[1] 纪国剑. 航空发动机典型篦齿封严泄漏特性的数值和实验研究[D].南京:南京航空航天大学, 2008. JI Guo-jian. Numerical and experimental investigation of sealing characteristics on typical labyrinth seals in aeroengine[D].Nanjing: Nanjing University of Aeronautics and Astronautics,2008.(in Chinese) [2] 沈虹, 郑天慧, 陈玉洁. 航空发动机封严技术的进展[J]. 燃气涡轮试验与研究, 2011,24(4):51-55. SHEN Hong, ZHENG Tian-hui, CHEN Yu-jie. Improvement of aero-engine sealing technology[J]. Gas Turbine Experiment and Research ,2011,24(4):51-55. (in Chinese) [3] Wellborn S R, Okiishi T H. The influence of shrouded stator cavity flows on multistage compressor performance[J]. Journal of Turbomachinery, 1999, 121(3):486-497. [4] 禄堃. 轴流压气机静叶气封间隙流的研究和流道优化[D]. 北京:清华大学, 2008. LU Kun. Research on axial-compressor shrouded stator cavity flows and flow path optimization[D]. Beijing: Tsinghua University,2008. (in Chinese) [5] Gier J, Stubert B, Brouillet B, et al. Interaction of shroud leakage flow and main flow in a three-stage LP turbine[J]. Journal of Turbomachinery, 2003, 127(4):105-116. [6] 马文生, 禄堃, 顾春伟. 压气机静叶气封几何优化与流动分析[J]. 工程热物理学报, 2009,30(8):1288-1290. MA Wen-sheng, LU Kun, GU Chun-wei. Compressor stator seal cavity geometry optimization and flow analysis[J]. Journal of Engineering Thermophysics, 2009,30(8): 1288-1290. (in Chinese) [7] 应银生, 马石. 叶冠齿数和齿顶间隙对涡轮气动性能的影响[J]. 航空制造技术, 2016,496(1/2):128-131. YING Yin-sheng, MA Shi. Effect of the shroud seal number and the tip clearance on the aerodynamic performance of the turbine[J].Aeronautical Manufacturing Technology, 2016,496(1/2):128-131. (in Chinese) [8] 温泉, 梁德旺, 王可. 旋转直管流场的数值模拟[J].南京航空航天大学学报,2000,32(5):539-544. WEN Quan, LIANG De-wang, WANG Ke. Rotary straight pipe field numerical simulation[J].Journal of Nanjing University of Aeronautics & Astronautics,2000,32(5):539-544.
[9] Kuwamura Y, Matsumoto K, Uehara H, et al. Development of new high-performance labyrinth seal using aerodynamic approach[C]∥ ASME Turbo Expo 2013: Turbine Technical Conference and Exposition. San Antonio, Texas, US: ASME ,2013.
[10] Rhode D L, Allen B F. Measurement and visualization of leakage effects of rounded teeth tips and rub-grooves on stepped labyrinths[J]. Journal of Engineering for Gas Turbines & Power, 1999, 123(3):604-611. [11] 张勃, 吉洪湖, 杜发青,等. 篦齿封严尺寸缩放与气流温度变化对流动与传热影响实验研究[J]. 推进技术, 2016,37(2):304-310. ZHANG Bo, JI Hong-hu, DU Fa-qing, et al. Experimental investigation of scaling and temperature effects on flowing and heat transfer characteristics in labyrinth seals[J]. Journal of Propulsion Technology, 2016,37(2):304-310.(in Chinese) [12] 塔鲁达纳斯基.非接触密封/间隙密封与迷宫密封的原理和应用[M].李均卿,刁元康,译. 北京:机械工业出版社,1986. Trutnovsky K. Berührungsfreie dichtungen: grundlagen und anwendungen der strmung durch spalte und labyrinth[M]. LI Jun-qing, DIAO Yuan-kang, translated. Beijing: China Machine Press,1986.(in Chinese) [13] Stocker H L. Determining and improving labyrinth seal perfor-mance in current and advanced high performance gas turbines[J]. AGARD Conference Proceedings,1978,237:13. [14] 赵海刚, 刘振侠. 航空发动机篦齿封严特性数值模拟[J]. 燃气涡轮实验与研究, 2010, 23(1):26-30. ZHAO Hai-gang, LIU Zhen-xia. Numerical analyses for the performance of straight labyrinth seal of aircraft engine[J]. Gas Turbine Experiment and Research, 2010,23(1):26-30.(in Chinese) [15] 王锁芳, 吕海峰. 转静态封严篦齿流场的数值分析和封严特性的实验[J]. 航空动力学报, 2005, 20(3):444-449. WANG Suo-fang, LYU Hai-feng. Numerical analysis of flow and experimental investigation of labyrinth sealing characteristics at rotational and static states[J]. Journal of Aerospace Power, 2005, 20(3):444-449.(in Chinese) [16] 吴丁毅. 两类常用篦齿密封和临界特性的分析与比较[J]. 航空动力学报, 1997,12(4):397-400. WU Ding-yi. Two types of commonly used grate tooth seal and critical features analysis and comparison[J]. Journal of Aerospace Power, 1997,12(4):397-400.(in Chinese)
[17] 朱高涛, 刘卫华. 迷宫密封泄漏量计算方法的分析[J]. 润滑与密封, 2006(4):123-126. ZHU Gao-tao, LIU Wei-hua. Analysis of calculational methods on leakage for labyrinth seals[J]. Lubrication Engineering, 2006(4): 123-126.(in Chinese)
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第38卷 第4期2017 年4月兵工学报ACTA ARMAMENTARIIVol.38No.4Apr.2017
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