• 항공우주시스템공학회지
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• 제1권3호
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• pp.13-20
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• 2007

The objective of this study is to investigate endurance test of localization part for T-50 aircraft engine. Major localization parts of the engine (F404-STW-102) was performed using Accelerated Simulated Mission Engine Test. The purpose of this test is to evaluate of quality demonstration capability, to verify design of engine localization parts, and to improvement safety and operation rate of T-50 advanced trainer by finding out operational problems in production phase and fixing it.

• 항공우주정책ㆍ법학회지
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• 제28권2호
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• pp.97-115
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• 2013

항공기 운항의 가장 기본이 되는 규정은 ICAO Annex 6. Operations of Aircraft(항공기 운항)이다. 이 중 Part I은 상업항공운송용 항공기에 대한 것이며, 민간항공의 대부분을 차지하고 있다. ICAO에서는 항공기 운항에 관한 표준과 권고사항(SARPs: Standards and Recommended Practices)을 제정하여 체약국(Contracting States)이 어느 정도 국내규정에 반영하여 적용하고 있는지를 평가하고 있는데 이를 항공안전평가(USOAP)라고 한다. 기존의 ICAO 항공안전평가는 순간포착(Snap-shop) 방식으로 평가하였으나, 2013년부터 항공안전상시평가(USOAP-CMA) 방식으로 바뀌게 되어 시행된다. ICAO 항공안전평가 결과는 국적사의 노선, 보험료, 항공사간 제휴 등 국가항공산업 전반에 큰 영향을 미친다. 낮은 등급으로 판정 시, 국제사회에서 집중 주목이 되고 우리나라 국적사들이 운항정지, 노선제한, 항공사간 제휴 제한, 보험료 등 직/간접적으로 영향을 받을 수 있다. 따라서 우리나라 항공산업의 글로벌 경쟁력을 위해서는 ICAO 항공안전평가에서 '우수국가' 지위를 유지하여 높은 신인도를 이어나가는 것이 매우 중요하다. 우리나라는 2008년 실시된 ICAO 항공안전평가에서 종합 평점 98.89점을 획득, 세계 1위를 차지한 바 있으나, 2008년 이후 개정된 사항이 제대로 반영되지 못하고 있는 실정이다. 이에 따라 본 논문에서는 가장 최신의 개정판을 이용하여 ICAO Annex 6 Part I의 국내 항공법규 반영정도를 파악해보고자 한다. 아울러 미반영된 부분과 부분반영된 부분에 대한 반영방안도 같이 제시하고자 한다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2007년도 춘계학술대회A
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• pp.274-278
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• 2007

The purpose of this study is to analyze the important loads related with crack-growth in aircraft. Al Alloys mainly used in aircraft are Al2024 and Al7075 in Duralumin. In random fatigue loading, it has been understood crack-growth characteristic using fractured surface photograph by SEM. In order to obtained CTOD, we measured a crack size in wing frame part. As a result of fatigue experiment that accumulating plenty of fatigue loadings, we find more cracks than that produces in the same fatigue loading. The important loads relating to crack-growth was found in the largest strain cycle. Applying strain block in fatigue experiment, it is actually loading in connection of aircraft. In conclusion, These results can be used for preventing an accident owing fatigue-fracture in aircraft.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2005년도 추계학술대회논문집
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• pp.131-134
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• 2005

This study examine the annoyance of transportation noise exposure and found the survey method about which noise induces more disturbance or annoyance when more than two kinds of noise exist. This study describes the noise annoyance survey performed in the vicinity of Sin-wol interchange. This residential area was exposed to aircraft noise and traffic noise simultaneously and aircraft noise exposure of this area is about 81 WECPNL, traffic noise exposure is about 81.2 dB(A) nearby road. Noise sources are grouped into three part, traffic noise, aircraft noise and community noise. The questionnaire includes how often, how loud each noise is heard. Also this deals with comparative annoyance reaction from specific noise sources such as aircraft or traffic and its disturbance of daily activities. Facade noise mapping are executed by using a commercial noise mapping software.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.194-197
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• 2017

항공기 엔진과 보조동력장치는 안전성에 기반하여 감항성 기준과 인증절차에 따라 반드시 인증을 받도록 규정하고 있다. 항공기 엔진은 형식증명을 통하여 설계와 제작에 대한 적합성을 입증하여야 하며, 보조동력장치의 경우는 기술표준품 표준서에서 요구하고 있는 최소성능표준(Minimum Performance Standards)에 대하여 설계와 생산에 대한 적합성을 입증하여야 한다. 우리나라는 항공기 엔진에 대한 항공기기술기준으로 Part 33을 제정하고 있으나, 보조동력장치에 대한 인증 기준은 고시되지 않은 상태이다. 항공기 엔진과 보조동력장치의 개발과 인증체계 구축은 우리나라 항공 산업을 한단계 향상시킬 수 있는 계기가 될 것이다. 이에 본 논문에서는 항공기 엔진 및 보조동력장치에 대한 인증 현황을 통하여 개선 방안을 제시하고자 한다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2002년도 추계학술발표대회 논문집
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• pp.189-192
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• 2002

The autoclave process is frequently utilized in the manufacturing of aircraft parts because of the low void content and high fiber volume fraction. However, due to the slow curing process (5∼8 hours per part) and it's limited producibility for complicated shape, this process is very expensive and applied to the relatively simple geometry structures. RTM is considered as an alternative process to overcome the limitation of autoclave process. In this study, the idea of RTM application on the secondary Fairing structure of aircraft has been proved to be technically feasible and very cost effective by changing the multiple part of subassembly into one integral composite structure.

• 한국군사과학기술학회지
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• 제2권2호
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• pp.83-91
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• 1999

Dynamic characteristic of manufacturing stage is understood and the utilization of each machine is maximized by developing on-line dynamic CAPP system to consider the overloads in the aircraft part manufacturing line. In this paper, a scheme of production planning and scheduling system was proposed through inspection about some predeveloped CAPP system. Developed production planning and scheduling system included process planning module. After precise inspection of some FMS line schema at domestic heavy industry, optimized FMS line was applied to aircraft part manufacturing and repairing factory. By virtue of considering overloads of factory and machine through on-line dynamic CAPP system, the utilization of resources is maximized and manufacturing lead time is minimized.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.78-83
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• 2000

Exterior noise generated by the aircraft induces a serious noise pollution near the airport. For the prediction of an exterior noise radiation of aircraft an empirical formula is employed to model the acoustic sources. It is shown that the fan/compressor noise is the most dominant part of the acoustic sources in all cases.

• International Journal of Aeronautical and Space Sciences
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• 제17권1호
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• pp.101-108
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• 2016

The RCS characteristics of stealth modified three-surface aircraft are analyzed in this paper. Prototype A is built with CATIA software and the three-dimensional digital models of modified stealth three-surface B and C are also designed based on carrier-based aircraft Su-33; the numerical simulation of RCS characteristics of three-surface aircraft is conducted with RCSAnsys software based on physical optics method and the method of equivalent currents; The following results are obtained by comparative analysis and mathematical statistics: (1) by the use of physical optics method and equivalent electromagnetic current method, the scattering intensity for each part of the model and RCS characteristic of the aircraft can be analyzed efficiently and accurately; (2) compared with model A, the mean RCS value of model B is reduced to 14.1% in forward direction and 48.1% in lateral direction; (3) compared with model A, the mean RCS value of model C decreases to 11.4% in forward direction and 21.6% in lateral direction. The results are expected to provide theoretical basis and technical support to the conceptual design of aircraft and stealth technology research.

• 한국항공운항학회지
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• 제22권2호
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• pp.34-39
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• 2014

Airworthiness authorities specify the technical standards of airworthiness that propose minimum requirement of the commercial transport category and apply the rules in the certification process to ensure the safety of the aircraft. The Federal Aviation Administration and other national airworthiness authorities define the fatal accident risk levels for the safety assessment of the aircraft system and establish standard procedures to apply both qualitative and quantitative analysis techniques. However, an accident or incident may occur by the combination of various factors, although the aircraft is designed in accordance with the strict standards and approval by the Airworthiness Authorities. There are some key factors, such as human error, unpredictable complex system failures, degradation of the components reliability, improper maintenance task and intervals. Risk can be reduced by reflecting aircraft operational experience with similar types of aircraft in the process of aircraft development and safety assessment. Result of the root cause analysis for the Airbus A300-600 incident in which the aircraft engine reverser was deployed in the air have been introduced to reflect the design of system and related components. Also, this paper suggests to create a big-database in order to provide a feed-back to the FAR Part 25 transport category design and safety assessment of the operational experience.