ENVIRONMENTAL FATIGUE OF AN AL-LI-CU ALLOY .1. INTRINSIC CRACK-PROPAGATION KINETICS IN HYDROGENOUS ENVIRONMENTS

被引:75
作者
PIASCIK, RS [1 ]
GANGLOFF, RP [1 ]
机构
[1] UNIV VIRGINIA,DEPT MAT SCI,CHARLOTTESVILLE,VA 22903
来源
METALLURGICAL TRANSACTIONS A-PHYSICAL METALLURGY AND MATERIALS SCIENCE | 1991年 / 22卷 / 10期
关键词
D O I
10.1007/BF02665008
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Deleterious environmental effects on steady-state, intrinsic fatigue crack propagation (FCP) rates (da/dN) in peak-aged Al-Li-Cu alloy 2090 are established by electrical potential monitoring of short cracks with programmed constant DELTA-K and K(max) loading. Such rates are equally unaffected by vacuum, purified helium, and oxygen but are accelerated in order of decreasing effectiveness by aqueous 1 pct NaCl with anodic polarization, pure water vapor, moist air, and NaCl with cathodic polarization. While da/dN depend on DELTA-K4.0 for the inert gases, water vapor and chloride induce multiple power laws and a transition growth rate "plateau." Environmental effects are strongest at low DELTA-K. Crack tip damage is ascribed to hydrogen embrittlement because of accelerated da/dN due to parts-per-million (ppm) levels of H2O without condensation, impeded molecular flow model predictions of the measured water vapor pressure dependence of da/dN as affected by mean crack opening, the lack of an effect of film-forming O2, the likelihood for crack tip hydrogen production in NaCl, and the environmental and DELTA-K-process zone volume dependencies of the microscopic cracking modes. For NaCl, growth rates decrease with decreasing loading frequency, with the addition of passivating Li2CO3 and upon cathodic polarization. These variables increase crack surface film stability to reduce hydrogen entry efficiency. Small crack effects are not observed for 2090; such cracks do not grow at abnormally high rates in single grains or in NaCl and are not arrested at grain boundaries. The hydrogen environmental FCP resistance of 2090 is similar to other 2000 series alloys and is better than 7075.
引用
收藏
页码:2415 / 2428
页数:14
相关论文
共 86 条
[1]  
ALIAGA D, 1981, AGARDCP616 REP
[2]  
BARKER C, 1986, ALUMINUM LITHIUM ALL, V3
[3]  
BOGAR FD, 1977, NRL8153 NAV RES LAB
[4]  
BRADSHAW FJ, 1969, INT J FRACTURE, V5, P255
[5]   LOCALIZED CORROSION BEHAVIOR OF ALLOY-2090 - THE ROLE OF MICROSTRUCTURAL HETEROGENEITY [J].
BUCHHEIT, RG ;
MORAN, JP ;
STONER, GE .
CORROSION, 1990, 46 (08) :610-617
[6]  
BUCHHEIT RG, 1991, NACE99 PAP
[7]   EFFECT OF GERMANIUM ADDITIONS ON THE CORROSION BEHAVIOR OF AN AILI ALLOY [J].
COLVIN, EL ;
CAHEN, GL ;
STONER, GE ;
STARKE, EA .
CORROSION, 1986, 42 (07) :416-421
[8]  
CRAIG JG, 1987, J PHYS COLLOQ C S9, V3, P825
[9]  
Davidson D. L., 1983, ASTM STP, P371
[10]   THE EFFECTS OF ALUMINUM-ALLOY MICROSTRUCTURE ON FATIGUE CRACK-GROWTH [J].
DAVIDSON, DL ;
LANKFORD, J .
MATERIALS SCIENCE AND ENGINEERING, 1985, 74 (02) :189-199