Tension and tensile fatigue tests of annealed and drawn Ta have been performed in vacuum at high temperature. Relations between tensile strength σ
B and fatigue strength for the annealed and the drawn Ta have been studied. The results obtained are as follows:
(1) Relation between σ
B and testing temperature
T in the range of 1073∼2273 K are approximately given by
(This article is not displayable. Please see full text pdf.)
\
oindentand a point of inflection appears in the lnσ
B-
T curve for the drawn Ta. Parameters
A and
B for the annealed Ta are 1.69×10
3 MPa and 2.17×10
−3 K
−1, and for the drawn Ta below 1600 K 8.40×10
3 MPa and 2.85×10
−3 K
−1, and above 1600 K 4.10×10
3 MPa and 2.40×10
−3 K
−1, respectively.
(2) Relations among fatigue life
N, cyclic tensile stress (of maximum value σ
o) and
T are approximately given by
(This article is not displayable. Please see full text pdf.)
\
oindentwhere
Ao and \Bar{
B} for the annealed Ta are 3.20×10
22 MPa
−\Bar{B} and –6.17, and \Bar{
B} for the drawn Ta –5.50 and
Ao 9.04×10
23 MPa
−\Bar{B} (below 1600 K) and 2.57×10
22 MPa
−\Bar{B} (above 1600 K). The inflection points in the lnσ
o-
T curves (for
N=constants) decrease to the lower temperature side with the increase of
N.
(3) The inflection points of the lnσ
B-
T and lnσ
o-
T curves for the drawn Ta are generated as the result of perfect recrystallization at about 1600 K. Below 2300 K, the tensile and fatigue strengths of the drawn Ta are higher than the strength for the annealed Ta. Above 2300 K, the strength of the drawn Ta is close to that of the annealed Ta, for the grain size of both materials approach the same level.
抄録全体を表示