海军航空工程学院学报
海軍航空工程學院學報
해군항공공정학원학보
JOURNAL OF NAVAL AERONAUTICAL ENGINEERING INSTITUTE
2013年
5期
527-532
,共6页
李钊%贺孝涛%哈欣宇%王远强
李釗%賀孝濤%哈訢宇%王遠彊
리쇠%하효도%합흔우%왕원강
离心压气机%积垢%性能参数%流场特性
離心壓氣機%積垢%性能參數%流場特性
리심압기궤%적구%성능삼수%류장특성
centrifugal compressor%incrustation%performance parameters%flow field characteristics
以某型离心压气机为研究对象,利用流场仿真软件对不同污染程度的压气机性能进行数值计算,对比流场特性的变化,分析了积垢造成压气机性能损失的程度。结果表明:积垢对离心压气机性能的主要影响是降低压气机效率,原因是积垢改变了叶片表面粗糙度,增加了摩擦损失;扩大了叶片后缘和出口附近的低速回流区的范围,增强了回流强度,加大了流动损失。
以某型離心壓氣機為研究對象,利用流場倣真軟件對不同汙染程度的壓氣機性能進行數值計算,對比流場特性的變化,分析瞭積垢造成壓氣機性能損失的程度。結果錶明:積垢對離心壓氣機性能的主要影響是降低壓氣機效率,原因是積垢改變瞭葉片錶麵粗糙度,增加瞭摩抆損失;擴大瞭葉片後緣和齣口附近的低速迴流區的範圍,增彊瞭迴流彊度,加大瞭流動損失。
이모형리심압기궤위연구대상,이용류장방진연건대불동오염정도적압기궤성능진행수치계산,대비류장특성적변화,분석료적구조성압기궤성능손실적정도。결과표명:적구대리심압기궤성능적주요영향시강저압기궤효솔,원인시적구개변료협편표면조조도,증가료마찰손실;확대료협편후연화출구부근적저속회류구적범위,증강료회류강도,가대료류동손실。
The performance of centrifugal compressor before and after being polluted is numerically calculated by floating field simulation software. The mechanism of compressor performance deterioration caused by incrustation was analyzed by comparing the chance of compressor flow field. The result was that the main effects of incrusta-tion on centrifugal compressor was to reduce compressor efficiency, because incrustation changed the blade sur-face roughness, increased friction loss, expanded the low speed range near the trailing edge and outlet, en-hanced the backflow, and increased the flow loss.