• 제목/요약/키워드: Flying safety

검색결과 82건 처리시간 0.024초

재해사례 분석을 통한 제철소 공정별 주요위험요인 도출 (Deduction of Main Hazard Cause to the Progress of Iron Work for Accident Analysis)

  • 홍성만;박범;선수빈
    • 대한안전경영과학회지
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    • 제11권3호
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    • pp.33-40
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    • 2009
  • Steel and iron manufacture works exist that many latency risk as melting liquid of high temperature, work of high place, and so on. Once in a while, the accident case make use of basic data for latency risk analysis in a place of business. In this paper, we investigated the cause of the accident in steel an iron works. The result, we came across that many latency risk in steel and iron manufacture works. The main type of risk are fall, narrow, come flying, etc. Most of the latency risk type are repetition and conventional accident. Accordingly, steel and manufacture works must prevent to repetition and conventional accident.

무인항공체계 기반 시설물 상태점검 최근 연구동향 분석 (A Literature Review of Unmanned Aircraft System (UAS) Integrated Constructed Facility Condition Inspections)

  • 권진혁;윤지영;윤종영;이동훈;김성진
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2021년도 봄 학술논문 발표대회
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    • pp.172-173
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    • 2021
  • In recent, unmanned Aircraft Systems (UAS) have been widely used for various purposes, such as safety inspection, facility condition inspection, progress monitoring, in the architecture engineering, and construction (AEC) industry. This technology can provide visual assets regarding the conditions of construction jobsites as well as constructed facilities during flying over the point of interests. With the significant interests in this advancement, the recent studies have presented how the UAS can be applied fro different types of facilities (e.g., buildings, power genereation systems, roads, or bridges) to inspect the current conditions of them for safe operations as well as public's safety. This study reviewed the receent studies to document their scientific findings and practical contributions, as well as provided the overview of further implications for future studies.

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드론의 안정적 비행을 위한 핵심요소와 도시 수평 공간 구획 (Identification of key elements for stable flight of drones and horizontal space compartment in urban area)

  • 김정훈;김홍배
    • 국토계획
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    • 제53권7호
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    • pp.39-48
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    • 2018
  • The purpose of this study is to verify the stable flight conditions of drones within a limited urban area by using the ICAO(International Civil Aviation Organization) reich model which is using to evaluate civil aircraft stability. The results of the study are summarized as follows. First, in order for the drones flying stably, the horizontal safety separation distance between a drone and another should be at least 1,852M. Second, assuming that no obstacles within 1,852M of horizontal space, two drones can be fly into upper and lower spaces. However there are obstacles such as buildings, it is impossible to secure a 1,852M distance between drones. Third, sensitivity analysis point out that the separation interval($s_x$) of drone aviation has the greatest influence on the TLS(Target Level of Safety). If future research is conducted to lower the numerical values, the safety distance between a drone and another drone will be drastically reduced, allowing more detailed urban space division, and will be presented as a scientific numerical value for establishing a dedicated path for the drones.

A Study on the Urban Air Mobility(UAM) Operation Pilot Qualification System

  • Kim, Su-Ro;Cho, Young-Jin;Jeon, Seung-Mok
    • International Journal of Internet, Broadcasting and Communication
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    • 제14권1호
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    • pp.201-208
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    • 2022
  • As around the world, ground and underground transportation capacity is reaching its limit, centering on urban areas. As urban traffic becomes congested, time and cost are astronomical, and environmental destruction caused by urban pollution is becoming increasingly serious. As a way to solve this problem, the means of flying over the air are in the spotlight as the next generation of future transportation, and the concept of urban air mobility (UAM, Urban Air Mobility) is defined as systematic planning. The development of an electric-powered vertical take-off (eVTOL) aircraft that obtains electric power through a battery using a personal aerial vehicle (PAV) as a means of transportation has accelerated. As the aircraft development of new technology aircraft in the evtol method is actively carried out, the need to prepare systems such as aircraft certification standards, pilot qualification systems, and qualification management is emerging. The Federal Aviation Administration (FAA) and the European Union Aviation Safety Agency (EASA), which lead international standards, announced new special technical conditions and temporary regulations SCVTOL-01, respectively. However, the pilot qualification system for operating the uam aircraft has not yet been clearly announced. Therefore, this paper analyzes the recently announced FAA regulations and EASA regulations to identify differences and directions in perspectives on UAMs and study the existing vertical take-off and landing aircraft (VTOL) pilot qualification system to present directions for qualification classification.

산업용드론 재해발생 특성과 원인분석을 통한 재해예방에 관한 연구 (A Study on Accident Prevention through Analysis of Industrial Drone Accidents and Their Causes)

  • 변형식;임종국
    • 한국안전학회지
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    • 제34권6호
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    • pp.88-95
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    • 2019
  • It has been only a few years since drones have been introduced to Korea, and as the use of drones has increased in industrial sites as well as in hobby activities, accidents such as workers' body parts coming into contact with rotating propellers have been occurring since 2016. Industrial accident cases are being filed. In the case of a remote control vehicle, if you release the remote controller in the event of an abnormal situation, it stops in place and no further danger occurs but in case of drones flying over the sky is different. Sudden motor stops during flight, uncontrolled changes in flight posture, loss of radio waves, loose propeller, etc, numerous factors can lead to accidents due to unintentional movements. Therefore, drone operators need safety knowledge as well as high knowledge about drones. However, drones with a weight of less than 12 kg can fly without a pilot's certification, and therefore, a minimum accident prevention measure is required. 10 accidents approved as industrial accidents since 2016, 23 accidents surveyed by general drone operator, 40 accidents surveyed by the Korean Consumer Resources Unfortunately for the purpose of writing this paper, drones are a new species and do not have many parameters for analysis but my experience has shown that the type of disaster does not deviate significantly. In addition, there is no paper that analyzes drone related industrial accidents not only in Korea but also in other countries. However, even if you watch an overseas drone accident video through YouTube, it is not much different from the case that occurs in Korea. I hope that this study will be of little help to all the drone pilots as well as the work safety of industrial drones used in industrial sites.

PUF-based Secure FANET Routing Protocol for Multi-Drone

  • Park, Yoon-Gil;Lee, Soo-Jin
    • 한국컴퓨터정보학회논문지
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    • 제25권9호
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    • pp.81-90
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    • 2020
  • 군집 드론을 효율적으로 운영하기 위해서는 기존 통제방식이 개선되어야 하며, 드론들이 자율적으로 통신망을 구성할 수 있어야 한다. 이러한 문제를 해결하기 위한 대안으로 검토되고 있는 FANET(Flying Ad-Hoc Network)은 애드혹 네트워크 기술을 기반으로 하고 있어 다양한 보안취약점에 노출될 수 있다. 그러나 FANET 노드들의 제한적인 연산능력과 메모리, 급격하고 잦은 네트워크 토폴로지 변화 등으로 인해 애드혹 네트워크에 제안되었던 보안대책을 수정 없이 FANET에 그대로 적용하는것은 쉽지 않다. 이에 본 논문에서는 PUF 기술을 활용하여 기존 애드혹 네트워크와는 차별화된 특성을 가지는 FANET에 적용 가능한 경량화된 보안대책을 제안한다. 제시된 보안대책은 복제 불가능한 PUF에서 생성되는 고유한 값을 활용하여 FANET의 Reactive 라우팅 프로토콜인 AODV의 안전성을 높이며, 다양한 공격에 대한 내성을 가진다.

유체-구조 연계 해석기법을 이용한 세장비가 큰 비행체 날개의 공탄성 해석 (Fluid-Structure Interaction Analysis of High Aspect Ratio Wing for the Prediction of Aero-elasticity)

  • 이기두;이영신;이대열;이인원
    • 한국항공우주학회지
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    • 제38권6호
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    • pp.547-556
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    • 2010
  • 항공기의 안전성 확보 및 투하되는 탄의 정확도 증대를 위한 새로운 개념의 활공비행체 개발이 많은 기업에서 진행 중에 있다. 항공기의 장착 공간 및 활공거리 증대를 고려하여 세장비가 큰 전개되는 날개를 채택하는 것이 일반적이다. 큰 세장비의 날개 구조물은 상대적으로 낮은 강성에 의하여 과도한 탄성변형 뿐 아니라 플러터 발생의 가능성이 높아지게 된다. 본 연구는 큰 세장비 날개에 대하여 유체-공력 연계기법을 이용, 구조변형에 의한 공력특성의 변화 및 플러터 발생가능성에 대하여 검토하였다. 공기력 계산을 위하여 FLUENT 코드가 구조 동특성 해석을 위하여 ABAQUS 상용코드가 사용되었으며, 국부지지 방사기저함수로 구성된 Code-bridge를 이용한 입력 자료의 보간 및 사상을 수행하였다. 해석 결과 고려된 활공 조건에서 구조 변형에 의한 공력 특성의 변화가 발생하는 것이 관측되었으며, 이에 의한 진동도 계속적으로 발생되는 것으로 표현되었다.

인천국제공항과 김포국제공항 서비스품질 비교 연구 (A Comparative Study of Service Quality between Incheon and Kimpo International Airport)

  • 장대성;황인천
    • 한국경영과학회:학술대회논문집
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    • 한국경영과학회 2001년도 추계학술대회 논문집
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    • pp.35-38
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    • 2001
  • This study was conducted a comparative study to identify the differences in service quality between Incheon and Kimpo international Airport and critical factors influencing satisfaction of airport customers. According the results of this study, all service quality factors except the service factor of geographical location of Incheon international airport are better than those of Kimpo international airport. However, all of service quality factors of Incheon airport are evaluated as inferior to those of american, western european and japanese international airports by both the airport visitors and the employees of one korean airliner. In addition the service factors such as response, safety, airport facility and geographical location are found as critical factors influencing satisfaction of the airport visitors and the airliner's employees. Among them the service quality factor of geographical location of Incheon airport is much inferior to that of Kimpo airport comparing with other service quality factors. Thus, the results of this study suggest that the managing team implement TQM and six sigma to enhance the service quality level of the Incheon international airport up to that of the american and western european international airport. Especially, it is strongly required that the Korean governmen deliberate in deciding the geographical location in case of planning new international airport because geographical location is related to not only traffic to airport but also safety of landing, taking off and flying.

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Optimization of Space Debris Collision Avoidance Maneuver for Formation Flying Satellites

  • Seong, Jae-Dong;Kim, Hae-Dong
    • Journal of Astronomy and Space Sciences
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    • 제30권4호
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    • pp.291-298
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    • 2013
  • The concept of the satellite formation flight is area where it is actively study with expandability and safety compare to existing satellite. For execution of duty with more safety issue, it needs to consider hot topic of space debris for operation of formation flight. In this paper, it suggests heuristic algorithm to have avoidance maneuver for space debris towards operating flight formation. Indeed it covers, using common software, operating simulation to nearest space environment and not only to have goal of avoidance but also minimizing the usage of fuel and finding optimization for maximizing cycle of formation flight. For improvement on convergence speed of existing heuristic algorithm, it substitute to hybrid heuristic algorithm, PSOGSA, and the result of simulation, it represents the satisfaction of minimum range for successful avoidance maneuver and compare to not using avoidance maneuver, it keeps more than three times of formation maintenance performance. From these, it is meaningful results of showing several success goals like simple avoidance collision and fuel usage and decreasing number of times of maintaining formation maneuver.

Safety Assessment of a Metal Cask under Aircraft Engine Crash

  • Lee, Sanghoon;Choi, Woo-Seok;Seo, Ki-Seog
    • Nuclear Engineering and Technology
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    • 제48권2호
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    • pp.505-517
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    • 2016
  • The structural integrity of a dual-purpose metal cask currently under development by the Korea Radioactive Waste Agency (KORAD) was evaluated, through numerical simulations and a model test, under high-speed missile impact reflecting targeted aircraft crash conditions. The impact conditions were carefully chosen through a survey on accident cases and recommendations from literature. In the impact scenario, a missile flying horizontally hits the top side of the cask, which is freestanding on a concrete pad, with a velocity of 150 m/s. A simplified missile simulating a commercial aircraft engine was designed from an impact loade-time function available in literature. In the analyses, the dynamic behavior of the metal cask and the integrity of the containment boundary were assessed. The simulation results were compared with the test results for a 1:3 scale model. Although the dynamic behavior of the cask in the model test did not match exactly with the prediction from the numerical simulation, other structural responses, such as the acceleration and strain history during the impact, showed very good agreement. Moreover, the containment function of the cask survived the missile impact as expected from the numerical simulation. Thus, the procedure and methodology adopted in the structural numerical analyses were successfully validated.