Elsevier

Intermetallics

Volume 9, Issues 10–11, October–November 2001, Pages 963-969
Intermetallics

Primary creep of Ni3(Al, Ta) in the anomalous flow regime

https://doi.org/10.1016/S0966-9795(01)00097-8Get rights and content

Abstract

The primary creep behavior of single-slip oriented Ni3(Al, Ta) has been characterized at low temperatures in the anomalous flow regime. For temperatures ranging from 20 to 200 °C, transient creep leading to eventual exhaustion has been measured at all stresses. The decline in the creep rate has been quantitatively shown to occur more quickly than in common metals, as the decline in the creep rate is faster than predicted by the logarithmic creep law. In addition, the temperature dependence of the primary creep behavior is consistent with the flow stress anomaly, as the measured amount of creep strain at a fixed stress decreases with increasing temperature.

Introduction

In this paper we present the results of a series of low-temperature tension creep experiments performed on single-slip oriented Ni3(Al, Ta) single crystals. We have tested these crystals at temperatures between 20 and 200 °C to further explore the active deformation mechanisms at low temperatures in the anomalous flow regime, where the flow stress and work-hardening rate are observed to have an anomalous temperature dependence. These test temperatures range from 0.18 to 0.28 of the melting temperature. Creep experiments are usually not performed at such low homologous temperatures, because the mechanical response of most metals is usually insensitive to time below temperatures of 0.3 Tm. However, time-dependent plastic flow does occur in all metals, even at temperatures as low as 4 K [1], [2], [3]. Low-temperature creep is often not considered as a viable failure mechanism, as creep strains at low temperatures are small and quickly terminate, so that failure due to low-temperature creep is unlikely (but for problems of dimensional stability, such creep effects can be of engineering importance). In the context of the present paper, creep experiments at low homologous temperatures provide a conceptually simple test method to investigate the active deformation mechanisms, and it is in this spirit that we explore the low-temperature creep properties of Ni3Al.

In contrast to conventional high-temperature creep experiments in which the applied stress is typically below the yield stress, most low-temperature creep experiments are performed at stresses above the yield stress in order to produce a measurable amount of creep strain. Upon loading, a sample undergoes plastic deformation characterized by two components: an instantaneous part and a time-dependent part. In general, the time-dependent strain is small compared to the instantaneous plastic response; however, in measuring the creep properties we ignore the initial strain component and focus solely on the time-dependent plastic response.

Equations that describe the form of the creep curve have been empirically derived for low-temperature creep. Unlike high-temperature creep where the creep processes may be characterized by a single value—the steady-state creep rate—the relations that characterize low-temperature creep must reflect the continuous decline in the creep rate with time. For most metals at low temperatures, it is found that the change in the creep rate (γ̇) with time (t) can be represented by the following equation [4]:γ̇=At−nwhere A and n are constants, and where 0⩽n⩽1. In the special case of logarithmic creep, the constant n is equal to 1, and integration of Eq. (1) produces the logarithmic creep law, which can be expressed in the modified form shown below:γ=γ0lnβt+1,where γ is the creep strain, γ0 is the instantaneous strain, α and β are constants, and t is measured from the time at which the strain is equal to γ0. Eq. (2) clearly demonstrates that the creep strain declines both quickly and monotonically with time.

Section snippets

Experimental procedure

Single crystal tension specimens of Ni75Al24Ta1 were prepared by electrode discharge machining (EDM) from a bulk single crystal, where the sample axis was oriented within 2° of the 〈123〉 direction. Each sample was vacuum annealed at 1250 °C for 2 h, after which all surfaces were wet ground using 400 and 600 grit SiC paper. This was followed by electropolishing for 30 s in a bath composed of ethanol and 10 vol.% perchloric acid at −10 °C and 25 V.

The creep experiments in this study were

Results

The data from a representative incremental creep test are shown in Fig. 1, and the incremental nature of these creep tests is readily apparent. In Fig. 1a, it appears that all of the plastic strain is time-independent, occurring instantaneously in response to each increment in the applied stress. However, closer examination of a single stress-increment test reveals the existence of a limited amount of time-dependent strain (see Fig. 1b). Note that in Fig. 1b, all of the strain displayed in this

Discussion

We have shown in the previous section that the transient creep behavior of Ni3Al is unlike the low-temperature creep behavior of any reported metal, and this is perhaps to be expected in view of all of the other unusual mechanical properties that Ni3Al exhibits in this temperature regime. In analyzing the data, we found it convenient to characterize the form of the primary creep curve with a simple power-law relation. However, this power-law curve fit is simply an empirical construct that does

Conclusion

We conclude with a few observations about the primary creep data shown in this study.

  • We believe that these creep experiments explore the same deformation mechanisms that are responsible for the anomalous temperature dependence of the flow stress. In Fig. 7, it is clear that the amount of creep strain and total strain decrease with increasing temperature.

  • This is the first time that a primary creep curve has been quantitatively shown to decrease at a rate faster than predicted by the logarithmic

Acknowledgements

This work was supported by the Air Force Office of Scientific Research under AFOSR Grant Number AF-F49620-95-1-0163, the Department of Energy under Sandia Grant LB-4572, and the National Science Foundation under Grant DMR-970342 and through graduate fellowship for M.D.U.

References (12)

  • R.P Reed et al.

    Mater. Sci. Eng.

    (1991)
  • D.C Chrzan et al.

    Mater. Sci. Eng. A

    (1993)
  • D.C Chrzan et al.

    Mater. Sci. Eng.

    (1995)
  • J.W Glen

    Phil. Mag.

    (1955)
  • G.I Kirichenko et al.

    Phys. Met. Metall.

    (1982)
  • A Graham

    Research

    (1952)
There are more references available in the full text version of this article.

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