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Effects of high-temperature ambient on cyclic fatigue of La0.8Sr0.2MnO3+δ

Published online by Cambridge University Press:  15 August 2011

Makoto Tanaka*
Affiliation:
Japan Fine Ceramics Center, Atsuta-ku, Nagoya 456-8587, Japan
Tsuneaki Matsudaira
Affiliation:
Japan Fine Ceramics Center, Atsuta-ku, Nagoya 456-8587, Japan
Daisuke Igimi
Affiliation:
Japan Fine Ceramics Center, Atsuta-ku, Nagoya 456-8587, Japan
Satoshi Kitaoka
Affiliation:
Japan Fine Ceramics Center, Atsuta-ku, Nagoya 456-8587, Japan
*
a)Address all correspondence to this author. e-mail: m_tanaka@jfcc.or.jp

Abstract

The effects of water vapor and oxygen on the cyclic fatigue behavior of oxygen-excess La0.8Sr0.2MnO3+δ (LSM) were investigated under three-point bending at 1273 K. Because the fatigue life did not obviously depend on the number of cycles, which also represented the effective time of the applied stress, the fracture was presumed to not be significantly controlled by stress-corrosion cracking. Under a low oxygen partial pressure (${\rm{P}}_{{\rm{O}}_2 } $), however, wet exposure inhibited both fatigue fracture and permanent deformation, in which the LSM crystal lattice was distorted and the unit cell free volume was reduced. Under a high ${\rm{P}}_{{\rm{O}}_2 } $, on the contrary, the crystal symmetry was increased by the wet exposure. The inhibition of fatigue fracture and deformation at both high ${\rm{P}}_{{\rm{H}}_2 {\rm{O}}} $ and low ${\rm{P}}_{{\rm{O}}_2 } $ was probably caused by retardation of lanthanum diffusion through its vacancies.

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Copyright © Materials Research Society 2011
Figure 0

FIG. 1. Schematic of cyclic bending fatigue tests (notch depth: 0.4 mm; notch width: 0.17 mm).

Figure 1

FIG. 2. Typical permanent deformation profile on the tensile surface of a V-notched specimen that survived fatigue testing under Pmax = 58 N at 1273 K while the vicinity of the notch tip was exposed to a wet O2 atmosphere (${\rm{P}}_{{\rm{H}}_2 {\rm{O}}} $ = 4 × 103 Pa; ${\rm{P}}_{{\rm{O}}_2 } $ = 105 Pa).

Figure 2

FIG. 3. Specimen survival ratio during fatigue testing under Pmax = 60 N at 1273 K as a function of ${\rm{P}}_{{\rm{O}}_2 }$ around the notch tip; n is the number of specimens tested under each condition.

Figure 3

FIG. 4. Deformation ratio, D, of the specimens that survived fatigue tests under Pmax = 58 N at 1273 K as a function of ${\rm{P}}_{{\rm{O}}_2 } $ around the notch tip; n is the number of specimens tested under each condition.

Figure 4

FIG. 5. Scanning electron microscopy micrographs of fracture surfaces after bending tests on specimens that survived fatigue tests under Pmax = 58 N at 1273 K. The bending tests were carried out in the same environments as the fatigue tests: (a) dry Ar (${\rm{P}}_{{\rm{H}}_2 {\rm{O}}} $ = 10 Pa; ${\rm{P}}_{{\rm{O}}_2 } $ = 1.5 Pa), (b) wet Ar (${\rm{P}}_{{\rm{H}}_2 {\rm{O}}} $ = 4 × 103 Pa; ${\rm{P}}_{{\rm{O}}_2 } $ = 1.5 Pa). The broken lines and arrows in the micrographs indicate the edges of the V-notch and the crack propagation directions, respectively.

Figure 5

FIG. 6. Mean valence of Mn ions in La0.8Sr0.2MnO3+δ (LSM) powders exposed at 1273 K for 105 s as a function of ${\rm{P}}_{{\rm{O}}_2 } $.

Figure 6

TABLE I. Molar fractions of cations and vacancies occupying the A and B sites in La0.8Sr0.2MnO3+δ powders exposed at 1273 K for 105 s.

Figure 7

FIG. 7. Structural parameters for LSM powders exposed at 1273 K for 105 s as a function of ${\rm{P}}_{{\rm{O}}_2 } $.

Figure 8

TABLE II. Lattice parameters and the fitness agreement index (Rwp/Re) for LSM powders exposed at 1273 K for 105 s.

Figure 9

FIG. 8. Specimen survival ratio in fatigue tests under Pmax = 60 N at 1273 K as a function of Vf; n is the number of specimens tested under each condition.

Figure 10

FIG. 9. Deformation ratio D of specimens that survived fatigue tests under Pmax = 58 N at 1273 K as a function of Vf; n is the number of specimens tested under each condition.