Retrogression, reaging and residual stresses in 7010 forgings

J. S. Robinson; D. A. Tanner; S. D. Whelan

doi:10.1046/j.1460-2695.1999.00137.x

Retrogression, reaging and residual stresses in 7010 forgings

J. S. Robinson
, D. A. Tanner
, S. D. Whelan

School of Engineering

Aluminium Corporation

Research output: Contribution to journal › Article › peer-review

Abstract

Open die forgings of the aluminum alloy 7010 (DTD5636) have been retrogressed at temperatures between 200 and 240 °C and then reaged (RRA). Tensile, fracture toughness and stress corrosion cracking values are reported. Retrogression at 200 °C offers the most promising combination of properties, and the long retrogression time of approx. 2500 s will enable thick sections to be treated. Residual stresses induced during quenching are also predicted, and initial experimental results suggest that some stress relief occurs during the retrogression heat treatment.

Original language	English
Pages (from-to)	51-58
Number of pages	8
Journal	Fatigue and Fracture of Engineering Materials and Structures
Volume	22
Issue number	1
DOIs	https://doi.org/10.1046/j.1460-2695.1999.00137.x
Publication status	Published - Jan 1999

Access to Document

10.1046/j.1460-2695.1999.00137.x

Cite this

@article{52a981ec86284bb0a6add009e752776d,

title = "Retrogression, reaging and residual stresses in 7010 forgings",

abstract = "Open die forgings of the aluminum alloy 7010 (DTD5636) have been retrogressed at temperatures between 200 and 240 °C and then reaged (RRA). Tensile, fracture toughness and stress corrosion cracking values are reported. Retrogression at 200 °C offers the most promising combination of properties, and the long retrogression time of approx. 2500 s will enable thick sections to be treated. Residual stresses induced during quenching are also predicted, and initial experimental results suggest that some stress relief occurs during the retrogression heat treatment.",

author = "Robinson, \{J. S.\} and Tanner, \{D. A.\} and Whelan, \{S. D.\}",

year = "1999",

month = jan,

doi = "10.1046/j.1460-2695.1999.00137.x",

language = "English",

volume = "22",

pages = "51--58",

journal = "Fatigue and Fracture of Engineering Materials and Structures",

issn = "8756-758X",

number = "1",

}

TY - JOUR

T1 - Retrogression, reaging and residual stresses in 7010 forgings

AU - Robinson, J. S.

AU - Tanner, D. A.

AU - Whelan, S. D.

PY - 1999/1

Y1 - 1999/1

N2 - Open die forgings of the aluminum alloy 7010 (DTD5636) have been retrogressed at temperatures between 200 and 240 °C and then reaged (RRA). Tensile, fracture toughness and stress corrosion cracking values are reported. Retrogression at 200 °C offers the most promising combination of properties, and the long retrogression time of approx. 2500 s will enable thick sections to be treated. Residual stresses induced during quenching are also predicted, and initial experimental results suggest that some stress relief occurs during the retrogression heat treatment.

AB - Open die forgings of the aluminum alloy 7010 (DTD5636) have been retrogressed at temperatures between 200 and 240 °C and then reaged (RRA). Tensile, fracture toughness and stress corrosion cracking values are reported. Retrogression at 200 °C offers the most promising combination of properties, and the long retrogression time of approx. 2500 s will enable thick sections to be treated. Residual stresses induced during quenching are also predicted, and initial experimental results suggest that some stress relief occurs during the retrogression heat treatment.

UR - https://www.scopus.com/pages/publications/0032629835

U2 - 10.1046/j.1460-2695.1999.00137.x

DO - 10.1046/j.1460-2695.1999.00137.x

M3 - Article

AN - SCOPUS:0032629835

SN - 8756-758X

VL - 22

SP - 51

EP - 58

JO - Fatigue and Fracture of Engineering Materials and Structures

JF - Fatigue and Fracture of Engineering Materials and Structures

IS - 1

ER -

Retrogression, reaging and residual stresses in 7010 forgings

Abstract

Access to Document

Other files and links

Fingerprint

Cite this