
遲重然
副教授所在系所:葉輪機(jī)械研究所
辦公電話:616480
電子郵件:chizr@sjtu.edu.cn
通訊地址:上海交大機(jī)械與動(dòng)力工程學(xué)院A樓921室
個(gè)人主頁(yè):www.researchgate.net/profile/Zhongran_Chi
教育背景
2011-2014 清華大學(xué) 博士
2009-2011 哈爾濱工業(yè)大學(xué) 碩士
2005-2009 哈爾濱工業(yè)大學(xué) 學(xué)士
工作經(jīng)歷
2014-2016 上海交通大學(xué) 機(jī)械與動(dòng)力工程學(xué)院 葉輪機(jī)械研究所 博士后
2016-2020 上海交通大學(xué) 機(jī)械與動(dòng)力工程學(xué)院 葉輪機(jī)械研究所 講師
2021-至今 上海交通大學(xué) 機(jī)械與動(dòng)力工程學(xué)院 葉輪機(jī)械研究所 副教授
研究方向
航空發(fā)動(dòng)機(jī)與燃?xì)廨啓C(jī)、涉及流動(dòng)傳熱的工程機(jī)械:
(1) 氣動(dòng)傳熱研發(fā)體系與設(shè)計(jì)優(yōu)化方法
· 復(fù)雜結(jié)構(gòu)參數(shù)化設(shè)計(jì)、CFD網(wǎng)格生成與數(shù)值模擬技術(shù)
· 增材制造新型冷卻結(jié)構(gòu)
· 冷效相似理論與模型試驗(yàn)技術(shù)
(2) 氣熱固性能衰減、壽命預(yù)測(cè)與健康管理
· 基于保真仿真與深度學(xué)習(xí)的熱部件壽命預(yù)測(cè)
· 非定常流動(dòng)傳熱機(jī)理與精準(zhǔn)診斷方法
(3) 新型動(dòng)力循環(huán)與特種葉輪機(jī)
碩士招生基礎(chǔ)要求:《葉輪機(jī)械原理》或《空氣動(dòng)力學(xué)》,基本的編程能力與三維建模能力。
博士招生名額已滿。
學(xué)術(shù)兼職
國(guó)際期刊審稿人:ASME Journal of Heat Transfer, International Journal of Heat and Mass Transfer, Applied Thermal Engineering, Chinese Journal of Aeronautics, International Journal of Turbo&Jet Engines, International Journal of Energy Research 等
國(guó)際會(huì)議審稿人:ASME IGTI Turbo Expo, Global Power and Propulsion Forum 等
? 燃?xì)廨啓C(jī)與汽輪機(jī) 本科生 32學(xué)時(shí) 2學(xué)分 2021~2022
? 熱力系統(tǒng)設(shè)計(jì)與實(shí)踐 本科生 48學(xué)時(shí) 3學(xué)分 2017~【2020國(guó)家級(jí)精品課程】
? 計(jì)算流體力學(xué)(中文) 研究生 48學(xué)時(shí) 3學(xué)分 2018~
科研項(xiàng)目
2023-2024 美的集團(tuán) 矢量熱風(fēng)技術(shù)研究 負(fù)責(zé)
2023-2023 國(guó)家重大專項(xiàng) 整機(jī)環(huán)境下渦輪部件特性修正方法研究 分工負(fù)責(zé)
2022-2024 航發(fā)606所 氣冷渦輪葉片流固熱耦合網(wǎng)格生成及超大變量?jī)?yōu)化算法研究 分工負(fù)責(zé)
2021-2024 國(guó)家自然基金 分形幾何應(yīng)用于渦輪冷卻的流熱耦合特性研究 負(fù)責(zé)
2020-2022 航發(fā)606所 渦輪復(fù)雜冷卻結(jié)構(gòu)網(wǎng)格參數(shù)化與氣熱耦合網(wǎng)格生成技術(shù) 負(fù)責(zé)
2017-2019 上海電氣 重型燃機(jī)透平整機(jī)非定常氣動(dòng)仿真與熱斑輸運(yùn)機(jī)制研究 負(fù)責(zé)
2017-2017 航發(fā)上海商發(fā) 航空發(fā)動(dòng)機(jī)葉型設(shè)計(jì)分析工具 負(fù)責(zé)
2017-2017 中船711所 某型渦輪增壓器氣動(dòng)分析與優(yōu)化 負(fù)責(zé)
2016-2018 國(guó)家自然基金 渦輪動(dòng)葉內(nèi)外流場(chǎng)畸變對(duì)氣膜冷卻流動(dòng)傳熱的影響機(jī)理研究 負(fù)責(zé)
2016-2017 中國(guó)博后基金 渦輪動(dòng)葉氣動(dòng)--氣膜冷卻并行三維優(yōu)化方法研究 負(fù)責(zé)
2015-2016 中船701所 燃?xì)廨啓C(jī)進(jìn)氣系統(tǒng)模型試驗(yàn) 主參
2014-2016 上海電氣 某型透平的通流計(jì)算及葉片熱障涂層的研究 主參
2012-2014 清華自主科研 自主知識(shí)產(chǎn)權(quán)重型燃?xì)廨啓C(jī)核心技術(shù)研究 參與
2011-2013 國(guó)家自然基金 高溫高濕透平中多物理場(chǎng)耦合機(jī)理研究 參與
2011-2011 中航商發(fā) 某型航空發(fā)動(dòng)機(jī)高壓渦輪氣動(dòng)傳熱初步設(shè)計(jì) 主參
2009-2011 863計(jì)劃 F級(jí)中低熱值燃料燃機(jī)關(guān)鍵技術(shù)與整機(jī)設(shè)計(jì)研究 參與
代表性論文專著
● 燃機(jī)氣熱故障精準(zhǔn)診斷理論與方法
? Chi Z*, He Q, Huang J, Xia S, Zang S. Quantification of Combustion Inhomogeneity Based on Sparsely Arranged Thermocouples at the Outlet of Multi-Stage Turbines. Journal of Turbomachinery, 2026 (Accepted).
? Huang J, He Q, Chi Z*, et al.. Experimental and Numerical Study on the Impact of Inlet Temperature Inhomogeneity on the Aerodynamic Performance of a Three-Stage Turbine. Energy, 2024.
? He Q, Liu Y, Chi Z*, Zang S. Performance Evaluation of Damaged Blades Using Numerical Simulation and Machine Learning[J]. Journal of Propulsion and Power, 2024, 40(2): 271-84.
? He Q, Chi Z*, Zang S. Multidisciplinary Prediction of Spatial-temporal Evolution of Creep Damage on an Internally Cooled Turbine Vane[J]. Journal of Engineering for Gas Turbines and Power, 2024,146(4).
? 何慶富,遲重然,臧述升.幾何損傷導(dǎo)致渦輪靜葉氣動(dòng)衰減的CNN預(yù)測(cè)[J].工程熱物理學(xué)報(bào),2022,43(12).
? Xia S, Chi Z*, Zang S. Comparative Study of Two Data-Driven Gas Path Fault Quantification Methods for a Single-Shaft Gas Turbine. ASME Turbo Expo 2022, GT2022-82406.
? 何慶富,遲重然*,臧述升.退化渦輪葉片形變與氣動(dòng)參數(shù)偏離的影響研究[J].熱能動(dòng)力工程,2021, 36(9):7.
? He Q, Chi Z*, Zang S. An Efficient Prediction Method for the Azimuthal Migration of Combustion Inhomogeneity in Multi-Stage Cooled Turbines[C]. ASME Turbo Expo 2021, GT2021-60220.
? 程新毓,遲重然*,臧述升.時(shí)間傾斜算法模擬渦輪熱斑輸運(yùn)的精確性驗(yàn)證[J].熱能動(dòng)力工程,2021,36(01):38-48.
? Xia S, Chi Z*, Zang S. Improving Gas Turbine Performance through Reassembling Degraded Components: An Experimental and Computational Study[C]. ASME Turbo Expo 2020, GT2020-14627.
? 夏碩成,王輝,遲重然*,臧述升.部件性能衰減影響燃機(jī)性能的試驗(yàn)與仿真研究[J].工程熱物理學(xué)報(bào),2020,41(08):1877-1882.
? Chi Z*, Liu H, Zang S, et al. Full-Annulus URANS Study on the Transportation of Combustion Inhomogeneity in a Four-Stage Cooled Turbine[J]. Journal of Turbomachinery, 2019, 141(11): 111003.
? Chi Z*, Liu H, Zang S, et al. Full-Annulus URANS Study of Inlet Hot-Streak Transportation in a Four-Stage Gas Turbine[C]. ASME Turbo Expo 2018, GT2018-75596.
? 陳小嶺,遲重然*,馬超,臧述升.高載荷低壓渦輪葉片尾緣劈縫的葉柵損失影響[J].工程熱物理學(xué)報(bào),2016,37(08):1635-1640.
● 渦輪復(fù)雜冷卻結(jié)構(gòu)的設(shè)計(jì)優(yōu)化方法
? He Q, Zhao, W, Chi Z*, Zang S. Application of Deep-Learning Method in the Conjugate Heat Transfer Optimization of Full-Coverage Film Cooling on Turbine Vanes[J]. International Journal of Heat and Mass Transfer, 2022, 195:123148.
? 章鎖誠(chéng),夏碩成,遲重然*,臧述升. 雙層壁葉片的模型化方法與冷卻設(shè)計(jì)流程研究[J].熱能動(dòng)力工程 2021, 36(10):8.
? Chi Z*, Liu H, Zang S. Multi-objective optimization of the impingement-film cooling structure of a gas turbine endwall using conjugate heat transfer simulations[J]. Journal of Thermal Science and Engineering Applications, 2018, 10(2).
? Chi Z*, Liu H, Zang S. Geometrical optimization of nonuniform impingement cooling structure with variable-diameter jet holes[J]. International Journal of Heat and Mass Transfer, 2017, 108: 549-560.
? Chi Z*, Liu H, Zang S. Semi-Inverse Design Optimization Method for Film-Cooling Arrangement of High-Pressure Turbine Vanes[J]. Journal of Propulsion and Power, 2016, 32(3): 659-673.
? 遲重然*,任 靜,蔣洪德,臧述升. 渦輪導(dǎo)葉氣膜冷卻結(jié)構(gòu)半反設(shè)計(jì)優(yōu)化方法[J].工程熱物理學(xué)報(bào), 2016,37(1):62-66.
? Chi Z, Ren J*, Jiang H. Coupled aerothermodynamics optimization for the cooling system of a turbine vane[J]. Journal of Turbomachinery, 2014, 136(5).
? Chi Z, Li X, Han C, et al. Optimization of the hole exit shaping of film holes without and with compound angles for maximal film cooling effectiveness[C]. ASME Turbo Expo 2014, GT2014-25212.
? Chi Z, Ren J*, Jiang H. Cooling Structure Optimization for a Rib-Roughed Channel in a Turbine Rotor Blade[C]. ASME Turbo Expo 2013, GT2013-94527.
? Chi Z, Wang S, Ren J*, Jiang H. Multi-dimensional platform for cooling design of air-cooled turbine blades[C]. ASME Turbo Expo 2012, GT2012-68675.
? 遲重然,溫風(fēng)波,王松濤*,馮國(guó)泰. 渦輪動(dòng)葉冷卻結(jié)構(gòu)設(shè)計(jì)方法 Ⅲ:氣熱耦合計(jì)算[J].工程熱物理學(xué)報(bào), 2011,32(9):1485-1488.
? 遲重然,溫風(fēng)波,王松濤*,馮國(guó)泰. 渦輪動(dòng)葉冷卻結(jié)構(gòu)設(shè)計(jì)方法 Ⅱ:管網(wǎng)計(jì)算[J].工程熱物理學(xué)報(bào), 2011,32(6):933-936.
? 王松濤*,遲重然,溫風(fēng)波,馮國(guó)泰. 渦輪動(dòng)葉冷卻結(jié)構(gòu)設(shè)計(jì)方法 Ⅰ:參數(shù)化設(shè)計(jì)[J].工程熱物理學(xué)報(bào), 2011,32(4):581-584.
● 先進(jìn)冷卻技術(shù)與模化相似理論
? Chi Z*, Wang L. A Novel Fractal Cooling Structure for Turbine Vanes. Journal of Turbomachinery, 2025.
? 劉亞非, 陶皓杰,遲重然*,. 蜂窩內(nèi)冷通道布局對(duì)葉片冷效的影響研究[J].熱能動(dòng)力工程,2022,37(12).
? Zhao W, Chi Z*, Zang S. Numerical and Experimental Study of Scaling Criteria Accuracy for Film Cooling Using CO2 Coolant[J]. International Journal of Heat and Mass Transfer, 2021, 181: 121984.
? Zhao W, Chi Z*, Zang S. Scaling criteria accuracy for turbine blade film cooling effectiveness at unmatched temperature ratio conditions[J]. Applied Thermal Engineering, 2021, 197: 117363.
? 陶皓杰,遲重然*,臧述升.渦輪動(dòng)葉吸力側(cè)單排氣膜孔冷卻性能研究[J].工程熱物理學(xué)報(bào),2021,42(03):595-600.
? Zhao W, Chi Z*, Zang S. Investigation of Similarity Criteria for an Internally-Cooled Turbine Vane Based on Artificial Neural Networks – PARTⅠ: Comparison of Scaling Criteria[C]. ASME Turbo Expo 2020, GT2020-14617.
? Zhao W, Wei J, Chi Z*, et al. Investigation of Similarity Criteria for an Internally-Cooled Turbine Vane Based on Artificial Neural Networks – PARTⅡ: Experimental Validation[C]. ASME Turbo Expo 2020, GT2020-16167.
? 韋景穎,遲重然*,臧述升.渦輪靜葉葉型對(duì)絕熱氣膜冷卻效率的影響[J].動(dòng)力工程學(xué)報(bào),2020,40(10):793-800.
? Chi Z*, Liu H, Zang S. Parametric Cooling Study of Single-Row Cylindrical Film Holes on Pressure Side of a Rotor Blade[C]. ASME Turbo Expo 2017, GT2017-65208.
? Chi Z*, Ren J, Jiang H, et al. Geometrical optimization and experimental validation of a tripod film cooling hole with asymmetric side holes[J]. Journal of Heat Transfer, 2016, 138(6).
? 遲重然,任 靜*,蔣洪德. 燃機(jī)葉片平行肋擾流內(nèi)冷通道傳熱特性研究Ⅱ:耦合傳熱特性[J].工程熱物理學(xué)報(bào), 2014,35(1):42-45.
? 遲重然,任 靜*,蔣洪德. 燃機(jī)葉片平行肋擾流內(nèi)冷通道傳熱特性研究Ⅰ:流動(dòng)傳熱機(jī)理[J].工程熱物理學(xué)報(bào), 2013,34(4):624-627.
? Chi Z, Kan R, Ren J*, et al. Experimental and numerical study of the anti-crossflows impingement cooling structure[J]. International Journal of Heat and Mass Transfer, 2013, 64: 567-580.
● 新型動(dòng)力循環(huán)與特種葉輪機(jī)
? Liu H, Chi Z*, Zang S. Transient behaviour and optimal start-up procedure of closed Brayton cycle with high thermal inertia[J]. Applied Thermal Engineering, 2021, 199: 117587.
? Liu H, Chi Z*, Zang S. Optimization of a closed Brayton cycle for space power systems[J]. Applied Thermal Engineering, 2020, 179: 115611.
? Liu H, Chi Z*, Zang S. Influence of Relative Velocity Ratio on Centrifugal Impellers Operating With Supercritical CO2[C]. ASME Turbo Expo 2018, GT2018-75590.
? Liu H, Chi Z*, Zang S. Influence of Root Fillet on the Structural and Aerodynamic Performance of a Centrifugal Impeller[C]. IGTC2015, No. 51.
軟件版權(quán)登記及專利
· 遲重然,何慶富. 專利名稱:具有分叉冷卻通道和蜂窩冷卻通道的渦輪葉片: CN 2023116184004, 2023.
· 蔣洪德,任 靜,遲重然. 專利名稱:一種用于燃?xì)鉁u輪發(fā)動(dòng)機(jī)冷卻的分支氣膜孔結(jié)構(gòu): CN 103437889 A[P]. 2013.
· 2020.01 聘期考核優(yōu)秀 (學(xué)院)
· 2019.12 優(yōu)秀班主任 (學(xué)校)
· 2018.06 青年教師教學(xué)競(jìng)賽一等獎(jiǎng)(學(xué)院)
· 2017.12 最受歡迎教師 (學(xué)院)
· 2016.12 優(yōu)秀班主任 (學(xué)校)
· 2013.09 研究生國(guó)家獎(jiǎng)學(xué)金 (博士)