Cyclic creep rupture behavior of three high temperature alloys
Tensile stress and tensile time-to-rupture relation determined from cyclic creep rupture tests on high temperature titanium alloy, cobalt alloy, and stainless steel
Engineering topics
Publications and source records attributed to Halford, G. R..
Tensile stress and tensile time-to-rupture relation determined from cyclic creep rupture tests on high temperature titanium alloy, cobalt alloy, and stainless steel
Creep-fatigue analysis by strain range partitioning, considering metals inelastic deformation at high temperature due to plastic flow
Strain range components and creep fatigue behavior of metals related independently to cyclic life by equations in both tension and compression
The framework of a new method is outlined for treating creep-fatigue behavior of metals. Inelastic strain-ranges are partitioned into the components of (1) completely reversed plasticity, (2) tensile plasticity reversed by compressive creep, or tensile creep reversed by compressive plasticity, and (3) completely reversed creep. Each of these components is shown to be related to cyclic life by a Manson-Coffin type power-law equation. A linear life fraction rule is used to combine the damaging effects of the individual components enabling the prediction of life. Test results are presented for a 2.25 Cr-1 Mo steel as well as limited information for a Type 316 stainless steel.
The significance of the role that creep can play in governing high-temperature, low-cycle fatigue resistance is investigated by conducting strain cycling tests on two high-temperature stainless steel alloys and making concurrent measurements of stress, temperature, and strain at various frequencies. The results are then analyzed in terms of damage imposed by creep and fatigue components. It is shown that creep can play an important and sometimes dominant role in low cycle fatigue at high temperatures. The results of the study include the findings that: (1) the simple life-fraction theory described is adequate for calculating creep damage when the cyclic creep rupture curve is used as a basis for analysis; (2) a method of universal slopes originally developed for room temperature use is sufficiently accurate at high temperature to be used to calculate pure fatigue damage; and (3) a linear creep-fatigue damage rule can explain the transitions observed from one failure mode to another.
Metal alloys high temperature low cycle strain fatigue resistance in creep range estimated from tensile and stress rupture data
High temperature low cycle creep range strain fatigue behavior estimation from tensile and stress rupture properties
Method of estimating high temperature, low-cycle strain fatigue behavior of materials from tensile and stress-rupture properties