2016
DOI: 10.1016/j.matdes.2016.03.102
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Effect of original layer thicknesses on the interface bonding and mechanical properties of Ti Al laminate composites

Abstract: It's of great significance in high-temperature aeroengine applications for large-surface-area Ti-Al laminate composites to be fabricated into Ti-Al 3 Ti parts by plastic forming and subsequent vacuum hot pressing. Then the original layer thicknesses have an important influence on the interface bonding and mechanical properties of Ti-Al laminate composites, but only few reports about it have been published so far. In the present study, vacuum hot pressing was employed to fabricate Ti-Al laminate composites usin… Show more

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Cited by 68 publications
(21 citation statements)
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“…wavy interface [1,4,15]. According to Figure 3b and 3c, the jet did not exist at the initial stage of the explosion, with the collision point moving forward, periodic wave structures were formed as the jetting appeared.…”
Section: Interface Morphology Of Composite Platementioning
confidence: 96%
See 4 more Smart Citations
“…wavy interface [1,4,15]. According to Figure 3b and 3c, the jet did not exist at the initial stage of the explosion, with the collision point moving forward, periodic wave structures were formed as the jetting appeared.…”
Section: Interface Morphology Of Composite Platementioning
confidence: 96%
“…In contrast, the bonding interface close to the detonation point showed a linear morphology (position "b"), while the bonding interface away from the detonation point achieved a wavy morphology (position "c"). It is generally accepted that the occurrence of jetting at the collision interface is one of the necessary conditions for the formation of a wavy interface [1,4,15]. According to Figure 3b,c, the jet did not exist at the initial stage of the explosion, with the collision point moving forward, periodic wave structures were formed as the jetting appeared.…”
Section: Interface Morphology Of Composite Platementioning
confidence: 96%
See 3 more Smart Citations