• Journal of Power Electronics
• /
• 제18권4호
• /
• pp.1255-1267
• /
• 2018

Parasitic parameters have a larger influence on Silicon Carbide (SiC) devices with an increase of the switching frequency. This limits full utilization of the performance advantages of the low switching losses in high frequency applications. By combining a theoretical analysis with a experimental parametric study, a mathematic model considering the parasitic inductance and parasitic capacitance is developed for the basic switching circuit of a SiC MOSFET. The main factors affecting the switching characteristics are explored. Moreover, a fast-switching double pulse test platform is built to measure the individual influences of each parasitic parameters on the switching characteristics. In addition, guidelines are revealed through experimental results. Due to the limits of the practical layout in the high-speed switching circuits of SiC devices, the matching relations are developed and an optimized layout design method for the parasitic inductance is proposed under a constant length of the switching loop. The design criteria are concluded based on the impact of the parasitic parameters. This provides guidelines for layout design considerations of SiC-based high-speed switching circuits.

• 대한기계학회논문집A
• /
• 제38권3호
• /
• pp.303-308
• /
• 2014

오늘날 비행기는 없어서는 안 되는 교통수단 중의 하나이다. 비행기는 교통 수단 뿐 만 아니라 여러 분야에서 널리 사용되고 있다. 예를 들어, 사람을 태우고, 짐을 실어 나르고, 군에서는 정찰 등의 임무를 수행하게 된다. 지상에서 이륙 착륙이 이루어 진다. 이륙할 때 보다는, 착륙할 시 랜딩기어에 많은 하중이 작용하게 된다. 착륙장치는 충격 에너지를 흡수하며, 사고 시에 동체가 파손되지 않도록 방지한다. 본 논문에서는 복합재와, 알루미늄을 적용한 판 스프링형 랜딩기어에 대하여 시뮬레이션을 수행하였다. 두 가지 재료의 랜딩기어에 대한 구조적 안전성이 평가되었다.

• 한국항공운항학회지
• /
• 제26권2호
• /
• pp.132-138
• /
• 2018

Aviation safety requires systematic national attention and management because aircraft accident produce greater undesired social impact, economical damage, and declining national credibility compare to other transportation accident. Specially, Republic of Korea has highly increased risk of air accident as a major air transportation point having small aerospace, connecting pacific ocean and Asia, and explosively increased air traffic produced by economical growth, operating numerous military aircraft for the South and North Koreas' confrontational situation. Also, greatly increased domestic and oversea air travels by Koreans and foreigners as well as air freight based on heightened Korea's national power, launching new low cost carriers, and popularized leasure aviation have produced large amount of aviation needs in various fields. However, national aviation safety management system gratifying increased aviation needs and aircraft operations is seem to be slow in progress. This paper will show optimized measures utilizing private, governmental, and military resources to prevent aircraft accident under circumstances of limited budget and an favorable conditions, then will propose several action items.

• 한국환경과학회지
• /
• 제23권12호
• /
• pp.2089-2099
• /
• 2014

Emissions from aircraft have impacts on the air pollution of airport and the surrounding area. There are methods of emissions calculated as Tier 1, Tier2, Tier 3A and Tier 3B. Thus, this study investigated emissions from aircraft at the Gimhae International Airport using EDMS(Emissions & Dispersion Modeling System) program. Results of estimation from aviation emissions, Tier 3B considering all parts which can occur at the airport has the largest amount emissions. In order to understand the relation between aviation emissions and distribution of ozone concentration over airport area, numerical evaluation were carried out. Although the difference of surface ozone distribution between numerical assessment with and without aviation emissions was little, effects of air pollution at airport area from aviation emissions of NOx and VOCs.

• 한국항공운항학회지
• /
• 제22권3호
• /
• pp.50-59
• /
• 2014

It has been focused on that the major reasons of aircraft accidents resulted not from human error but from the failure of teamwork or communication in 1980's. Such opinions were suggested in the workshop, so called, "Resource Management on the Flight Deck" by NASA in 1979. The researchers agreed the fact the source of human error was originated from the failure in teamwork, communication or even in leadership of captain. Due to the rapid development of aircraft technologies, the reasons for aircraft accident could be easily found out. According to the analysis results of the technology, most of reasons for the accident might directly be connected not to human error or stick-Rudder skill but to situational awareness, communication, leadership or decision making in the aircraft. This paper has tried to research empirically the satisfaction of flight crews who have gone thorugh CRM training in the commercial airline. Based on the quantitative scale by J. Ford et al. (2014), this paper has proved which characteristics of CRM training has a positive impact on the overall satisfaction of CRM training. It was proven that the teamwork and decision making programs among CRM training have a major effect to the satisfaction level of flight crews.

• 항공우주시스템공학회지
• /
• 제13권5호
• /
• pp.24-31
• /
• 2019

본 연구에서는 항공기용 전원분배장치에서 발생한 소손현상의 원인을 분석하고 개선 방안을 제안하였다. 항공기용 전원분배장치는 교류와 직류로 분류하며, 두 장비 사이에 정류기가 존재한다. 전원분배 장치의 전원이 켜지고 꺼질 때 전원 보드내의 커패시터가 소손되었다. 주요 원인은 정류기에 내장되어 있는 인덕턴스로 인해 과도한 전압이 발생했기 때문이다. 고장이 발생 할 수 있는 경우를 분류하였다. 그리고 그에 따른 영향성을 분석하였으며, 실험적인 방법을 통해서 해결책을 수립하였다.

• 한국지능시스템학회논문지
• /
• 제25권6호
• /
• pp.607-614
• /
• 2015

본 논문은 항공기 정비사의 핵심역량 16개에 대하여 정비능력향상을 목적으로 FSM을 이용하여 구조분석을 실시하여 최상층 3개, 중간층 3개, 하위층 10개로 분류되는 계층별 구조를 핵심역량간의 연결상태와 중요도를 파악하였다. 또한 항공기 정비사의 핵심역량은 업무를 통해서 정비품질 및 생산성이 향상될 수 있다는 관점에서 핵심역량과 업무를 퍼지관계를 이용하여 100명의 항공기 정비사의 설문을 통하여 퍼지관계행렬을 구하여 업무를 평가하는 기준으로 사용하고자 하였다. 본 논문에서는 모델링데이터 100개와 체킹데이터 67개를 사용하여 모델의 유효성을 보였다.

• 한국항공운항학회지
• /
• 제12권2호
• /
• pp.29-42
• /
• 2004

This paper performs a historical review on aviation threats through a statistical survey. The impact factor, as a criterion to measure the seriousness of the threats occurred, is introduced and evaluated based on annual totals of hijacking and fatalities against aircraft 1948 through 2004. Also, the paper suggests processes of evaluating the level of threats and key functions for an effective management of the aviation security.

• 대한기계학회논문집
• /
• 제19권9호
• /
• pp.2105-2113
• /
• 1995

The compressive tests under impact conditions were performed to establish a design guide for impact damage tolerance. The composition of layup was selected for the real cases of composite aircraft structure. The energy level of visible of visible damage threshold was determined as 7 Joules. It was found that the normalized bending stiffnesses in the direction of closely fixed boundary affected the area of damage. Graphite/epoxy used in the tests exhibited 60% reduction in compression strength at the energy level of visible damage threshold. Wet-conditioned specimens represented 9% reduction in residual compressive strength in comparison with room temperature ambient specimens. In this study, a design factor of 2.1 was proposed for the low velocity impact damage.

• International Journal of Advanced Culture Technology
• /
• 제11권2호
• /
• pp.381-388
• /
• 2023

Small-scale environmental impact assessments have limitations in terms of survey duration and evaluation resources, which can hinder the assessment and analysis of the current situation. In this study, we propose the use of drone technology during the environmental impact assessment process to supplement these limitations in the current situation analysis. Drone photography can provide rapid and accurate high-resolution images, allowing for the collection of various information about the target area. This information can include different types of data such as terrain, vegetation, landscape, and real-time 3D spatial information, which can be collected and processed using GIS software to understand and analyze the environmental conditions. In this study, we confirmed that terrain and vegetation analysis and prediction of the target area using drone photography and GIS analysis software is possible, providing useful information for environmental impact assessments.