영풍전자주식회사

IBC EMA (Electro-Mechanical Actuator)

We are in the process of developing a highly reliable, high-performance, redundancy EMA control to be integrated into aviation mobility as a key challenge for the future.

APPLICATION

AAM(Advanced Air Mobility) eVTOL

Overview

IBC EMA (Electro-Mechanical Actuator)

The IBC EMA enhances flight safety by modifying the direction of rotor thrust during eVTOL transition flight and also adjusts a thrust level during cruise.

FEATURES

It is scheduled for environmental and electromagnetic compatibility tests in 2024. If these tests are successful, the system will be installed on an aircraft for operational testing.

Linear Actuator Controller
Control PMSM motors via LVDT, resolver sensor inputs 01
Redundancy
Electrically isolated 100% redundant controller structure 02
Built-In Test
If a malfunction occurs, transmit information to system through CAN communication 03
High efficiency · High powered
1kw compact, highly efficient, highly powered controller 04

Configuration

RELIABILITY · EFFICIENCY

We aim at compact, highly efficient, powered,
and reliable system with a redundant structure.

UAV·AAM

IBC EMA (Electro-Mechanical Actuator)

APPLICATION

IBC EMA (Electro-Mechanical Actuator)

FEATURES

RELIABILITY · EFFICIENCY