The Stick Position Augmentation System (SPAS) features an electric actuator that, as a function of airspeed and collective pitch, introduces an aft cyclic control input as airspeed increases.
The winch arm operates during rescue missions and is mostly installed on Airbus Helicopters platforms. It is a well-proven technology and has supported many rescue missions worldwide.
The actuator is used for opening the hatch, supported by a gas spring. It was designed with a reversible ball screw, transmission spur gear, bearings, and a permanent magnet DC motor.
The ramp actuators are responsible for moving the ramp on the NH90 helicopter. They were designed with a reversible ball screw, transmission spur gear, bearings, and a permanent magnet DC motor.
With two independent electrical drive systems and position or speed feedbacks, the pitch and roll trim actuator stands for high reliability and robust work environments.
The actuator is used to trim the pitch elevator wing flap. It uses two independent permanent magnet DC motors and is designed in a “Fail-safe” layout with a dual static load path and friction clutch.
The cargo loading joystick is designed for rugged, reliable day-to-day service. The design is optimized for 5 positions and control container power drive units.
The inside joystick is meant to operate an aircraft cargo loading system. It automatically springs back into a neutral position if not operated. It was improved to be operated with gloves.
The cargo loading joystick is designed for rugged, reliable day-to-day service. The design is optimized for 5 positions and control container power drive units.
EME supported the IPTN N250 program. A stall testing has identified the need for an artificial stall warning (stick shaker). The product was successfully developed for the intended purpose.
