首页> 外国专利> LOW-PRESSURE TURBINE BLADE HAVING WAVY SUCTION SURFACE

LOW-PRESSURE TURBINE BLADE HAVING WAVY SUCTION SURFACE

机译:具有波浪形抽吸表面的低压涡轮叶片

摘要

A low-pressure turbine blade having a wavy suction surface, applicable to reducing profile loss of a high-load low-pressure turbine blade and an ultra-high-load low-pressure turbine blade on an aero engine. The low-pressure turbine blade comprises a blade leading edge (1), a blade suction side (2), a blade pressure side (3), and a blade trailing edge (4). The shape of the blade suction side (2) is a wavy surface extending in a height direction of the blade. The wavy surface starts at the blade leading edge (1), and ends at the blade trailing edge (4). The wavy surface is formed by alternately arranging crests and troughs. From the blade leading edge (1) to the blade trailing edge (4), the distance between the wavy crest and the wavy trough in a vane pitch direction increases linearly from 0 to 2A and decreases linearly from 2A to 0, where A is the greatest amplitude of the wavy surface. Fluid separates from the blade in the position corresponding to the greatest amplitude. The blade structure effectively reduces separation of the fluid from the blade, reduces loss, and improves the performance of a low-pressure turbine.
机译:一种具有波浪形吸力面的低压涡轮叶片,适用于减少航空发动机上的高负荷低压涡轮叶片和超高负荷低压涡轮叶片的轮廓损失。低压涡轮机叶片包括叶片前缘(1),叶片吸力侧(2),叶片压力侧(3)和叶片后缘(4)。叶片吸入侧(2)的形状是在叶片的高度方向上延伸的波浪面。波浪形表面始于叶片前缘(1),结束于叶片后缘(4)。波浪表面是通过交替布置波峰和波谷而形成的。从叶片前缘(1)到叶片后缘(4),波峰和波谷之间的距离在叶片桨距方向上从0线性增加到2A,从2A线性减少到0,其中A是波浪表面的最大振幅。流体在对应于最大振幅的位置从叶片分离。叶片结构有效地减少了流体与叶片的分离,减少了损失,并改善了低压涡轮机的性能。

著录项

  • 公开/公告号WO2020220498A1

    专利类型

  • 公开/公告日2020-11-05

    原文格式PDF

  • 申请/专利权人 ZHEJIANG UNIVERSITY;

    申请/专利号WO2019CN99411

  • 发明设计人 CUI JIAHUAN;LIU JIAN;WANG WEN;

    申请日2019-08-06

  • 分类号F01D5/14;

  • 国家 WO

  • 入库时间 2022-08-21 11:08:45

相似文献

  • 专利
  • 外文文献
  • 中文文献
获取专利

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