本文以某F级重型燃气轮机压气机亚音级静叶为研究对象，对于静叶端区产生的闭式角区分离流动，采用了端弯叶片控制技术，并在此基础上开发出“端弯联合弯叶片”技术。通过对比分析角区分离起始点和吸力面回流区范围，探讨了端弯叶片和“端弯联合弯叶片”对角区分离的影响规律。
In this paper, the subsonic stator of an F-class heavy duty gas turbine compressor has been studied. The endbend blade has been used to control the stator corner separation flow. Afterwards an ＂endbend-bow＂ blade was designed. By way of comparison and analysis of the changing pattern of the corner separation start point and the reflect flow boundary on the suction surface, the controlling pat- tern of the endbend blade and endbend-bowed blade on the corner separation flow have been discussed.
参考文献
| [1] | 王会社,钟兢军,王仲奇,刘艳明,袁新.叶片正弯对扩压叶栅气动性能的影响[J].推进技术,2002(04):321-324. |
| [2] | 吴国华.压气机“端弯”叶栅流场结构的试验研究[J].航空动力学报,1990(03):257. |
| [3] | 蔡运金.应用端弯叶片增加压气机喘振裕度[J].航空动力学报,1988(03):215. |
| [4] | 柯婷凤,郑群,明玉周.某三级轴流式低速压气机零级气动优化设计[J].机械工程学报,2011(06):160-167. |
| [5] | 杜鑫,王松涛,王仲奇.弯叶片对大展弦比扩压叶栅角区分离控制机理研究（一）--弯叶片对角区分离起始和发展的影响[J].汽轮机技术,2010(03):195-198,201. |
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