| Citation: | Simplification method of complex air cooling bladed disk structure’s deformation analysis model[J]. Journal of Aerospace Power, 2017, 32(7): 1712-1717. doi: 10.13224/j.cnki.jasp.2017.07.023 |
| [1] |
STEINETZ B M,LATTIME S B,TAYLOR S,et al.Evaluation of an active clearance control system concept[R].NASA TM-213856,2005.
|
| [2] |
张少平,苏廷铭,罗秋生,等.航空发动机压气机径向间隙设计方法研究[J].燃气涡轮实验与研究,2011,24(4):25-31.ZHANG Shaoping,SU Tingming,LUO Qiusheng,et al.Design method for compressor radial clearance of an aero-engine[J].Gas Turbine Experiment and Research,2011,24(4):25-31.(in Chinese)
|
| [3] |
周骁,张海波,王继强,等.考虑主动间隙控制的涡轮叶尖间隙建模计算研究[J].推进技术,2015,36(7):1093-1102.ZHOU Xiao,ZHANG Haibo,WANG Jiqiang,et al.Re-search on turbine tip clearance modeling considering active tip clearance control[J].Journal of Propulsion Technology,2015,36(7):1093-1102.(in Chinese)
|
| [4] |
杨晓光,黄佳.采用改进减缩模型的涡轮叶尖间隙快速分析方法[J].航空动力学报,2012,27(9):2048-2055.YANG Xiaoguang,HUANG Jia.Modified reduced model for rapid analysis of tip clearance of high pressure turbine[J].Journal of Aerospace Power,2012,27(9):2048-2055.(in Chinese)
|
| [5] |
杨冬,李琳.关于航空发动机结构间隙设计方法研究[R].北京:中国航空学会第10届强度、振动分会,2000.
|
| [6] |
赖焕新,吴克启.轴流压气机转子内流数值模拟及叶顶间隙泄漏分析[J].工程热物理学报,1998,19(5):576-580.LAI Huanxin,WU Keqi.Numerical analysis of internal flow field and tip clearance leakage in axial compressor ro-tor[J].Journal of Engineering Thermophysics,1998,19(5):576-580.(in Chinese)
|
| [7] |
王大磊,朴英.叶尖间隙高度对某高压涡轮级损失分布的影响[J].航空动力学报,2012,27(1):169-175.WANG Dalei,PIAO Ying.Influence of tip clearance size on flow losses of transonic high pressure turbine stage[J].Journal of Aerospace Power,2012,27(1):169-175.(in Chinese)
|
| [8] |
郭淑芬,徐波.涡轮叶尖径向主动间隙控制研究[J].航空发动机,2000(2):47-50.GUO Shufen,XU Bo.Active clearance control analysis of turbine tip clearance[J].Aero-engine,2000(2):47-50.(in Chinese)
|
| [9] |
王凯,段发阶,郭浩天,等.基于大频差双频激光的发动机叶尖间隙测量技术[J].光电子·激光,2013,24(10):1984-1988.WANG Kai,DUAN Fajie,GUO Haotian,et al.Blade tip clearance measurement using dual frequency laser with large frequency difference[J].Journal of Optoelectronics·Laser,2013,24(10):1984-1988.(in Chinese)
|
| [10] |
SCOTT B L,BRUCE M S.Turbine engine clearance control systems:current practices and future directions[R].AIAA-2002-3790,2002.
|
| [11] |
张晓波,杨瑞,李其汉.航空发动机涡轮径向间隙设计方法研究[J].航空发动机,2004,30(2):14-17.ZHANG Xiaobo,YANG Rui,LI Qihan.A method of tur-bine rotor radial clearance of an aero engine[J].Aeroengine,2004,30(2):14-17.(in Chinese)
|
| [12] |
ZHU J,SUN L,LU X.Experimental investigation on the layout of tip clearance for an axial-flow compressor rotor[J].AIAA-2005-0808,2005.
|
| [13] |
郭文,吉洪湖,蔡毅,等.高压涡轮动叶内部冷却结构的改进设计[J].南京航空航天大学学报,2006,38(4):408-412.GUO Wen,JI Honghu,CAI Yi,et al.Optimized design approach for internal cooling structure in turbine blades[J].Journal of Nanjing University of Aeronautics and Astro-nautics,2006,38(4):408-412.(in Chinese)
|
| [14] |
AGARWAL H,AKKARAM S,SHETYE S,et al.Reduced order clearance models for gas turbine[R].AIAA-2008-2177,2008.
|
| [15] |
贾丙辉,张小栋,彭凯.机动飞行下的涡轮叶尖间隙动态变化规律[J].航空动力学报,2011,26(12):2757-2764.JIA Binghui,ZHANG Xiaodong,PENG Kai.Effect of rotor on changes phenomena of turbine tip clearance[J].Journal of Aerospace Power,2011,26(12):2757-2764.(in Chinese)
|
| [16] |
倪萌,朱惠人,裘云,等.航空发动机涡轮叶片冷却技术综述[J].燃气轮机技术,2005,18(4):25-33.NI Meng,ZHU Huiren,QIU Yun,et al.Review of aero-turbine blade cooling technologies[J].Gas Turbine Tech-nology,2005,18(4):25-33.(in Chinese)
|
| [17] |
申秀丽,周莹胪.圆弧齿榫接结构应力的数值计算与分析[J].航空动力学报,2012,27(3):610-616.SHEN Xiuli,ZHOU Yinglu.Numerical calculation and analysis of arc tooth tenon joint[J].Journal of Aerospace Power,2012,27(3):610-616.(in Chinese)
|
| [18] |
张野.典型发动机涡轮榫接结构设计方法研究[D].北京:北京航空航天大学,2014.ZHANG Ye.Research on typical aero-engine turbine tenon structure design method[D].Beijing: Beijing University of Aeronautics and Astronautics,2014.(in Chinese)
|