Earticle

초록

영어

A four-seat tandem-wing electric vertical take-off and landing aircraft was conceptually designed, and a nominal quarter-scale prototype was fabricated and tested in hovering flight. The design payload and target mission range were 340 kg and approximately 100 km, respectively. Eight lift rotors and one pusher propeller were arranged in a lift-and-cruise configuration. At a representative full-scale mass of 1,720 kg, a hover-to-maximum-thrust ratio of 0.65 required a total maximum static thrust of 25.96 kN. A preliminary maneuver envelope gave a positive stall speed of 117.5 km/h and a maneuvering speed of 229.1 km/h under the adopted assumptions. The subscale component mass budget was 18.125 kg. A separate 15.945 kg component configuration gave a longitudinal center of gravity of 979 mm aft of the nose; the two configurations were distinguished in the mass-property assessment. The fabricated prototype completed hovering flight in a GPS-assisted position-hold mode, and stable hovering was observed. The test confirmed initial hovering capability of the integrated prototype. Full-scale performance and quantitative flight-control accuracy were outside the evaluation presented here.

목차

Abstract
1. 서론
2. 4인승 항공기의 개념설계
2.1 임무 및 요구조건
2.2 형상 선정 및 모델링
2.3 공력 모델 구성
3. 중량 및 기초 성능 산정
3.1 중량 및 무게중심 산정 방법
3.2 리프트 로터 및 호버 동력
3.3 고정익 비행 모드의 V–n 선도
4. 축소기 설계 및 제작
4.1 축소비와 구성품 적용
4.2 부품 구성 및 중량 정리
4.3 부품 기반 무게중심 계산
4.4 제작 및 조립
5. 축소기 호버링 시험
5.1 시험 기체 및 비행모드
5.2 호버링 시험 결과
6. 결론
References

키워드

저자

• 김우진 [ Woojin Kim | Member, Hanseo University of Aviation Maintenance ]
• 김태욱 [ Taewook Kim | Professor, Dept. of Aircraft Mechanical Engineering, Inha Technical College, Incheon, Republic of Korea. ] Corresponding Author

참고문헌

발행기관

간행물

표지보기 관심저널 등록

• 간행물명

  한국기계항공기술학회지(구 한국기계기술학회지) [Journal of the Korean Society of Mechanical and Aviation Technology ]

• 간기

  격월간

• pISSN

  1229-604X

• eISSN

  2508-3805

• 수록기간

  1999~2026

• 등재여부

  KCI 등재

• 십진분류

  KDC 550 DDC 620