Recovery of creep properties of alloy 625 after long term service

Mathew, M. D. ; Bhanu Sankara Rao, K. ; Mannan, S. L. ; Paknikar, K. ; Singh, Ranbir (2000) Recovery of creep properties of alloy 625 after long term service Key Engineering Materials, 171-174 . pp. 537-544. ISSN 1013-9826

Full text not available from this repository.

Official URL: http://www.scientific.net/KEM.171-174.537

Related URL: http://dx.doi.org/10.4028/www.scientific.net/KEM.171-174.537

Abstract

Creep rupture properties of alloy 625, that has been in service for 60,000 h at 993 K, have been evaluated between 923 and 1173 K, after subjecting the service exposed material to resolution annealing treatment at 1433 K for one hour. The isostress and Larson-Miller parameter methods were employed to estimate the residual life of the service exposed material. Creep rupture strength and rupture ductility recovered substantially following re-solution annealing. The variations in rupture life and rupture ductility with creep test variables have been rationalized on the basis of the microstructural changes that occurred in the material.

Item Type:Article
Source:Copyright of this article belongs to Trans Tech Publications Inc.
Keywords:Aging; Al Alloy 625; Creep; Delta-phase; Life Extension; Precipitation
ID Code:18325
Deposited On:17 Nov 2010 12:46
Last Modified:18 May 2011 06:15

Repository Staff Only: item control page