지원사업
학술연구/단체지원/교육 등 연구자 활동을 지속하도록 DBpia가 지원하고 있어요.
커뮤니티
연구자들이 자신의 연구와 전문성을 널리 알리고, 새로운 협력의 기회를 만들 수 있는 네트워킹 공간이에요.
논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 발행연도
- 2013.1
- 수록면
- 771 - 778 (8page)
이용수
초록· 키워드
오류제보하기
Transmission is a core component of helicopter to transmit power from engine to rotor and must have a endurance to be able to show satisfactorily its performance required during its life time. When developing a new helicopter, both military and civil airworthiness authorities require a tie-down test to verify its endurance. Procedure for transmission endurance test is described in FAR part 29 or US military specification but its details are more or less ambiguous. In this paper, we have proposed a proper procedure for transmission endurance test by giving KUH transmission endurance test example including determination of applicable torque, load and test profile.
목차
등록된 정보가 없습니다.
참고문헌 (5)
참고문헌 신청
2007 / Airworthiness Standards : Transport Category Rotorcraft Amdt 47 / Federal Aviation Administration
2006 / Advisory Circular 29-2C Certification of Transport Category Rotorcraft Federal Aviation Administration
1996 / ADS-50—PRF, Rotorcraft Propulsion Performance and Qualification Requirements and Guidelines / US Army Aviation and Troop Command
1954 / MIL-T-8679, Test Requirements, Ground, Helicopter / US Department of Defense
1975 / Ground Test Vehicle 1200-Hour Military Qualification Test Report
2006 / Advisory Circular 29-2C Certification of Transport Category Rotorcraft Federal Aviation Administration
1996 / ADS-50—PRF, Rotorcraft Propulsion Performance and Qualification Requirements and Guidelines / US Army Aviation and Troop Command
1954 / MIL-T-8679, Test Requirements, Ground, Helicopter / US Department of Defense
1975 / Ground Test Vehicle 1200-Hour Military Qualification Test Report
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