首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >HEAT TRANSFER IN A VANE TRAILING EDGE PASSAGE WITH CONICAL PINS AND PIN-TURBULATOR INTEGRATED CONFIGURATIONS
【24h】

HEAT TRANSFER IN A VANE TRAILING EDGE PASSAGE WITH CONICAL PINS AND PIN-TURBULATOR INTEGRATED CONFIGURATIONS

机译:带圆锥销和针形涡轮集成配置的叶片尾缘传热中的传热

获取原文

摘要

The trailing edge sections of gas turbine vanes and blades are generally subjected to extremely high heat loads due to the combined effects of high external accelerating Mach numbers and gas temperatures. In order to maintain the metal temperatures of these trailing edges to a level, which fulfills the mechanical integrity of the parts, highly efficient cooling of the trailing edges is required without increasing the coolant consumption, as the latter has a detrimental effect on the overall gas turbine performance. In this paper the characteristics of the heat transfer and pressure drop of two novel integrated pin bank configurations were investigated. These include a pin bank with conical pins and a pin bank consisting of cylindrical pins and intersecting broken turbulators. As baseline case, a pin bank with cylindrical pins was studied as well. All investigations were done in a converging channel in order to be consistent with the real part. The heat transfer and pressure drop of all the pin banks were investigated initially with the use of numerical predictions and subsequently in a scaled experimental wind tunnel. The experimental study was conducted for a range of operational Reynolds numbers. The TLC (thermochromic liquid crystal) method was used to measure the detailed heat transfer coefficients in scaled Perspex models representing the various pin bank configurations. Pressure taps were located at several positions within the test sections. Both local and average heat transfer coefficients and pressure loss coefficients were determined. The measured and predicted results showed that the local internal heat transfer coefficient increases in the flow direction. This was due to the flow acceleration in the converging channel. Furthermore, both the broken ribs and the conical pin banks resulted in higher heat transfer coefficients compared with the baseline cylindrical pins. The conical pins produced the highest average internal heat transfer coefficients in contrast to the pins with the broken ribs, though this was also associated with a higher pressure drop.
机译:由于高外部加速马赫数和气体温度的组合效应,通常对燃气轮机叶片和叶片的后缘部分通常受到极高的热负荷。为了将这些后缘的金属温度保持在满足部件的机械完整性的水平,因此在不增加冷却剂消耗的情况下,需要高效地冷却后缘,因为后者对整体气体有不利影响涡轮机性能。本文研究了两种新型集成销库配置的传热和压降的特性。这些包括具有锥形销的销库和由圆柱形销和交叉破裂的湍流器组成的销库。作为基线案例,也研究了具有圆柱形销的销库。在融合渠道中完成所有调查,以便与实际部分保持一致。最初通过使用数值预测和随后在缩放的实验风洞中进行了所有引脚库的传热和压降。实验研究进行了一系列操作雷诺数。 TLC(Thermochromic液晶)方法用于测量表示各种引脚库配置的缩放Perspex模型中的详细传热系数。压力抽头位于试验部分内的几个位置。确定局部和平均传热系数和压力损失系数。测量和预测结果表明,局部内部传热系数在流动方向上增加。这是由于融合通道中的流量加速度。此外,与基线圆柱形销相比,断肋和锥形销库都导致较高的传热系数。锥形销产生与具有破碎肋的销相比的最高平均内部传热系数,尽管这也与较高的压降相关。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号