KOREASCHOLAR

프로펠러의 피치각도와 엔진 RPM 변화에 따른 항공기소음 및 추력 평가 Aircraft noise and thrust evaluation according to propeller pitch angle and engine RPM change

김재필, 류종현, 김병삼
  • 언어KOR
  • URLhttp://db.koreascholar.com/Article/Detail/420267
한국기계기술학회지 (韓國機械技術學會誌)
제24권 제6호 (2022.12)
pp.1144-1151
한국기계기술학회 (Korean Society of Mechanical Technology)
초록

Most domestic pilots are trained at local airfields using propeller aircraft. Training aircraft are mainly trained in the airspace around the aerodrome, and mainly take-off and landing exercises that require a lot of practice among flight control skills. Aircraft noise is a sound that humans do not want. In this study, based on the Rotax 914 engine used in Korea, the propeller blade angle was changed by 1 degree for the 3-leaf “K company” propeller and the 3-leaf GSC wooden propeller, and the engine RPM was changed to examine the noise and thrust changes. The purpose of this study is to check whether noise and thrust loss are the least at the engine's maximum RPM, and to propose an aircraft operation plan in the noisy aerodrome area based on the values.

저자
  • 김재필(경운대학교) | Jae-Pil Kim
  • 류종현(경운대학교) | Jong-Hyeon Ryu Corresponding author
  • 김병삼 (원광대학교) | Byoung-Sam Kim