首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Reduction of aerodynamic forces on turbine blading by asymmetric layout of struts based on flow interaction between rotor-strut-volute
【24h】

Reduction of aerodynamic forces on turbine blading by asymmetric layout of struts based on flow interaction between rotor-strut-volute

机译:基于转子-支柱-蜗壳之间的流动相互作用,通过支柱的不对称布置减少涡轮叶片上的空气动力

获取原文
获取原文并翻译 | 示例
           

摘要

The flows in the power turbine and nonaxisymmetric exhaust volute with struts are closely coupled and inherently unsteady for marine gas turbines, and the flow interactions between them have a significant influence on the rotor and strut blade aerodynamic force characteristics; however, the asymmetric flow interactions have not been taken into account properly in current turbine design approaches. This paper is a continuation of the previous work and aims to clarify effects of different symmetrical and asymmetric layouts of struts on the flow interactions between power turbine and exhaust volute, in an attempt to seek an optimal layout of struts with the objective of making use of the mentioned asymmetric flow interactions to reduce the rotor and strut blade aerodynamic forces. This work was carried out using coupled unsteady simulations with the full annulus computational domain including 76 rotor blades, 9 strut blades, and an exhaust volute. Results show that the level of aerodynamic force at specific frequencies on the power turbine blade surface can be reduced by applying a proper distribution of asymmetric layout of struts; using the asymmetric strut design, although the reduction of the rotor blade aerodynamic force is weak, the strut blade aerodynamic force has been reduced significantly; the asymmetric layout of struts does not improve the overall flow characteristics of turbines very much. The present results indicate that it is possible to reduce vibration and increase blade fatigue life by asymmetric strut designs.
机译:动力涡轮机和带有支柱的非轴对称排气蜗壳中的气流紧密耦合,对于船用燃气轮机来说固有地不稳定,并且它们之间的流相互作用对转子和支柱叶片的空气动力特性具有重大影响;然而,在当前的涡轮机设计方法中没有适当考虑非对称流动的相互作用。本文是先前工作的延续,旨在阐明支柱的对称和不对称布局的不同对动力涡轮和蜗壳之间的流相互作用的影响,以期寻求一种最优的支柱布局,以期利用提到的非对称流动相互作用可减少转子和支撑叶片的空气动力。这项工作是通过非稳态模拟与完整的环空计算域进行的,该环空计算域包括76个转子叶片,9个支撑叶片和一个排气蜗壳。结果表明,通过适当地分布不对称的支撑杆,可以降低动力涡轮叶片表面特定频率的空气动力水平。使用非对称支柱设计,虽然转子叶片空气动力的减小较弱,但支柱叶片空气动力已大大减小。支柱的不对称布置并不能极大地改善涡轮的整体流动特性。目前的结果表明,通过不对称的支柱设计可以减少振动并增加叶片疲劳寿命。

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