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基于熵產(chǎn)理論的多級(jí)液力透平能量耗散機(jī)理分析
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國(guó)家自然科學(xué)基金項(xiàng)目(52169019)、甘肅省杰出青年基金項(xiàng)目(20JR10RA203)和中國(guó)博士后科學(xué)基金項(xiàng)目(2022M712676)


Analysis of Energy Dissipation Mechanism of Multistage Hydraulic Turbine Based on Entropy Production Theory
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    摘要:

    液力透平作為一種液體余壓能回收裝置,在小水電建設(shè)和能量回收領(lǐng)域得到廣泛應(yīng)用,但其內(nèi)部能量損失特性不清。以兩級(jí)徑流式液力透平為研究對(duì)象,基于熵產(chǎn)理論和Omega渦識(shí)別準(zhǔn)則分析了各過(guò)流部件內(nèi)能量耗散機(jī)理。結(jié)果表明:速度脈動(dòng)和壁面效應(yīng)是能量損失的主要來(lái)源,設(shè)計(jì)工況下二者總占比為98.03%。葉輪和導(dǎo)葉是透平內(nèi)能量耗散的主要區(qū)域;小流量工況,葉輪損失占比較高;大流量工況下,導(dǎo)葉損失占比較高。葉輪內(nèi)的能量損失源于葉片前緣分離渦、吸力面回流渦以及葉片尾緣渦等不穩(wěn)定流動(dòng)現(xiàn)象,而相對(duì)液流角與葉片進(jìn)口安放角的不匹配是導(dǎo)致葉輪內(nèi)產(chǎn)生不穩(wěn)定流動(dòng)的根本原因;在導(dǎo)葉和導(dǎo)葉Ⅱ-反導(dǎo)葉中,不同流量下導(dǎo)致其能量耗散的因素基本保持一致,葉片前緣失速渦和流動(dòng)分離等劣態(tài)流動(dòng)引起的動(dòng)量交換是導(dǎo)致能量損失的主要原因。環(huán)形吸水室內(nèi)流動(dòng)的非對(duì)稱性導(dǎo)致導(dǎo)葉Ⅰ各流道內(nèi)熵產(chǎn)率分布不均勻,而導(dǎo)葉Ⅱ-反導(dǎo)葉通過(guò)正導(dǎo)葉的整流減小了沖擊效應(yīng),各流道內(nèi)熵產(chǎn)率分布均勻且高熵區(qū)較小。

    Abstract:

    As a liquid residual pressure energy recovery device, hydraulic turbine is widely used in the field of small hydropower construction and energy recovery, but its internal energy loss characteristics are unclear. The two-stage radial hydraulic turbine was taken as the research object. Based on the entropy production theory, the energy loss in each flow component was quantitatively analyzed, and the energy dissipation mechanism in the turbine was further revealed by combining the Omega vortex identification criterion and flow field distribution. The results showed that velocity pulsation and wall effect were the primary sources of energy dissipation. The total proportion of the two was 98.03% under the design condition. The impeller and the guide vane were the main areas of energy dissipation in the turbine; the impeller loss accounted for a higher percentage in the small flow condition, while the guide vane loss accounted for a higher percentage in the large flow condition. The energy loss in the impeller originated from the unstable flow phenomena such as vortex separation at the leading edge of the blade, return vortex at the suction surface, and vortex at the trailing edge of the blade, and the matching of the relative liquid flow angle and the angle of placement of the inlet of the blade was the fundamental reason for the unstable flow in the impeller; in the guide vane Ⅰ and the guide vane Ⅱ-anti-guide vane, the factors leading to the dissipation of their energy at different flow rates were basically the same, and the poor flow such as the stagnation vortex at the leading edge of the blade and the flow separation. The momentum exchange caused by the blade leading edge stall vortex and flow separation was the main cause of energy loss. Due to the asymmetry of the flow inside the annular suction chamber, the entropy yield distribution in each channel of the guide vane Ⅰ was not uniform, while the guide vane Ⅱ-anti-guide vane reduced the shock effect through the rectification of the positive guide vane, and the entropy yield distribution in each channel was uniform and the high entropy area was small.

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王曉暉,蔣虎忠,苗森春,白小榜,祁炳.基于熵產(chǎn)理論的多級(jí)液力透平能量耗散機(jī)理分析[J].農(nóng)業(yè)機(jī)械學(xué)報(bào),2024,55(3):162-172. WANG Xiaohui, JIANG Huzhong, MIAO Senchun, BAI Xiaobang, QI Bing. Analysis of Energy Dissipation Mechanism of Multistage Hydraulic Turbine Based on Entropy Production Theory[J]. Transactions of the Chinese Society for Agricultural Machinery,2024,55(3):162-172.

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  • 收稿日期:2023-08-05
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