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      항공기 엔진 감항기준에 대한 비교분석 = Comparative Study on Airworthiness Standards for Aircraft Engines

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      https://www.riss.kr/link?id=A101834989

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      다국어 초록 (Multilingual Abstract)

      An aircraft engine is considered as the most important element among aircraft systems. Thus type certificate is required for an aircraft engine to ensure its safety under appropriate airworthiness standard. U.S. FAR Part 33 or European CS-E is widely adopted as an airworthiness standard for aircraft engines, and other representative countries of the world established own airworthiness standards under their regulations. In this paper, we compared differences of the requirements between FAR Part 33 and CS-E, and proposed the rulemaking items to harmonize Korean Airworthiness Standard for Aircraft Engines with worldwide standards and to contribute to growth of aviation industry.
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      An aircraft engine is considered as the most important element among aircraft systems. Thus type certificate is required for an aircraft engine to ensure its safety under appropriate airworthiness standard. U.S. FAR Part 33 or European CS-E is widely ...

      An aircraft engine is considered as the most important element among aircraft systems. Thus type certificate is required for an aircraft engine to ensure its safety under appropriate airworthiness standard. U.S. FAR Part 33 or European CS-E is widely adopted as an airworthiness standard for aircraft engines, and other representative countries of the world established own airworthiness standards under their regulations. In this paper, we compared differences of the requirements between FAR Part 33 and CS-E, and proposed the rulemaking items to harmonize Korean Airworthiness Standard for Aircraft Engines with worldwide standards and to contribute to growth of aviation industry.

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      참고문헌 (Reference)

      1 이강이, "항공기 엔진제어시스템 인증기술 개발" 한국항공우주학회 33 (33): 104-109, 2005

      2 홍덕곤, "국내 항공인증과 미국 인증체계의 비교" 한국항공우주학회 36 (36): 298-305, 2008

      3 FAA, "Technical Implementation Procedures for Airworthiness and Environmental Certification"

      4 Yongwun Jung, "Study on the Qualification Criteria for Aircraft Turbine Engine" 2367-2373, 2012

      5 Kang-Yi Lee, "Safety Analysis for Turbine Case Cooling System of Turbofan Engine" Pusan National University 2012

      6 Baisong Chen, "Reliability Analysis Method of an Aircraft Engine FADEC System" 289-292, 2009

      7 Federal Aviation Administration, "Order 8110. 4C : Type Certification" 5 : 2011

      8 Ministry of Land, Infrastructure and Transport, "KAS Part 33 : Airworthiness Standard for Aircraft Engines" 2013

      9 Yongmin Jun, "Introduction to the Software Planning Phase for an Aero Engine according to RTCA DO-178C" 248-251, 2013

      10 Federal Aviation Administration, "FAR Part 33 : Airworthiness Standard; Aircraft Engines" 33-33, 2012

      1 이강이, "항공기 엔진제어시스템 인증기술 개발" 한국항공우주학회 33 (33): 104-109, 2005

      2 홍덕곤, "국내 항공인증과 미국 인증체계의 비교" 한국항공우주학회 36 (36): 298-305, 2008

      3 FAA, "Technical Implementation Procedures for Airworthiness and Environmental Certification"

      4 Yongwun Jung, "Study on the Qualification Criteria for Aircraft Turbine Engine" 2367-2373, 2012

      5 Kang-Yi Lee, "Safety Analysis for Turbine Case Cooling System of Turbofan Engine" Pusan National University 2012

      6 Baisong Chen, "Reliability Analysis Method of an Aircraft Engine FADEC System" 289-292, 2009

      7 Federal Aviation Administration, "Order 8110. 4C : Type Certification" 5 : 2011

      8 Ministry of Land, Infrastructure and Transport, "KAS Part 33 : Airworthiness Standard for Aircraft Engines" 2013

      9 Yongmin Jun, "Introduction to the Software Planning Phase for an Aero Engine according to RTCA DO-178C" 248-251, 2013

      10 Federal Aviation Administration, "FAR Part 33 : Airworthiness Standard; Aircraft Engines" 33-33, 2012

      11 European Aviation Safety Agency, "Certification Specification for Engines" 2010

      12 Cosimo J, "Certification Issues for Electrical and/or Electronic Engine Controls" 15-24, 1987

      13 Federal Aviation Administration, "AC 33-2C : General Type Certification Guideline for Turbine Engines" 2013

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      학술지 이력

      학술지 이력
      연월일 이력구분 이력상세 등재구분
      2026 평가예정 재인증평가 신청대상 (재인증)
      2020-01-01 평가 등재학술지 유지 (재인증) KCI등재
      2017-01-01 평가 등재학술지 선정 (계속평가) KCI등재
      2015-01-01 평가 등재후보학술지 선정 (신규평가) KCI등재후보
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      학술지 인용정보

      학술지 인용정보
      기준연도 WOS-KCI 통합IF(2년) KCIF(2년) KCIF(3년)
      2016 0.29 0.29 0.29
      KCIF(4년) KCIF(5년) 중심성지수(3년) 즉시성지수
      0.28 0.26 0.323 0.31
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