The Relative Susceptibility Of Four Commercial Titanium Alloys To Salt Stress Corrosion At 550 F PDF Download

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NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 306
Release: 1966
Genre:
ISBN:

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Salt Stress Corrosion of Residually Stressed Ti-8Al-1Mo-1V Alloy Sheet After Exposure at Elevated Temperatures

Salt Stress Corrosion of Residually Stressed Ti-8Al-1Mo-1V Alloy Sheet After Exposure at Elevated Temperatures
Author: Howard Benson Dexter
Publisher:
Total Pages: 28
Release: 1966
Genre: Titanium-aluminum-molybdenum-vanadium alloys
ISBN:

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An experimental investigation of the salt-stress-corrosion cracking of residually stressed Ti-8A1-1Mo-1V alloy sheet (duplex annealed) has been carried out.


Relative Susceptibility of Titanium Alloys to Hot-salt Stress-corrosion

Relative Susceptibility of Titanium Alloys to Hot-salt Stress-corrosion
Author: Hugh R. Gray
Publisher:
Total Pages: 68
Release: 1971
Genre: Corrosion and anti-corrosives
ISBN:

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Susceptibility of titanium alloys to hot-salt stress-corrosion cracking increased as follows: Ti-2Al-11Sn-5Zr-0.2Si(679), Ti-6Al-2Sn-4Zr-2Mo(6242), Ti-6Al-4V(64), Ti-6Al-4V-3Co(643), Ti-8Al-1Mo-1V(811), and Ti-13V-11Cr-3A1(13-11-3). The Ti-5Al-6Sn-2Zr-1Mo-0.25Si(5621S) alloy was both the least and most susceptible depending on heat treatment. Such rankings can be drastically altered by heat-to-heat and processing variations. Residual compressive stresses and cyclic exposures also reduce susceptibility to stress-corrosion. Simulated turbine-engine compressor environmental variables such as air velocity, pressure, dewpoint, salt concentration, and salt deposition temperature have only minor effects. Detection of substantial concentrations of hydrogen in all corroded alloys confirmed the existence of a hydrogen embrittlement mechanism.--P. [i].


The Ti-8A1-1Mo-1V Alloy

The Ti-8A1-1Mo-1V Alloy
Author: R. A. Wood
Publisher:
Total Pages: 120
Release: 1965
Genre: Titanium alloys
ISBN:

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