국립중앙도서관 "우편 복사 서비스"로 연결 됩니다.
DBpia??Currently, 60㎾ class gas turbine - fuel cell hybrid power generation system is being developed by Korea Aerospace Research Institute. Because of connection problems between gas turbine and fuel cell, the combustor is necessarily to have flame stab...
다국어 입력
あ
ぁ
か
が
さ
ざ
た
だ
な
は
ば
ぱ
ま
や
ゃ
ら
わ
ゎ
ん
い
ぃ
き
ぎ
し
じ
ち
ぢ
に
ひ
び
ぴ
み
り
う
ぅ
く
ぐ
す
ず
つ
づ
っ
ぬ
ふ
ぶ
ぷ
む
ゆ
ゅ
る
え
ぇ
け
げ
せ
ぜ
て
で
ね
へ
べ
ぺ
め
れ
お
ぉ
こ
ご
そ
ぞ
と
ど
の
ほ
ぼ
ぽ
も
よ
ょ
ろ
を
ア
ァ
カ
サ
ザ
タ
ダ
ナ
ハ
バ
パ
マ
ヤ
ャ
ラ
ワ
ヮ
ン
イ
ィ
キ
ギ
シ
ジ
チ
ヂ
ニ
ヒ
ビ
ピ
ミ
リ
ウ
ゥ
ク
グ
ス
ズ
ツ
ヅ
ッ
ヌ
フ
ブ
プ
ム
ユ
ュ
ル
エ
ェ
ケ
ゲ
セ
ゼ
テ
デ
ヘ
ベ
ペ
メ
レ
オ
ォ
コ
ゴ
ソ
ゾ
ト
ド
ノ
ホ
ボ
ポ
モ
ヨ
ョ
ロ
ヲ
―
http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.
변환된 중국어를 복사하여 사용하시면 됩니다.
예시)
- 中文 을 입력하시려면 zhongwen을 입력하시고 space를누르시면됩니다.
- 北京 을 입력하시려면 beijing을 입력하시고 space를 누르시면 됩니다.
А
Б
В
Г
Д
Е
Ё
Ж
З
И
Й
К
Л
М
Н
О
П
Р
С
Т
У
Ф
Х
Ц
Ч
Ш
Щ
Ъ
Ы
Ь
Э
Ю
Я
а
б
в
г
д
е
ё
ж
з
и
й
к
л
м
н
о
п
р
с
т
у
ф
х
ц
ч
ш
щ
ъ
ы
ь
э
ю
я
′
″
℃
Å
￠
￡
￥
¤
℉
‰
＄
％
Ｆ
￦
㎕
㎖
㎗
ℓ
㎘
㏄
㎣
㎤
㎥
㎦
㎙
㎚
㎛
㎜
㎝
㎞
㎟
㎠
㎡
㎢
㏊
㎍
㎎
㎏
㏏
㎈
㎉
㏈
㎧
㎨
㎰
㎱
㎲
㎳
㎴
㎵
㎶
㎷
㎸
㎹
㎀
㎁
㎂
㎃
㎄
㎺
㎻
㎽
㎾
㎿
㎐
㎑
㎒
㎓
㎔
Ω
㏀
㏁
㎊
㎋
㎌
㏖
㏅
㎭
㎮
㎯
㏛
㎩
㎪
㎫
㎬
㏝
㏐
㏓
㏃
㏉
㏜
㏆
RISS 인기검색어
https://www.riss.kr/link?id=A76288168
- 저자
- 발행기관
- 학술지명
- 권호사항
-
발행연도
2006
-
작성언어
Korean
- 주제어
-
KDC
550
-
자료형태
학술저널
- 발행기관 URL
-
수록면
1816-1821(6쪽)
- 제공처
-
0
상세조회 -
0
다운로드
부가정보
다국어 초록 (Multilingual Abstract)
??Currently, 60㎾ class gas turbine - fuel cell hybrid power generation system is being developed by Korea Aerospace Research Institute. Because of connection problems between gas turbine and fuel cell, the combustor is necessarily to have flame stability and wide flamability range at the starting stages. Furthermore, in order to enhance the efficiency of the whole system, high combustion efficiency and low pressure loss are required. It also should satisfy the temperature limitations of turbine blade by supplying sufficiently low and uniform thermal energy. In the present study, for the optimization of the combustor, its stability characteristics are tested with change of various operating conditions such as injector shape, swirler air mass flow rate etc.
??Currently, 60㎾ class gas turbine - fuel cell hybrid power generation system is being developed by Korea Aerospace Research Institute. Because of connection problems between gas turbine and fuel cell, the combustor is necessarily to have flame stability and wide flamability range at the starting stages. Furthermore, in order to enhance the efficiency of the whole system, high combustion efficiency and low pressure loss are required. It also should satisfy the temperature limitations of turbine blade by supplying sufficiently low and uniform thermal energy. In the present study, for the optimization of the combustor, its stability characteristics are tested with change of various operating conditions such as injector shape, swirler air mass flow rate etc.
목차 (Table of Contents)
- Abstract
- 1. 서론
- 2. 연소기 개발시험
- 3. 연소기 시스템 적용시험
- 4. 결론
- Abstract
- 1. 서론
- 2. 연소기 개발시험
- 3. 연소기 시스템 적용시험
- 4. 결론
- 후기
- 참고문헌
동일학술지(권/호) 다른 논문
-
Mechanical properties of biodegradable coconut fibre reinforced polylactic acid composite
- 대한기계학회
- Kim Yon Jig(김연직)
- 2006
-
증기발생기 2차측 Free-Span 잔류물질 영향 평가 프로그램 개발
- 대한기계학회
- 유현주(Yoo hyun joo)
- 2006
-
- 대한기계학회
- 박재학(Jai Hak Park)
- 2006
-
- 대한기계학회
- 김종호(Jong-Ho Kim)
- 2006
이 자료와 함께 이용한 RISS 자료
나만을 위한 추천자료
