System Design for the More Electric Engine Incorporated in the Electrical Power Management for More Electric Aircraft IHI AEROSPACE Company Limited

Format:

Conference/Event

Author/Creator:

Oyori, Oyori, author.

Contributor:

Kakiuchi, Daiki

Morioka, Noriko

Onishi, Keisuke

Sano, Fumito

Shimomura, Yukio

Conference Name:

SAE 2012 Power Systems Conference (2012-10-30 : Phoenix, Arizona, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 2012

Summary:

This paper describes a study on electrical power management for the More Electric Aircraft (or MEA) and the More Electric Engine (or MEE). This study explored power management solutions based on an integrated engine/power control system and a permanent magnet motor. In recent years, electrical power management has emerged as a key aspect of aircraft system design. In cases in which the Electromechanical Actuator (or EMA) systems are used for flight control, the power bus systems must also be designed to dissipate the power regenerated from flight control systems. In their study, the authors focused on achieving an optimal balance between aircraft power management and operational requirements of the aero-engines. The study results suggest an effective and novel power control concept based on integrated engine control technologies that ensure stable power systems

Notes:

Vendor supplied data

Publisher Number:

2012-01-2169

Access Restriction:

Restricted for use by site license