Zobrazeno 1 - 10
of 13
pro vyhledávání: '"Hiromasa Sasa"'
Autor:
Asato Kobun, Yohei Masuda, Shun Miura, Hiroshi Miyazaki, Koichi Yoshida, Seiki Sato, Hiromasa Sasa, Masataka Iwakuma
Publikováno v:
IEEE Transactions on Applied Superconductivity. 33:1-6
Autor:
Shun Miura, Asato Kobun, Yohei Masuda, Kazuki Nakamura, Hiroshi Miyazaki, Akifumi Kawagoe, Hiromasa Sasa, Koichi Yoshida, Seiki Sato, Masataka Iwakuma
Publikováno v:
IEEE Transactions on Applied Superconductivity. 33:1-6
Autor:
Atsushi Takashima, Yuki Onamyuda, Asato Kobun, Hiroshi Miyazaki, Akifumi Kawagoe, Shun Miura, Koichi Yoshida, Seiki Sato, Hiromasa Sasa, Masataka Iwakuma
Publikováno v:
IEEE Transactions on Applied Superconductivity. 33:1-5
Autor:
Yuta Okade, Hiroshi Miyazaki, Hiromasa Sasa, Koichi Yoshida, Shun Miura, Teruyoshi Sasayama, Takashi Yoshida, Akifumi Kawagoe, Masataka Iwakuma
Publikováno v:
IEEE Transactions on Applied Superconductivity. 32:1-6
Publikováno v:
IEEE Transactions on Applied Superconductivity. 32:1-5
Autor:
Akira Tomioka, Yuichiro Sasamori, Takashi Yoshida, Hiromasa Sasa, S. Sato, Masayuki Konno, Shun Miura, Masataka Iwakuma, Miyuki Nakamura, Y. Aoki, Teruyoshi Sasayama, Sergey Lee, Kaoru Yamamoto, Teruo Izumi, Takahiro Umeno, Shinya Hasuo, Koichi Yoshida, Akifumi Kawagoe, Masao Syutoh, Takayo Hasegawa, Y. Hase, Hirokazu Honda
Publikováno v:
IEEE Transactions on Applied Superconductivity. 31:1-6
For the development of electric propulsion aircrafts with light weight, low emission and high efficiency, MW-class fully superconducting synchronous machines operating at liquid nitrogen temperature were conceptually designed with REBa2Cu3O7- δ (REB
Autor:
Teruyoshi Sasayama, Masataka Komiya, Masataka Iwakuma, Ryota Sugouchi, Kaoru Yamamoto, Shun Miura, Hiromasa Sasa, Masayuki Konno, Akira Tomioka, Teruo Izumi, Takashi Yoshida
Publikováno v:
IEEE Transactions on Applied Superconductivity. 30:1-7
Currently, feasibility studies on fully turboelectric propulsion systems for electric aircrafts are being conducted worldwide. A fully superconducting rotating machine can realize fully turboelectric propulsion systems with light weight and high powe
Autor:
Hiromasa Sasa, Teruyoshi Sasayama, Teruo Izumi, Takuya Aikawa, Masayuki Konno, Shun Miura, Akira Tomioka, Masataka Iwakuma, Masataka Komiya, Takashi Yoshida
Publikováno v:
IEEE Transactions on Applied Superconductivity. 29:1-6
Future aircraft are expected to have low noise pollution, low emission, and low fuel consumption. A fully turbo-electric propulsion system was proposed by NASA with these aims. The advantages of fully superconducting rotating machines are their weigh
Autor:
Kaito Noda, Hiromasa Sasa, Hiroshi Miyazaki, Shun Miura, Takashi Yoshida, Teruyoshi Sasayama, Masataka Iwakuma, Akifumi Kawagoe, Teruo Izumi, Masayuki Konno, Yuichiro Sasamori, Hirokazu Honda, Yoshiji Hase, Masao Shutoh
Publikováno v:
Journal of Physics: Conference Series. 2323:012037
Generators used in electric aircraft require a high-power density, and AC loss is also a significant problem. We designed 10 MW REBCO superconducting synchronous generators at 64 K to achieve a power density of 20 kW/kg and low AC loss. In this study
Autor:
Hiromasa Sasa, Shun Miura, Hiroshi Miyazaki, Teruyoshi Sasayama, Takashi Yoshida, Kaoru Yamamoto, Masataka Iwakuma, Yoshiji Hase, Yuichiro Sasamori, Hirokazu Honda, Msayuki Konno, Teruo Izumi
Publikováno v:
IEEE Transactions on Applied Superconductivity. :1-1