• KIEAE Journal
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• 제9권1호
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• pp.99-106
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• 2009

This study aims to survey the acoustical environment in the region around airport where there are various transportation noises such as aircraft noise, railway noise and traffic noise, and to analyze the subjective response on the noise to the people who live in house or work in office nearby airport. Measurement and subjective response evaluation were carried out at the same time and outdoor noise level was measured all day long to calculate one day results such as average Leq or one day WECPNL etc. The results showed that the military aircraft produces very high level comparing with commercial aircraft, for instance the sound level of commercial outdoor was lower than that of military aircraft indoor. Double and triple window were more effective for controlling the noise than single window, which showed the possibility of sound insulation treatment by installing windows having higher sound insulation performance. Finally the subjective response was resulted that the most annoying noise is from aircraft and counterplan they hope is 'airport moving out'. Leq 65 dB(A), the criteria value of sound insulation treatment, was corresponding to the subjective response of median annoyance '4' out of 7th scale.

• 항공우주정책ㆍ법학회지
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• 제27권1호
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• pp.75-101
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• 2012

As the Reublic of Korea revised the Commercial Code including 40 articles of air transport enacted newly on May 23, 2011, so Korea became first legislative examples in the Commercial Code of the developed and developing countries. I would like to explain briefly the main contents of my paper such as (1) history of enacting newly Part VI (air transport) in the Korea's revised commercial law, (2) legal background enacting newly Part VI (air transport) in the Korea's revised commercial law and the problems on the conditions of air transport, (3) every countries' legislative examples on the civil liability of aircraft's operator, (4) unlawful Interference Convention and general risk convention of 2009, (5) main contents and prospects of the revised Commercial Code for the liability of aircraft's operator etc as the followings. Meanwhile as the Aviation Act, Commercial Code and Civil Code in Korea and Japan did not regulated at all the legal basis of solution on the disputes between victims and offender for the amount of compensation for damage due to personal or property damage caused by aircraft accidents in Korea and Japan, so it has been raised many legal problems such as protection of victims, standard of decision in trial in the event of aircraft accident's lawsuit case. But the Korean Revised Commercial Code including Part VI, air transport regulations was passed by the majority resolution of the Korean National Assembly on April 29, 2011 and then the South Korean government proclaimed it on May 23 same year. The Revised Commercial Code enforced into tothe territory of the South Korea from November 24, 2011 after six month of the proclaimed date by the Korean Government. Thus, though Korean Commercial Code regulated concretely and respectively the legal relations on the liability of compensation for damage in the contract of transport by land in it's Part II (commercial activities) and in the contract of transport by sea in its Part V (marine commerce), but the Amended Commercial Act regulated newly 40 articles in it's Part VI (air transport) relating to the air carrier's contract liability on the compensation for damage caused by aircraft accidents in the air passengers and goods transport and aircraft operator's tort liability on compensation for damage caused by the sudden falling or collision of aircraft to third parties on the surface and so it was equipped with reasonable and unified system among the transport by land, marine and air. The ICAO adopted two new air law conventions setting out international compensation and liability rules for damage caused by aircraft to third parties at a diplomatic conference hosted by it from April 20 to May 2, 2009. The fight against the effects of terrorism and the improvement of the status of victims in the event of damage to third parties that may result either from acts of unlawful interference involving aircraft or caused by ordinary operation of aircraft, forms the cornerstone of the two conventions. One legal instrument adopted by the Conference is "the Convention on Compensation for Damage to Third Parties, Resulting from Acts of Unlawful Interference Involving Aircraft" (Unlawful Interference Convention). The other instrument, "the Convention on Compensation for Damage Caused by Aircraft to Third Parties" (General Risk Convention), modernizes the current legal framework provided for under the 1952 Rome Convention and related Protocol of 1978. It is desirable for us to ratify quickly the abovementioned two conventions such as Unlawful Interference Convention and General Risk Convention in order to settle reasonably and justly as well as the protection of the South Korean peoples.

• 항공우주산업기술동향
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• 제6권2호
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• pp.154-160
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• 2008

항공기의 개발에 있어 비행시험은 통상적으로 크게 민간용과 군용의 두 분류로 나눌 수 있다. 민간용 항공기의 비행시험은 해당 정부의 감항당국에서 제시하는 안전/성능 요구도를 항공기가 충족하는지 여부를 개발자가 확인하는 것이다. 이에 반해 군용항공기의 비행시험은 소요제기를 한 해당 정부의 요구도를 항공 기기가 충족하는지 여부를 개발자의 사전점검(DT: Developmental Test) 이후에 정부의 독립적인 평가팀에 의해 Operational Test(OT)가 수행되어 최종적으로 확인하는 과정으로 진행된다. 이 논문에서는 민수용 항공기와 군용항공기 각각의 목적상 추진되던 인증업무가 비용의 효율성 제고, 민간항공기의 군용화 추세에 따라 민간항공기 인증방안을 사용해 군용항공기의 감항인증을 추진하는 선진국의 최신동향을 살펴보고 국내의 여건 및 향후 발전발향을 제시하고자 한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1997년도 춘계학술대회논문집; 경주코오롱호텔; 22-23 May 1997
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• pp.643-648
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• 1997

Concern for noise problems of a commercial aircraft in community and cabin is increasing due to the more restrictive regulation and customer requirements. This paper introduces to the work packages of the aircraft noise engineer for the development of a commercial aircraft. First of all, the noise engineer establish the design requirement and objectives(DR&O). Then the design and analysis are performed to satisfy with the DR&O during the conceptual and preliminary design phase. And the test and evaluation(T&E) are carried out to verify the analysis results and to acquire the type certification.

• 항공우주정책ㆍ법학회지
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• 제29권2호
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• pp.3-54
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• 2014

오랜 논의와 노력 끝에 우리나라 상법 제6편 항공운송편이 신설되어 2011년 11월부터 시행되었다. 상법 항공운송편은 국내항공운송으로 인해 발생한 항공 운송인의 손해배상책임 문제와 항공기 운항으로 인해 발생한 지상 제3자에 대한 항공기운항자의 손해배상책임 문제 등을 규율하기 위해 제정되었다. 상법 항공운송편은 관련 국제 조약들과 항공선진국들의 국내입법을 충분히 비교 검토하여 우리 법으로 수용하였기 때문에 국제 기준에 부합한다는 장점도 있지만, 항공기운항자의 지상 제3자에 대한 손해배상책임 규정을 중심으로 다음과 같이 개선해야 할 내용들도 포함하고 있다. 첫째, 상법 항공운송편상 항공기운항자의 지상 제3자 손해에 대한 배상책임 한도액은 피해자에 대한 적절한 배상을 하기에는 너무 낮은 수준으로 규정되어 있어 상향될 필요성이 있다. 따라서 독일과 같이 2009년 체결된 일반위험협약 및 불법방해배상협약의 관련 내용을 수용하여 항공기의 중량에 따른 분류기준을 10단계로 세분화하고 총 책임한도액을 최대 7억 SDR까지 상향시키면서, 인적 손해에 대한 배상책임한도액은 기존의 법무부 검토안처럼 최근의 물가상승률을 반영하여 현 규정의 5배 수준인 1인당 62만5천SDR까지 상향 조정하는 방안을 생각해 볼 수 있다. 이 방안이 한 사고당 항공사에게 일반적으로 보험으로서 보장되는 단일배상책임한도액이나 다양화 된 항공기 제원을 반영하면서도 지상 제3자에게 현실에 맞는 적절한 손해배상을 할 수 있다는 점에서 가장 바람직하다고 본다. 둘째, 항공기운항자는 현 상법 항공운송편상 항공기 납치 공격이나 9 11 테러와 같은 항공기를 이용한 공격행위 등과 같은 항공기테러에 의한 지상 제3자의 손해에 대하여도 무과실책임을 부담한다. 이에 관하여는 항공기운항자에게 지나치게 가혹하고 불합리한 입법이라는 견해가 있지만, 항공기운항자에게도 일정 부분 테러를 방지할 법적 의무가 있고 피해를 입은 제3자 구제 측면에서 그것이 항공기운항자에게 지나치게 가혹하거나 불합리하다고 생각되지는 않는다. 그러나 9 11테러와 같이 조직화 된 테러단체에 의해 항공기가 테러에 이용되어 지상 제3자 피해가 발생한 경우에도 항공기운항자가 피해자들에게 무과실책임을 지도록 하는 것은 불합리하며, 이러한 경우에는 항공기운항자의 책임이 면제되는 방향으로 상법 항공운송편 규정은 개정되어야 할 것이다. 셋째, 항공기사고와 같은 항공기 운항으로 인한 피해의 엄청난 규모를 고려해 볼 때, 다수의 피해자들이 경제적 어려움에 직면할 수 있으므로 항공여객의 인적 손해에 대한 항공운송인의 배상책임 발생 시 적용되는 선급금 지급 규정을 항공기운항자의 책임 발생 사례에도 준용할 필요가 있다고 본다. 넷째, 현행 상법 항공운송편상 항공기운항자의 손해배상책임 규정은 항공기 운항으로 인한 피해가 지상 또는 수면 및 수중에서 발생된 경우에만 적용되고 공중에서 발생한 피해에는 적용되지 않는다. 하지만 다른 항공기의 운항으로 인한 공중에서 발생된 항공기 등의 손해가 지상이나 수면 및 수중에서 발생한 손해와 차이가 있다고 볼 수 없다. 그러므로 상법 항공운송편상 '지상 제3자'라는 용어에서 '지상'이란 용어를 삭제하여 다른 항공기 운항으로 인한 공중에서의 항공기 등의 손해에도 상법 항공운송편상 항공기운항자의 지상 제3자 손해 배상책임 관련 규정이 적용될 수 있게 하는 것이 바람직하다고 본다. 위에서 제시된 상법 항공운송편상 항공기운항자의 지상 제3자 손해에 대한 배상책임 관련 규정의 개선방안 검토와 동 규정의 보완을 위한 지속적인 관심과 노력을 통하여, 상법 항공운송편이 피해를 입은 지상 등의 제3자에게 현실에 맞는 적절한 배상을 할 수 있게 하면서도 항공기운항자에게 과도한 부담을 지우지 않는 상호 간의 이익 균형상 더욱 바람직한 방향으로 발전되기를 희망한다.

• 항공우주산업기술동향
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• 제9권1호
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• pp.15-26
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• 2011

금융위기에 따른 경기침체로 위축되었던 항공운항시장은 빠르게 회복되고 있으며, 국제유가 급등에 따른 영향으로 구형항공기의 퇴역 및 신형항공기로의 교체가 활발히 이루어지고 있다. 2010년의 항공기 순 주문대수는 2009년과 비교하여 감소하였으나 수주잔량은 역대 최고수준을 기록하고 있어, 민간항공기 시장의 호황은 앞으로도 한동안 이어질 것으로 예상되고 있다. 이러한 시장 성장은 100~200인승 급의 단일 통로기가 선도하고 있으며, Airbus, Boeing의 기존 제작업체의 신규 항공기 개발과 Bombardier 및 중국, 러시아 등의 신규 업체에서도 시장에 새로이 진입하기 위해 노력하고 있다. 이러한 신형기체 수요의 증가와 기존 기체의 퇴역은 기존 기체에 대한 MRO 및 임대 시장을 위축을 가져오고 있으며, 국제 유가 불안과 경쟁심화에 따른 고효율 신형항공기에 대한 선호는 더욱 강조되고 있는 상황이다. 향후 20여 년간의 시장 전망을 살펴보면, 신흥시장의 성장과 기존 시장의 회복에 따라 견고한 성장세를 이어갈 것으로 예상된다.

• Nuclear Engineering and Technology
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• 제52권2호
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• pp.381-396
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• 2020

Investigations of the commercial aircraft impact effect on nuclear island infrastructures have been drawing extensive attention, and this paper aims to perform the safety assessment of Generation III nuclear power plant (NPP) buildings subjected to typical commercial aircrafts crash. At present Part I, finite element (FE) models establishment and validations for both the aircrafts and NPP buildings are performed. (i) Airbus A320 and A380 aircrafts are selected as the representative medium and large commercial aircrafts, and the corresponding fine FE models including the skin, beam, fuel and etc. are established. By comparing the numerically derived impact force time-histories with the existing published literatures, the rationality of aircrafts models is verified. (ii) Fine FE model of the Chinese Zhejiang Sanao NPP buildings is established, including the detailed structures and reinforcing arrangement of both the containment and auxiliary buildings. (iii) By numerically reproducing the existing 1/7.5 scaled aircraft model impact tests on steel plate reinforced concrete (SC) panels and assessing the impact process and velocity time-history of aircraft model, as well as the damage and the maximum deflection of SC panels, the applicability of the existing three concrete constitutive models (i.e., K&C, Winfrith and CSC) are evaluated and the superiority of Winfrith model for SC panels under deformable missile impact is verified. The present work can provide beneficial reference for the integral aircraft crash analyses and structural damage assessment in the following two parts of this paper.

• Nuclear Engineering and Technology
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• 제52권2호
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• pp.397-416
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• 2020

Investigations of the commercial aircraft impact effect on nuclear island infrastructures have been drawing extensive attention, and this paper aims to perform the safety assessment of Generation III nuclear power plant (NPP) buildings subjected to typical commercial aircrafts crash. At present Part II, based on the verified finite element (FE) models of aircrafts Airbus A320 and A380, as well as the NPP containment and auxiliary buildings in Part I of this paper, the whole collision process is reproduced numerically by adopting the coupled missile-target interaction approach with the finite element code LS-DYNA. The impact induced damage of NPP plant under four impact locations of containment (cylinder, air intake, conical roof and PCS water tank) and two impact locations of auxiliary buildings (exterior wall and roof of spent fuel pool room) are evaluated. Furthermore, by considering the inner structures in the containment and raft foundation of NPP, the structural vibration analyses are conducted under two impact locations (middle height of cylinder, main control room in the auxiliary buildings). It indicates that, within the discussed scenarios, NPP structures can withstand the impact of both two aircrafts, while the functionality of internal equipment on higher floors will be affected to some extent under impact induced vibrations, and A380 aircraft will cause more serious structural damage and vibrations than A320 aircraft. The present work can provide helpful references to assess the safety of the structures and inner equipment of NPP plant under commercial aircraft impact.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2007년도 추계학술대회논문집
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• pp.425-429
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• 2007

The noise problem has been a public interest for several years in Korea. Especially, the noises which were emitted from aircrafts on the airport and in the air have injurious effects on people over a vast range. Hence, there need vast data on the aircraft noise to evaluate the effect of various parameters. In present study, the works which consist of social surveys and noise measurements were conducted at points near the airport and the airbase. Total of 1,784 participants give effective responses in forty-five areas nearby the measurement points. Questionnaires asked the responses concerned with attitude, noise sensitivity, directive effects, secondary effects, annoyance and attempts to lower noise level exposed. From the field survey, the doseresponse relationship of community response to aircraft noise was established and there are different characteristics between civil and military aircraft. Though the study is still continuing on a few interest, one among some results is that %HA (%highly annoyed) of civil aircraft is higher than military's under the 70 WECPNL.

• Nuclear Engineering and Technology
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• 제54권1호
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• pp.326-342
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• 2022

Comparative analyses of a shield building subjected to a large commercial aircraft impact between decoupling method and coupling method are performed in this paper. The decoupling method is applying impact force time-history curves on impact area of the shield building to study impact damage effects on structure. The coupling method is using a model including aircraft and shield building to perform simulation of the entire impact process. Impact force time-history curves of the fuselage, wing and engine and their total impact force time-history curve are obtained by the entire aircraft normally impacting the rigid wall. Taking aircraft structure and impact progress into account some loading areas are determined to perform some comparative analyses between decoupling method and coupling method, the calculation results including displacement, plastic strain of concrete and stress of steel plate in impact area are given. If the loading area is determined unreasonably, it will be difficult to assess impact damage of impact area even though the accurate impact force of each part of aircraft obtained already. The coupling method presented at last in this paper can more reasonably evaluate the dynamic response of the shield building than the decoupling methods used in the current nuclear engineering design.