刘传凯 - 北京航空航天大学 - 航空发动机研究院

个人简介

刘传凯，男，1979年4月生，副研究员，博士生导师，北京航空航天大学航空发动机研究院基础前沿部部长、总体与仿真方向执行PI，工信部两机基础科学中心技术专家，教育部2011 “先进航空发动机协同创新中心-航空发动机复杂系统安全性与适航协同创新团队”成员、中国航发涡轮院外聘专家、航空发动机型号合格审查组（TCT）成员、“中国航发重点型号支撑团队（空气系统与传热）”团队骨干。主讲课程为《航空发动机原理》、《航空发动机适航技术原理》、《航空发动机安全性与适航》。

研究领域

致力于航空发动机总体技术、空气系统与传热、航空发动机适航技术研究。提出了微秒量级时间尺度的强瞬变空气系统模块化仿真模型，解决了航空发动机系统仿真的维度缩放、时域协同问题，创立了航空发动机瞬态空气系统与过渡态性能模型的直接耦合方法，构建“航空发动机数字双胞胎”，支撑型号研制；提出了空气系统鲁棒性设计的基本理论和方法体系，并在行业初步推广

近期论文

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刘传凯, 邓宏武, 陶智等. 旋转蛇形通道内冷气流动和换热的数值模拟[J]. 航空动力学报, 2005, 20(4):662-667. 刘传凯, 陶智, 丁水汀等. 旋转对光滑U形通道内换热的影响研究[J]. 航空动力学报, 2006, 21(3):512-517. 刘传凯, 陶智, 丁水汀等. 3种转角下旋转U形方通道的局部换热[J]. 北京航空航天大学学报, 2006, 32(3):284-287. 刘传凯, 陶智, 丁水汀等. 旋转光滑及带肋U形通道的局部换热[J]. 航空学报, 2006, 27(5):751-755. Liu Chuankai, Deng Hongwu, Tao Zhi, et al. Prediction of Turbulent Flow and Heat Transfer Within Rotating U-shaped Passages[J]. Heat Transfer-Asian Research, 2006, 35(6):410-420. Tao Zhi, Liu Chuankai, Ding Shuiting, et al. Flow and Heat Transfer Computations in a Rotating Square Channel with Transverse Ribs Non-symmetrically Installed on Two Walls[C]. International Symposium on Jet Propulsion and Power Engineering. 2006:341-347 刘传凯, 丁水汀, 邱天, 陶智. 旋转方位角对斜肋通道内部流动与换热的影响[J]. 北京航空航天大学学报, 2009, 35(10):1188-1191. 刘传凯, 丁水汀, 陶智. 旋转附加力对方通道内流动与换热的影响机理[J]. 北京航空航天大学学报, 2009, 35(03):276-279. Liu Chuankai，Qiu Tian. Analysis of Component Degradations upon Aero-engine Safety Level[C]. International Symposium on Aircraft Airworthiness, Beihang Univ, Beijing, PEOPLES R CHINA, F Nov 02-04, 2009. Ding Shuiting, Li Guo, Liu Chuankai, et al. Turbine Disk Safety Boundary Assessment Using an Active Control Thermal Stress Distribution[C] International Symposium on Aircraft Airworthiness. 2009:356-361. Liu Chuankai, Qiu Tian, Ding Shuiting. Transient analysis of volume packing effects on turbofan engine [J]. Procedia Engineering, 2011, 17: 549-558. Che Weiwei, Ding Shuiting, Liu Chuankai. A Modeling Method on Aircraft Engine Based on the Component Method of Secondary Air System [J]. Procedia Engineering, 2014, 80: 258-271. 刘传凯, 刘海明, 李艳茹, 等. 强瞬变空气系统的模块化仿真建模[J]. 航空动力学报, 2015, 30(8): 1826-1833. Ding Shuiting, Wang Ziyao, Li Guo, Liu Chuankai. Transient stress control of aeroengine disks based on active thermal management[J]. Applied Thermal Engineering, 2016,103, 16-27. 刘传凯, 李圆圆, 李艳茹, 等. 涡轮轴断裂条件下空气系统强瞬变过程分析[J]. 北京航空航天大学学报, 2016, 42(1):47-53. 丁水汀, 车巍巍, 刘传凯. 空气系统双腔模型的压力动态特性分析[J]. 北京航空航天大学学报, 2016, 42(04):654-661. 丁水汀, 车巍巍,刘传凯. 熵方程在瞬态空气系统流动方向判断中的应用[J]. 航空动力学报, 2017, 32(10):2305-2313. 刘传凯, 李艳茹, 邱天, 丁水汀. 涡轮轴断裂条件下的涡扇发动机性能建模[J]. 航空动力学报, 2017, 32(12):2855-2861. 刘传凯, 姜宏超, 李艳茹, 等. 航空发动机性能与二次空气系统的耦合仿真模型[J]. 航空动力学报, 2017, 32(7):1623-1630. 刘传凯, 李艳茹. 毫米级微型涡轮发动机性能仿真模型[J]. 北京航空航天大学学报, 2018, 44(07):1430-1437. Ding Shuiting, Yu Hang, Qiu Tian, Liu Chuankai. Modeling of The Cavity Response to Rapid Transient Considering The effect of Heat Transfer[C] ASME Turbomachinery Technical Conference and Exposition. 2018. Li Jianghan, Ding Shuiting, Qiu Tian, Liu Chuankai, Yu Hang, Shan Xiaoming, He Yihong. Optimization and application of sensitivity-based spatial discrete method for numerical solution of transient flow and heat transfer [J]. Numerical Heat Transfer Part B-Fundamentals, 2019, 75(6): 383-403. Shi Yu, Ding Shuiting, Qiu Tian, Liu Chuankai, Zhang Shenghui. Bi-Fo time scaling method in the numerical simulation of transient conjugate heat transfer [J]. Propulsion and Power Research, 2021, 10(3): 209-223. Zhang Shenghui, Ding Shuiting, Liu Chuankai, et al. A Discussion: Issue Improving the Accuracy of Turbine Blade Heat Transfer Simulation[C]. Turbo Expo: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2021, 84980: V05BT13A003. 丁水汀, 王家俊, 刘传凯. 大涵道比分排涡扇发动机涡轮轴断裂过渡态性能仿真[J]. 航空动力学报, 2022, 37(03): 564-572. Liu Xiaojing, Ding Shuiting, Qiu Tian, Liu Chuankai, Liu Peng, Li Guo, Zhang Xiaozhe. Analysis of Entropy Generation and Potential Inhibition in an Aeroengine System Environment [J]. International Journal of Aerospace Engineering, 2022, 2022: 3637181. Shi Yu, Ding Shuiting, Qiu Tian, Liu Peng, Liu Chuankai. Nonuniform Clearance Effects on Pressure Distribution and Leakage Flow in the Straight-through Labyrinth Seals [J]. International Journal of Aerospace Engineering, 2022, 2022: 9684007. Shi Yu, Ding Shuiting, Qiu Tian, Liu Peng, Liu Chuankai. Nonuniform Clearance Effects on Windage Heating and Swirl Development in Straight-Through Labyrinth Seals [J]. Journal of Aerospace Engineering, 2022, 35(3): 1-20. Shi Yu, Ding Shuiting, Liu Peng, Qiu Tian, Liu Chuankai, Qiu Changbo, Ye Dahai. Swirl Flow and Heat Transfer in a Rotor-Stator Cavity with Consideration of the Inlet Seal Thermal Deformation Effect [J]. Aerospace, 2023, 10(2): 1-34. management[J]. Applied Thermal Engineering, 2016,103, 16-27.