THE STRESS RELIEF OF TITANIUM WELDS FOR LOW-TEMPERATURE APPLICATIONS

reportActive / Technical Report | Accession Number: AD0609350 | Open PDF

Abstract:

Stress-relaxation annealing times and temperatures for different alloys are presented. The actual temperature and time should be determined for each heat of base metal, base-metal filler-metal combination, base-metal condition, and weld structure because they can vary with any or all of these variables.

Author(s):
Evans, R. M.
Author Organization(s):
BATTELLE MEMORIAL INST COLUMBUS OH DEFENSE METALS INFORMATION CENTER
Descriptive Note:
Technical note
Pagination:
0007

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release, Document Partially Illegible
Distribution Statement:
Approved For Public Release; Distribution Is Unlimited. Document Partially Illegible.

RECORD

Collection: TR
Identifying Numbers
Monitor Series:
DMIC
 Subject Terms
Joint Capability Areas:
JCA_6.4.1_Secure Information Exchange; JCA_1_Force Support; JCA_6_Net Centric; JCA_1.2_Force Preparation; JCA_6.4_Information Assurance
Communities of Interest:
Air Platforms
Descriptor(s):
*TITANIUM, *TITANIUM ALLOYS, *WELDING, STRESSES, TEMPERATURE, LOW TEMPERATURE, ALUMINUM ALLOYS, VANADIUM ALLOYS, TIN ALLOYS, TENSILE PROPERTIES, ELASTIC PROPERTIES, FRACTURE(MECHANICS), HEAT TREATMENT, WELDS
Field(s)/Group(s):
Couplers, Fasteners and Joints, Fabrication Metallurgy
Keyword(s):
TITANIUM ALLOY 5AL 2 5SN, TITANIUM ALLOY 6AL 4V
Report Date:
1964 May 26