Title:
ハイブリッド推進のための電気アーキテクチャ
Document Type and Number:
Japanese Patent JP7408647
Kind Code:
B2
Abstract:
An aircraft with hybrid thermal/electrical propulsion includes a turbomachine; a first electrical source; a second electrical source equipped with an electrical energy storage device; a non-propulsion electrical distribution network; a low-voltage electrical distribution network; and a propulsion electrical distribution network. The three electrical distribution networks are electrically supplied by the first and second electrical sources and electrically interconnected by static converters.
Inventors:
Philip del Bosk
Anne Lian Heart
Clement Dupei
Christoph Biggie
Sonia docker
Anne Lian Heart
Clement Dupei
Christoph Biggie
Sonia docker
Application Number:
JP2021518560A
Publication Date:
January 05, 2024
Filing Date:
October 01, 2019
Export Citation:
Assignee:
Saffron Aircraft Engines
International Classes:
B64D27/24; B60L9/18; B60L15/20; B60L50/16; B60L50/60; B60L53/16; B60L58/18; H02J1/00
Domestic Patent References:
| JP2015053848A |
Foreign References:
| US20060061213 | ||||
| US20180118356 | ||||
| US20160016670 |
Attorney, Agent or Firm:
Atsushi Aoki
Shinji Mihashi
Yuichi Morimoto
Keiji Akagi
Shinji Mihashi
Yuichi Morimoto
Keiji Akagi