Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Ozan Can Ozaner"'
Autor:
Ozan Can Ozaner, Angshuman Kapil, Yuji Sato, Yoshihiko Hayashi, Keiichiro Ikeda, Tetsuo Suga, Masahiro Tsukamoto, Sener Karabulut, Musa Bilgin, Abhay Sharma
Publikováno v:
Lubricants, Vol 11, Iss 12, p 523 (2023)
Inconel 718 (IN718), a Ni-based superalloy, is immensely popular in the aerospace, nuclear, and chemical industries. In these industrial fields, IN718 parts fabricated using conventional and additive manufacturing routes require subsequent machining
Externí odkaz:
https://doaj.org/article/273ba88932a344528a20ad4438e20659
Publikováno v:
Materials, Vol 16, Iss 5, p 2055 (2023)
Wire and arc additive manufacturing (WAAM) technology has recently become attractive due to the fact of its high production capacity and flexible deposition strategy. One of the most prominent drawbacks of WAAM is surface irregularity. Therefore, WAA
Externí odkaz:
https://doaj.org/article/2c2c7a4e92214672a5ac368fdf745244
Publikováno v:
Journal of Manufacturing Processes. 79:47-59
In this study, Inconel 939 turbine blade fir tree samples were fabricated by the additive manufacturing method using a direct metal laser sintering (DMLS) machine. This critical gas turbine connection part requires high geometric accuracy and excelle
Publikováno v:
Materials Today: Proceedings. 38:1861-1865
Inconel 939 is nickel-based superalloy which offers remarkable material characteristics at high temperature applications. It is therefore mainly used in hot section of gas turbine engines parts that require high temperature corrosion resistance and c
Publikováno v:
Procedia CIRP. 87:31-34
This research focuses on experimental studies on Inconel 939, which is a material used in aerospace applications where more commonly preferred Inconel 718 is not usable due to high-temperatures. Inconel 939 parts are often wrought or cast, while the
Autor:
Ozan Can Ozaner, Ronan Martin, Cansinem Tuzemen, Aydemir Gunaydin, Jérémie Diboine, Levent Subasi
Publikováno v:
Journal of Laser Applications. 33:012015
The hot section parts in a gas turbine are subject to high working temperatures and mechanical forces. In order to endure the harsh conditions, these parts are generally made of nickel-based superalloys. Furthermore, microholes are drilled on them to