Modern Developments in Powder Metallurgy 1966
DOI: 10.1007/978-1-4684-7712-2_15
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Powder Metallurgy Applications in Space Vehicle Systems

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“…Finally, the hardness values shown in Fig. 12 are similar to those found in other work starting from prealloyed hydride-dehydride or PREP powders [13] or the ␣ + ␤ Ti-6Al-7Nb alloy processed by means of vacuum hot-pressing under similar processing conditions [14]. Moreover, the final hardness of vacuum hotpressed Ti-6Al-4V materials is generally higher than the nominal values of 321 HV of the wrought alloy [16], even though of some residual porosity, due to the greater amount of oxygen dissolved in the hot-pressed specimens (at least 0.42 wt.%) in comparison to the value specified for the wrought alloy (0.20 wt.%).…”
Section: Resultssupporting
confidence: 86%
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“…Finally, the hardness values shown in Fig. 12 are similar to those found in other work starting from prealloyed hydride-dehydride or PREP powders [13] or the ␣ + ␤ Ti-6Al-7Nb alloy processed by means of vacuum hot-pressing under similar processing conditions [14]. Moreover, the final hardness of vacuum hotpressed Ti-6Al-4V materials is generally higher than the nominal values of 321 HV of the wrought alloy [16], even though of some residual porosity, due to the greater amount of oxygen dissolved in the hot-pressed specimens (at least 0.42 wt.%) in comparison to the value specified for the wrought alloy (0.20 wt.%).…”
Section: Resultssupporting
confidence: 86%
“…The values shown in Fig. 2, which are comparable to that of other author when processing the Ti-6Al-4V alloy [13] or the Ti-6Al-7Nb alloy [14] by vacuum hot-pressing or by inductive hot-pressing [15], are higher that those obtained from conventional pressing and sintering process, approximately 95% of the theoretical density [12]. Fig.…”
Section: Resultssupporting
confidence: 81%