가스터빈 엔진의 대기온도 변화에 따른 연소시간에 관한 연구

• 영문명: Analysis of Combustion Time Based on Atmospheric Temperature Variations of a Gas Turbine Engine
• 발행기관: 한국산업기술융합학회(구. 산업기술교육훈련학회)
• 저자명: 김영호(Young-Ho Kim)
• 간행물 정보: 『산업기술연구논문지』산업기술연구논문지 제25권 3호, 99~105쪽, 전체 7쪽
• 주제분류: 공학 > 공학일반
• 파일형태: PDF
• 발행일자: 2020.09.30

영문 초록

In this study, the combustion instability of a gas turbine engine and the associated combustion delay time were analyzed on the basis of atmospheric temperature variations. A power generating device for combat equipment, which is currently being used in the military, was employed as the gas turbine engine. One of the primary functions of combat equipment is to fully demonstrate maneuverability, and the role and importance of power generating devices for ensuring such maneuverability has always been emphasized on. Additionally, to secure the reliability of the power generation device’s starting performance, it is necessary to stabilize various parameters such as the initial starting stability of the engine, the operation rate, and the output power. Owing to the combustion instability caused by seasonal temperature variations, the gas turbine engine employed in this study is one of the important problematic factors affecting engine performance, durability, and operation. Consequently, in several cases, normal operation and usage of the engine were restricted owing to repeated cases. Hence, in this study, the maneuverability and reliability of the equipment were improved by analyzing the changes in combustion time based on atmospheric temperature variations. Furthermore, the operational environment of the equipment is also summarized in this study.

목차

Ⅰ. 서 론

Ⅱ. 실 험

Ⅲ. 실험결과 및 고찰

Ⅳ. 결 론

참고문헌

키워드

가스터빈엔진 연소 온도 조절기 불완전연소 연소시간 Gas Turbine Engine Combustion Atmospheric Temperature Incomplete Combustion Combustion Time