• 한국항공운항학회지
• /
• 제31권2호
• /
• pp.89-94
• /
• 2023

Recently, domestic small airport development plans are being promoted centering on islands, and among them, Baengnyeong Island Airport is located very close to North Korea due to its geographical characteristics. In particular, since it is located in the P-518, which is prohibited airspace, it is essential to configure the arrival/departure flight procedure route similarly to the current ship in terms of securing flight safety. Therefore, in this study, a plan for airport location and facility scale was proposed by focusing on the runway operated for the purpose of aircraft operation through consultations with the Ministry of National Defense. It was proposed to meet the standards of the Airport Facility Act as an airport dedicated to domestic flights for airside facilities such as runway length and direction, target aircraft, landing pad, apron, runway and taxiway width appropriate for the topographical characteristics of Baengnyeong Island. As a result, the flight procedure is generally established as a two-way visual flight, but the 10-way arrival/departure procedure was planned to be changed to an instrument (non-precision) according to the specificity of the region. In addition, a flight procedure was established and presented for safe and systematic operation by reflecting the changes in airport facility size (landing pad, runway end safety area, etc.) following the change in instrument flight procedure in the visual flight procedure.

• 한국항행학회논문지
• /
• 제17권3호
• /
• pp.279-284
• /
• 2013

운항의 여러 단계 중 착륙단계에서 조종사들이 많은 부담을 느낀다. 이는 조종사들이 항공기 속도를 줄이고 접지하여 완전히 정지하는 동안 착륙안전에 영향을 미치는 여러 요소가 있기 때문이다. 만일 착륙하는데 활주로길이가 충분하다면 부담이 적을 수도 있다. 그러나 항상 그런 경우만 있는 것은 아니다. 따라서 착륙성능이 제한범위 내에 있는지 아닌지를 확인할 필요가 있다. 필요착륙거리는 시험비행 조종사에 의해 실증되어진 실제착륙거리에다가 항공사의 평균적인 조종사들을 위한 여유분을 포함한 것이다. FAR의 AFM(항공기 비행규정) 인가는 건조 및 습윤 활주로에서 수동착륙을 기반으로 한다. 기타 다른 활주로 조건에서는 인가가 필요하지 않다. JAR에서는 빙설/윤활활주로에서도 정해진 여유분을 포함시키도록 규정하고 있다. 자동착륙은 인가사항이 아니므로 실제착륙거리만 제공된다. 본 논문에서는 각 활주로 조건에서 포함된 거리 여유분을 분석하고자 한다. 또한 특정한 활주로 조건에서 여유분이 규정되어 있지 않은 경우 대안을 제시하고자 한다.

• 한국도로학회논문집
• /
• 제13권1호
• /
• pp.185-195
• /
• 2011

항공기 관련 사고는 많은 인명피해 및 물질적 손해가 크게 발생한다. 현재 국내 항공기 활주로 관련 사고는 전체 사고의 28%를 차지하고 있으며, 국제적으로 33%의 항공기 활주로 사고가 발생하였다. 이러한 사고를 예방하기 위하여 FAA에서는 규정에 미치지 못하는 활주로 종단안전구역에 과주방지 포장시스템의 설치를 의무화하고 있으며, 안전성 확보를 위하여 활주로 종단안전구역이 규정에 만족하더라도 과주방지 포장시스템의 설치를 권고하고 있다. 이러한 국제적 정세에 맞추어 국내에서도 과주방지 포장시스템에 대한 연구가 진행되고 있으며 과주방지 포장시스템의 국내 도입에 대한 절차도 이루어지고 있다. 이에 따라 본 연구에서는 과주방지 포장시스템에 대한 합리적인 성능평가를 하기위하여 FAA에서 사용하고 있는 ARRESTOR 프로그램과 3차원 비선형 동적해석이 가능한 LSDYNA를 이용하여 항공기의 활주로 과주에 따른 제동거리, 견인력, 수직력 및 관입량을 비교하였다. 해석 결과 제동거리는 비슷하게 해석되었고, 견인력 및 수직력은 다소 차이가 발생하였으나 경향은 비슷하게 도출되었다. 추후 다양한 항공기 조건 및 포장재료의 특징을 고려한 3차원 시뮬레이션 해석이 필요하며, 지속적인 시뮬레이션 해석 기법을 개발하여 보다 정확한 해석방법을 개발할 필요가 있다.

• 한국안전학회지
• /
• 제36권5호
• /
• pp.92-92
• /
• 2021

• 항공우주정책ㆍ법학회지
• /
• 제33권2호
• /
• pp.199-224
• /
• 2018

Aviation's safety record continues to improve yearly, especially with respect to passenger and crew injuries and deaths. However, although the number of accidents has decreased over the decades, there are still many events, such as landings short of the runway and runway excursions, both of which pose threats to passenger and crew safety. Surviving any kind of aviation accident depends on the physiological threat and stress of the impact(s), the extent to which the physical structure surrounding the passengers and crew remains intact, and the ability of the passengers and crew to be able to escape the wreckage. The one action that both passengers and crew can carry out to help decrease the likelihood of crash-related injury or death is to assume an emergency brace position. Doing so has been demonstrated over several decades to improve survivability. While cabin crew are taught (and then might have to teach passengers in an emergency about the emergency brace position), passengers in many parts of the world never learn about the brace position unless they are involved in an emergency in which there is time to prepare for the landing. This lack of provision of information is related to the fact that most airlines do not provide information in the preflight safety briefing and some do not even provide the information in the passenger safety cards. Many countries do not require their airlines to do so, a fact, which in turn, is related to the lack of mention of the brace position in ICAO's Annex 6. Until standards and recommended practices are changed at the highest world level, passengers will continue to be deprived of this vital, life-saving information that they can use, potentially to help save their own lives.

• 한국항행학회논문지
• /
• 제28권3호
• /
• pp.375-378
• /
• 2024

The instrument landing system (ILS) is an international standard established by the International civil aviation organization (ICAO) as one of the landing support facilities for aircraft. This system consists of a localizer (LOC) that provides orientation information about the runway to indicate the approach direction, a glide path (GP) that indicates the appropriate approach glide slope, and three of marker beacons (MB) that indicates the distance to the runway landing edge. In this study, we predicted the received signal strength by altitude and distance for LOC signals transmitted from the ground and analyzed the difference with the signal strength measured in the actual environment. Our objective is to develop signal strength prediction technology and apply it to the real environment.

• 한국항공운항학회지
• /
• 제31권3호
• /
• pp.93-102
• /
• 2023

Jeju International Airport is characterized by the occurrence of low-level windshear due to its location, surrounding terrain, and its weather characteristics. Especially the low-level windshear accompanied by tailwinds on both sides of the runway i.e., bidirectional tailwind, is a hazardous weather phenomenon with unique characteristics that are difficult to find at any other airports. This study focuses on bidirectional tailwind occurrence at Jeju International Airport in 2020-2021. As a result, characteristic pressure patterns of the types that cause bidirectional tailwind was identified as it was possible to categorize strong wind types such as 1) strong southwest wind, 2) strong east wind, and 3) strong northwest wind, which do not cause bidirectional tailwind, and wind direction variation types such as 4) bidirectional tailwind, and 5) south wind followed by southwest wind, which cause bidirectional tailwind. The results of this study are expected to contribute to improving aviation safety by enabling aviation operators to predict and take appropriate safety measures based on their understanding of the causes and characteristics of bidirectional tailwind.

• 한국도로학회논문집
• /
• 제12권3호
• /
• pp.59-70
• /
• 2010

최근 몇 년간 국내 외에서는 연평균 10건 이상의 항공기 과주사고가 발생하고 있으며, 이러한 사고를 방지하고자 활주로 종단안전구역 기준을 설정하였다. 그러나 대부분의 공항은 종단안전구역 기준을 설정하기 전에 시공되어 기존 활주로의 경우 대부분이 활주로 종단안전구역 기준을 만족하지 못하고 있는 실정이며 자연장애물, 환경, 지역개발 등으로 활주로 종단안전구역의 기준에 부합하도록 활주로 종단을 확장하기 곤란한 경우가 많다. 이러한 이유로 미연방항공청은 활주로 종단에 항공기 과주방지 포장시스템을 설치하도록 권고하고 있으며, 현재 많은 미국 공항에서 설치완료 하였거나 설치 중에 있다. 이에 따라 본 논문에서는 국내 기술을 이용하여 항공기 과주방지 포장시스템에 적합한 재료를 개발하기 위하여 저강도 펄라이트 콘크리트의 기초적인 연구를 수행하였다. 저강도 펄라이트 콘크리트의 단위중량은 배합조건에 따라 $4.5{\sim}6.4kN/m^3$의 범위를 나타내었으며, 일축압축강도는 $400{\sim}1,470kN/m^2$의 강도 범위를 가지고 있었다. CBR 시험기를 이용하여 관입압축강도시험을 수행한 결과 전체 높이에서 관입량이 약 60% 이후부터 강도가 증가하기 시작하였으며, 덤프트럭을 이용하여 관입시험을 수행한 결과 약 40%의 관입량이 측정되었다.

• Advances in concrete construction
• /
• 제12권5호
• /
• pp.411-418
• /
• 2021

Roller compacted concrete (RCC) used in the island reef airport runway will be subjected to the coupling actions of the fatigue impacts and the salt spray cycles, which will accelerate the deterioration of runway concrete and even threaten the flight safety. A cyclic impact testing machine and a climatic chamber were used to simulate the low-velocity fatigue impact and the salt spray cycles, respectively. The physical properties, the microstructures and the porosity of RCC were investigated. The results show the flexural strength firstly increases and then decreases with the increase of the fatigue impacts and the salt spray cycles. However, the decrease in the flexural strength is significantly earlier than the compressive strength of RCC only subjected to the salt spray cycles. The chlorine, sulfur and magnesium elements significantly increase in the pores of RCC subjected to 30000 fatigue impacts and 300 salt spray cycles, which causes the decrease in the porosity of RCC. The coupling effects of the fatigue impacts and the salt spray cycles in the later period accelerates the deterioration of RCC.

• 한국안전학회지
• /
• 제36권3호
• /
• pp.24-30
• /
• 2021

Heat is generated during the synthesis and mixing process of chemical compounds due to a change in activation energy during the reaction. A runaway reaction occurs when sufficient heat is not removed during the heat control process within a reactor, rapidly increasing the temperature, reaction speed, and rate of heat generation inside the reactor. A risk assessment was executed using an RC-1 (Reaction Calorimeter) during Friedel-Crafts acylation. Friedel-Crafts acylation runs the risk of rapid heat generation during Active Pharmaceutical Ingredient (API) manufacturing; it was used to confirm the risk of a runaway reaction at each synthesis stage and during the mixing process. This study used experimental data to develop a safety efficiency improvement plan to control the risks of runaway and other exothermic reactions, which was implemented at the production site of a chemical plant.