영풍전자주식회사

Actuator

EMA (Electro-Mechanical Actuator)

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EMA (Electro-Mechanical Actuator)

We are in the process of developing a highly reliable, redundant EMA steering controller for single-path civilian aircrafts as a key challenge for the future.

APPLICATION

Single-path civilian aircrafts

Overview

EMA (Electro-Mechanical Actuator)

The DRESS (Distributed and Redundant Electromechanical nose gear Steering System) program has allowed advanced European companies to gain expertise in creating steering mechanisms for single-path aircrafts. To ensure equal cooperation and related development technologies in the future, we will promote localization of the DRESS program.

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.

Rotary actuator control
Control PMSM motors with position, temperature 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
Brake · Clutch
Control brake and clutch 04

Configuration

RELIABILITY · EFFICIENCY

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

UAV·AAM

EMA (Electro-Mechanical Actuator)

APPLICATION

EMA (Electro-Mechanical Actuator)

FEATURES

RELIABILITY · EFFICIENCY