the aircraft. Results are then presented. In this paper, a test configuration diagram consisting of the hydraulic and load control equipment, data acquisition system, and pneumatic supply unit used in the structural test was explained. Test installation and test load application plan for each test condition were provided. As results of the structural test, it was found that test load and internal pressure of the test specimen were properly controlled within the allowable range in each test. It was confirmed that serious structural defects in the test specimen did not occur under required load conditions. In conclusion, through structural test for design limit load and design ultimate load, it was proven that the fin and pivot of the external fuel tank for aircraft covered in this study had sufficient structural strength.

• Journal of Internet of Things and Convergence
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• v.9 no.2
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• pp.61-69
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• 2023

In recent years, due to heightened environmental awareness, Electric Power Steering (EPS) has been increasingly adopted as the steering control unit in manufactured vehicles. This has had numerous benefits, such as improved steering power, elimination of hydraulic hose leaks and reduced fuel consumption. However, for EPS systems to respond to actions, sensors must be employed; this means that the consistency of the sensor's linear variation is integral to the stability of the steering response. To ensure quality control, a reliable method for detecting defects and assessing linearity is required to assess the sensitivity of the EPS sensor to changes in the internal design characters. This paper proposes a data-driven defect and linearity assessment monitoring system, which can be used to analyze EPS component defects and linearity based on vehicle speed interval division. The approach is validated experimentally using data collected from an EPS test jig and is further enhanced by the inclusion of a Graphical User Interface (GUI). Based on the design, the developed system effectively performs defect detection with an accuracy of 0.99 percent and obtains a linearity assessment score at varying vehicle speeds.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.02a
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• pp.311-311
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• 2011

$TiN{\times}$박막은 우수한 내마모성 및 내부식성, 높은 경도 그리고 열적 안정성 등으로 인하여, 절삭공구 및 기계적 부품의 하드코팅, 2차 연료 전지용 확산방지막의 코팅재료로서 광범위하게 사용되어지고 있다. 일반적으로 $TiN{\times}$ 박막은 화학 기상 증착법(CVD)을 이용하였으나, 최근에는 대면적에 균일한 코팅이 가능하고 기판과 박막상의 부착력이 우수하며, 프로세스를 제어하기 쉬운 물리적 기상 증착법(PVD)의 스퍼터링법에 대한 관심이 고조되고 있다. 그러나 스퍼터링법으로 증착된 $TiN{\times}$ 박막의 물성은 주상구조와 국부적 표면결함을 포함하는 박막의 미세구조에 의존하기 때문에 주상구조 사이에 존재하는 Void 와 Pinhole 그리고 crack들이 원인으로 작용하여, 내부식성 및 기계적 특성이 급속도로 저하되는 단점이 있다. 이러한 단점을 보완하기 위해서, 본 연구에서는 기판온도를(RT, $200^{\circ}C$, $400^{\circ}C$)증가시켜 실험 하였다. 이는 온도증가에 따른 박막의 치밀화가 이루어지고 결함이 감소하여 내부식성 특성향상이 기대되어진다. 또한 플라즈마 밀도를 높이기 위해서, 기존 DC 마그네트론 스퍼터링법에 전자기장을 추가로 인가하였다. 이는 플라즈마 밀도증가에 따른 고반응성의 질소 래디컬의 생성율 증가에 기인하여 박막 형성시 질화반응을 촉진시킴으로써 박막의 치밀화 및 내부식성 특성향상이 기대되어진다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.6
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• pp.448-454
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• 2020

This study aims to determine the cause of structural defects occurring during aircraft operations and to verify the structural integrity of the improved features. The fracture plane was analyzed to verify the characteristics of the cracks and the fatigue failure leading to the final fracture was determined by the progress of the cracks by the repeated load. During aircraft operations, the comparative analysis of the load measurement data at the cracks with the aircraft design load determined that the measured load was not at the level of 30% of the design to be capable of being damaged. A gap analysis resulted in a significant stress of approximately 32 ksi at the crack site. Pre-Load testing also confirmed that the M.S. was reduced by more than 50% from +0.71 to +0.43, resulting in a sharp increase in aircraft load and the possibility of cracking when combined. Thus, structural reinforcement and the removal of the gap for aircraft cracking sites improved the defect. Based on the structural strength analysis of the improvement features, the bulkhead has a margin of about +0.88 and the fitting feature is about +0.48 versus allowable stress. In addition, the life analysis results revealed an improvement of approximately 84000 hours.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.4
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• pp.164-172
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• 2020

The fuel oil/heat exchanger installed in military aircraft is a device that cools the lubricant oil supplied to other devices, such as an AMAD, and a hydraulic pump using the low temperature of the fuel is cracked at the AMAD lubricant inlet port. If a crack in the heat exchanger occurs, the lubricant oil supplied to other equipment is not cooled. Therefore, the flight can no longer be performed. In this study, non-destructive inspection and microscopic examination of the fracture surface of the oil port were performed to analyze the crack tendency. The oil pipe connected to the oil port is a titanium pipe, which is fastened with over torque and has been identified as the leading cause of heat exchanger oil port cracks. In addition, it was verified as the main reason for cracking by finite element analysis. The material and diameter of the pipe were changed to improve this defect, and the applied torque was adjusted. In addition, the bending value of the pipe was adjusted to minimize the fatigue accumulation due to pulsating pressure. As a result, no cracks occurred on the heat exchanger via the ground test after the installation of an improved pipe under the same conditions.

• Journal of the Korean Institute of Gas
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• v.20 no.6
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• pp.16-22
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• 2016

Coating pipe(PLP) has been generally used in buried site for protecting the corrosion. To prevent the damage by occurring the defect, other construction or execution works, an anti-oxidation environment was forcibly made by using protective potential. Coating and protective potential are applied simultaneously, but corrosion rate or defects are not easy to observe because soil composition has many uncertainty. Also, defect of coating pipe can not be directly observed. A corrosion coupon can easily measure a corrosion rate directly. The corrosion rate was measured with 6 scenarios using corrosion coupon during about 1 year(6 scenarios are based on soil type and protective potential or not in this research. Resultingly, the corrosion coupon has not occurred in the case of protected by potential current, but corrosion has occurred in a non-protected site. The corrosion rate was measured at least in the clay, and the propensity of corrosion rate was similar in other soil(sand and loams). The local corrosion has occurred in the clay because of high water content. On the other hand, general corrosion was occurred in sand and loams. Commonly, sand is not to corrosive soil. Although, corrosion occurred in sand can be estimated by chemical component and valid with chemical analysis report.

• Nuclear Engineering and Technology
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• v.21 no.2
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• pp.143-149
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• 1989

In order to investigate the in-reactor performance of the 14$\times$14 PWR fuel burner: for 3 cycles in power reactor, non-destructive examination was carried out in KAERI Hot Facility. The results obtained are as follows. 1) The surface of middle and bottom parts of the fuel rod was dark and the upper part was gray. 2) Severe defect such as through-hole was not found. 3) The diameter of rod was shrinked by about 0.65%, while the length was increased by about 0.55% Compared with the design values. 4) The burnup was decreased by about 2% at the inconel grid region compared to other parts.

• Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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• v.35 no.6
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• pp.599-608
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• 2017

Cracks on the asphalt road surface can affect the speed of the car, the consumption of fuel, the ride quality of the road, and the durability of the road surface. Such cracks in roads can lead to very dangerous consequences for long periods of time. To prevent such risks, it is necessary to identify cracks and take appropriate action. It takes too much time and money to do it. Also, it is difficult to use expensive laser equipment vehicles for initial cost and equipment operation. In this paper, we propose an effective detection method of road surface defect using ROI (Region of Interest) setting and cany edge detection method using UAV image. The results of this study can be presented as efficient method for road surface flaw detection and maintenance using UAV. In addition, it can be used to detect cracks such as various buildings and civil engineering structures such as buildings, outer walls, large-scale storage tanks other than roads, and cost reduction effect can be expected.

• Journal of Advanced Navigation Technology
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• v.27 no.4
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• pp.436-446
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• 2023

In the field of safety-critical systems, analyzing the effects of various failure factors (failure modes) is essential through Failure Mode and Effects Analysis (FMEA). However, with the increasing importance of software in systems, applying FMEA analysis to the design phase has become challenging. This paper proposes the use of Automatic FMEA, which can automatically perform FMEA using model-based design techniques, and presents a case study of FMEA for automotive engines. A comparison is made between the model-based Automatic FMEA analysis tool and existing FMEA tools. The study aims to demonstrate the performance of the Automatic FMEA analysis tool and propose future research plans.

• Proceedings of the Materials Research Society of Korea Conference
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• 2011.05a
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• pp.23.1-23.1
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• 2011

최근 화석연료를 대체하기 위한 지속가능한 신에너지에 대한 요구가 증대됨에 따라 태양광 발전에 대한 연구도 폭발적으로 늘어가고 있는 추세이다. 태양광이 화석연료 대체에너지로 실효성을 가지기 위해서는 태양광 발전 시스템의 발전효율을 높이고 생산 비용을 저감하는 문제가 선결되어야 한다. 기존 실리콘 태양전지 시스템 설비 비용의 60% 이상을 차지하는 모듈의 제조과정에서 소재 손실을 최소화함으로써 저가격화를 실현하고자 박막형 태양전기 기술이 태동되었다. 현재 박막 태양전지와 관련하여 활발한 기술 개발이 진행되고 있으며 상당한 시장 점유율을 보이고 있는 실정이다. 박막 태양전지 분야에서 CIGS와 같은 화합물 반도체 박막 태양전지 시장이 확대되고 있는 실정을 고려한다면 실리콘 박막 태양전지의 경우 고효율화 저가격화 달성은 더욱 절실한 문제이다. 실리콘 박막의 경우 독성이 없으며 고갈 우려가 없는 소재이면서 기존의 직접회로 산업의 인프라 구조를 활용할 수 있어 많은 기대와 관심을 끌고 있는 박막 태양전지 후보이다. 박막 태양전지 제조에 있어서 핵심기술은 도핑된 실리콘층과 광흡수를 위한 진성 실리콘층을 합성하는 공정 기술이다. 현재 박막 태양전지 산업에서 실리콘 박막 소재의 합성은 주로 PECVD법에 의해 이루어지고 있다. 그러나 스퍼터 공정을 이용한 실리콘 박막 합성 연구 또한 20년 이상의 오랜 기간 동안 연구되어 오고 있다. 스퍼터 공정을 이용한 실리콘 박막합성는 독성 가스를 사용하지 않으며, 디스플레이와 같은 기존의 소자 공정 기술을 채용할 수 있다는 장점을 가지고 있어 주목 받고 있다. 실제로 반응성 마그네트론 스퍼터링에 의해 제조된 실리콘 박막은 PECVD공정에 의한 실리콘 박막에 상응하는 우수한 광전자적 특성을 보인다. 스퍼터 공정에서는 박막 성장을 위한 수송 물질들이 열적 평형 상태에 근접한 라디칼들이라기 보다 대부분 고에너지 원자종과 이온들이 주류를 이루고 있어 합성된 실리콘 박막의 결함 제어가 어렵다는 문제가 있다. 박막 합성 기구의 규명을 통하여 이러한 문제를 해결하기 위한 시도들이 이루어 지고 있으며, 본 발표를 통하여 스퍼터 공정을 이용한 태양전지용 실리콘 박막 합성기술에 대한 현황을 소개하고자 한다.