• 제목/요약/키워드: aircraft noise

검색결과 352건 처리시간 0.023초

항공기 소음자동측정망 자료를 이용한 소음평가단위와 WECPNL과의 상관관계 비교 연구 (A correlation comparative method with noise assessment unit and WECPNL that use aircraft noise automatic measuring system)

  • 전형준;장서일;이기정
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2006년도 춘계학술대회논문집
    • /
    • pp.296-299
    • /
    • 2006
  • This study is about correlation between WECPNL and other units such as NNI, Leq and Ldn for aircraft noise that ere measured by automatic measuring system networks for grasping the effect of aircraft noise and investigated the aircraft noise level from 2004 to 2005 nearby 10 airports in Korea. It is very important to find the relationship among the various noise units, because exchange between the results of many other nation's study can improve the assessment and mitigation study of the aircraft noise. Correlation between WECPNL and M is better than one between WECPNL and Leq and between WECPNL and Ldn, because WECPNL and NNI are based on the PNL.

  • PDF

항공기 소음의 평가 척도에 대한 비교 연구 (A compare study on the Evaluation Method of Aircraft Noise)

  • 전지현;안병옥;송민정;장길수;김선우
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2001년도 추계학술대회논문집 II
    • /
    • pp.703-706
    • /
    • 2001
  • Currently domestic criteria for the aircraft noise is being adapted WECPNL(weighted equivalent continuous perceived noise level), while internationally preferred method is which is originated from $L_{eq}$ and can evaluate even environmental noise. WECPNL used in domestic as a evaluation method is only for the aircraft noise. It is, therefore, not adequate for the evaluation of residents' injury, moreover, it is very difficult to measure the aircraft noise with WECPNL due to the complicated calculating procedures as long as automatic measuring system is not used. Accordingly, this study aims to propose alternative evaluation method for the aircraft noise. To achieve this purpose, the data measured by automatic measuring system were gathered and calculated with three evaluation methods: WECPNL, $L_{eq}$ and $L_{dn}$ and the results calculated from different methods were compared and analyzed.

  • PDF

택지개발예정지구 항공기 소음 실태조사 연구 (Actual Condition of the Aircraft Noise in the Building Site Development Arranged District)

  • 김흥식;박영민;주시웅
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2004년도 추계학술대회논문집
    • /
    • pp.1040-1043
    • /
    • 2004
  • The purpose of this study is to present a fundamental data for evaluating aircraft noise of building site development. By the field experiments and an predicted equal noise level contour using the INM program, actual condition in the building site development arranged district was investigated. In order to get the results, Analysis of factors effected on noise level, sound level on the rate of increase to aircraft demand and difference on the aircraft noise levels according to floor level in apartment house was carried out.

  • PDF

터보프롭 항공기(C90GT)의 소음 분석 (Noise Analysis of Turbo Prop Aircraft(C90GT))

  • 류종현;김우진;김규범
    • 융합정보논문지
    • /
    • 제9권9호
    • /
    • pp.141-146
    • /
    • 2019
  • 여러 종류의 항공기가 운용되고 있는 훈련 비행장에서 항공기의 소음을 실제 측정하여 분석하는 것은 어렵다. 이러한 실제적인 한계를 극복하고 적절한 소음 대책을 수립하기 위해서 FAA에서 사용하는 INM 7.0(Integrated Noise Model Version 7.0)을 사용하여 소음 지도를 작성하였다. 터보프롭 항공기 (C90GT)가 이륙 경로, 착륙 경로 및 장주경로를 비행하면서 발생하는 소음을 측정하였고 법적으로 소음의 피해가 되는 70 WECPNL 이상인 지역을 조사하였다. 터보프롭 항공기가 운용되고 있는 모든 경로에서 70 WECPNL을 초과하는 지역은 발견되지 않았다.

군용 비행장 내 실내소음 기준 설정에 관한 연구 (Study on Establishing the Indoor Noise Standard in Military Airport)

  • 고준희;최남수;백철;조만희
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2014년도 추계학술대회 논문집
    • /
    • pp.701-703
    • /
    • 2014
  • The intense noise generated by military aircraft hans a significant impact on ground crews and their families on airbase. For minimizing the impact of the aircraft noise on the airport, appropriate indoor noise standard is required. This paper studied to establish the indoor noise standard on the military airport. The aircraft noise was measured and analyzed the frequence characteristics. the remodeling of office for the noise mitigation was enforced to verify the appropriate internal noise standard and to select the method of reinforcement. The noise standard was classified three categories according to the dwelling, office and usage of building with flight train facilities and banishment in military airfield.

  • PDF

제주국제공항에서의 항공기 소음 예측에 관한 고찰 (A Study on the Prediction of Aircraft Noise Level at Jeju International Airport)

  • 이준호;이기호
    • 한국환경과학회지
    • /
    • 제23권3호
    • /
    • pp.387-397
    • /
    • 2014
  • This study is carried out to propose an empirical equation which can promptly predict the aircraft noise level at a specific point (a receptor) near Jeju international airport by using the information of the flight path data. For this purpose, Analyses of multiple linear regression with the slant distances (SD) calculated from the gate analyses of the flight path data, aircraft noise certification levels with unit of EPNL(effective perceived noise level) and noise levels measured at receptors are performed by SPSS package. From these regression analyses for approach and departure of aircraft, we can propose empirical equations which is statistically significant. The noise levels predicted by these empirical equations are highly correlated the measured data.

군용항공기의 운항 경로에 따른 WECPNL 변화에 관한 연구 (Study on the WECPNL Variation due to the Change of Military Aircraft Flight Path)

  • 이진영;이찬;길현권;황성국
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2007년도 추계학술대회논문집
    • /
    • pp.793-795
    • /
    • 2007
  • The present study investigates the effect of the flight path of military aircraft on noise map and its WECPNL distribution. Aircraft noise modeling and simulation are made on a Korean military airport by INM(Integrated Noise Model) 6.2 version, and the flight path of military aircraft is modeled by combining takeoff, overfly, approach and touch-and-go modes. The present INM simulations are conducted for two cases with different overfly modes and show that the change of overfly mode remarkably affects the noise influence region and the WECPNL distribution around the aircraft.

  • PDF

항공기 소음 측정 시 이동측정지점에 대한 소음도 예측방법 (A Noise Prediction Method on the Movement Measuring Points at Measurement for Aircraft Noise)

  • 우정하;이병찬
    • 한국소음진동공학회논문집
    • /
    • 제25권12호
    • /
    • pp.901-906
    • /
    • 2015
  • It is difficult to measure aircraft noise at many points, because the noise measurement is need to long time, 24 hours and consecutive 7 days, which results in high costs. As an alternative, movement measuring points are set to measure aircraft noise for less than 24 hours, and so it is needed to overcome the limitation of shorter measuring time. Thus, this study measured military aircraft noise on movement measuring points and conducted a comparative analysis on the data according to each measuring time. The data of measuring noise for 24 hours and less than 24 hours were compared to suggest appropriate measuring time on the movement measuring points. As a result of comparing data of measuring noise, an error was within 3 dB in case of measuring time of 3 hours, and an error was within 1 dB in case of 6 hours of measurement.

항공기 소음 성가심 반응에 영향을 미치는 변수에 관한 연구 (A Study on the Effect of Variables on Aircraft Noise Annoyance Response)

  • 이기정;이건;장서일;손진희
    • 대한환경공학회지
    • /
    • 제29권3호
    • /
    • pp.341-347
    • /
    • 2007
  • 본 연구는 국내 항공기 소음에 대한 성가심 반응을 정량화하는 연구에서 성가심 반응에 영향을 주는 변수에 대해 알아보고자 하였다. 이를 위해 영향이 예상되는 변수를 설문조사 시 함께 질의하고, 그 결과를 통해 성가심 반응과의 통계적 유의성을 검증해 보았다. 본 연구에서 사용한 성가심 반응에 영향이 예상되는 독립변수는 크게 소음/비소음 변수로 나누었다. 소음 변수로서 항공기 소음원의 소음도, 비소음 변수로서 연령, 학력, 성별, 직업, 주택형태, 거주기간에 대해서 일원분산분석을 하였다. 또한 대상지역의 민원 발생 여부에 대해서 조사하였다.

항공기 외부소음 예측기법의 개발 (Development of the prediction method of aircraft exterior noise)

  • 심인보;이덕주
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2000년도 춘계학술대회논문집
    • /
    • pp.78-83
    • /
    • 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.

  • PDF