Zobrazeno 1 - 9
of 9
pro vyhledávání: '"thin film sulphuric acid anodizing"'
Publikováno v:
Metals, Vol 11, Iss 4, p 644 (2021)
The feasibility for friction stir welding (FSW) surface-treated AA2099-T83 aluminium extrusions with AA2060-T8E30 aluminium sheets in the overlap configuration and using a sealant at the interface was investigated in this work. New Cr-free surface tr
Externí odkaz:
https://doaj.org/article/43269fffab87445ca0b367b9e7def564
Autor:
Liu, Junyi1 (AUTHOR), Huang, Xiaohu1 (AUTHOR), Ren, Yi1 (AUTHOR), Wong, Lai Mun1 (AUTHOR), Liu, Hongfei1 (AUTHOR), Wang, Shijie1 (AUTHOR) sj-wang@imre.a-star.edu.sg
Publikováno v:
Scientific Reports. 3/16/2022, Vol. 12 Issue 1, p1-10. 10p.
Akademický článek
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Autor:
Karanika, Alexandra, Carelas, Evangelos, Aldanondo, Egoitz, Idel, Snir, Abramoivich, Alexander, Geest, Marc Van Der, Visser, Peter
Publikováno v:
Journal of Physics: Conference Series; 2024, Vol. 2716 Issue 1, p1-8, 8p
Publikováno v:
Scientific Reports, Vol 12, Iss 1, Pp 1-10 (2022)
Abstract Al-alloy/carbon fibre reinforced polymer (CFRP) joint systems offer exceptionally lightweight, superior fatigue behaviour and impact resistance for aerospace applications. Nevertheless, the galvanic corrosion at the joint interfaces accelera
Externí odkaz:
https://doaj.org/article/ad793c7228604aac9d8d6a111834fa21
Publikováno v:
Journal of Manufacturing & Materials Processing; Oct2022, Vol. 6 Issue 5, p94-N.PAG, 15p
Publikováno v:
Scientific reports. 12(1)
Al-alloy/carbon fibre reinforced polymer (CFRP) joint systems offer exceptionally lightweight, superior fatigue behaviour and impact resistance for aerospace applications. Nevertheless, the galvanic corrosion at the joint interfaces accelerates the a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a6a1ead1926f690ecbb9e61d0c9db017
https://pubmed.ncbi.nlm.nih.gov/35296790
https://pubmed.ncbi.nlm.nih.gov/35296790
Publikováno v:
Procedia Structural Integrity
Innovative, last generation Al-Li alloys were evaluated in terms of mechanical performance and corrosion protection in order to be used in aircraft structures. Involved alloys are AA2060 and AA2198, where tensile, fatigue, rolling and formability tes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d92bfc0d4a47132823f143f66cdf866d
https://doi.org/10.1016/j.prostr.2018.09.010
https://doi.org/10.1016/j.prostr.2018.09.010
Publikováno v:
Journal of Adhesion; Feb2010, Vol. 86 Issue 2, p192-221, 30p, 1 Black and White Photograph, 4 Diagrams, 13 Charts, 3 Graphs