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소형항공기 3엽 프로펠러의 피치각도 변경에 따른 소음 비교

원문정보

Comparison of noise according to pitch angle change of small aircraft 3-blade propeller

박진석, 김재필

피인용수 : 0(자료제공 : 네이버학술정보)

초록

영어

In the past, aviation technology developed from wood to alloys to composite materials. Propellers have also evolved from wood to composite materials for modern small aircraft. In this context, research is needed on a three-blade composite propeller based on the Rotax 912 engine, which is widely used in Korea. In this study, the goal is to select the optimal propeller pitch angle by investigating noise changes according to changes in blade angle and engine 4000RPM of three types of three-blade propellers different from each propeller manufacturer. By comparing the noise of the three types of propellers most commonly used in Korea and suggesting the minimum noise blade angle for each propeller, we aim to help aircraft operators select propellers and resolve noise complaints around airfields.

목차

ABSTRACT
1. 서론
2. 본론
2.1 프로펠러 구조
2.2 항공기 제작회사의 프로펠러 선정
2.3 항공기 소음인증 및 법규
2.4 소음측정 방법
2.5 소음 및 추력 결과 분석
2.6 프로펠러 소음 및 추력 비교
3. 결론
후기
References

저자정보

  • 박진석 Jin-Suk Park . Member, Kyungwoon University of Aero Mechnical Engineering, Professor
  • 김재필 Jae-Pil Kim. Member, Kyungwoon University of Aero Mechanical Engineering, Professor

참고문헌

자료제공 : 네이버학술정보

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