间隙高度对自发射流抑制叶尖泄漏的影响
Effect of clearance height on tip leakage reduced by spontaneous tip injection
-
摘要: 通过数值求解三维定常黏性雷诺时均N-S方程,获得了单孔叶尖自发射流条件下不同叶顶间隙的叶栅流场,对比分析了间隙高度对自发射流与叶尖泄漏流相互作用特性、叶尖泄漏流量以及叶片载荷的影响.结果表明:当叶顶间隙高度为1mm(t/H=0.5%)时,自发射流对泄漏流有明显的阻挡作用,泄漏流量比减少0.06%,同时叶片载荷增加1.39%.当叶顶间隙高度增大到4mm(t/H=2%)时,自发射流的阻挡作用及对叶片载荷的增加作用基本消失;减小间隙高度可以有效提高自发射流的控制效果,同时降低因分离造成的流动损失;自发射流的存在显著改变了间隙流场分布及叶尖吸力面附近静压系数分布,计算发现当泄漏流绕自发射流流过时,下游流场出现类似卡门涡街的涡分布现象.Abstract: The steady cascade flow field with different tip clearance height was obtained by numerically solving three-dimensional Reynolds-averaged N-S equations(RANS)and energy equations under the condition of single-hole spontaneous tip injection.The influences of clearance height on the interaction characteristics of the spontaneous injection with the tip leakage flow,the mass flow rate of leakage flow and the blade load were analyzed.The results show that the spontaneous jet has significant blocking effect on the leakage flow, the leakage ratio decreases by 0.06% with 1mm(t/H=0.5%) tip clearance,and meanwhile the blade load increases by 1.39%.The blocking effect decays with the increasing clearance height and can be ignored when the clearance height rises to 4 mm (t/H=2%);decreasing clearance height can effectively improve the controlling effect of spontaneous jet on leakage flow and reduce the flow losses caused by flow separation;the presence of spontaneous tip injection significantly changes the flow field of tip gap and the distribution of static pressure coefficient near the suction.The calculation results show that a vortex similar to the Karman vortex street appears downstream the jet flow when the leakage flow moves around the spontaneous jet.
-
Key words:
- tip leakage flow /
- spontaneous tip injection /
- clearance height /
- numerical simulation /
- control effect
-
[1] Booth T C.Importance of tip clearance flows in turbine design.VKI Lecture Series 1985-05,1985. [2] Bindon J P.The measurement and formation of tip clearance loss[J].ASME Journal of Turbomachinery,1990,111(3):257-263. [3] 李钢,徐燕骥,林彬,等.利用介质阻挡放电等离子体控制压气机叶栅端壁二次流[J].中国科学:技术科学,2009,39(11):1843-1849. LI Gang,XU Yanji,LIN Bin,et al.Stability analysis of dielectric elastomer film actuator[J].Scientia Sinica Techologica,2009,39(11):1843-1849.(in Chinese) [4] Rao N M,Camci C.Axial turbine tip desensitization by injection from a tip trench:Part Ⅰ effect of injection mass flow rate.ASME Paper GT-2004-53256,2004. [5] Harvey N W,Newman D A,Haselbach F,et al.An investigation into a novel turbine rotor winglet:Part 2 numerical simulation and experimental results.ASME Paper GT-2006-90459,2006. [6] Lee S W,Kim S U,Kim K H.Aerodynamic performance of winglets covering the tip gap inlet in a turbine cascade[J].International Journal of Heat and Fluid Flow,2012,34:36-46. [7] 胡建军,徐进良,曹海亮,等.超微型涡轮中极低展弦比静叶栅流场特性的数值研究[J].动力工程,2009,29(7):656-663. HU Jianjun,XU Jinliang,CAO Hailiang,et al.Flow field characteristics of stator cascade with extremely low aspect ratio in an ultra-micro gas turbine[J].Journal of Power Engineering,2009,29(7):656-663.(in Chinese) [8] 胡建军,徐进良,曹海亮,等.超微涡轮动叶栅叶顶间隙对流场影响的数值模拟[J].热能动力工程,2010,25(2):134-140. HU Jianjun,XU Jinliang,CAO Hailiang,et al.Numerical simulation of the influence of the blade tip clearance on the flow field of an ultra-micro turbine rotating cascade[J].Journal of Engineering for Thermal Energy and Power,2010,25(2):134-140.(in Chinese) [9] 蔡晋,陈波,闫雪,等.带小翼肋条的涡轮叶尖泄漏流场的数值模拟[J].动力工程学报,2010,30(12):919-925. CAI Jin,CHEN Bo,YAN Xue,et al.Numerical simulation on tip leakage flow of turbine blade with suction-side winglet ribs[J].Journal of Chinese Society of Power Engineering,2010,30(12):919-925.(in Chinese) [10] 李伟,乔渭阳,许开富,等.涡轮叶尖泄漏流被动控制数值模拟[J].推进技术,2008,29(5):591-597. LI Wei,QIAO Weiyang,XU Kaifu,et al.Numerical simulation of passive control on tip leakage flow in axial turbine[J].Journal of Propulsion Technology,2008,29(5):591-597.(in Chinese) [11] Auxier T A.Aerodynamic tip sealing for rotor blades: USA,5.403.158.1995-04-04. [12] Hamik M,Willinger R.An innovative passive tip-leakage control method for axial turbines:basic concept and performance potential[J].Journal of Thermal Science,2007,16(3):215-222. [13] 曹传军,黄国平,夏晨.一种减小涡轮叶尖泄漏流的方法[J].航空动力学报,2011,26(1):99-107. CAO Chuanjun,HUANG Guoping,XIA Chen.Method for reducing tip clearance leakage of turbine[J].Journal of Aerospace Power,2011,26(1):99-107.(in Chinese) [14] FLUENT Inc. FLUENT user's guide[M].Version 6.2.Lebanon,NH:Fluent Inc.,Centerra Resource Park,2005. [15] Gregory-Smith D G,Cleak J G E.Secondary flow measurements in a turbine cascade with high inlet turbulence[J].Journal of Turbomachinery,1992,114(1):173-183.
点击查看大图
计量
- 文章访问数: 1583
- HTML浏览量: 3
- PDF量: 1136
- 被引次数: 0