Zobrazeno 1 - 10
of 11
pro vyhledávání: '"Maho Matsukura"'
Publikováno v:
Journal of Spacecraft and Rockets. 59:342-347
Publikováno v:
2022 Wireless Power Week (WPW).
Publikováno v:
2022 Wireless Power Week (WPW).
Autor:
Tsuyoshi Imai, Maho Matsukura, Shigeru Yokota, Tsuyoshi Kariya, Kaisei Miyawaki, Kohei Shimamura, Naoto Ozaki, Ryutaro Minami
Publikováno v:
Journal of Spacecraft and Rockets. 57:632-635
Publikováno v:
2021 IEEE Asia-Pacific Microwave Conference (APMC).
Autor:
Ryoma Moro, Masafumi Fukunari, Koichi Mori, Maho Matsukura, Kota Motozuka, Kohei Shimamura, Naoki Keicho
Publikováno v:
2021 IEEE Wireless Power Transfer Conference (WPTC).
28 GHz microwave power transmission to free-flight drone experiment was conducted in a 10 m anechoic chamber. An AR-drone were controlled by IFT algorithm with indoor GPS. We developed a 50 % maximum efficiency rectifier and single-axis beam forming
Publikováno v:
2020 IEEE 21st International Conference on Vacuum Electronics (IVEC).
To develop the vacuum-type microwave DC converter for high frequency, in a region of the whole converter where the z-axial magnetic field was reserved, the motion and z-axial velocity of the electron were simulated. The results showed that the increm
Autor:
Kohei Shimamura, Mizojiri, Tsuyoshi Imai, Ryutaro Minami, Shigeru Yokota, Masatoshi Suzuki, Maho Matsukura, Tsuyoshi Kariya
Publikováno v:
The Review of scientific instruments. 90(2)
An instantaneous measurement system of high-power millimeter-wave was proposed and demonstrated with a 28 GHz gyrotron at the Plasma Research Center, University of Tsukuba. The high-power detector consists of an attenuator and a linear polarized micr
Autor:
Kohei Shimamura, Satoru Suganuma, Maho Matsukura, Tsuyoshi Kariya, Sei Mizojiri, Ryutaro Minami, Shigeru Yokota, Masatoshi Suzuki
Publikováno v:
2018 IEEE Wireless Power Transfer Conference (WPTC).
To demonstrate the high-power millimeter wave WPT, the class F-load rectenna array was used with a 28 GHz 300 kW-class Gyrotron. As a result, the output DC power and the transmission efficiency for 0.9 m distance and 52.9 kW input were respectively 1
Autor:
Kohei Shimamura1, Maho Matsukura2, Naoto Ozaki2, Kaisei Miyawaki2, Shigeru Yokota3, Ryutaro Minami4, Tsuyoshi Kariya2, Tsuyoshi Imai5
Publikováno v:
Journal of Spacecraft & Rockets. May2020, Vol. 57 Issue 3, p632-635. 4p.