NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
External stress-corrosion cracking of a 1.22-m-diameter type 316 stainless steel air valveAn investigation was conducted to determine the cause of the failure of a massive AISI Type 316 stainless steel valve which controlled combustion air to a jet engine test facility. Several through-the-wall cracks were present near welded joints in the valve skirt. The valve had been in outdoor service for 18 years. Samples were taken in the cracked regions for metallographic and chemical analyses. Insulating material and sources of water mist in the vicinity of the failed valve were analyzed for chlorides. A scanning electron microscope was used to determine whether foreign elements were present in a crack. On the basis of the information generated, the failure was characterized as external stress-corrosion cracking. The cracking resulted from a combination of residual tensile stress from welding and the presence of aqueous chlorides. Recommended countermeasures are included.
Document ID
19930017012
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Moore, Thomas J.
(NASA Lewis Research Center Cleveland, OH, United States)
Telesman, Jack
(NASA Lewis Research Center Cleveland, OH, United States)
Moore, Allan S.
(NASA Lewis Research Center Cleveland, OH, United States)
Johnson, Dereck F.
(NASA Lewis Research Center Cleveland, OH, United States)
Kuivinen, David E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1993
Subject Category
Metallic Materials
Report/Patent Number
E-6810
NAS 1.60:3190
NASA-TP-3190
Report Number: E-6810
Report Number: NAS 1.60:3190
Report Number: NASA-TP-3190
Accession Number
93N26201
Funding Number(s)
PROJECT: RTOP 505-62-84
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available