Volume 29 Issue 1
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LIU Hong-bin, HUANG Wei-na, CHEN Wei. Investigation on high cycle fatigue-low cycle fatigue life of alloy material[J]. Journal of Aerospace Power, 2014, 29(1): 74-80. doi: 10.13224/j.cnki.jasp.2014.01.010
Citation: LIU Hong-bin, HUANG Wei-na, CHEN Wei. Investigation on high cycle fatigue-low cycle fatigue life of alloy material[J]. Journal of Aerospace Power, 2014, 29(1): 74-80. doi: 10.13224/j.cnki.jasp.2014.01.010

Investigation on high cycle fatigue-low cycle fatigue life of alloy material

doi: 10.13224/j.cnki.jasp.2014.01.010
  • Received Date: 2012-11-30
  • Publish Date: 2014-01-28
  • The effects of high cycle fatigue-low fatigue life(HCF-LCF) on titanium alloy (TC4 and TC11) were researched experimentally with foreign object damage (FOD) simulation through pendulum method and air-gas gun method and the features of these two different damage notches were analyzed and compared. Fatigue tests on nondestructive and destructive specimens were further conducted to analyze and compare the effects of FOD on the titanium alloy fatigue life.The conclusions show that:pendulum impact test method simulation lacks of representativeness, while air-gas gun projectile method simulation is much closer to the truth; FOD leads to severe decline of HCF-LCF life of titanium alloy, and air-gas gun projectile method simulation decreases the titanium alloy fatigue life from 105 to 104 order of magnitude.

     

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  • [1]
    刘红彬, 陈伟, 杜文军.TC11材料高低周复合疲劳试验研究[J].燃气涡轮试验与研究, 2011, 24(2):23-26. LIU Hongbin, CHEN Wei, DU Wenjun.Experimental investigation on low and high cycle combined fatigue performance of TC11 titanium alloy[J].Gas Turbine Experiment and Research, 2011, 24(2):23-26.(in Chinese)
    [2]
    Makhutov N, Romanov A, Gadenin M.High-temperature low-cycle fatigue resistance under superimposed stresses at two frequencies[J].Fatigue and Fracture of Engineering Materials and Structures, 1979, 1(3):281-285.
    [3]
    Zaitsev G Z, Faradzhov R M.The fatigue limit of steels under loads of differing frequencies[J].Metal Science and Heat Treatment, 1970, 12(2):128-130.
    [4]
    Ouyand J, Wang Z, Song D, et al.Influence of high frequency vibrations on the low cycle fatigue behavior of a supperalloy at elevated temperature, low cycle fatigue[R].American Society for Testing and Materials, ASTM STP 942, 1988.
    [5]
    许风旌, 聂景旭, 赵长占.平板构件的高低周复合疲劳研究[J].航空动力学报, 1992, 7(2):121-124. XU Fengjing, NIE Jingxu, ZHAO Changzhan.A compound fatigue investigation of plate specimen under low-cycle load superposed on high cycle load[J].Journal of Aerospace Power, 1992, 7(2):121-124.(in Chinese)
    [6]
    侯静泳, 蔡肇云, 屠一鹤.TC-11钛合金高低周复合疲劳及损伤累积研究[J].航空动力学报, 1992, 7(2):135-138. HOU Jingyong, CAI Zhaoyun, TU Yihe.Research on high-low cycle complex fatigue and accumulative damage for Ti-alloy TC11[J].Journal of Aerospace Power, 1992, 7(2):135-138. (in Chinese)
    [7]
    Nowell D, Duo P, Stewart I F.Prediction of fatigue performance in gas turbine blades after foreign object damage[J]. International Journal of Fatigue, 2003, 25(9/10/11):963-969.
    [8]
    孙振德, 鲁启新.外物撞击损伤叶片的模拟试验方法[J].航空动力学报, 1989, 4(1):30-32. SUN Zhende, LU Qixin.Investigation on simulation of foreign object impact damage to compressor blade[J].Journal of Aerospace Power, 1989, 4(1):30-32.(in Chinese)
    [9]
    康继东, 陈士煊, 徐志怀.压气机叶片外物损伤模拟的撞击能量当量法[J].南京航空航天大学学报, 1998, 30(6):611-615. KANG Jidong, CHEN Shixuan, XU Zhihuai.Impact energy equivalent method for simulation of foreign object damage to compressor blades[J].Journal of Nanjing University of Aeronautics and Astronautics, 1998, 30(6):611-615. (in Chinese)
    [10]
    Mall S, Hamrick J L, Nicholas T. High cycle fatigue behavior of Ti-6Al-4V with simulated foreign object damage[J].Mechanics of Materials, 2001, 33(11):679-692.
    [11]
    Gallagher J, Nicholas T, Gunderson A, et al.Advanced high cycle fatigue life assurance methodologies[R].AFRL-ML-WP-TR-2005-4102, 2005.
    [12]
    Ding J, Hall R F, Byrne J, et al.Fatigue crack growth from foreign object damage under combined low and high cycle loading:Part I experimental studies[J]. International Journal of Fatigue, 2007, 29(7):1339-1349.
    [13]
    Oakley S Y, Nowell D.Prediction of the combined high-and low-cycle fatigue performance of gas turbine blades after foreign object damage[J].International Journal of Fatigue, 2007, 29(1):69-80.
    [14]
    郑光华, 赵长占.压气机叶片高低周复合疲劳的裂纹扩展研究[J].北京航空航天大学学报, 1996, 22(1):33-37. ZHENG Guanghua, ZHAO Changzhan.Research on crack propagation of compressor blade on low cycle fatigue combined with high cycle fatigue[J].Journal of Beijing University of Aeronautics and Astronautics, 1996, 22(1):33-37.(in Chinese)
    [15]
    刘红彬, 陈伟.TC11材料高低周疲劳裂纹萌生与扩展特性研究[J].燃气涡轮试验与研究, 2012, 25(2):49-53. LIU Hongbin, CHEN Wei.Study on initiation and propagation characteristics of high and low cycle combined fatigue crack in TC11[J].Gas Turbine Experiment and Research, 2011, 25(2):49-53.(in Chinese)
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