| 计及机匣相对运动的涡轮叶片叶顶凹槽流动研究 |
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| 引用本文： | 杜金霖,邹正平,黄霖,轩笠铭,王元鹏. 计及机匣相对运动的涡轮叶片叶顶凹槽流动研究[J]. 实验流体力学, 2021, 35(2): 22-35,82. DOI: 10.11729/syltlx20200073 |
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| 作者姓名： | 杜金霖 邹正平 黄霖 轩笠铭 王元鹏 |
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| 作者单位： | 北京航空航天大学 能源与动力工程学院,航空发动机气动热力国防科技重点实验室,北京 100191;北京航空航天大学 能源与动力工程学院,航空发动机气动热力国防科技重点实验室,北京 100191;北京航空航天大学 航空发动机研究院,北京 102206 |
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| 基金项目： | 国家自然科学基金51676005 |
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| 摘 要： | 叶尖泄漏流是造成航空发动机涡轮内部损失的重要因素,而凹槽叶尖是控制叶尖泄漏流的有效手段,准确了解凹槽内的流动结构有助于认识泄漏流的流动规律和泄漏损失的物理机制.为了详细研究考虑机匣相对运动时叶尖凹槽腔内流动结构变化及其对泄漏流的影响,搭建了可模拟机匣相对运动的低速平面叶栅实验台,该实验台可以进行不同叶型、不同叶顶结构以...
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| 关 键 词： | 叶栅 机匣运动 凹槽叶尖 泄漏流动 PIV |
| 收稿时间： | 2020-06-10 |
Experimental and numerical study of squealer tip flow field considering relative casing motion |
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| Affiliation: | 1.National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy & Power Engineering, Beihang University, Beijing 100191, China2.Research Institute of Aero-Engine, Beihang University, Beijing 102206, China |
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| Abstract: | The tip leakage flow is an important factor that causes the internal loss of the aeroengine turbine. The squealer tip can effectively control the tip leakage flow. Accurate understanding of the tip leakage flow structures in the cavity contributes to the understanding of the flow characteristics of the leakage flow and the physical mechanism of the leakage loss. In order to study the change of flow structures in the tip cavity when considering the relative casing motion and the effect on the leakage flow, a low-speed turbine cascade testing facility is built that can model the relative casing motion. The test facility can study factors such as blade profiles, different tip structures, and different incidence angles. A visual testing method of Particle Image Velocimetry (PIV) is proposed to obtain the complex flow structures within the tip cavity. The measurement method developed can obtain the complex flow field and successfully capture the scraping vortex in the tip cavity. In addition, the evolution of the flow structures in the tip cavity is analyzed with the help of numerical results under different casing motion conditions. An aero-labyrinth like sealing effect is formed by the scraping vortex. This sealing effect reduces the equivalent flow area at the gap outlet and diminishes the discharge coefficient of the squealer tip, therefore finally achieving the purpose of controlling the leakage flow. Choosing the appropriate blade load distribution and cavity geometry can improve the clogging effect and expand the control range of the scraping vortex. Mid-loaded blades have a more obvious effect on controlling the leakage flow when using the cavity tip. The tip gap height affects the generation and evolution of the flow structure in the tip cavity by which changes the effect of controlling the leakage flow. |
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