Volume 29 Issue 4
Apr.  2014
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LU Shan, ZHAO Lei. Structural optimization design method of twin-web turbine disk with tenon[J]. Journal of Aerospace Power, 2014, 29(4): 875-880. doi: 10.13224/j.cnki.jasp.2014.04.018
Citation: LU Shan, ZHAO Lei. Structural optimization design method of twin-web turbine disk with tenon[J]. Journal of Aerospace Power, 2014, 29(4): 875-880. doi: 10.13224/j.cnki.jasp.2014.04.018

Structural optimization design method of twin-web turbine disk with tenon

doi: 10.13224/j.cnki.jasp.2014.04.018
  • Received Date: 2013-01-18
  • Publish Date: 2014-04-28
  • A 3-D structural optimization design method for twin-web turbine disk with tenon was presented, covering strategies of partial speedy optimization/totality-subtle optimization for disk and tenon structure with total mass of disk with tenon as the objective function and the partial management of design parameters. The structural optimization design platform for twin-web turbine disk with tenon was established based on software of ANSYS. Two models of twin-web turbine disk with tenon were designed for a high-pressure turbine rotor. And the influence of basic parameters, such as radius of disk outside edge neck, thickness of disk outside edge, on the stresses of several critical points of disk with tenon was studied. According to the optimization results, the method presented is proved feasible, as the distribution of stress in twin-web turbine disks is more uniform than that in single-web turbine disk; the masses of two models of twin-web turbine disk are 19.90% and 17.35% lighter than that of the single-web turbine disk model under the condition of meeting structure strength criterions, while the calculational time for optimizing the twin-web turbine disk with tenon model by the method presented is just 1/3 of that by the conventional 3-D optimization method. It is demonstrated that the method presented is reasonable and highly efficient.

     

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  • [1]
    Koop W.The integrated high performance turbine engine technology (IHPTET) program .ISABE 97-7175,1997.
    [2]
    Ballal D R,Zelina J.Progress in aero engine technology(1939-2003)[J].Journal of Aircraft,2004,41(1):43-50.
    [3]
    梁春华.IHPTET计划的最新进展[J].国际航空,2004(2):58-60. LIANG Chunhua.Advance of IHPTET[J].International Aviation,2004(2):58-60.(in Chinese)
    [4]
    李兆庆.大型军用航空发动机的先进涡轮技术[J].航空科学技术,2007(4):12-15. LI Zhaoqing.Turbine technology of large military aircraft engine[J].Aeronautical Science and Technology,2007(4):12-15.(in Chinese)
    [5]
    胡晓煜.美国全面实施下一代军用航空发动机技术发展计划VAATE[J].国际航空,2007(12):40-43. HU Xiaoyu.USnew advanced turbine engine technology development program VAATE[J].International Aviation,2007(12):40-43.(in Chinese)
    [6]
    Cairo R R.Twin-web rotor disk:United States,US005961287A .2005-11-23.
    [7]
    Cairo R R,Sargent K A.Twin web disk:a step beyond convention[J].Journal of Engineering for Gas Turbines and Power,2002,124(2):298-302.
    [8]
    赵熙,徐国强,罗翔,等.等重量空心盘冷气布置方案[J].北京航空航天大学学报,2009,35(5):527-531. ZHAO Xi,XU Guoqiang,LUO Xiang,et al.Cooling structure on double-web turbine disk with equal mass scheme[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(5):527-531.(in Chinese)
    [9]
    刘超.涡轮盘结构拓扑与形状优化方法研究 .南京:南京航空航天大学,2010. LIU Chao.Research on structure topology and shape optimal method of turbine disk .Nanjing:Najing University of Aeronautics and Astronautics,2010.(in Chinese)
    [10]
    王营,余朝蓬.航空发动机涡轮盘结构优化设计[J].机械设计与制造,2010(5):4-6. WANG Ying,YU Zhaopeng.Optimization design for the turbine disk of a gas engine[J].Machinery Design & Manufacture,2010(5):4-6.(in Chinese)
    [11]
    栾永先.双辐板涡轮盘结构强度分析[J].航空发动机,2012,38(5):38-41. LUAN Yongxian.Structure strength analysis of dual-web turbine disk[J].Aeroengine,2012,38(5):38-41.(in Chinese)
    [12]
    陆山,李伦未.航空发动机高负荷涡轮盘双辐板结构优化设计[J].推进技术,2011,32(5):631-636. LU Shan,LI Lunwei.Twin-web structure optimization design for heavy duty turbine disk based for aero-engine[J].Journal of Propulsion Technology,2011,32 (5):631-636.(in Chinese)
    [13]
    陶冶,陆山.涡轮盘/榫整体结构优化设计方法[J].航空动力学报,2012,27(6):1249-1254. TAO Ye,LU Shan.Method of structural optimization design for turbine disk/tenon[J].Journal of Aerospace Power,2012,27(6):1249-1254.(in Chinese)
    [14]
    申秀丽,齐晓东,王荣桥,等.航空发动机涡轮榫接结构齿形基本参数研究[J].航空动力学报,2011,26(4):735-744. SHEN Xiuli,QI Xiaodong,WANG Rongqiao,et al.Research on the dentiform basic parameters of aero-engine turbine joint structure[J].Journal of Aerospace Power,2011,26(4):735-744.(in Chinese)
    [15]
    吕文林.航空涡喷、涡扇发动机结构设计准则(研究报告):第二册 轮盘 .北京:中国航空工业总公司发动机系统工程局,1997.
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