Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Manabu Nakai"'
Publikováno v:
Materials Science Forum. 879:2153-2157
The 7000 series alloys have the highest strength in the aluminum alloys, but lower fatigue properties than 2000 series alloys. Thus, 7000 series alloys are not applied to a large proportion of the aircraft components. However, the mechanism for this
Publikováno v:
Journal of the Japan Institute of Metals. 80:745-752
Autor:
Goroh Itoh, Manabu Nakai
Publikováno v:
Journal of Japan Institute of Light Metals. 65:123-130
Autor:
Manabu Nakai, Goroh Itoh
Publikováno v:
MATERIALS TRANSACTIONS. 55:114-119
The relationship between the microstructure and the yield strength after T6 tempering was investigated using 6061 aluminum alloy manufactured at various levels of temperature and strain rate during hot forging. Non-recrystallized structures (continuo
Publikováno v:
Journal of Japan Institute of Light Metals. 60:19-25
For medium-strength aluminum alloys 7003 and 7N01 having average (symbolized with S) or upper limit (symbolized with H) in the contents specified in JIS, SSRT tests were carried out in humid air with 90% relative humidity by using a smooth tensile sp
Autor:
Takehiko Eto, Manabu Nakai
Publikováno v:
Materials Science Forum. :3643-3648
New affordable 2024 series aerospace aluminum alloy has been developed. Fracture toughness has been demonstrated increase in inverse proportion to the root of the distance between constituents, Cu2FeAl7, formed during ingot solidification. Higher fra
Fatigue crack growth behaviour of high strength aluminum alloys for aircraft components was studied experimentally in relation to testing environment. Crack path was mainly transgranular. Crack growth rate was slightly larger in 7075-type alloy with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1948e406b25f373d3dda532b43f0a3bb
https://doi.org/10.1533/9780081002254.123
https://doi.org/10.1533/9780081002254.123
Publikováno v:
Journal of Japan Institute of Light Metals. 51:222-227
Stress corrosion cracking (SCC) behaviors of extruded 7050 series aluminum alloys in T6 and RRA (Retrogression and re-aging) tempers were studied as compared with that of the conventional 7075 aluminum alloy. 7050 and 7055 aluminum alloys in T6 showe
Autor:
Manabu Nakai, Takehiko Eto
Publikováno v:
Materials Science and Engineering: A. 285:62-68
New aspect of developing the materials in lights of interrelationship among alloy/process microstructure (mainly the second phase particles) — properties combined with micromechanics has been carried out in 2024 aluminum alloys. The fracture toughn