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Evaluation of a hydrogen resistant titanium aluminide alloyThe Ti-24Al-11Nb (Ti-24-11) alloy heat treated to the fine basketweave microstructure was shown previously to be hydrogen tolerant. In order to assess its limit of hydrogen tolerance, the tensile, creep, fracture toughness, and sustained load crack growth behaviors of this alloy were studied as a function of hydrogen content. All test specimens were thermally charged with internal hydrogen and tested at 25 and 600 C. Coupon specimens were used for developing the hydrogen charging procedures and for studying compatibility of the alloy with high temperature, high pressure gaseous hydrogen. The mechanical test results indicated that the fine basketweave microstructure was tolerant to hydride embrittlement for hydrogen contents up to approximately 1500 wt. ppm, providing that the hydride formed was of the TiH2 type. On the other hand, hydrogen charging experiments indicated that the Ti-24-11 alloy was severely cracked and pulverized under zero load when the hydrogen content exceeded 3000 wt. ppm. X-ray diffraction results revealed that the dichotomous behaviors might be due to the formation of TiH(1.924) type hydrides at higher hydrogen contents. Thus, hydrogen embrittlement in the Ti-24-11 alloy with the fine basketweave microstructure depends on hydrogen content and the nature of the hydrides formed.
Document ID
19920006869
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chan, K. S.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Subject Category
Metallic Materials
Report/Patent Number
NAS 1.26:189769
NASA-CR-189769
Report Number: NAS 1.26:189769
Report Number: NASA-CR-189769
Accession Number
92N16087
Funding Number(s)
CONTRACT_GRANT: NAG2-683
PROJECT: SWRI PROJ. 3943
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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