{"title":"Effects of rim seal exit geometry on the cooling characteristics of turbine endwall and blade suction side","authors":"","doi":"10.1016/j.tsep.2024.102797","DOIUrl":null,"url":null,"abstract":"<div><p>For a turbine blade endwall, the leakage (purge flow) exits through rim seal to prevent hot gas ingress and provide some cooling to the endwall. However, changes in the rim seal geometry will inevitably affect the leakage flow over the endwall. To obtain a clearer and quantitative understanding of the effect of rim seal variation on the cooling performance and flow structure, this paper investigated the effects of width and inclined angle of rim seal exit geometry, as well as the flow structure inside the gap and above the passage. A correlation fitting was constructed using the area-averaged cooling effectiveness to quantify the cooling performance on the suction side. The results indicate that the cooling performance of endwall is not sensitive to changes in width. However, a decrease in the inclined angle benefits the inhibition of the cavity vortex, prevents the gas ingress and improves the cooling performance over<!--> <!-->the endwall. The cooling performance of blade suction side is sensitive to the leakage mass flow ratio. As the mass flow rate increases from 0.5 % to 1.0 % and 1.5 %, the area-averaged cooling effectiveness on suction side for original case increases by 44.4 % and 30.7 %. The correlation established for the cooling of suction side shows a good fit, which provide a possible evaluation method for cooling design.</p></div>","PeriodicalId":23062,"journal":{"name":"Thermal Science and Engineering Progress","volume":null,"pages":null},"PeriodicalIF":5.1000,"publicationDate":"2024-08-13","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Thermal Science and Engineering Progress","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S2451904924004153","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENERGY & FUELS","Score":null,"Total":0}
引用次数: 0
Abstract
For a turbine blade endwall, the leakage (purge flow) exits through rim seal to prevent hot gas ingress and provide some cooling to the endwall. However, changes in the rim seal geometry will inevitably affect the leakage flow over the endwall. To obtain a clearer and quantitative understanding of the effect of rim seal variation on the cooling performance and flow structure, this paper investigated the effects of width and inclined angle of rim seal exit geometry, as well as the flow structure inside the gap and above the passage. A correlation fitting was constructed using the area-averaged cooling effectiveness to quantify the cooling performance on the suction side. The results indicate that the cooling performance of endwall is not sensitive to changes in width. However, a decrease in the inclined angle benefits the inhibition of the cavity vortex, prevents the gas ingress and improves the cooling performance over the endwall. The cooling performance of blade suction side is sensitive to the leakage mass flow ratio. As the mass flow rate increases from 0.5 % to 1.0 % and 1.5 %, the area-averaged cooling effectiveness on suction side for original case increases by 44.4 % and 30.7 %. The correlation established for the cooling of suction side shows a good fit, which provide a possible evaluation method for cooling design.
期刊介绍：
Thermal Science and Engineering Progress (TSEP) publishes original, high-quality research articles that span activities ranging from fundamental scientific research and discussion of the more controversial thermodynamic theories, to developments in thermal engineering that are in many instances examples of the way scientists and engineers are addressing the challenges facing a growing population – smart cities and global warming – maximising thermodynamic efficiencies and minimising all heat losses. It is intended that these will be of current relevance and interest to industry, academia and other practitioners. It is evident that many specialised journals in thermal and, to some extent, in fluid disciplines tend to focus on topics that can be classified as fundamental in nature, or are ‘applied’ and near-market. Thermal Science and Engineering Progress will bridge the gap between these two areas, allowing authors to make an easy choice, should they or a journal editor feel that their papers are ‘out of scope’ when considering other journals. The range of topics covered by Thermal Science and Engineering Progress addresses the rapid rate of development being made in thermal transfer processes as they affect traditional fields, and important growth in the topical research areas of aerospace, thermal biological and medical systems, electronics and nano-technologies, renewable energy systems, food production (including agriculture), and the need to minimise man-made thermal impacts on climate change. Review articles on appropriate topics for TSEP are encouraged, although until TSEP is fully established, these will be limited in number. Before submitting such articles, please contact one of the Editors, or a member of the Editorial Advisory Board with an outline of your proposal and your expertise in the area of your review.
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