연소장에서 보조공기주입에 따른 가스터빈 모델의 연소특성

• 영문명: A Study on the Combustion Characteristics of Gas Turbine Model with Changing Auxilliary Air Injection in Combust ion Field
• 발행기관: 한국산업기술융합학회(구. 산업기술교육훈련학회)
• 저자명: 임경달(Kyung-Dal Lim)
• 간행물 정보: 『산업기술연구논문지』산업기술교육훈련논문지 제16권 4호, 83~90쪽, 전체 8쪽
• 주제분류: 공학 > 공학일반
• 파일형태: PDF
• 발행일자: 2011.12.30

영문 초록

Due to recent air pollution and energy consumption limitations, improving energy efficiency and low pollution combustion have been proposed as a practical plan to solve environmental problems. The phenomena in gas turbine combustor which stands for practical combustors and heavy-duty uninterrupted flow combustor are extremely complex, and its variables to affect combustion conditions and performance are also so much. Especially auxiliary air that enters through the auxiliary air holes affects the combustion in the primary combustion zone, and it is an important variable influencing the performance of combustor, too. In this study, researchers measured the average temperature, the combustion gas concentration, NOx concentration and so on about the experimental conditions which are formed by changes in the auxiliary air flow. Through the measurement, impacts of the combustion characteristics that were caused by changes of the auxiliary air injection were examined.

목차

Ⅰ. 서 론

Ⅱ. 시험방법 및 조건

Ⅲ. 실험결과 및 고찰

Ⅳ. 결 론

키워드

Primary Air(주류방향공기) Auxiliary Air Injection(보조공기 주입) Combustion Field(연소장) Model Gas Turbine Combustor(모형 가스터빈 연소기) Excess Air Ratio(공기과잉율) Emission Characteristics(배출특성)