Earticle

초록

영어

Large bore LNG dual fuel (DF) engines are increasingly adopted in marine propulsion systems due to their high thermal efficiency and reduced regulated emissions. However, as the cylinder bore increases, combustion stability and knock propensity become more sensitive, while the isolated geometric effects of bore scaling governing these trends remain insufficiently clarified. In particular, the pure effect of bore scaling on wall heat loss, in-cylinder thermal conditions, and knock-related combustion characteristics has not been systematically investigated under identical operating conditions. In this study, a CFD based geometric scaling framework was developed and applied to investigate the influence of cylinder bore variation on combustion behavior and knock sensitivity in a four stroke LNG DF diesel engine. A reference engine geometry with a 350 mm bore was defined, and the bore diameter was systematically varied while maintaining identical stroke, compression ratio, combustion chamber geometry, valve timing, fuel properties, and injection conditions to isolate pure geometric effects. A sector based three dimensional in cylinder CFD model with dynamic mesh treatment was employed. The results indicate that increasing the bore diameter reduces the wall-area-to-volume ratio, leading to a reduction in relative wall heat loss and enhanced thermal energy retention in the core region. Consequently, the in cylinder core gas temperature increases near the end of compression and during the early combustion phase, which promotes higher heat release rates, advanced combustion phasing, and increased maximum pressure rise rates. As a result, the knock margin decreases and knock sensitivity increases under identical operating conditions. Rather than providing absolute quantitative predictions, this study presents a physically consistent, trend oriented framework to interpret bore-scaling effects on combustion stability and knock sensitivity in large bore LNG DF engines. The proposed framework provides a fundamental guideline for subsequent high-fidelity CFD simulations and experimental investigations aimed at knock mitigation and combustion control.

목차

Abstract
1. 서론
2. 선행연구 고찰
2.1 LNG DF 엔진의 연소 및 배출 특성
2.2 파일럿 연료 분사 및 노킹 제어
2.3 LNG DF 엔진의 보어 및 기하학적 영향
2.4 선행연구의 한계 및 본 연구의 차별성
3. 연구 방법
3.1 연구 목적 및 해석
3.2 대상 엔진 및 기준 조건
3.3 계산 도메인 및 기하학적 모델링
3.4 격자 생성 및 동적 격자 처리
3.5 난류 및 연소 모델 설정
3.6 연료 모델링 및 화학반응 메커니즘
3.7 경계조건 및 초기조건 설정
3.8 모델 검증 전략 및 신뢰성 확보
3.9 분석 변수 정의
3.10 해석 범위 및 연구의 한계
4. 연소 및 노킹 특성 경향 분석
4.1 보어 변화에 따른 체적 대비 벽면 면적비 변화
4.2 보어 변화에 따른 연소실 온도 분포 특성
4.3 보어 변화에 따른 반응속도 및 열발생률 형성 메커니즘
4.4 보어 변화에 따른 최대 압력 상승률 특성
4.5 노킹 민감도 및 knock margin 변화
5. 결론
References

키워드

저자

• 김선태 [ Suntae Kim | Professor, Korea Institute of Maritime and Fisheries Technology ]
• 송명호 [ Myeongho Song | Member, Professor, Mokpo National Maritime University ] 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