The temperature switch is a high-class and accurate sensing device particularly developed for combat helicopter platforms. It is used and proven on Airbus Helicopters Tiger, meeting all performance data.
The pressure switch is meant for aviation potable water and waste systems. Our prime customer Airbus successfully operates the product on multiple systems in its legacy and next-generation aircraft.
The pressure switch provides an electrical signal at a specific hydraulic pressure. It transforms hydraulic pressure into a mechanical movement via a multi-thickness pressure sensing membrane. A snap mechanism amplifies it into a usable stroke for the micro-switch.
The ramp system of the NH90 is managed and controlled by the control unit. There are connections to the ramp and hatch actuators, the cabin control panel, the cockpit control panel, and more.
The sill actuator is a component of the cargo loading system of the airplane. The ram rod end operates the sill door latches, allowing the movement to open the “Y” latches of the sill doors.
The tail rotor actuator is installed on the rear end of a heavy-lift transport helicopter. It operates the angle-of-attack rear rotor blades and prevents the turning of the tail rotor in the air system. It is equipped with a thermal overload protection system.
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 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.
As a lead supplier of floor-to-floor harnesses, our products are used in today’s most modern aircraft cabins. EME excels in time-to-market and quality on both build-to-print and build-to-design basis.
The PC-12 NG flight testing dictated the aircraft to use a stall protection system. EME design engineers developed and introduced the perfect solution to safeguard the PC-12 NG flight envelope at all times.
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 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 manufactures special application harnesses for the use of the latest versions of the twin-engine rotorcraft product line. Utmost quality requirements are key to stay in the business.
