Volume 30 Issue 9
Sep.  2015
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BAO Zhen-qiang, HU Xu-teng, SONG Ying-dong. Effect of foreign object damage at different impact angles onhigh cycle fatigue strength of TC4 titanium alloys[J]. Journal of Aerospace Power, 2015, 30(9): 2226-2233. doi: 10.13224/j.cnki.jasp.2015.09.023
Citation: BAO Zhen-qiang, HU Xu-teng, SONG Ying-dong. Effect of foreign object damage at different impact angles onhigh cycle fatigue strength of TC4 titanium alloys[J]. Journal of Aerospace Power, 2015, 30(9): 2226-2233. doi: 10.13224/j.cnki.jasp.2015.09.023
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Effect of foreign object damage at different impact angles onhigh cycle fatigue strength of TC4 titanium alloys

doi: 10.13224/j.cnki.jasp.2015.09.023

  • 1. Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;

  • 2. State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China

  • Received Date: 2014-03-21
  • Publish Date: 2015-09-28
    Abstract
  • Based on the air-gun impact test device, the foreign object damage (FOD) simulation test of TC4 titanium alloy plate specimens was conducted at different impact angles. The high cycle fatigue (HCF) strength of smooth and impact damage samples was obtained with the step-test method. The relationship among the impact angles, impact positions, macroscopic geometry of impact damage and HCF strength of the damaged samples was studied. Results show that, the effect of impact damages on the HCF strength at different impact angles is not the same. When the impact damage appears at the edge of sample, the maximum decrease of HCF strength occurs in the impaction of 30°; while the impact damages appear at the middle of sample, the maximum decrease of HCF strength occurs in the impaction of 60°. In most cases, impact notches at the samples' edge compared to impact pits at the sample's intermediate surface have a more seriously effect on the HCF strength. However, at the impaction of 60°, the impact pit damage has a more serious effect. The geometry of the impact damage to a certain extent can characterize the changes of the HCF strength severity of damaged sample.

     

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    • References(17)
  • [1]
    国防科学技术工业委员会.GJB241-87航空涡轮喷气和涡轮风扇发动机通用规范[S].北京:国防科学技术工业委员会军标出版发行部,1987.
    [2]
    Cowles B A.High cycle fatigue in aircraft gas turbines:an industry perspective[J].International Journal of Fracture,1996,80(2/3):147-163.
    [3]
    North Atlantic Treaty Organization.Best practices for the mitigation and control of foreign[R].Research and Technology Organization,RTO TR-AVT-094,2005.
    [4]
    Martinez C M.Effects of ballistic impact damage on fatigue crack initiation in Ti-6Al-4V simulated engine blades[D].Dayton,Ohio:University of Dayton,2000.
    [5]
    Storace A F.Foreign object impact design criteria[R].Air Force Aerospace Propulsion Laboratory,AFAPL-TR-78-81.
    [6]
    Nicholas T,Barber J P,Bertke R S.Impact damage on titanium leading edges from small hard objects[J].Experimental Mechanics,1980,20(3):357-364.
    [7]
    Huber N.Plan to control high cycle fatigue in engines[R].San Antonio,Texas:USAF Structural Integrity Program Conference,1995.
    [8]
    Peters J O,Ritchie R O.Foreign object damage and high cycle fatigue:role of microstructure in Ti-6Al-4V[J].International Journal of Fatigue,2001,23(suppl.1):413-421.
    [9]
    Peters J O,Ritchie R O.Foreign object damage and high cycle fatigue of Ti-6Al-4V[J].Material Science and Engineering:A,2001,319/320/321:597-601.
    [10]
    Ruschau J,Nicholas T,Thompson S.Influence of foreign object damage (FOD) on the fatigue life of simulated Ti-6Al-4V airfoils[J].International Journal of Impact Engineering,2001,25(3):233-250.
    [11]
    Weeks C,Bastnagel P,Cook T,et al.FOD analytical modeling:FOD event modeling[R].Air Force Research Laboratory,AFRL-ML-WP-TR-2001-4159,2001.
    [12]
    国家标准化管理委员会.GB/T 13810-2007外科植入物用钛及钛合金加工材[S].北京:中国标准出版社,2007.
    [13]
    Nowell D,Duo,P,Stewart I F.Prediction of fatigue performance in gas turbine blades after foreign object damage[J].International Journal Fatigue,2003,25(9/10/11):963-969.
    [14]
    Dunham J M A,Mech G I E,Grad R.Damage to axial compressors[J].Journal of the Royal Aeronautical Society,1959,63:576-580.
    [15]
    国家标准化管理委员会.GB 3075-82 金属轴向疲劳试验方法[S].北京:中国标准出版社,1982.
    [16]
    高镇同.疲劳性能测试[M].北京:国防工业出版社,1980.
    [17]
    Maxwell D C,Nicholas T.A rapid method for generation of a haigh diagram for high cycle fatigue[R].ASME Paper STP 1332-EB,1999.
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